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GOL 737-8 Operation Manual

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Table of Contents

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Title Page
File Highlight
Title Page
Volume 1
Title Page
March 1, 2021
2
Flight Crew
Operations Manual
Gol Linhas Aereas S.A.
Document Number MN-FLT-OH-201
Revision Number: 0 (Temporary Revision)
Revision Date: October 26, 2021
737-8

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Summary of Contents for GOL 737-8

  • Page 1 Title Page Volume 1 Title Page Title Page File Highlight 737-8 Flight Crew Operations Manual Gol Linhas Aereas S.A. Document Number MN-FLT-OH-201 Revision Number: 0 (Temporary Revision) Revision Date: October 26, 2021 March 1, 2021...
  • Page 2 GOL Linhas Aéreas S.A. fleet and flight operations. This Gol 737 FCOM has been prepared for the exclusive use of Gol Linhas Aéreas S.A. flight operations personnel under its direction and authority and shall, at all times, remain the property of Gol Linhas Aéreas S.A.
  • Page 3 Preface Table Of Contents 737 MAX Flight Crew Operations Manual Preface Chapter 0 Chapter Table of Contents Section TOC Volume 1 Title Page ..........0 Preface .
  • Page 4 Preface - Chapter Table of Contents 737 MAX Flight Crew Operations Manual Intentionally Blank 0.TOC.2 MN-FLT-OH-201 March 1, 2021...
  • Page 5 File Highlight Model Identification General This manual applies to the 737 MAX 8 fleet operated by Gol Linhas Aéreas S.A. 737MAX series: Powered by two LEAP1B series engines. They may be equipped with advanced technology winglet, as follow: -MAX8: 39,47m length version with up 186 passengers seat. Engine rating is 28K Package with a two position tail skid.
  • Page 6 Preface - Model Identification 737 MAX Flight Crew Operations Manual Intentionally Blank 0.1.2 MN-FLT-OH-201 October 26, 2021...
  • Page 7 This 737 Flight Crew Operations Manual has been prepared for the exclusive use of Gol Linhas Aéreas S.A. flight operations personnel under its direction and authority and shall, at all times, remain the property of Gol Linhas Aéreas S.A. The holder hereof acknowledges and agrees that this manual contains or may contain trade secrets, copyrighted material and commercial and proprietary information, privileged and confidential, to the interest of Gol Linhas Aéreas S.A.,...
  • Page 8 It is understood and agreed to by such other party that it shall release indemnify and hold Gol Linhas Aéreas S.A., its officers, employees and agents harmless against any and all claims or actions of whatever nature which may arise or claim to arise from the use hereof.
  • Page 9 Preface - Introduction 737 MAX Flight Crew Operations Manual Example Page Number Chapter (Hydraulics) Page Number 13.20.3 Section (Systems Description) Warnings, Cautions, and Notes The following levels of written advisories are used throughout the manual. WARNING: An operating procedure, technique, etc., that may result in personal injury or loss of life if not carefully followed.
  • Page 10 Preface - Introduction 737 MAX Flight Crew Operations Manual Schematic Symbols Symbols shown are those which may not be identified on schematic illustrations. GENERAL ELECTRICAL DC BUS DRIVE AC BUS GENERATOR & BUSSES INVERTER TR UNIT GENERATOR DRIVE RESERVOIR HEAT DUAL HEAT EXCHANGER EXCHANGER...
  • Page 11 Preface - Introduction 737 MAX Flight Crew Operations Manual VALVES MOTORS AND SOLENOIDS ELECTRIC MOTOR ALTERNATING DIRECT SOLENOID MOTOR CURRENT CURRENT LIQUID LIQUID LIQUID LIQUID DRIVEN MOTOR MOTOR SHUT-OFF 2-WAY 3-WAY 4-WAY ACTUATOR INDICATORS PNEUMATIC PNEUMATIC PNEUMATIC SHUT-OFF MODULATING FLOW LIMITING KILOWATT INDICATOR AMMETER...
  • Page 12 Preface - Introduction 737 MAX Flight Crew Operations Manual Intentionally Blank 0.2.6 MN-FLT-OH-201 March 1, 2021...
  • Page 13 737 MAX Flight Crew Operations Manual Preface Chapter 0 Abbreviations Section 3 Abbreviations General The following abbreviations may be found throughout the manual. Some abbreviations may also appear in lowercase letters. Abbreviations having very limited use are explained in the chapter where they are used Amplitude Modulation Actual Navigation Autopilot...
  • Page 14 Preface - Abbreviations 737 MAX Flight Crew Operations Manual Bromotrifluropropene EASA European Aviation (fire extinguishers) Safety Agency EBAW Enhanced Bank Angle Warning Captain Celsius Environmental Control Center System CANC/ Cancel/Recall Electronic Engine Control Circuit Breaker EFIS Electronic Flight Instrument System Control Display Unit EGPWS Enhanced Ground...
  • Page 15 Preface - Abbreviations 737 MAX Flight Crew Operations Manual Flight Management IASC Integrated Air Supply Computer Controller Flight Management IDENT Identification System Instrument Landing Flight Path Angle System Flight Path Vector Inches FSEU Flap Slat Electronic Unit INBD Inboard Inbound IND LTS Indicator Lights Glide Slope...
  • Page 16 Preface - Abbreviations 737 MAX Flight Crew Operations Manual Manual MCAS Maneuver Characteristics PASS Passenger Augmentation System Power Control Unit Mode Control Panel PERF INIT Performance Minimum Descent Initialization Altitude Pilot Flying MAX Display System Primary Flight Minimum Equipment Computers List Pilot Monitoring Multi-Function Display...
  • Page 17 Preface - Abbreviations 737 MAX Flight Crew Operations Manual Step Climb Universal Time Coordinated Select SMYD Stall Management Yaw Damper Vertical Speed Speed Takeoff Decision Speed SPLR Spoiler Takeoff Safety Speed Station Design Maneuvering Speed STAB Stabilizer Very High Frequency STAT Status Maximum Operating...
  • Page 18 Preface - Abbreviations 737 MAX Flight Crew Operations Manual Intentionally Blank 0.3.6 MN-FLT-OH-201 March 1, 2021...
  • Page 19 Filed March, 2021 General The Gol 737 FCOM revisions are issued to provide new or revised procedures and information. Formal revisions also incorporate appropriate information from previously issued Fleet Bulletins. The revision date is the approximate date the manual is approved for printing. The revision is mailed a few weeks after this date.
  • Page 20 Preface - Revision Record 737 MAX flight Crew Operations Manual Filing Instructions Consult the List of Effective Pages (0.5). Pages identified with an asterisk (*) are either replacement pages or new (original) issue pages. Remove corresponding old pages and replace or add new pages. Remove pages that are marked DELETED;...
  • Page 21 System (RAAS) Inhibit Operation SP.15.2 - Temporary Revision - Added Supplementary Procedures regarding RAAS system Performance Package 10 737-8 LEAP-1B27 KG C M FAA CATB TO1-10% TO2-20% Section 10 - Pkg Model Identification New Performance Inflight Package 10 Section 10 - General...
  • Page 22 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10...
  • Page 23 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual PI.10.59 - Reformatted all tables for improved readability. Included 1000 ft increments of airport altitude from -2000 ft to 14000 ft. Data revised for Maneuver Speeds to be based on airplane altitude instead of airport altitude. Added configurations for Flaps 5, Flaps 10, and Flaps 25 with Gear Up.
  • Page 24 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual PI.10.69 - Reformatted all tables for improved readability. Included 1000 ft increments of airport altitude from -2000 ft to 14000 ft. Data revised for Maneuver Speeds to be based on airplane altitude instead of airport altitude. Added configurations for Flaps 5, Flaps 10, and Flaps 25 with Gear Up.
  • Page 25 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual PI.10.77 - Reformatted all tables for improved readability. Included 1000 ft increments of airport altitude from -2000 ft to 14000 ft. Updated table due to calculation change that are now based on KIAS instead of KEAS. PI.10.77 - Reformatted all tables for improved readability.
  • Page 26 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 Section 11 - All Engine New Performance Inflight Package 10 New Performance Inflight Package 10 Section 12 - Advisory Information New Performance Inflight Package 10 New Performance Inflight Package 10...
  • Page 27 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual Section 15 - Alternate Mode EEC New Performance Inflight Package 10 Section 16 - GearDown New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 New Performance Inflight Package 10 Section 17 - Gear Down, Engine Inop...
  • Page 28 Preface - Revision Highlights 737 MAX Flight Crew Operations Manual Chapter 13 - Hydraulics Section 20 - System Description Introduction 13.20.2 - Added Hydraulic Power Distribution Schematic for One-Poistion Tail Skid variant Chapter 15 - Warning Systems Section 10 - Controls and Indicators Altitude Alert 15.10.7 - Added "200 feet"...
  • Page 29 V1V2 List of Effective Pages V1V2 List of Effective Pages V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual Preface Chapter 0 V1V2 List of Effective Pages Section 5 Bulletin Record Volume 1 0.6.1-4 October 26, 2021 B.2.1 March 1, 2021 * Title Page 1-2 October 26, 2021...
  • Page 30 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual B.18.6 March 1, 2021 NP.21.7 March 1, 2021 B.18.7 March 1, 2021 NP.21.8 March 1, 2021 NP.21.9 March 1, 2021 B.18.8 March 1, 2021 B.18.9 March 1, 2021 NP.21.10 March 1, 2021 B.18.10...
  • Page 31 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual NP.21.54 March 1, 2021 NP.21.101 March 1, 2021 NP.21.55 March 1, 2021 NP.21.102 March 1, 2021 NP.21.56 March 1, 2021 Supplementary Procedures NP.21.57 March 1, 2021 SP.TOC.1-8 October 26, 2021 NP.21.58 March 1, 2021...
  • Page 32 Performance Inflight SP.11.21 March 1, 2021 PI.TOC.1-2 October 26, 2021 SP.11.22 March 1, 2021 SP.11.23 March 1, 2021 737-8 LEAP-1B27 KG C M FAA CATB TO1-10% SP.11.24 March 1, 2021 TO2-20% SP.12.1 March 1, 2021 PI.TOC.10.1-6 October 26, 2021 SP.12.2 March 1, 2021 PI.ModID.10.1-2...
  • Page 33 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual PI.10.10 October 26, 2021 PI.10.57 October 26, 2021 PI.10.11 October 26, 2021 PI.10.58 October 26, 2021 PI.10.59 October 26, 2021 PI.10.12 October 26, 2021 PI.10.13 October 26, 2021 PI.10.60 October 26, 2021 PI.10.14...
  • Page 34 PI.18.15 October 26, 2021 PI.13.7 October 26, 2021 PI.18.16 October 26, 2021 PI.13.8 October 26, 2021 737-8 TS2 LEAP-1B28 KG C M FAA CATB PI.13.9 October 26, 2021 TO1-10% TO2-20% ALT-AB (FMC Model 737-8.2) PI.13.10 October 26, 2021 AOA-DIAL PI.13.11 October 26, 2021 PI.TOC.30.1-6...
  • Page 35 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual PI.30.5 March 1, 2021 PI.30.52 March 1, 2021 PI.30.6 March 1, 2021 PI.30.53 March 1, 2021 PI.30.54 March 1, 2021 PI.30.7 March 1, 2021 PI.30.8 March 1, 2021 PI.30.55 March 1, 2021 PI.30.9...
  • Page 36 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual PI.32.27 March 1, 2021 PI.36.6 March 1, 2021 PI.32.28 March 1, 2021 PI.37.1 March 1, 2021 PI.37.2 March 1, 2021 PI.32.29 March 1, 2021 PI.32.30 March 1, 2021 PI.37.3 March 1, 2021 PI.32.31...
  • Page 37 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 1.20.16 March 1, 2021 1.40.27 October 26, 2021 1.30.1 March 1, 2021 1.40.28 October 26, 2021 1.40.29 October 26, 2021 1.30.2 March 1, 2021 1.30.3 March 1, 2021 1.40.30 October 26, 2021 1.30.4...
  • Page 38 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 2.30.5 March 1, 2021 4.10.16 March 1, 2021 2.30.6 March 1, 2021 4.10.17 March 1, 2021 4.10.18 March 1, 2021 2.30.7 March 1, 2021 2.30.8 March 1, 2021 4.10.19 March 1, 2021 2.30.9...
  • Page 39 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 5.10.2 October 26, 2021 6.20.4 March 1, 2021 5.10.3 October 26, 2021 6.20.5 March 1, 2021 6.20.6 March 1, 2021 5.10.4 October 26, 2021 5.10.5 October 26, 2021 6.20.7 March 1, 2021 5.10.6...
  • Page 40 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 7.20.6 March 1, 2021 9.10.9 March 1, 2021 7.20.7 March 1, 2021 9.10.10 March 1, 2021 9.10.11 March 1, 2021 7.20.8 March 1, 2021 7.20.9 March 1, 2021 9.10.12 March 1, 2021 7.20.10...
  • Page 41 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 10.10.11 March 1, 2021 10.10.58 March 1, 2021 10.10.12 March 1, 2021 10.10.59 March 1, 2021 10.10.60 March 1, 2021 10.10.13 March 1, 2021 10.10.14 March 1, 2021 10.10.61 March 1, 2021 10.10.15...
  • Page 42 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 10.20.7 March 1, 2021 11.10.7 March 1, 2021 10.20.8 March 1, 2021 11.10.8 March 1, 2021 10.20.9 March 1, 2021 11.10.9 March 1, 2021 10.20.10 March 1, 2021 11.10.10 March 1, 2021 10.20.11...
  • Page 43 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 11.30.2 March 1, 2021 11.32.5 March 1, 2021 11.30.3 March 1, 2021 11.32.6 March 1, 2021 11.32.7 March 1, 2021 11.30.4 March 1, 2021 11.31.1 March 1, 2021 11.32.8 March 1, 2021 11.31.2...
  • Page 44 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 11.33.44 March 1, 2021 11.34.25 March 1, 2021 11.33.45 March 1, 2021 11.34.26 March 1, 2021 11.34.27 March 1, 2021 11.33.46 March 1, 2021 11.33.47 March 1, 2021 11.34.28 March 1, 2021 11.33.48...
  • Page 45 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 11.34.72 March 1, 2021 11.41.1 March 1, 2021 11.40.1 March 1, 2021 11.41.2 March 1, 2021 11.41.3 March 1, 2021 11.40.2 March 1, 2021 11.40.3 March 1, 2021 11.41.4 March 1, 2021 11.40.4...
  • Page 46 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 11.42.14 March 1, 2021 11.43.19 March 1, 2021 11.42.15 March 1, 2021 11.43.20 March 1, 2021 11.43.21 March 1, 2021 11.42.16 March 1, 2021 11.42.17 March 1, 2021 11.43.22 March 1, 2021 11.42.18...
  • Page 47 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 11.60.34 March 1, 2021 14.10.3 March 1, 2021 11.60.35 March 1, 2021 14.10.4 March 1, 2021 11.60.36 March 1, 2021 14.10.5 March 1, 2021 11.60.37 March 1, 2021 14.10.6 March 1, 2021 11.60.38...
  • Page 48 Preface - V1V2 List of Effective Pages 737 MAX Flight Crew Operations Manual 15.20.11 October 26, 2021 15.20.12 October 26, 2021 15.20.13 October 26, 2021 15.20.14 October 26, 2021 15.20.15 October 26, 2021 15.20.16 October 26, 2021 15.20.17 October 26, 2021 15.20.18 October 26, 2021 15.20.19...
  • Page 49 737 MAX Flight Crew Operations Manual Preface Chapter 0 Bulletin Record Section 6 Bulletin Record Bulletin Record Bulletin Record File Highlight Bulletin Record General The Boeing Company issues Flight Crew Operations Manual Bulletins to provide important information to flight crews prior to the next formal revision of the Flight Crew Operations Manual.
  • Page 50 Preface - Bulletin Record 737 MAX Flight Crew Operations Manual Number Subject Date Status GOT-1 Cabin Pressurization Panel March 1, 2021 Blanking/Dimming Issues GOT-2 Incorrect FMC Constraint Altitude March 1, 2021 on a Standard Terminal Arrival Route (STAR) with a Common Waypoint, after Selection of another Approach GOT-3...
  • Page 51 Preface - Bulletin Record 737 MAX Flight Crew Operations Manual Number Subject Date Status GOT-16 Elevator Jam Landing Assist March 1, 2021 Switch GOT-18 Speed Trim System (STS) and March 1, 2021 Autopilot Flight Director System (AFDS) with new Flight Control Computer (FCC) P12.1.2 software March 1, 2021 MN-FLT-OH-201...
  • Page 52 Preface - Bulletin Record 737 MAX Flight Crew Operations Manual Intentionally Blank 0.6.4 MN-FLT-OH-201 March 1, 2021...
  • Page 53 Covers File Highlight Cabin Pressurization Panel Blanking /Dimming Issues. GOT-1 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-1 IssueDate: March 15, 2018 Subject: Cabin Pressurization Panel Blanking/Dimming Issues Reason: To inform the crew of failures of the Cabin Pressurization Panel where the indications flicker, become too dim to read, or completely blank.
  • Page 54 Flight Crew Operations Manual Bulletin No. GOT-1 , Dated March 15, 2018 (continued) Currently the line number effectivity is not known therefore this FCOM bulletin will be revised when the information becomes available. Also included in the revision will be confirmation of the cause of the Cabin Pressurization Panel failures and a time line for the fix.
  • Page 55 Flight Crew Operations Manual Bulletin No. GOT-1 , Dated March 15, 2018 (continued) No crew action is required. Operate the airplane at the new higher cruise altitude. Note:Flying above the selected FLT ALT will drive the cabin to the maximum differential pressure. When the maximum cabin differential pressure is reached, the automatic control system will prioritize limiting differential pressure and will stop controlling cabin...
  • Page 56 Flight Crew Operations Manual Bulletin No. GOT-1 , Dated March 15, 2018 (continued) Intentionally Blank B-1 Page 4 of 4 MN-FLT-OH-201 March 1, 2021...
  • Page 57 Gol Linhas Aereas S.A. Number: GOT-2 R1 IssueDate: August 15, 2019 Airplane Effectivity: 737-8/-9 Airplanes with FMC U13 Subject: Incorrect FMC Constraint Altitude on a Standard Terminal Arrival Route (STAR) with a Common Waypoint, after Selection of another Approach Reason: To inform crews about the incorrect FMC Constraint Altitude, when selecting another approach that has a common waypoint with the original STAR in the active flight plan.
  • Page 58 Flight Crew Operations Manual Bulletin No. GOT-2 R1, Dated August 15, 2019 (continued) Intentionally Blank B-2 Page 2 of 2 MN-FLT-OH-201 March 1, 2021...
  • Page 59 Covers File Highlight VNAV INVALID-PERF Scratch pad Message GOT-3 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-3 IssueDate: March 15, 2018 Airplane Effectivity: B737-7/8/9 Airplanes with FMC Software U13 Subject: VNAV INVALID-PERF Scratchpad Message Reason: To inform the Flight Crews of an anomaly in which the VNAV INVALID-PERF scratchpad message cannot be cleared unless an approach is selected in the active flight plan.
  • Page 60 Flight Crew Operations Manual Bulletin No. GOT-3 , Dated March 15, 2018 (continued) Operating Instructions When wind data is entered into the DES FORECAST page with no approach selected in the active flight plan, and the VNAV INVALID-PERF scratchpad message is shown in flight, an approach should be entered into the active flight plan.
  • Page 61 THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT Background Information Certification flights on the 737-8 revealed intermittent and momentary illumination of the DFDR amber OFF light after the first engine start. Illumination of the OFF light also simultaneously caused the two master caution lights and amber OVERHEAD light on the system annunciator panel to momentarily illuminate.
  • Page 62 Flight Crew Operations Manual Bulletin No. GOT-4 R1, Dated February 21, 2019 (continued) Intentionally Blank B-4 Page 2 of 2 MN-FLT-OH-201 March 1, 2021...
  • Page 63 THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT Background Information During flight test the 737-8 has exhibited bleed system pressure oscillations. These oscillations were observed with takeoff or climb thrust set with Engine or Wing Anti-Ice ON or OFF. The oscillations have also been observed at reduced thrust settings during cruise or descent with Engine Anti-Ice ON and Wing Anti- Ice OFF.
  • Page 64 Flight Crew Operations Manual Bulletin No. GOT-5 , Dated March 15, 2018 (continued) Intentionally Blank B-5 Page 2 of 2 MN-FLT-OH-201 March 1, 2021...
  • Page 65 THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT Background Information During 737-8 flight tests, illumination of the amber wing VALVE lights occurred during use of the wing anti-ice system under the following conditions: • Engine idle thrust descent above FL230 •...
  • Page 66 Flight Crew Operations Manual Bulletin No. GOT-6 , Dated April 4, 2018 (continued) Operating Instructions If above FL230: If the L VALVE or R VALVE light(s) illuminate with the master caution and the amber ANTI-ICE light on the system annunciator panel, wait 20 seconds after illumination of the master caution.
  • Page 67 THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT Background Information During 737-8 flight tests, nuisance illumination of the amber COWL VALVE light(s) occurred when engine anti-ice was used at altitudes below FL230. Depending on bleed air demands, the high stage valve modulates open to maintain adequate bleed air pressure.
  • Page 68 Flight Crew Operations Manual Bulletin No. GOT-7 , Dated April 4, 2018 (continued) Operating Instructions If above FL230: If the COWL VALVE light(s) illuminate with the master caution and the amber ANTI-ICE light on the system annunciator panel, do the ENGINE COWL VALVE OR TAI INDICATION Non-Normal Checklist.
  • Page 69 Covers File Highlight START VALVE OPEN Alert Blinking at Starter Cu tout GOT-8 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-8 IssueDate: May 10, 2018 Subject: START VALVE OPEN Alert Blinking at Starter Cutout Reason: This bulletin informs flight crews of nuisance blinking of the START VALVE OPEN alert after reaching starter cutout speed.
  • Page 70 Flight Crew Operations Manual Bulletin No. GOT-8 , Dated May 10, 2018 (continued) Operating Instructions After starter cutout speed is reached: If the START VALVE OPEN alert blinks momentarily then extinguishes, no flight crew or maintenance action is needed. If the START VALVE OPEN alert continues to blink for up to 10 seconds then illuminates steady, do the START VALVE OPEN Non-Normal Checklist.
  • Page 71 THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT Background Information During certification for the 737-8, analysis was conducted for engine ground starts on cold engines and in hot ambient conditions. A cold engine is an engine with indicated EGT of 74°C or less. Analysis showed that engine starts conducted on cold engines and when the OAT was 47°C / 117°F or greater, the...
  • Page 72 Flight Crew Operations Manual Bulletin No. GOT-9 R1, Dated November 17, 2018 (continued) In addition, operators have reported several situations when aborted engine starts were needed in order to avoid exceeding the EGT start limit. These situations occurred when the OAT was 40°C / 104°F and greater, and were not dependent on a cold or warm engine.
  • Page 73 Flight Crew Operations Manual Bulletin No. GOT-9 R1, Dated November 17, 2018 (continued) ENGINE HYDRAULIC PUMP switches ........ON Verify all hydraulic panel LOW PRESSURE lights are extinguished. Do the Before Taxi Procedure. MN-FLT-OH-201 B-9 Page 3 of 4 March 1, 2021...
  • Page 74 Flight Crew Operations Manual Bulletin No. GOT-9 R1, Dated November 17, 2018 (continued) Intentionally Blank B-9 Page 4 of 4 MN-FLT-OH-201 March 1, 2021...
  • Page 75 File Highlight 73 7 MAX Integrated ADIRU (I-ADIRU) an d Au tomatic Nav igation Realign (ANR) Mo de GOT-10 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-10 IssueDate: August 20, 2018 Subject: 737 MAX Integrated ADIRU (I-ADIRU) and Automatic Navigation...
  • Page 76 Flight Crew Operations Manual Bulletin No. GOT-10 , Dated August 20, 2018 (continued) 737 MAX airplanes with I-ADIRU part number HG2050BC04 that have been connected to the Multi-Mode Receiver (MMR) are capable of automatically accepting GPS position for IRS initializations (i.e. full alignment, Fast Realignment, and post-flight ANR mode).
  • Page 77 (motionless). The following is more specific information on 737 MAX models affected by this bulletin: • 737-7 – All • 737-8 •Line number 6854 and earlier if Service Bulletin 737-34-3141 is incorporated •All from line number 6855 and on •...
  • Page 78 Flight Crew Operations Manual Bulletin No. GOT-10 , Dated August 20, 2018 (continued) Compass rose RANGE 0838.4 / 35 32.5 Figure 1 Track line RANGE 0838.4 / 35 32.5 Figure 2 Track line SEL HDG Figure 3 B-10 Page 4 of 8 MN-FLT-OH-201 March 1, 2021...
  • Page 79 Flight Crew Operations Manual Bulletin No. GOT-10 , Dated August 20, 2018 (continued) Current track RANGE 0838.4 / 35 32.5 Figure 4 1.9 L VOR 1 VOR 2 Lateral path deviation Figure 5 GPS POSITION Figure 6 MN-FLT-OH-201 B-10 Page 5 of 8 March 1, 2021...
  • Page 80 Flight Crew Operations Manual Bulletin No. GOT-10 , Dated August 20, 2018 (continued) Ground speed RANGE 0838.4 / 35 32.5 1.2 R 1.00 0.04 Figure 7 ADIRU position Figure 8 B-10 Page 6 of 8 MN-FLT-OH-201 March 1, 2021...
  • Page 81 Flight Crew Operations Manual Bulletin No. GOT-10 , Dated August 20, 2018 (continued) SPEEDBRAKE Speedbrake Warning Figure 9 Operating Instructions Before each flight complete a full IRS alignment and enter the most accurate latitude and longitude to initiate the alignment. If time does not allow a full alignment, do the Fast Realignment Supplementary Procedure.
  • Page 82 Flight Crew Operations Manual Bulletin No. GOT-10 , Dated August 20, 2018 (continued) Intentionally Blank B-10 Page 8 of 8 MN-FLT-OH-201 March 1, 2021...
  • Page 83 Covers File Highlight Predictive Windsh ear Sy stem Anomaly GOT-12 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-12 IssueDate: October 22, 2018 Subject: Predictive Windshear System Anomaly Reason: This bulletin informs flight crews of the susceptibility of certain airports to false Predictive Windshear System (PWS) alerts.
  • Page 84 Flight Crew Operations Manual Bulletin No. GOT-12 , Dated October 22, 2018 (continued) Flight crews should use the following criteria to help determine if windshear exists: • reports of windshear from other aircraft • visual indications • tower windshear alerts •...
  • Page 85 Covers File Highlight Lateral Path Exceedance on Approach Procedures with a Course Reversal GOT-14 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-14 IssueDate: November 16, 2018 Airplane Effectivity: 737 MAX Airplanes with FMC Software U13 Subject: Lateral Path Exceedance on Approach Procedures with a Course...
  • Page 86 Flight Crew Operations Manual Bulletin No. GOT-14 , Dated November 16, 2018 (continued) Operating Instructions When executing approaches containing distance constrained course reversals on airplanes with FMC Software U13, crews should be aware of this anomaly and pay particular attention that the lateral path on the Navigation Display (ND) does not exceed the limits indicated on the approach procedure.
  • Page 87 Gol Linhas Aereas S.A. Number: GOT-13 IssueDate: November 6, 2018 Airplane Effectivity: 737-8 / -9 Subject: Uncommanded Nose Down Stabilizer Trim Due to Erroneous Angle of Attack (AOA) During Manual Flight Only Reason: To Emphasize the Procedures Provided in the Runaway Stabilizer Non- Normal Checklist (NNC).
  • Page 88 Operating Instructions In the event an uncommanded nose down stabilizer trim is experienced on the 737-8 /-9, in conjunction with one or more of the above indications or effects, do the Runaway Stabilizer NNC ensuring that the STAB TRIM CUTOUT switches are set to CUTOUT and stay in the CUTOUT position for the remainder of the flight.
  • Page 89 Covers File Highlight Electronic Engine Control (EEC) Pressure Sensors Freezing GOT-15 Flight Crew Operations Manual Bulletin Gol Linhas Aereas S.A. Number: GOT-15 IssueDate: December 21, 2018 Airplane Effectivity: 737-7/-8/-9 Subject: Electronic Engine Control (EEC) Pressure Sensors Freezing Reason: To inform flight crews that if the pressure sensing system contains moisture, freezing can occur which can cause N1 oscillations.
  • Page 90 Flight Crew Operations Manual Bulletin No. GOT-15 , Dated December 21, 2018 (continued) Boeing is working with CFM on hardware modifications to improve elimination of moisture in the PS3 sensing system and to prevent any freezing. Improvements in EEC software 6.7, expected for release 2Q 2019, will prevent the oscillations. This FCOM bulletin will be revised to include Service Bulletin information when it becomes available.
  • Page 91 2 position switch. The 2 positions are ON and OFF with the switch guard closed to the OFF position. During production testing on a 737-8 airplane, it was discovered that the Elevator Jam Landing Assist switch installed on some airplanes has a 3 position switch, an ON position, an OFF position and a middle position.
  • Page 92 Flight Crew Operations Manual Bulletin No. GOT-16 , Dated March 27, 2019 (continued) Boeing has determined that airplanes from line number 7065 to line number 7278 might have the incorrect 3 position switch installed. However, airplanes outside of this line number range might also be affected since spare switches may have been sent directly from Honeywell to operators.
  • Page 93 THE FOLLOWING PROCEDURE AND/OR INFORMATION IS EFFECTIVE UPON RECEIPT Background Information On November 6, 2018, Boeing issued a bulletin to the 737-8/-9 fleet regarding uncommanded nose down stabilizer trim. That bulletin described how the Maneuvering Characteristics Augmentation System (MCAS) function of the Speed Trim System in the existing FCC software could trim the stabilizer nose down due to erroneous elevated Angle of Attack (AOA) input.
  • Page 94 All deliveries of 737-7/-8/-8200/-9 airplanes after the issue date of this bulletin will include the new FCC P12.1.2 software. For 737-8/-9 airplanes not delivered with FCC P12.1.2, Service Bulletin 737-22A1342 will be made available to provide FCC P12.1.2 software installation instructions.
  • Page 95 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Automatic Flight Chapter 4 - Controls and Indicators Section 10 Autopilot / Autothrottle Indicators STAB OUT OF TRIM LEFT FORWARD PANEL Stabilizer Out Of Trim (STAB OUT OF TRIM) Light Illuminated (amber) –...
  • Page 96 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Automatic Flight Chapter 4 - System Description Section 20 Autopilot Disengagement In addition to those conditions already listed in the FCOM, the autopilot automatically disengages for these additional conditions: •...
  • Page 97 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Flight Director Display Turning a F/D switch ON displays command bars on the respective pilot’s attitude indicator if command pitch and roll modes are engaged. If command pitch and roll modes are not engaged, the F/D command bars do not appear.
  • Page 98 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Flight Director Display (continued) If a generator is lost during a F/D TO or GA, or while in dual F/D APP mode below 800 feet, the FCC on the unaffected side positions the F/D command bars on both attitude indicators.
  • Page 99 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Minimum Speed Reversion The AFDS and A/T do not control to a speed which is less than minimum speed for the current flap configuration. This speed is approximately 1.3 Vs. Minimum speed, FMC speed, or selected speed, whichever is higher, becomes the AFS commanded speed.
  • Page 100 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Minimum Speed Reversion (continued) There is no minimum speed reversion from the following modes: • ALT HOLD • VNAV ALT (as installed) • VNAV PTH (in a level segment) •...
  • Page 101 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Flight Controls Chapter 9 - Controls and Indicators Section 10 Flight Control Panel STANDBY FLT CONTROL STANDBY FLT CONTROL STBY STBY QUANTITY STBY STBY PRESSURE A ON B ON B ON A ON...
  • Page 102 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Stabilizer CONTROL WHEEL Main Electric Stabilizer Trim Switches (spring-loaded to neutral) Push (both) – • electrically commands stabilizer trim in desired direction • autopilot disengages if engaged •...
  • Page 103 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Stabilizer (continued) STAB TRIM NORMAL CONTROL STAND Stabilizer Trim PRI (primary) Cutout switch NORMAL – normal operating position. CUTOUT – stops stabilizer trim inputs from main electric, autopilot and Speed Trim System (Speed Trim function and MCAS function).
  • Page 104 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Aileron / Elevator / Flight Spoilers CREW STATION Control Column Push - • operates elevators in the nose down direction • interrupts main electric, autopilot and Speed Trim System (Speed Trim function and MCAS function) nose up stabilizer trim commands.
  • Page 105 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Flight Controls Chapter 9 - System Description Section 20 Stabilizer Trim Main electric stabilizer trim switches on each control wheel actuate the electric trim motor through the main electric stabilizer trim circuit when the airplane is flown manually.
  • Page 106 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Stabilizer Trim (continued) Manual stabilizer control is accomplished through cables which allow the pilot to position the stabilizer by rotating the stabilizer trim wheels. The stabilizer is held in position by two independent brake systems.
  • Page 107 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Speed Trim System The Speed Trim System (STS) provides speed and pitch stability augmentation. Speed stability augmentation is provided by the Speed Trim function in the Speed Trim System. Pitch stability augmentation is provided by the MCAS function in the Speed Trim System.
  • Page 108 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Speed Trim Function (continued) The Speed Trim function operates most frequently during takeoff, climb and go- around. Conditions for operation are listed below: • Up to Mach 0.68 •...
  • Page 109 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Maneuvering Characteristics Augmentation System (MCAS) Function MCAS is a pitch stability augmentation function designed to operate at elevated angles of attack (AOAs). The purpose is to increase control column forces by commanding the stabilizer in the nose down direction at elevated AOAs.
  • Page 110 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Stall Identification Stall identification and control is enhanced by the yaw damper, the Elevator Feel Shift (EFS) module and the Speed Trim System. These three systems work together to help the pilot identify and prevent further movement into a stall condition.
  • Page 111 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Flight Control Computer Monitors The Flight Control Computers contain monitors which provide protection against possible runaway stabilizer conditions caused by erroneous FCC stabilizer trim commands. The FCCs continuously monitor each other’s stabilizer trim commands, and in the event an erroneous command is detected, stabilizer trim commands, autopilot trim commands, and CWS trim commands are stopped and inhibited for the remainder of the flight for that FCC.
  • Page 112 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Non-Normal Checklists This bulletin outlines the revisions to seven NNCs. An overview of the revisions to each NNC is included below. Section 9, Flight Controls (NNC.9): Runaway Stabilizer NNC The Runaway Stabilizer NNC memory steps have been reformatted and the reference steps have been revised for standardization purposes.
  • Page 113 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Non-Normal Checklists (continued) Section 10, Flight Instruments, Displays (NNC.10): Airspeed Unreliable NNC The Airspeed Unreliable NNC has been revised as follows: • Added a step to allow the flight crew to bypass the use of the Flight with Unreliable Airspeed table if the flight crew is able to determine a reliable airspeed source.
  • Page 114 Flight Crew Operations Manual Bulletin No. GOT-18 , Dated March 1, 2021 (continued) Operating Instructions This bulletin outlines the revisions to QRH Non-Normal Checklists in Section 9, Flight Controls (NNC.9) and Section 10, Flight Instruments, Displays (NNC.10). This bulletin also outlines the revisions to the QRH-CI and system description content.
  • Page 115 Limitations Limitations Limitations Table Of Contents 737 MAX Flight Crew Operations Manual Limitations Chapter L Table of Contents Section TOC Limitations and Operational Information ....L.10 General .
  • Page 116 Limitations - Table of Contents 737 MAX Flight Crew Operations Manual Flight Controls ........L.10.7 AFM Limitations.
  • Page 117 Assuming that the remaining items are available to the flight crew by reference, they do not need to be memorized. In some cases Gol Linhas Aéreas S.A. policies may direct more restrictive limitations. For example, a specific 737 may be AFM approved for takeoffs and...
  • Page 118 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Airplane General AFM Limitations Runway slope ±2% # Maximum Takeoff and Landing Tailwind 10 knots 1B401, 1B402, 1B801 - 1B824 Component Maximum Speeds Observe gear and flap placards Maximum Operating Altitude 41,000 feet pressure altitude Maximum Takeoff and Landing Altitude...
  • Page 119 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual AFM Operational Information # Severe Turbulent Air Penetration speed is 280 KIAS / .76M, whichever is lower. Applicable to Climb and Descent only. During Cruise, refer to SP.16, Severe Turbulence Supplementary Procedure.
  • Page 120 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Weight Limitations AFM Limitations Note: The maximum weight limitations can be further limited as referenced in the WEIGHT LIMITATIONS section of the CERTIFICATE LIMITATIONS chapter of the AFM. Note: Possible conflicts between the AFM and the FCOM may occur due to separate publication release dates.
  • Page 121 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Airplanes operating under FAA Rules: # For single channel operation during approach, the autopilot shall not remain engaged below 50 feet AGL. # Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: •...
  • Page 122 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Electrical 1B401 - 1B785, 1B801 - 1J594 AFM Limitations The use of Flight Deck Auxiliary Power outlets in the flight deck requires operational regulatory approval. Engines and APU AFM Limitations Thrust Operation with assumed temperature reduced takeoff thrust is not permitted with...
  • Page 123 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Non-AFM Operational Information APU bleed valve must be closed when: • ground air connected and isolation valve is open • engine no. 1 bleed valve is open • isolation and engine no. 2 bleed valves open. APU bleed valve may be open during engine start, but avoid engine power above idle.
  • Page 124 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Flight Management, Navigation AFM Limitations Air Data Inertial Reference Unit (ADIRU) ADIRU alignment must not be attempted at latitudes greater than 78 degrees 15 minutes. All flight operations based on magnetic heading or magnetic track angle are prohibited in geographic areas where the installed IRS MagVar table errors are greater than 5 degrees.
  • Page 125 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Non-AFM Operational Information # Avoid weather radar operation in a hangar. Avoid weather radar operation when personnel are within the area normally enclosed by the aircraft nose radome. Note: The hangar recommendation does not apply to the weather radar test mode.
  • Page 126 Limitations - Limitations and Operational Information 737 MAX Flight Crew Operations Manual Landing Gear Non-AFM Operational Information Do not apply brakes until after touchdown. L.10.10 MN-FLT-OH-201 March 1, 2021...
  • Page 127 Normal Procedures Normal Procedures Normal Procedures Table Of Contents 737 MAX Flight Crew Operations Manual Normal Procedures Chapter NP Table of Contents Section TOC Flight Crew Operations ManualNP - Normal Pro cedures Introduction ........NP.11 General .
  • Page 128 Normal Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Takeoff Flap Retraction Speed Schedule ....NP.21.59 After Takeoff Procedure ......NP.21.60 Climb and Cruise Procedure .
  • Page 129 737 MAX Flight Crew Operations Manual Normal Procedures Chapter NP Introduction Section 11 11 Introd uction Introduction File Highlight General This chapter gives: • an introduction to the normal procedures philosophy and assumptions • step by step normal procedures. Normal Procedures Philosophy and Assumptions Normal procedures verify for each phase of flight that: •...
  • Page 130 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual MAY or CAN: it is used with situations where the pilot will decide the best course of action in accordance with company’s policies. Configuration Check It is the crew member’s responsibility to verify correct system response. Before engine start, use system lights to verify each system's condition or configuration.
  • Page 131 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual Each crewmember is responsible for moving the controls and switches in their area of responsibility: • the phase of flight areas of responsibility for both normal and non-normal procedures are shown in the Area of Responsibility illustrations in this section.
  • Page 132 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual In flight, the PM usually makes the CDU entries. The PF may also make simple, CDU entries when the workload allows. The pilot making the entries executes the change only after the other pilot verifies the entries. During high workload times, for example departure or arrival, try to reduce the need for CDU entries.
  • Page 133 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual Preflight and Postflight Scan Flow -MAX 8 fleet only TYPICAL PANEL TYPICAL PANEL LOCATIONS ARE SHOWN. LOCATIONS ARE SHOWN CAPTAIN ITEMS FIRST OFFICER ITEMS CAPTAIN ITEMS FIRST OFFICER Captain Items ITEMS Captain Items First Officer Items...
  • Page 134 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual Areas of Responsibility - Captain as Pilot Flying or Taxiing -MAX 8 fleet only: CUTOFF TYPICAL PANEL LOCATIONS ARE SHOWN CAPTAIN ITEMS FIRST OFFICER ITEMS INCLUDING: JOINT RESPONSIBILITY -AUDIO CONTROL ITEM INCLUDING: -TRIM - WEATHER RADAR...
  • Page 135 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual Areas of Responsibility - First Officer as Pilot Flying -MAX 8 fleet only: CUTOFF TYPICAL PANEL LOCATIONS ARE SHOWN CAPTAIN ITEMS FIRST OFFICER ITEMS INCLUDING: JOINT RESPONSIBILITY -AUDIO CONTROL ITEM INCLUDING: -TRIM - WEATHER RADAR March 1, 2021...
  • Page 136 Normal Procedures - Introduction 737 MAX Flight Crew Operations Manual Intentionally Blank March 1, 2021 MN-FLT-OH-201 NP.11.8...
  • Page 137 737 MAX Flight Crew Operations Manual Normal Procedures Chapter NP Amplified Procedures Section 21 Amplified Pro cedures Threats and errors associated with this phase of flight are: • Distractions; • Interruption of procedures; • Circuit breaker; • Wing anti-ice ON; •...
  • Page 138 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Aircraft Manuals ..............Check According to the area of responsibility. Verify if the QRH and Normal Checklist correspond to the aircraft type. Maintenance documents............Check If necessary crosscheck any operational procedure on the MEL. Flight deck door access system.............Test Verify if flight deck door operational system is working properly according to Flight Deck Door Access System Test...
  • Page 139 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual MAX8 Fleet Only MAINT light ............Verify extinguished -700 and -800 Fleet Only PSEU light ............Verify extinguished GPS light ............. Verify extinguished ILS light (as installed) ......... Verify extinguished GLS light (as installed) ........
  • Page 140 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Verify that the PASS OXY ON light is extinguished. Landing gear indicator lights ........ Verify illuminated Flight recorder switch ........... Guard closed MACH AIRSPEED WARNING TEST switches .......... Push and hold one at time Verify that the clacker sounds.
  • Page 141 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Exterior inspection - Captain or First Officer Perform on: • The first flight of the crew on the aircraft; • When the aircraft has been on the ground for three or more hours: •...
  • Page 142 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • The tires are not too worn, not damaged and there is no tread separation; • The gear struts are not fully compressed; The engine inlets and tailpipes are clear, the access panels are secured, the exterior including the bottom of the nacelles, is not damaged and the reversers are stowed;...
  • Page 143 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Oxygen pressure relief green disc ..........In place Doors and access panels (not in use) ........Latched Right Wing Root, Pack, and Lower Fuselage Ram air deflector door ............Extended Pack and pneumatic access doors ..........Secure Probes, sensors, ports, vents and drains (as applicable) ..
  • Page 144 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Hydraulic lines .................Secure Gear pin ................As needed Right Main Wheel Well APU FIRE CONTROL handle ............Up NGS operability indicator light (as applicable) ....... Check Verify that the light is green. Wheel Well ................
  • Page 145 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Hydraulics lines ...............Secure Gear pin ................As needed Left Main Wheel Well Wheel well ................Check Engine fire bottle pressure ............Check Left Wing Tip and Trailing Edge Aileron and trailing edge flaps ..........Check Static discharge wicks ..............
  • Page 146 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual March 1, 2021 MN-FLT-OH-201 NP.21.10...
  • Page 147 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual CDU Preflight Procedure - Captain and First Officer The initial data entries must be complete before the flight instrument check during the Preflight Procedure. The Navigation and Performance Data entries must be complete prior to the reading of the before Start Checklist.
  • Page 148 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Preflight Procedures - Captain Objective: to check and configure aircraft systems. Do the following procedures when any of the following criteria is met: • First flight; • After crew change or maintenance action; •...
  • Page 149 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual SPKR switch - ON TEST/RESET switch - Push and hold EMERGENCY/Test Selector (as installed) - Push and hold Advise any maintenance personnel using the FLT Interphone that a test will be done on this communication channel. Simultaneously push the Push-to-Talk switch, the EMERGENCY/Test selector (if installed) and the RESET/TEST switch.
  • Page 150 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Display selector panel ..............Set MAIN PANEL DISPLAY UNITS selector - NORM LOWER DISPLAY UNIT selector - NORM TAKEOFF CONFIG light (as installed) ..... Verify extinguished CABIN ALTITUDE light (as installed) ....Verify extinguished Disengage light TEST switch ..........
  • Page 151 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Standby instruments (as installed) ........... Check Standby horizon ............... Set Gyro caging control ........Pull, then release Approach mode selector ........... OFF Verify that the flight instrument indications are correct. Verify that no flags are shown Standby altimeter ..............
  • Page 152 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Verify that the parking brake warning light is illuminated if the parking brake is applied. Note: do not assume that the parking brake will prevent airplane movement. Accumulator pressure can be insufficient. Check the Hydraulic Brake Pressure Indicator.
  • Page 153 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Preflight Procedures - First Officer Objective: to check and configure aircraft systems. Do the following procedures when any of the following criteria is met: • First flight; • After crew change or maintenance action; •...
  • Page 154 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual NAVIGATION panel ..............Set VHF NAV transfer switch - NORMAL IRS transfer switch - NORMAL FMC source select switch - NORMAL DISPLAYS panel ................Set SOURCE selector - AUTO CONTROL PANEL select switch - NORMAL Fuel panel ..................
  • Page 155 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual GALLEY power switch (as installed) - ON STANDBY POWER switch - Guard closed Verify that the STANDY PWR OFF light is extinguished. Verify that the BAT DISCHARGE light is extinguished. Verify that the TR UNIT light is extinguished.
  • Page 156 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual WINDOW HEAT switches ............ON Position switches ON at least 10 minutes before takeoff. Verify that the OVERHEAT lights are extinguished. Verify that the ON lights are illuminated (except at high ambient temperatures, when some of the lights may not be illuminated).
  • Page 157 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual AIR TEMPERATURE source selector - As needed Note:always monitor supply duct temperatures TRIM AIR switch (as installed) - ON Verify that the DUCT OVERHEAT or the ZONE TEMP lights (as installed) are extinguished.
  • Page 158 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual MAX8 Fleet Only Verify that the BLEED lights are extinguished. Note:if necessary refer to the Supplementary Procedures - Maximum Cooling on the Ground to help keep the airplane as cool as possible. Cabin pressurization panel ............
  • Page 159 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Advise any maintenance personnel using the FLT Interphone that a test will be done on this communication channel. Simultaneously push the Push-to-talk switch, the EMERGENCY/Test selector (if installed) and the RESET/TEST switch.
  • Page 160 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual CABIN ALTITUDE light (as installed) ....Verify extinguished Disengage light TEST switch ..........Hold to 1 Verify that the A/P light is illuminated steady amber. Verify that the A/T light is illuminated steady amber. Verify that the FMC light is illuminated steady amber.
  • Page 161 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual MAX8 Fleet Only Display Select panel............... Set Display Selector switch - PFD/MFD NORMAL GROUND PROXIMITY panel ..........Check FLAP INHIBIT switch - Guard Closed GEAR INHIBIT switch - Guard Closed TERRAIN INHIBIT switch (as installed) - Guard Closed Verify that the GROUND PROXIMITY INOP light is extinguished.
  • Page 162 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual MAX8 Fleet Only Right SELECTOR switch ..............C Overheat and fire protection panel ........... Check Do this check on the first flight in the aircraft if the flight crew did not do the Electrical Power Up supplementary procedure.
  • Page 163 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights stay illuminated. Verify that the WHEEL WELL light stays illuminated. EXTINGUISHER TEST switch - Check TEST switch - Position to 1 and hold Verify that the three green extinguisher test lights are illuminated.
  • Page 164 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual WARNING: Do not key the HF radio while airplane is been fueled. Injury to personnel or fire can occur. WEATHER RADAR control panel ..........Set Note:perform WX Radar Test on the first flight in the aircraft. STABILIZER TRIM override switch ......
  • Page 165 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Preflight Checklist (C): Request “Preflight checklist” (F/O): Do (read aloud) the requested checklist. (F/O): Inform “Preflight Checklist Completed” Note: Preflight checklist must be done when any of the following criteria is met: •First flight;...
  • Page 166 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Before start procedures Objective: to configure the aircraft for each flight. Threats and errors associated with this phase of flight are: • Time pressure; • MCP setting; • Flight documentation; •...
  • Page 167 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Lighting panel ..............Set (F/O) LOGO light switch - As needed Note:ON for night flights. POSITION light switch - As needed Note:STEADY on all night flights, daytime on international flights or when visibility is less than 2000 meters.
  • Page 168 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual FLIGHT DIRECTOR switches - ON Move the switch for the pilot flying to ON first. Bank Angle selector - As needed HDG Selector - Normally set to runway heading (if known). Autopilot DISENGAGE bar - UP EFB .
  • Page 169 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual TRANSPONDER panel ............. Set (F/O) Note:set transponder switches according to master flight director switch. Left Master Flight Director: 1. Right Flight Director: CDU ................Set (C, F/O) Navigation Data - Set ROUTE page: •enter the ORIGIN/Enter the route.
  • Page 170 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Verify that the origin and destination airport are correct. Enter the ETD. Enter the flight time. Enter Fuel Onboard page 2/2. Enter the Captain and First Officer identification number Page on 2/2. When loadsheet is available: OPT ..................Set (C, F/O) Each pilot must calculate the performance data on their own EFB.
  • Page 171 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Verify that a trim value is shown; Enter the takeoff speeds. TAKEOFF REF page 2: Verify or enter the Acceleration Height as indicated on the takeoff analysis; minimum value 400 ft; Verify or enter the Engine Out Acceleration Height as indicated on the takeoff analysis;...
  • Page 172 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Takeoff Briefing OPT BRIEFING ........... Complete (C, F/O) Pilot Flying Pilot Monitoring When all OPT fields are completed OPT compare calculation....Select “No mismatches found”....CALL All performance data must match between OPTs and message “No mismatches found”...
  • Page 173 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual In case of any changes after takeoff briefing is done, pilot flying may address only information that changed. There is no need to perform the complete takeoff briefing again. CDU and EFB display ............Set (C, F/O) The PF selects the TAKEOFF REF page on CDU.
  • Page 174 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual HYDRAULIC PANEL ............Set (F/O) Electric HYDRAULIC PUMP switches - ON Verify that the electric pump LOW PRESSURE lights are extinguished. Verify that the brake accumulator pressure is 2.800 psi minimum.
  • Page 175 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual (F/O): Inform “Before start checklist completed to the line” Start Clearance ATC clearance for pushback and engine start should be obtained after the reading of the Before Start Checklist and all external doors are verified closed.
  • Page 176 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Note:if pushback is not required or LPU (Low Pressure Unit) will be used, the parking brake MUST remain APPLIED after reading the check list. (F/O): Inform “Before Start Checklist completed” (C): Inform to maintenance: “Cleared for pushback, parking brake released”...
  • Page 177 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual CAUTION:do not hold or turn the nose wheel steering wheel during PUSH BACK or towing. This can damage the nose gear or the tow bar. CAUTION:do not use airplane brakes to stop the airplane during PUSH BACK or towing.
  • Page 178 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Engine Start Considerations Normal starter duty cycle: -700 and -800 Fleets Only • Multiple consecutive start attempts are permitted. Each start attempt has a limit of 2 minutes of starter usage. -MAX 8 Fleet Only •...
  • Page 179 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • Failure of the ENGINE START switch to stay in GRD until the starter cutout can cause a hot start. Do not re-engage the ENGINE START SWITCH until engine RPM is below 20% N2; •...
  • Page 180 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Engine Start Procedure Verify that the secondary engine indications are shown ..(C, F/O) Start sequence ..............Announce (C) Obtain the clearance with ground personnel to start the engines. Call “Start Eng. No.___” Air conditioning PACK switches ........
  • Page 181 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual MAX8 Fleet Only At 63% N2, verify that the ENGINE START switch moves to OFF. If not, move the ENGINE START switch to OFF manually. Verify that the START VALVE OPEN alert extinguishes when the ENGINE START switch is in the OFF position.
  • Page 182 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Before Taxi Procedures Threats and errors associated with this phase of flight are: • Aircraft flap configuration; • Wrong taxiways and ramp exits; • Abrupt steering inputs; • Use of prohibited PED’s; •...
  • Page 183 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual APU BLEED air switch ............____ (F/O) Flight controls ..............Check (C) Perform the flight controls check after releasing ground personnel. It is not necessary to wait for the maintenance to move away from the aircraft to start this check.
  • Page 184 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual If both engines have to be started before taxi: After the “Starter Cutout” for the first engine, call for the start of the other engine .................. (C) ISOLATION VALVE switch ......... Closed (F/O) Perform this item only if Engine No.2 was started first.
  • Page 185 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Before Taxi Checklist (Dual Engine) (C): Request “Dual Engine Before Taxi Checklist” (F/O): Do (read aloud) the requested checklist (F/O): Inform “Before Taxi Checklist completed” Lower Display Unit or Secondary Engine Indications The Lower Display Unit or Secondary Engine Indications are to be blanked by the first officer after both engines are running and both pilots check that all respective indications are in the normal range.
  • Page 186 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Taxi Speed Limits: Normal taxi speed is approximately 20 knots, adjusted for conditions. On long straight taxi route speed up to 30 knots is acceptable, however, at speeds higher than 20 knots use caution when using the nose wheel steering wheel to avoid over controlling the nose wheels.
  • Page 187 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual If Single Engine Taxi Out is being performed: When it is predicted to comply with engine warm up recommendations before takeoff, start the second engine considering normal starter duty cycle and abort start conditions.
  • Page 188 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Monitor fuel flow and EGT indications ........(F/O) -700 and -800 Fleets Only At 56% N2, verify that the ENGINE START switch moves to OFF. If not, move the ENGINE START switch to OFF manually. MAX8 Fleet Only At 63% N2, verify that the ENGINE START switch moves to OFF.
  • Page 189 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual FOR SINGLE ENGINE TAXI OUT AFTER BOTH ENGINES ARE RUNNING GENERATORS..................ON (F/O) ANTI ICE....................___ (F/O) APU......................___ (F/O) ENG START SWITCHES..............CONT (F/O) RECALL................CHECKED (BOTH) ENGINE START LEVERS..............IDLE (C) (F/O): Inform “Before Takeoff Checklist completed”...
  • Page 190 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Before Takeoff Procedures Captain First Officer WHEN CLEARED TO ENTER THE TAKEOFF RUNWAY After cabin is secured for take-off: Strobe Lights: ON Wing Lights (night flight): ON Transponder: TA/RA Weather Radar* or TERR on ND Weather Radar* or TERR on ND *Weather radar may be off in daytime VMC flights.
  • Page 191 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual To start the takeoff, the captain advances the thrust levers to approximately 40% N1, allow the engines stabilize and push the TO/GA switch with the aircraft aligned with the runway. Takeoff Threats and errors associated with this phase of flight are: •...
  • Page 192 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring During strong headwinds, if the thrust levers do not advance to the planned takeoff thrust, manually advance the thrust levers before 60 knots. Verify that the correct takeoff thrust is Request “Check Thrust”.
  • Page 193 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Monitor Roll Mode or Request as Monitor or Select a roll mode as needed (LNAV or HDG SEL). requested. Autopilot may be selected ON. Inform FMA Set “Autopilot CMD” Verify and Inform “Autopilot CMD”...
  • Page 194 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Close - In Turn Takeoff Perform this specific procedure only when a turn is to be made after departure, and there is a concern to radius distance limit during this turn. If a close-in turn takeoff will be made, do not arm VNAV.
  • Page 195 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Call “AFTER TAKEOFF CHECKLIST”. Do the “after takeoff checklist”. Inform: “AFTER TAKEOFF If VNAV is not in use, set or request CHECKLIST COMPLETED” VNAV, or “Set speed 250kt”, or in accordance with ATC Takeoff Flap Retraction Speed Schedule TAKEOFF FLAPS...
  • Page 196 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual After Takeoff Procedure The After-Take off phase is one of the last opportunities to properly configure Air Conditioning and Pressurization System. Do the after takeoff checklist meticulously. Threat and errors associated with this phase of flight are: •...
  • Page 197 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual After Takeoff Checklist AFTER TAKEOFF ENGINE BLEEDS ON (PM) ISOLATION AUTO (PM) PACKS AUTO (PM) LANDING GEAR UP and OFF (PM) FLAPS UP, NO LIGHTS (PM) Note:FMC pages for climb PF: CLIMB / PM: LEGS. Note:for Unpressurized Takeoff or No Engine Bleeds Takeoff refer to Supplementary Procedures.
  • Page 198 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Inform: “10.000ft” Fixed Landing Lights / Wing Lights: Acknowledge 10.000ft Pressurization: Check normal operation Supply duct temperature: Check in adequate range Center Tank Fuel Pump must be ON if any quantity of remaining fuel exists.
  • Page 199 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual GMORA Check Verify on Navigation Plan and Inform the PF all GMORA above 10.000 ft. FMS: LEGS FMS: PROGRESS Trim the aircraft using the Primary Rudder Trim Technique, if needed After the first hour of flight, the fuel temperature must be checked every hour in order to avoid fuel freezing.
  • Page 200 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Descent Procedures Threat and errors associated with this phase of flight are: • Rhyming briefing; • Not verbalizing FMA and MCP changes; • Lack of pilot’s dual check prior to FMC changes; •...
  • Page 201 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Refer to EFB’s manual for OPT calculations. Pilot Flying Pilot Monitoring When both OPT fields are completed OPT compare calculation (if available)........Select “No mismatches found”.....CALL All performance data must match between OPTs and message “No mismatches found”...
  • Page 202 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Start the Descent Procedure before the airplane descends below the cruise altitude for arrival at destination. Pilot Flying Pilot Monitoring Before Descent Verify that pressurization is set to landing altitude. Logo Light (if applicable) –...
  • Page 203 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Maintain descent ECON speed according to company policy, airspace, ATC or arrival’s speed restrictions. Acknowledge Inform: “MSA” Select TERRAIN on the NAV Display. WARNING: GPWS – Any alert received below MSA must be considered as real.
  • Page 204 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual “B” - When NAV Radios are not in use for navigation If after the approach briefing is done and the NAV radios will not be used during the descent (RNAV Star for example), the “set radios for approach” procedure should be done immediately after the “approach briefing”...
  • Page 205 For a GLS approach, select the appropriate GLS channel. For an ILS, LOC, BCRS, SDF or LDA approach, select the appropriate localizer frequency. GOL does not perform BCRS approaches. Flap Extension Schedule Current flap position and speed Select flaps and command speed 30 or 40 Note: the PM must callout “Speed check”...
  • Page 206 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Autoland Must be performed landing flaps 30 or 40. Wind information: Obtained from FMC Progress Page 2/4 Landing Checklist Notes • If a runway change occurs after the LANDING CHECKLIST is read, perform the LANDING CHECKLIST once again.
  • Page 207 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • When on localizer intercept heading, verify that the ILS is tuned and identified, and that the LOC and G/S pointers are shown. • ILS based on RNAV STAR: The ILS should be intercepted in LNAV/VNAV when executing a RNAV ILS.
  • Page 208 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual ILS APPROACHES Pilot Flying Pilot Monitoring Request flaps extension on schedule up Set Flap lever as directed. to Flaps 5. Fasten Belts Switch – ON: when “Flap 1” is requested If on radar vectors, the following modes Inform: “LOCALIZER ALIVE”...
  • Page 209 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual ILS APPROACHES Pilot Flying Pilot Monitoring 100FT above minimum Acknowledge Inform: “approaching minimums”. 200FT AFE Acknowledge Inform: “wind: _____” Inform: “RWY / APP lights in Sight / Inform: “Minimums” Not in sight”.
  • Page 210 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual ILS CAT II (Autoland) Pilot Flying Pilot Monitoring Shortly after the APP MODE has been selected engage the second A/P. Inform “VOR/LOC and G/S armed”. Verify that the localizer is captured. Outer Marker Confirm OM__________ft- Inform: “OM ________ft”...
  • Page 211 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual ILS CAT 2 NOTES Before starting this procedure the crew must read the ILS CAT II Crew Review at QRH Operator Information chapter. Set “BARO minimums” in accordance with the approach chart to have the bug set in the altimeter, and than set “RADIO minimums”.
  • Page 212 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • Do not use LVL CHG mode after IAF. VNAV should be used or V/S may be used. • A follow up of the procedure is mandatory to the crew. Altitude must be released step by step and can only be released to the next restriction when compliance is assured, and should occur about 2 NM prior to the next waypoint;...
  • Page 213 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • Insert the VDP in non-precision approaches if a glide path is not available (FIX page FMC). The VDP defines the point where a missed approach should be initiated: Land or Missed Approach (at MDA height).
  • Page 214 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring Set or request the next “Step Down Set the next “Step Down Restriction” or Restriction” or “MDA“ on MCP “MDA” on MCP on request Just before 1000FT AFE, or 4 NM to RWY THR (whichever occur first) Request: “Flap _____”...
  • Page 215 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual RNAV - APV BARO V-NAV • Do not use LVL CHG mode after IAF. VNAV should be used or V/S may be used. • The above pattern is indicated for standard operation. Deviations by ATC, heavy or light gross weight, head or tailwind, must be worked upon.
  • Page 216 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • Check if GPS is installed (FMC - POS INIT page 2/3) and check GPS update ON (FMC - NAV Options page 2/2); • Approach is not allowed with “UNABLE REQUIRED NAV PERF”...
  • Page 217 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • 3 nm prior FAF, the PF requests “Landing Gear Down, Flaps 15, Landing Checklist”. This will be the final configuration for a One Engine Inoperative approach; • PM reads aloud and do “Landing Checklist”. Visually confirms flap and gear positions;...
  • Page 218 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Select Gear and flap lever as requested. Request: “Gear Down, Flaps 15, Callout “Gear Down” when 3 green Landing Checklist” lights are on. Verify green SPEEDBRAKE ARMED Set SPEEDBRAKE handle in ARM. light illuminated.
  • Page 219 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • Do not use LVL CHG mode after IAF. VNAV should be used. • RNP - AR APPROACH CREW REVIEW CARD must be read before the approach; • RNP - AR operations should not exceed the temperature charts limits;...
  • Page 220 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • After FAF and at least 300ft below the missed approach altitude, set the existing Go Around altitude restriction on the missed approach altitude on the MCP; • 3 nm prior FAF, the PF requests “Landing Gear Down, Flaps 15 and Landing Checklist”.
  • Page 221 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual RNP AR APCH Pilot Flying Pilot Monitoring When NAV Radios are not in use for navigation: “Set Radios” flow procedure: • Rwy_____; Dry or Wet Set the RNP-AR APCH final •...
  • Page 222 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring After FAF and at least 300ft below the missed approach altitude Set the existing Go around altitude restriction or the missed approach altitude on Verify if the MCP is correctly set. the MCP.
  • Page 223 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Visual Approach • Select Flap 5 before entering downwind leg; • Abeam of landing threshold start chronometer; • 20 seconds after threshold, select Landing Gear down and Flaps 15, perform Landing Check List (this will be the final configuration for a One Engine Inoperative Landing);...
  • Page 224 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual VISUAL APPROACHES Pilot Flying Pilot Monitoring When cleared for approach confirm conditions: Adjust: “Panel or Radios” according to the PF request. • Rwy; If applicable, before starting visual • Dry or Wet; traffic pattern, insert on FMC Approach •...
  • Page 225 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual AT 1000FT AFE Acknowledge Inform: “1000 ft” For the ‘NOT STABILIZED GO-AROUND” callout, inform: Observe and inform: ‘STABILIZED” or ”GO-AROUND”, and perform the “NOT STABILIZED-GO-AROUND” MISSED APPROACH 500FT AFE Inform: “500 ft - wind:______”.
  • Page 226 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Go–around and missed approach procedures Pilot Flying Pilot Monitoring Inform decision: “Go-Around”. Disengage Autopilot Push TOGA switch and advance thrust Verify / adjust Go-Around Thrust. levers to Go-Around Thrust “Go-Around Thrust Set”...
  • Page 227 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Go–around and missed approach procedures ILS CAT II Pilot Flying Pilot Monitoring Inform decision: “Go-Around”. Push TOGA switch Monitor A/P rotates to go–around attitude; Monitor A/T sets go–around Thrust. Push TOGA switch again to obtain full Verify / adjust Go-Around Thrust Go-around N1 thrust (if necessary)
  • Page 228 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Landing Threat and errors associated with this phase of flight are: • Long flare; • Touchdown beyond AIMING POINT; • Adverse weather conditions; • Lack of reject landing decision; •...
  • Page 229 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Circling Approaches As determined by company policy, the Circling Approaches can only be performed when authorized in the Airport Briefing chart. In this case the weather minimums must be always greater than: •...
  • Page 230 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring Apply reverse thrust as needed. By 60 knots, start movement of the reverse thrust levers to be at the reverse idle detent before taxi speed. After the engines are at reverse idle, move the reverse thrust levers full down.
  • Page 231 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual WARNING: After the reverse thrust levers are moved, a full stop landing must be made. If an engine stays in reverse, safe flight is not possible. After landing procedures Start the After Landing Procedure only when clear of the active runway or initiating back track.
  • Page 232 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Transponder ............As Required (F/O) Set the transponder mode selector as needed.When crossing runaway or backtracking set transponder ON. At airport where ground tracking is not available, select STBY. At airport equipped to track airplanes on the ground, select an active transponder setting, but not TCAS mode.
  • Page 233 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual • During “taxi in” it is prohibited to the first officer to perform procedures other than those related as “after landing procedures” and assisting the Captain. The MCP, overhead panel and FMC should not be prepared to the next flight at this time.
  • Page 234 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Shutdown Procedures Start the Shutdown Procedures after aircraft comes to a complete stop. PARKING BRAKE ..............Set (C) Verify warning light is illuminated. Check Electrical Power. Engine start levers...............Cutoff (C) Operate the engines at or near idle thrust for a minimum of three minutes before shutdown to thermally stabilize the engines and reduce undercowl soak-back temperatures.
  • Page 235 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual After Parking Brake is released and aircraft is confirmed to be parked: FUEL PUMP switches ............OFF (F/O) Note:whenever the APU is running and AC electrical power is on the buses, turn on one fuel bust pump to supply fuel under pressure to the APU to extend the service life of its fuel control unit.
  • Page 236 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Verify IRS left and right residual Ground Speed, at maximum 2 minutes after shutting down engines. Ground speed above 15kt requires maintenance action, and must be reported in the Technical Log.
  • Page 237 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual (F/O): Inform “Shutdown Checklist completed” Secure Checklist Perform this procedure when: • Aircraft will stay overnight; • Crew change (not immediately); • Considerable aircraft ground time with crew on board. IRS mode selectors ...............OFF (C) CAB/UTIL power switch (as installed) ....As required (F/O) Switching CAB/UTIL OFF in Sky Interior equipped aircraft will...
  • Page 238 Normal Procedures - Amplified Procedures 737 MAX Flight Crew Operations Manual Intentionally Blank March 1, 2021 MN-FLT-OH-201 NP.21.102...
  • Page 239 Supplementary Procedures Supplementary Procedures Supplementary Procedures Table Of Contents 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Table of Contents Section TOC Introduction .........SP.05 General .
  • Page 240 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual #No Engine Bleed Takeoff and Landing ....SP.2.7 Takeoff ......... . .SP.2.7 After Takeoff.
  • Page 241 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Communications ........SP.5 Aircraft Communication Addressing and Reporting System (ACARS) .
  • Page 242 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Inadvertent Selection of Attitude Mode (while on the ground) ........SP.11.3 IRS Entries .
  • Page 243 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Intervention of FMC Altitude Constraints during VNAV Climb ........SP.11.16 Intervention of FMC Cruise Altitude during VNAV Cruise SP.11.16 Intervention of FMC Altitude Constraints during VNAV Descent .
  • Page 244 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Refueling ......... . .SP.12.4 Fuel Load Distribution .
  • Page 245 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Secure Procedure ....... . . SP.16.16 # Maximum Cooling on the Ground - APU Bleed .
  • Page 246 Supplementary Procedures - Table of Contents 737 MAX Flight Crew Operations Manual Intentionally Blank SP.TOC.8 MN-FLT-OH-201 October 26, 2021...
  • Page 247 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Introduction Section 05 05 Introd uction Introduction File Highlight General This section contains procedures (adverse weather operation, engine crossbleed start, and so on) that are accomplished as required rather than routinely performed on each flight.
  • Page 248 Supplementary Procedures - Introduction 737 MAX Flight Crew Operations Manual Intentionally Blank SP.05.2 MN-FLT-OH-201 March 1, 2021...
  • Page 249 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Airplane General, Emer. Equip., Doors, Windows Section 1 1 Airplane General, Emer. Equip., Doors, Windows Airplane General, Emer. Equip ., Doors, Windows File Highlight Interior Inspection Emergency exit lights ..............Check Passenger signs ................
  • Page 250 Supplementary Procedures - Airplane General, Emer. Equip., Doors, Windows 737 MAX Flight Crew Operations Manual Before the Flight The availability, accessibility and serviceability of the emergency systems and equipment must be checked. All supernumeraries must be briefed by one of the pilots on the safety information: •...
  • Page 251 Supplementary Procedures - Airplane General, Emer. Equip., Doors, Windows 737 MAX Flight Crew Operations Manual The imminent takeoff must be announced on the PA in accordance to the SOP, reinforcing the need to remain seated with the seat belts fastened. During the Flight If turbulence is expected or encountered the Fasten Seat Belts sign must be switched ON and an announcement is to be made on the PA regarding to...
  • Page 252 Supplementary Procedures - Airplane General, Emer. Equip., Doors, Windows 737 MAX Flight Crew Operations Manual Water System Draining Lavatory water supply selector valves ......SUPPLY/DRAIN Galley water supply shutoff valves ........SUPPLY ON The shutoff valve is found adjacent to each wet galley sink. Drain line ...............Connect to drain ports •...
  • Page 253 Supplementary Procedures - Airplane General, Emer. Equip., Doors, Windows 737 MAX Flight Crew Operations Manual Power distribution panel number 1 • POT WATER COMPRESSOR • WATER QTY IND Oxygen Mask Microphone Test YA201 - YA611, YA648 - YA6 57, YB271, YC453, YD256, YN107 - YN11 2 MASK/BOOM switch ..............
  • Page 254 Supplementary Procedures - Airplane General, Emer. Equip., Doors, Windows 737 MAX Flight Crew Operations Manual Fuel Crossfeed Valve Check Unless accomplished by maintenance personnel prior to the ETOPS flight, do the following steps on the ground prior to engine start: Crossfeed selector ..............
  • Page 255 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Air Systems Section 2 2 Air Systems Air Systems File Highlight Wing–Body Overheat Test Wing–body OVHT TEST switch ............Push Hold for a minimum of 5 seconds. Both WING–BODY OVERHEAT lights – illuminated MASTER CAUTION –...
  • Page 256 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual APU BLEED air switch ............ON APU supplies left pack and external air source supplies right pack. # Air Conditioning from an External Air Conditioning Unit (ACU) Before connecting ground conditioned air: PACK switches ..................OFF Packs can be damaged if they are operated while ground conditioned air is connected.
  • Page 257 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual Outflow valve switch ..............CLOSE Verify outflow valve position indicator moves toward CLOSE. Outflow valve switch ..............OPEN Verify outflow valve position indicator moves toward OPEN. Pressurization mode selector ............AUTO Verify outflow valve position indicator moves toward OPEN.
  • Page 258 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual Outflow valve switch (momentarily) ........ CLOSE During descent, intermittently position the outflow valve switch toward CLOSE, observing cabin altitude decrease as the airplane descends. Before entering the landing pattern, slowly position the outflow valve to full open to depressurize the airplane.
  • Page 259 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual If landing altitude is above 6000 feet: Do the Automatic Pressurization Control - Landing Airport Elevation Above 6000 Feet supplementary procedure. Return to Departure Airport is Needed HIGH ALT LDG switch ..............ON If landing elevation is above 10,000 feet: Oxygen masks and regulators ........
  • Page 260 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual LAND ALT indicator ....Destination field elevation #Unpressurized Takeoff and Landing When making a no engine bleed takeoff or landing with the APU inoperative, or operative but not providing bleed air: Takeoff PACK switches ................
  • Page 261 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual #No Engine Bleed Takeoff and Landing When making a no engine bleed takeoff or landing with the APU operating. Takeoff Note: If anti–ice is required for taxi, configure for a “No Engine Bleed Takeoff”...
  • Page 262 Supplementary Procedures - Air Systems 737 MAX Flight Crew Operations Manual Engine No. 1 BLEED air switch ............ON ISOLATION VALVE switch ............AUTO Landing If additional go–around thrust is desired, configure for a “No Engine Bleed Landing.” When below 10,000 feet: WING ANTI-ICE switch .............OFF Right PACK switch ..............
  • Page 263 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Anti–Ice, Rain Section 3 3 Anti–Ice, Rain Anti–Ice, Rain File Highlight Anti–Ice Operation Requirements for use of anti–ice and operational procedures for engine and wing anti–ice are contained in Supplementary Procedures, Adverse Weather Section SP.16.
  • Page 264 Supplementary Procedures - Anti–Ice, Rain 737 MAX Flight Crew Operations Manual If there is frost or ice on the lower surface outboard of measuring stick 4, there may also be frost or ice on the upper surface. The distance that the frost extends outboard of measuring stick 4 can be used as an indication of the extent of the frost on the upper surface.
  • Page 265 Supplementary Procedures - Anti–Ice, Rain 737 MAX Flight Crew Operations Manual If there is frost or ice on the lower surface outboard of measuring stick 4, there may also be frost or ice on the upper surface. The distance that the frost extends outboard of measuring stick 4 can be used as an indication of the extent of the frost on the upper surface.
  • Page 266 Supplementary Procedures - Anti–Ice, Rain 737 MAX Flight Crew Operations Manual Window Heat System Tests Overheat Test The overheat test simulates an overheat condition to check the overheat warning function of the window heat system. WINDOW HEAT switches ..............ON WINDOW HEAT TEST switch ............
  • Page 267 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Automatic Flight Section 4 4 Auto matic Flight Automatic Flight File Highlight Level Change Climb/Descent ALTITUDE selector ..........Set desired altitude Note: If a new MCP altitude is selected while in ALT ACQ, the AFDS engages in V/S and the existing vertical speed is maintained.
  • Page 268 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual Pitch mode – V/S IAS/MACH Selector .......... Set desired speed Intervention of FMC Altitude Constraints during VNAV Climb YC09 5, YC572, YC573 , YF631 - YF832, YL801 - YM648, YN701 - YV671 MCP altitude selector .............
  • Page 269 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual ALT INTV switch ................Push Each push of the ALT INTV switch will delete an FMC altitude constraint. If all FMC altitude constraints are deleted, the descent mode will revert to a VNAV speed descent.
  • Page 270 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual When on an intercept heading to the VOR course: VOR LOC mode switch ............Push Verify VOR LOC armed mode annunciates. A/P automatically captures the VOR course. Verify VOR LOC engaged mode annunciates upon course capture.
  • Page 271 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring Use LNAV or other roll mode to intercept the final approach course as needed. Approximately 2 NM before the final Approximately 2 NM before the final approach fix, set the first intermediate approach fix, call “APPROACHING altitude constraint or MDA(H).
  • Page 272 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual At the final approach fix, crosscheck the altimeters. Verify they agree within 100 feet. Approximately 300 feet above MDA(H): MCP altitude ........Set missed approach altitude At MDA(H)/missed approach point: If suitable visual reference is not established, execute missed approach.
  • Page 273 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual HDG SEL switch ................Push Verify HDG SEL mode annunciates. Before starting the turn to base: • Landing flaps (if not previously selected) • Do the LANDING checklist. Intercepting the landing profile: Autopilot disengage switch ............Push Autothrottle disengage switch ..........Push Instrument Approach - RNAV (RNP) AR...
  • Page 274 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual Note: Do the Go-Around and Missed Approach Procedure if the UNABLE REQD NAV PERF-RNP, FMC DISAGREE, or any VERIFY POS alerting message is shown unless suitable visual reference is established and maintained. (SB Changes YF631, YF632, YL621, YR619) WARNING: If an UNABLE REQD NAV PERF-RNP is shown during the approach, whether the lateral or vertical...
  • Page 275 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual Descent Procedure Pilot Flying Pilot Monitoring In the approach briefing include speed Select VOR UPDATE - OFF on the and altitude restrictions, missed NAV OPTIONS page. approach, engine failure, and unable Inhibit other navaids as needed per RNP procedures.
  • Page 276 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring Select TERR on map. Select TERR or WX radar on map. Select CDU: ACT RTE X LEGS page. Use LNAV and VNAV or other pitch mode for initial descent. VNAV is required from the FAF inbound.
  • Page 277 Supplementary Procedures - Automatic Flight 737 MAX Flight Crew Operations Manual Pilot Flying Pilot Monitoring At the final approach fix, verify the crossing altitude and crosscheck altimeters within 100 feet between primary altimeters. Monitor the approach. If suitable visual reference is established at DA(H), disengage the autopilot in accordance with regulatory requirements, and disengage the...
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  • Page 279 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Communications Section 5 5 Communications Commu nications File Highlight Aircraft Communication Addressing and Reporting System (ACARS) YA605 - YA6 10, YA631 , YA683, YA684, YB107 - YB112, YB271, YC095, YC572, YC573, YD303, YD307, YF703 - YK653, YK727 - YV671 The following procedures are applicable to the noted ACARS functions from the company pages.
  • Page 280 Supplementary Procedures - Communications 737 MAX Flight Crew Operations Manual Cockpit Voice Recorder Test YA201, YA202, YA571 - YA657, YB104 - YC453, YD256 - YF632, YF801, YK652 - YN702, YR601 - YR663, YT702 - YV671 YA571, YA608 - YA 657, YB104 - YC453, YD256, YF631, YF632, YF801, YL621, YL954 - YN112, YV401 - YV6 71 Note: The Cockpit VOICE RECORDER switch must be in the ON position or at least one engine must be operating to perform this test.
  • Page 281 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Electrical Section 6 6 Electrical Electrical File Highlight #Electrical Power Up The following procedure is accomplished to permit safe application of electrical power. BATTERY switch ............... Guard closed Note: Do not move the airplane until Integrated Standby Flight Display (ISFD) alignment is complete.
  • Page 282 Supplementary Procedures - Electrical 737 MAX Flight Crew Operations Manual If the FAULT light fails to illuminate, the fault monitoring system is inoperative. Verify that the APU DET INOP light is illuminated. Do not operate the APU if the APU DET INOP light fails to illuminate.
  • Page 283 Supplementary Procedures - Electrical 737 MAX Flight Crew Operations Manual Note: If extended APU operation is needed on the ground and the airplane busses are powered by AC electrical power, position an AC powered fuel pump ON. This will extend the service life of the APU fuel control unit.
  • Page 284 Supplementary Procedures - Electrical 737 MAX Flight Crew Operations Manual Verify that the WHEEL WELL fire warning light is illuminated. #Electrical Power Down This procedure assumes the Secure procedure is complete. APU switch and/or GRD POWER switch ........OFF If APU was operating: Delay approximately 2 minutes after the APU GEN OFF BUS light extinguishes before placing the BATTERY switch OFF.
  • Page 285 Supplementary Procedures - Electrical 737 MAX Flight Crew Operations Manual DC meter selector ................BAT Check DC voltmeter for normal indication: 24 +/- 2 volts. Check DC ammeter for discharge indication: a negative value. DC meter selector ..............AUX BAT Check DC voltmeter for normal indication: 24 +/- 2 volts.
  • Page 286 Supplementary Procedures - Electrical 737 MAX Flight Crew Operations Manual Intentionally Blank SP.6.6 MN-FLT-OH-201 March 1, 2021...
  • Page 287 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Engines, APU Section 7 7 Engines, APU Engin es, APU File Highlight Battery Start (With APU bleed or ground air available) Maintenance documents ..............Check FLIGHT DECK ACCESS SYSTEM YA201 - YA2 21, YA571 , YA605 - YA657 , YB104 - YC095, YD2 56, YF631 - YV671 switch ..................
  • Page 288 Supplementary Procedures - Engines, APU 737 MAX Flight Crew Operations Manual APU switch (bleed air source, if available)..........START On the captain's command, the first officer reads and the captain does the following items: Oxygen ................ Test and set YA221, YA631 - YA 650, YA683, YA684, YB11 2, YB119, YC095, YC453, YD256 - YV671 CAB/UTIL power switch (as installed) ........
  • Page 289 Supplementary Procedures - Engines, APU 737 MAX Flight Crew Operations Manual Engine Start Engine No. 1 start ............Accomplish Only N1, N2, and oil quantity are displayed until the EECs are powered. Generator 1 switch ..............ON IRS mode selectors ..........OFF, then NAV Verify that the ON DC lights illuminate, then extinguish Verify that the ALIGN lights are illuminated.
  • Page 290 Supplementary Procedures - Engines, APU 737 MAX Flight Crew Operations Manual ENGINE panel ................Set Verify that the REVERSER lights are extinguished Verify that the ENGINE CONTROL lights are extinguished EEC switches - ALTN then ON Oxygen panel ................Set CREW OXYGEN pressure indicator - Check Verify that the pressure meets dispatch requirements.
  • Page 291 Supplementary Procedures - Engines, APU 737 MAX Flight Crew Operations Manual WARNING: To minimize the hazard to ground personnel, the external air should be disconnected, and engine No. 2 started using the Engine Crossbleed Start procedure. March 1, 2021 MN-FLT-OH-201 SP.7.5...
  • Page 292 Supplementary Procedures - Engines, APU 737 MAX Flight Crew Operations Manual #Engine Crossbleed Start Do not accomplish a crossbleed start during pushback. Before using this procedure, ensure that the area to the rear is clear. Engine BLEED air switches............... ON APU BLEED air switch ..............OFF PACK switches ..................OFF ISOLATION VALVE switch ............
  • Page 293 Supplementary Procedures - Engines, APU 737 MAX Flight Crew Operations Manual High Altitude Airport Engine Start (Above 8400 Feet) YK721 - YK725, YR601 - YR605 Engine start ................Accomplish An indication of N1 rotation plus maximum motoring and a minimum of 20% N2 are required prior to introducing fuel to the engine.
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  • Page 295 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Fire Protection Section 8 8 Fire Protectio n Fire Protection File Highlight Fire and Overheat System Test with an Inoperative Loop YA201 - YT602 To determine the specific inoperative loop: OVHT DET switches..............
  • Page 296 Supplementary Procedures - Fire Protection 737 MAX Flight Crew Operations Manual Intentionally Blank SP.8.2 MN-FLT-OH-201 March 1, 2021...
  • Page 297 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Flight Instruments, Displays Section 10 10 Flig ht Instruments, Display s Flight Instrumen ts, Displays File Highlight Altimeter Difference Note: If flight in RVSM airspace is planned use the RVSM table in the limitations section.
  • Page 298 Supplementary Procedures - Flight Instruments, Displays 737 MAX Flight Crew Operations Manual If it is not possible to identify which altimeter is indicating the correct altitude: ATC ..................Notify SP.10.2 MN-FLT-OH-201 March 1, 2021...
  • Page 299 Supplementary Procedures - Flight Instruments, Displays 737 MAX Flight Crew Operations Manual Setting Airspeed Bugs with No Operative FMC (Manual Airspeed Bug Setting) To set reference airspeed bugs for takeoff: Speed reference selector (outer) ..........V1 Default speed of 80 knots is displayed. Speed reference selector (inner) .......
  • Page 300 Supplementary Procedures - Flight Instruments, Displays 737 MAX Flight Crew Operations Manual Note: When the flap lever is set to any takeoff flap setting above flaps 1, a bug comes into view for the next smaller flap maneuvering speed, between takeoff flaps and flaps up. For example, if the flap lever is set to 15 for takeoff, a bug for flaps 5 maneuvering speed will appear.
  • Page 301 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Flight Management, Navigation Section 11 11 Flig ht Management, Navigatio n Flight Management, Navigation File Highlight Tests Transponder Test This procedure requires the IRSs to be aligned and in NAV mode. Transponder reply selector..........ON or AUTO YA201 - YA2 21, YL95 4 - YL956 Transponder ..................
  • Page 302 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual WXR (EFIS control panel) ............ON Weather Radar Mode ............TEST Verify the amber WINDSHEAR caution, red WINDSHEAR warning and PWS FAIL annunciations display momentarily and then extinguish. Note: In the short time the weather radar is on and not in the TEST position, it will radiate.
  • Page 303 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Note: Approximately five to seventeen minutes are required for alignment. If ALIGN light continues to flash, maintenance action is required. Fast Realignment Prior to commencing procedure the airplane must be parked and not moved until procedure is complete and ALIGN lights extinguish.
  • Page 304 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Latitude ....................Enter Key–in latitude in the data display, beginning with N or S, then press the ENT Key (the Cue Lights extinguish). Longitude ..................Enter Key–in longitude in the data display, beginning with E or W, then press the ENT key (the cue lights extinguish).
  • Page 305 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Proceeding Direct to a Waypoint (DIR/INTC) YA251 - YA601, YA611, YA648, YA650, YB104, YB119, YC453 , YF6 31, YF632, YK652, YK653 DIR INTC key .................. Push Observe DIRECT TO box prompts displayed in line 6L. Enter desired waypoint on the DIRECT TO line.
  • Page 306 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Correct any ROUTE DISCONTINUITY if the entered waypoint was not in original flight plan. EXEC key ..................Push Observe MOD RTE LEGS page changes to ACT. LNAV may disengage after execution of an intercept leg to a waypoint.
  • Page 307 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Route Copy YA601 - YA648, YA657, YA683, YB111 - YB119, YC095, YC453 , YC5 73, YD256, YF631 - YF 801, YK721 - YK728, YK730 - YK737, YK739, YK740, YK751, YK752, YK758, YK760 - YK762, YK764 - YK767, YK769, YK770, YL801 - YL809, YL811 - Y L813, YL815 - YN109, YN 261 - YN702, YR602 - YR617, YR619, YR624, YR626 - YR628, YR630, YR631, YR634 - YR661, YR663 - YV671 (SB Changes YK753 - YK756, YL621) ACT RTE x LEGS or ACT RTE x page .........
  • Page 308 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Note: If ETA and DTG are not displayed, the fix radial and/or distance do not intersect the route. Changing Destination RTE page ..................Select Enter the new destination over the original DEST. Enter desired routing to the new destination using the RTE, RTE LEGS, and ARRIVALS pages, as appropriate.
  • Page 309 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual EXIT HOLD line select key ............. Push Observe EXIT HOLD prompt changes to EXIT ARMED. EXEC key ..................Push Observe EXIT ARMED is highlighted in reverse video and LNAV flight returns to the holding fix and resumes the active route.
  • Page 310 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Enter into the route by line selecting to the appropriate waypoint sequence. Repeat the above steps to define additional created waypoints as desired. Correct any ROUTE DISCONTINUITY. EXEC key ..................Push Observe the MOD RTE or MOD RTE LEGS page changes to ACT (for an inactive route, activate and execute on the RTE or RTE LEGS page).
  • Page 311 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual EXEC key illuminates when data has been entered into all box prompts. EXEC key ..................Push Repeat above steps to define additional created waypoints as desired. To enter a new identifier in the same category, simply overwrite the previous identifier.
  • Page 312 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Line select the desired intersection (lines 2L–5L) into the scratch pad and observe the new created waypoint displayed as FIX/Radial/Distance. RTE LEGS page ................Select Line select the new created waypoint, displayed in the scratch pad, to the desired waypoint sequence.
  • Page 313 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual TRANSITION (if required) ............Reselect RTE LEGS page ................Select WAYPOINT SEQUENCE and ALTITUDES ........ Check Modify as necessary to agree with clearance. EXEC key ..................Push Change STAR, PROF DES, or APP The associated airport must be entered as route origin or destination.
  • Page 314 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Other Operations FMC Navigation Check YA601 - YA648, YA 657, YA683, YB111 - YB119, YC095, YC453, YC573, YD256, YF631 - YF 801, YK721 - YK728, YK730 - YK737, YK739, YK740, YK751, YK752, YK758, YK760 - YK762, Y K764 - YK767, YK769, YK770, YL801 - YL809, YL811 - Y L813, YL815 - YN109, YN 261 - YN702, YR602 - YR617, YR619, YR624, YR626 - YR628, YR630, YR631, YR634 - YR661, YR66 3 - YV6 71 Do the following as needed to ensure navigation accuracy if any alerting (SB Changes YK753 - YK756, YL621)
  • Page 315 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Inhibiting VOR/DME Use for Position Updating Note: This procedure inhibits the use of VOR/DME information for FMC position updating. Use DEL key to remove a VOR/DME from inhibit status. PROG page ..................
  • Page 316 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual ALT INTV switch (as installed) ..........Push YC09 5, YC572, YC573, YD3 03, YD307, YF703 - YF832, YR528, YR61 8 - YV671 Climb or descent is initiated. Mode annunciations appear as initial climb or descent.
  • Page 317 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual ALT INTV switch ................Push Each push of the ALT INTV switch will delete an FMC altitude constraint. If all FMC altitude constraints are deleted, the descent mode will revert to a VNAV speed descent.
  • Page 318 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual EXEC key ..................Push Observe MOD RTE LEGS page changes to ACT and restriction is deleted and replaced with an FMC predicted value (small size characters). Changing Speed and/or Altitude Restriction during Climb or Descent CLB/DES page ................
  • Page 319 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Step Climb or Descent from Cruise MCP altitude selector ................Set Set new level–off altitude. FLT ALT indicator ................Set Set new level–off altitude. CRZ page ..................Select Enter new altitude on the CRZ ALT line. The display changes to MOD CRZ CLB or MOD CRZ DES.
  • Page 320 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual RTE DATA page ................Select Enter the estimated true wind direction/speed on the appropriate line(s). Step Climb Evaluation CRZ page ..................Select Enter the desired step climb altitude on the STEP line. If known, enter the estimated average true wind direction/speed for the desired step climb altitude on the ACTUAL WIND line.
  • Page 321 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Engine Out Engine out climb and cruise pages provide advisory information for engine out operation. Refer to section 11.41 and 11.42 for a complete description of ENG OUT CLB and ENG OUT CRZ pages. Required Time of Arrival (RTA) Note: An active FMC flight plan complete with all performance data must exist before the required time of arrival (RTA) mode can be...
  • Page 322 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual Entering New Time Error Tolerances for RTA Navigation PERF LIMITS page ............... Select Enter desired time error tolerance (5 to 30 seconds) for the RTA waypoint on line 1L (Example: 25). Observe MOD PERF LIMITS page displayed and EXEC key illuminated.
  • Page 323 Supplementary Procedures - Flight Management, Navigation 737 MAX Flight Crew Operations Manual RWY ..................Enter Reenter runway on RTE page. Check and reenter other performance data as required. March 1, 2021 MN-FLT-OH-201 SP.11.23...
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  • Page 325 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Fuel Section 12 12 Fuel Fu el File Highlight Spar Fuel Shutoff Valve Operational Check YA201 - YB271, YC453 - YD25 6, YF631, YF632 , Y K652 - YL815, YN107 - YN70 2, YR601 - YR648, YR661 - YR663 (SB Cha nges YD303, Y D307) Note: Regulatory approval for use of the following flight crew procedure(s) is required.
  • Page 326 Supplementary Procedures - Fuel 737 MAX Flight Crew Operations Manual 2. Spar Fuel Shutoff Valve Operational Check During Engine Start Engine start lever (first engine) ............IDLE Verify SPAR VALVE CLOSED light transitions from dim, to bright and then extinguishes. Engine start lever (second engine) ..........
  • Page 327 Supplementary Procedures - Fuel 737 MAX Flight Crew Operations Manual When quantities are balanced: Fuel pump switches (main tank) ........ON Center tank fuel pump switches ........ON Crossfeed selector ............Close If the center tank contains no fuel: Crossfeed selector ..............Open Fuel pump switches (low tank) ..........
  • Page 328 Supplementary Procedures - Fuel 737 MAX Flight Crew Operations Manual Refueling Fuel Load Distribution Main tanks No. 1 and No. 2 should normally be serviced equally until full. Additional fuel is loaded into the center tank until the desired fuel load is reached.
  • Page 329 Supplementary Procedures - Fuel 737 MAX Flight Crew Operations Manual Note: Main tanks No. 1 and No. 2, and the center tank refueling valves each have a red override button that must be pressed and held while fuel is being pumped into the tank.
  • Page 330 Supplementary Procedures - Fuel 737 MAX Flight Crew Operations Manual Crossfeed selector ................Close Main tank fuel pump switches ............OFF Main Tanks ..................Refill Refueling panel and defuel panel access doors ....... Close Fuel Crossfeed Valve Check Crossfeed selector ................Open Verify crossfeed VALVE OPEN light illuminates bright and then dim.
  • Page 331 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Warning Systems Section 15 15 Warning Systems Warning Systems File Highlight Ground Proximity Warning System (GPWS) Test Verify IRS alignment is complete. Verify that the guards are closed for all GROUND PROXIMITY INHIBIT switches.
  • Page 332 Supplementary Procedures - Warning Systems 737 MAX Flight Crew Operations Manual • “TERRAIN TERRAIN PULLUP" aural sounds • terrain display test pattern shows on navigation displays • TERRAIN caution message shows on navigation displays. • "OBSTACLE OBSTACLE PULLUP" aural sounds •...
  • Page 333 Supplementary Procedures - Warning Systems 737 MAX Flight Crew Operations Manual • Landing OAT on the ground is below -40°C or greater than +50°C • Gross weight is greater than maximum landing weight. RUNWAY INHIBIT switch ..........INHIBIT Note: If the RUNWAY INHIBIT switch is in the INHIBIT position, and the airspeed is 250 knots or greater for 60 seconds or more, the RUNWAY INOP light illuminates.
  • Page 334 Supplementary Procedures - Warning Systems 737 MAX Flight Crew Operations Manual Intentionally Blank October 26, 2021 SP.15.4 MN-FLT-OH-201...
  • Page 335 737 MAX Flight Crew Operations Manual Supplementary Procedures Chapter SP Adverse Weather Section 16 16 Adv erse Weather Adverse Weather File Highlight Introduction Airplane operation in adverse weather conditions may require additional considerations due to the effects of extreme temperatures, precipitation, turbulence and windshear.
  • Page 336 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Icing conditions exist when OAT (on the ground) or TAT (in flight) is 10°C or below and any of the following exist: • visible moisture (clouds, fog with visibility of one statute mile (1600m) or less, rain, snow, sleet, ice crystals, and so on) is present, •...
  • Page 337 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Air conditioning inlets and exits ............ Check Verify that the air inlets and exits, including the outflow valve, are free of snow and ice. If the APU is operating, verify that the outflow valve is fully open. Engine inlets ..................
  • Page 338 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Engine Start Procedure Do the normal Engine Start Procedure with the following modifications: • If the engine has been cold soaked for one or more hours at ambient temperatures below -40°C, do not start or motor the engine. Maintenance personnel should do appropriate procedures for adverse weather heating of the Hydro-Mechanical Unit.
  • Page 339 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Note: If the COWL VALVE OPEN lights remain illuminated bright with engines at IDLE, do the following: • verify APU BLEED air switch is in the OFF posiiton, • verify ISOLATION VALVE switch is in the AUTO position, •...
  • Page 340 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Before Taxi Procedure Do the normal Before Taxi Procedure with the following modifications: GENERATOR 1 and 2 switches ........ON Normally the IDG’s stabilize within one minute, although due to cold oil, up to five minutes can be needed to produce steady power.
  • Page 341 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual CAUTION: When operating the engines over significant amounts of standing de-icing or anti-icing fluid, limit thrust to the minimum required. Excessive ingestion of de-icing or anti-icing fluid can cause the fluid to build up on the engine compressor blades resulting in compressor stalls and engine surges.
  • Page 342 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual The APU should be shut down unless APU operation is necessary. Call “FLAPS UP”. Flaps ..............UP Prevents ice and slush from accumulating in flap cavities during de-icing. Thrust levers ............Idle Reduces the possibility of injury to personnel at inlet or exhaust areas.
  • Page 343 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual An increase in control forces can be expected at low temperatures. Before Takeoff Procedure Do the normal Before Takeoff Procedure with the following modifications: Call “FLAPS ___” as needed for takeoff. Flap lever ........
  • Page 344 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual ENGINE ANTI-ICE switches ......ON Verify that the COWL VALVE OPEN lights illuminate bright, then dim. Verify that the COWL ANTI-ICE lights are extinguished. Note: If the COWL VALVE OPEN lights remain illuminated bright with engines at IDLE, do the following:.
  • Page 345 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Thrust ... Reduce as needed for flight conditions Wait 15 seconds. This allows engine vibration level to stabilize. If engine vibration is less than 4.0 units after thrust is reduced, repeat the above steps at approximately 15 minute intervals or sooner as needed.
  • Page 346 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Verify that the L and R VALVE OPEN lights illuminate bright, then extinguish. Cold Temperature Altitude Corrections Extremely low temperatures create significant altimeter errors and greater potential for reduced terrain clearance. When the temperature is colder than ISA, true altitude will be lower than indicated altitude.
  • Page 347 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual An altitude correction due to cold temperature is not needed for the following conditions: • While under ATC radar vectors • When maintaining an ATC assigned flight level (FL) •...
  • Page 348 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual After Landing Procedure CAUTION: Taxi at a reduced speed. Use smaller nose wheel steering wheel and rudder inputs and apply minimum thrust smoothly. Differential thrust may be used to help maintain airplane momentum during turns.
  • Page 349 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Verify that the COWL ANTI-ICE lights are extinguished. Note: If the COWL VALVE OPEN lights remain illuminated bright with engines at IDLE, do the following: • verify APU BLEED air switch is in the OFF posiiton, •...
  • Page 350 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Secure Procedure Do the normal Secure Procedure with the following modifications: If the airplane will be attended and warm air circulation throughout the cargo E/E compartments is desired: CAUTION: Do not leave the interior unattended with a pack operating and all doors closed.
  • Page 351 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Cold weather maintenance procedures for securing the airplane may be required. These procedures are normally done by maintenance personnel, and include, but are not limited to: • protective covers and plugs installed •...
  • Page 352 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual # Maximum Cooling on the Ground - APU Bleed During ground operation the following considerations will help keep the airplane as cool as possible: • While the airplane is electrically powered, packs should be run or cooling air supplied to the airplane when the OAT exceeds 40°...
  • Page 353 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual PACK switches ................HIGH Temperature selectors ............AUTO COOL Prior to takeoff: PACK switches ................AUTO Engine BLEED 2 air switch ............... ON APU BLEED air switch..............OFF Engine BLEED 1 air switch ............... ON ISOLATION VALVE switch ............AUTO Temperature selectors ..............
  • Page 354 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Operation in a Sandy or Dusty Environment The main hazards of a sandy or dusty environment are erosion (especially of engine fan blades), accumulation of sand or dust on critical surfaces and blockage.
  • Page 355 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Leading edge flaps ................. Check Verify that all leading edges are undamaged. Engine inlets .................. Check Verify that the inlet cowling is free of sand and dust. Verify that the fan is free to rotate and fan blades are undamaged. Fuel tank vents ................
  • Page 356 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Note: Use a filtered ground cart for pneumatic air for engine start, if available. ENGINE START switch ..........GRD Verify that the N2 RPM increases. C, F/O Motor the engine for 2 minutes to help remove contaminants. YT702 - YV671 CAUTION: Do not apply rotational force when moving the engine start lever.
  • Page 357 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual • In the event of a crosswind during 180° turns, turn away from the wind if possible to minimize sand and dust ingestion. • Whenever possible, avoid situations that would require the airplane to be brought to a complete stop.
  • Page 358 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual If bleed air is needed to maintain tolerable flight deck and cabin temperatures, use APU bleed air rather than engine bleed air during the taxi in. Limit APU bleed air use as much as possible to reduce sand and dust ingestion.
  • Page 359 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Additional procedures for securing the airplane during sandy or dusty conditions may be needed. These procedures are normally done by maintenance personnel, and include, but are not limited to: •...
  • Page 360 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual PHASE OF FLIGHT AIRSPEED CLIMB 280 knots or .76 Mach whichever is lower. CRUISE Use FMC recommended thrust settings. If the FMC is inoperative, refer to the Unreliable Airspeed page in the Performance–Inflight section of the QRH for approximate N1 settings that maintain near optimum penetration airspeed.
  • Page 361 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Windshear Windshear is a change of wind speed and/or direction over a short distance along the flight path. Indications of windshear are listed in the Windshear non-normal maneuver in this manual. Avoidance The flight crew should search for any clues to the presence of windshear along the intended flight path.
  • Page 362 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual • Know the all–engine initial climb pitch attitude. Rotate at the normal rate to this attitude for all non–engine failure takeoffs. Minimize reductions from the initial climb pitch attitude until terrain and obstruction clearance is assured, unless stick shaker activates •...
  • Page 363 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Ice Crystal Icing (ICI) At temperatures below freezing near convective weather, the airplane can encounter visible moisture made up of high concentrations of small ice crystals. Ice crystals can accumulate aft of the engine fan in the engine core.
  • Page 364 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual • Humidity increase • Static discharge around the windshield (St. Elmo’s fire) SP.16.30 MN-FLT-OH-201 March 1, 2021...
  • Page 365 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Avoiding Ice Crystal Icing During flight in IMC, avoid flying directly over significant amber or red radar returns, even if there are no returns at airplane altitude. Use the weather radar controls to assess weather radar reflectivity below the airplane flight path.
  • Page 366 Supplementary Procedures - Adverse Weather 737 MAX Flight Crew Operations Manual Ice Crystal Icing Suspected If conditions allow, exit the ice crystal icing conditions laterally. Climbing or descending to exit ice crystal icing conditions is not recommended. Request a route change to minimize the time above red and amber radar returns.
  • Page 367 TO1-10% TO2-20% - - - - - - - - - - - - - - - - - - - - - - - PI.10.1 737-8 TS2 LEAP-1B28 KG C M FAA CATB TO1-10% TO2-20% ALT-AB (FMC Model 737-8.2) AOA-DIAL PI.30.1 MN-FLT-OH-201 PI.TOC.1...
  • Page 368 Performance Inflight - Table of Contents 737 MAX Flight Crew Operations Manual Intentionally Blank PI.TOC.2 MN-FLT-OH-201 October 26, 2021...
  • Page 369 737-8 LEAP-1B27 KG C M FAA CATB TO1-10% TO2-20% Section 737-8 LEAP-1B27 KG C M FAA CATB TO1-10% TO2-20% 737 Flight Crew Operations Manual Performance Inflight Chapter PI Table of Contents Section 10 737-8 LEAP-1B27 KG C M FAA CATB TO1-10% TO2-20% Pkg Model Identification .
  • Page 370 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual TO2 Takeoff %N1 ....... . . PI.10.50 TO2 Assumed Temperature Reduced Thrust .
  • Page 371 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual Airport Altitude = 4000 FT ....PI.10.77 Airport Altitude = 5000 FT ....PI.10.77 Airport Altitude = 6000 FT .
  • Page 372 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual LEADING EDGE FLAPS TRANSIT (Flaps 15) ..PI.12.16 LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 15) ........PI.12.17 LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 30) .
  • Page 373 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual Long Range Cruise Diversion Fuel and Time ... PI.13.11 Holding ......... PI.13.12 Gear Down Landing Rate of Climb Available .
  • Page 374 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual Alternate Mode EEC, Engine Inoperative ....PI.18.14 Gear Down ........PI.18.15 Gear Down, Engine Inoperative .
  • Page 375 Section 10 Pkg Model Identification Pkg Model Identification Pkg Model Identification File highlight Pkg Model Identification General Performance Inflight number 10 package was chosen to represent all 737 MAX 8 EB1 27K CATB from GOL’s fleet. October 26, 2021 MN-FLT-OH-201 PI.ModID.10.1...
  • Page 376 Performance Inflight - Pkg Model Identification 737 Flight Crew Operations Manual Intentionally Blank PI.ModID.10.2 MN-FLT-OH-201 October 26, 2021...
  • Page 377 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI General Section 10 General Takeoff Speeds - Dry Runway General File Highlight General Max Takeoff Thrust Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10...
  • Page 378 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual General Takeoff Speeds - Dry Runway Max Takeoff Thrust Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 October 26, 2021 PI.10.2...
  • Page 379 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Takeoff Speeds - Wet Runway File Highlight Max Takeoff Thrust Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 380 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Takeoff Speeds - Wet Runway Max Takeoff Thrust Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 October 26, 2021 PI.10.4...
  • Page 381 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Stabilizer Trim Setting File Highlight Max Takeoff Thrust Flaps 1 and 5 STABILIZER TRIM SETTING (UNITS) WEIGHT C.G. (%MAC) (1000 KG) 8 1/2 8 1/2 8 1/4 7 3/4 7 1/2 7 1/4 6 3/4 6 1/2 6 1/4 5 3/4 5 1/2...
  • Page 382 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual VREF File Highlight Based on 14500 ft reference pressure altitude VREF (KIAS) WEIGHT FLAPS (1000 KG) October 26, 2021 PI.10.6 MN-FLT-OH-201...
  • Page 383 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flap Maneuver Speeds File Highlight FLAP POSITION MANEUVER SPEED VREF40 + 70 VREF40 + 50 VREF40 + 30 VREF40 + 30 VREF40 + 20 VREF40 + 10 VREF30 VREF40 October 26, 2021 MN-FLT-OH-201 PI.10.7...
  • Page 384 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Slush/Standing Water Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH 3 mm (0.12 INCHES) 6 mm (0.25 INCHES) 13 mm (0.50 INCHES)
  • Page 385 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Slush/Standing Water Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH 3 mm (0.12 INCHES) 6 mm (0.25 INCHES) 13 mm (0.50 INCHES)
  • Page 386 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Dry Snow Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH 30 mm (1.18 INCHES) 60 mm (2.36 INCHES) 100 mm (4.00 INCHES)
  • Page 387 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Dry Snow Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH 30 mm (1.18 INCHES) 60 mm (2.36 INCHES) 100 mm (4.00 INCHES)
  • Page 388 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Wet Snow Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH 5 mm (0.20 INCHES) 13 mm (0.50 INCHES) 30 mm (1.18 INCHES)
  • Page 389 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Wet Snow Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH 5 mm (0.20 INCHES) 13 mm (0.50 INCHES) 30 mm (1.18 INCHES)
  • Page 390 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Slippery Runway Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION GOOD MEDIUM POOR FIELD/OBSTACLE LIMIT WEIGHT PRESS ALT (FT)
  • Page 391 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Slippery Runway Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION GOOD MEDIUM POOR FIELD/OBSTACLE LIMIT WEIGHT PRESS ALT (FT) PRESS ALT (FT)
  • Page 392 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Slippery Runway Takeoff No Reverse Thrust Table 3 of 3: V1 Adjustment (KIAS) REPORTED BRAKING ACTION GOOD MEDIUM POOR WEIGHT (1000 KG) PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT) S.L.
  • Page 393 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Takeoff %N1 File Highlight Max Takeoff Thrust Based on engine bleed for packs on and anti-ice off AIRPORT AIRPORT PRESSURE ALTITUDE (1000 FT) 14 14.5 (°C) 85.6 86.1 86.6 86.7 86.2 85.7 85.2 84.8 84.3 83.9 83.5 83.0 82.5 81.6 80.6 79.5 78.6 78.2 86.9 87.3 87.7 87.8 87.4 86.9 86.4 85.9 85.5 85.1 84.6 84.2 83.7 82.7 81.8 80.7 79.8 79.4...
  • Page 394 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Assumed Temperature Reduced Thrust File Highlight Maximum Assumed Temperature (Table 1 of 3) Based on 25% Takeoff Thrust Reduction AIRPORT PRESSURE ALTITUDE (1000 FT) OAT (°C) 14 14.5 -5 & BELOW 64...
  • Page 395 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Assumed Temperature Reduced Thrust %N1 Adjustment for Temperature Difference (Table 3 of 3) ASSUMED OUTSIDE AIR TEMPERATURE (°C) TEMP MINUS OAT (°C) 1. Determine Maximum Assumed Temperature allowed from Table 1.
  • Page 396 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO1 Takeoff Speeds - Dry Runway File Highlight 10% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 397 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual TO1 Takeoff Speeds - Dry Runway 10% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 October 26, 2021 MN-FLT-OH-201 PI.10.21...
  • Page 398 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO1 Takeoff Speeds - Wet Runway File Highlight 10% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 399 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual TO1 Takeoff Speeds - Wet Runway 10% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 October 26, 2021 MN-FLT-OH-201 PI.10.23...
  • Page 400 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO1 Stabilizer Trim Setting File Highlight 10% Thrust Reduction Flaps 1 and 5 STABILIZER TRIM SETTING (UNITS) WEIGHT C.G. (%MAC) (1000 KG) 8 1/2 8 1/2 8 1/2 8 1/4 7 3/4 7 1/2 7 1/4 6 3/4 6 1/2...
  • Page 401 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Slush/Standing Water Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO1 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES)
  • Page 402 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO1 Slush/Standing Water Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO1 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES) 13 mm (0.50 INCHES)
  • Page 403 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Dry Snow Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO1 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES)
  • Page 404 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO1 Dry Snow Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO1 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES) 100 mm (4.00 INCHES)
  • Page 405 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Wet Snow Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO1 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES)
  • Page 406 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO1 Wet Snow Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO1 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES) 30 mm (1.18 INCHES)
  • Page 407 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Slippery Runway Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO1 DRY GOOD MEDIUM POOR...
  • Page 408 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO1 Slippery Runway Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO1 DRY GOOD MEDIUM POOR FIELD/OBSTACLE LIMIT WEIGHT...
  • Page 409 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO1 Slippery Runway Takeoff 10% Thrust Reduction No Reverse Thrust Table 3 of 3: V1 Adjustment (KIAS) REPORTED BRAKING ACTION GOOD MEDIUM POOR WEIGHT (1000 KG) PRESS ALT (FT)
  • Page 410 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO1 Takeoff %N1 File Highlight 10% Thrust Reduction Based on engine bleed for packs on and anti-ice off AIRPORT AIRPORT PRESSURE ALTITUDE (1000 FT) 14 14.5 (°C) 81.9 82.4 82.9 83.0 82.5 82.0 81.6 81.1 80.7 80.3 79.8 79.4 78.9 78.0 77.1 76.0 75.5 75.5 83.3 83.6 84.1 84.1 83.7 83.2 82.7 82.3 81.9 81.4 81.0 80.6 80.1 79.1 78.2 77.2 76.3 75.9...
  • Page 411 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual TO1 Assumed Temperature Reduced Thrust File Highlight Maximum Assumed Temperature (Table 1 of 3) Based on 25% Takeoff Thrust Reduction AIRPORT PRESSURE ALTITUDE (1000 FT) OAT (°C) 14 14.5 -5 & BELOW 64...
  • Page 412 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO1 Assumed Temperature Reduced Thrust %N1 Adjustment for Temperature Difference (Table 3 of 3) ASSUMED OUTSIDE AIR TEMPERATURE (°C) TEMP MINUS OAT (°C) 1. Determine Maximum Assumed Temperature allowed from Table 1.
  • Page 413 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual TO2 Takeoff Speeds - Dry Runway File Highlight 20% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 414 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO2 Takeoff Speeds - Dry Runway 20% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 October 26, 2021 PI.10.38...
  • Page 415 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual TO2 Takeoff Speeds - Wet Runway File Highlight 20% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 416 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO2 Stabilizer Trim Setting File Highlight 20% Thrust Reduction Flaps 1 and 5 STABILIZER TRIM SETTING (UNITS) WEIGHT C.G. (%MAC) (1000 KG) 8 1/2 8 1/2 8 1/2 8 1/2 8 1/4...
  • Page 417 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Slush/Standing Water Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO2 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES)
  • Page 418 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO2 Slush/Standing Water Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO2 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES) 13 mm (0.50 INCHES)
  • Page 419 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Dry Snow Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO2 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES)
  • Page 420 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO2 Dry Snow Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO2 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES) 100 mm (4.00 INCHES)
  • Page 421 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Wet Snow Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO2 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES)
  • Page 422 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO2 Wet Snow Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO2 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES) 30 mm (1.18 INCHES)
  • Page 423 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Slippery Runway Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO2 DRY GOOD MEDIUM POOR...
  • Page 424 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO2 Slippery Runway Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO2 DRY GOOD MEDIUM POOR FIELD/OBSTACLE LIMIT WEIGHT...
  • Page 425 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION TO2 Slippery Runway Takeoff 20% Thrust Reduction No Reverse Thrust Table 3 of 3: V1 Adjustment (KIAS) REPORTED BRAKING ACTION GOOD MEDIUM POOR WEIGHT (1000 KG) PRESS ALT (FT)
  • Page 426 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO2 Takeoff %N1 File Highlight 20% Thrust Reduction Based on bleed packs on and anti-ice off AIRPORT AIRPORT PRESSURE ALTITUDE (1000 FT) 14 14.5 (°C) 77.8 78.3 78.8 78.9 78.4 78.0 77.5 77.1 76.7 76.3 75.9 75.5 75.4 75.4 75.4 75.4 75.5 75.5 79.2 79.6 80.0 80.1 79.6 79.1 78.7 78.2 77.8 77.3 76.9 76.5 76.1 75.2 74.9 74.9 74.9 74.9...
  • Page 427 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual TO2 Assumed Temperature Reduced Thrust File Highlight Maximum Assumed Temperature (Table 1 of 3) Based on 25% Takeoff Thrust Reduction AIRPORT PRESSURE ALTITUDE (1000 FT) OAT (°C) 14 14.5 -5 & BELOW 63...
  • Page 428 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual TO2 Assumed Temperature Reduced Thrust %N1 Adjustment for Temperature Difference (Table 3 of 3) ASSUMED OUTSIDE AIR TEMPERATURE (°C) TEMP MINUS OAT (°C) 1. Determine Maximum Assumed Temperature allowed from Table 1.
  • Page 429 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Max Climb %N1 File Highlight Based on engine bleed for packs on and anti-ice off PRESSURE ALTITUDE (1000 FT) / SPEED (KIAS OR MACH) (°C) 0.78 0.78 0.78 0.78 0.78 80.8...
  • Page 430 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Go-Around %N1 File Highlight Based on engine bleed for packs on and anti-ice off REPORTED AIRPORT PRESSURE ALTITUDE (1000 FT) (°C) 14 14.5 (°C) 60 85.8 86.3 86.8 86.9 86.4 86.0 85.5 85.0 84.6 84.2 83.8 83.3 82.9 81.9 81.0 79.9 79.0 78.6 55 87.2 87.6 88.0 88.0 87.6 87.1 86.7 86.2 85.8 85.3 84.9 84.5 84.0 83.1 82.2 81.1 80.2 79.8...
  • Page 431 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration File Highlight Altitude and/or vertical speed indications may also be unreliable. CLIMB (280/.76) Flaps Up, Set Max Climb Thrust PRESSURE WEIGHT (1000 KG)
  • Page 432 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. DESCENT (.76/280) Flaps Up, Set Idle Thrust PRESSURE WEIGHT (1000 KG) ALTITUDE (FT) PITCH ATT -1.0...
  • Page 433 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = -2000 FT...
  • Page 434 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = -1000 FT...
  • Page 435 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = SEA LEVEL...
  • Page 436 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 1000 FT...
  • Page 437 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 2000 FT...
  • Page 438 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 3000 FT...
  • Page 439 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 4000 FT...
  • Page 440 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 5000 FT...
  • Page 441 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 6000 FT...
  • Page 442 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 7000 FT...
  • Page 443 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 8000 FT...
  • Page 444 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 9000 FT...
  • Page 445 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 10000 FT...
  • Page 446 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 11000 FT...
  • Page 447 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 12000 FT...
  • Page 448 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 13000 FT...
  • Page 449 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight Airport Altitude = 14000 FT...
  • Page 450 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = -2000 FT...
  • Page 451 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = SEA LEVEL...
  • Page 452 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 2000 FT...
  • Page 453 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 4000 FT...
  • Page 454 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 6000 FT...
  • Page 455 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 8000 FT...
  • Page 456 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 10000 FT...
  • Page 457 737-8/LEAP-1B27 Performance Inflight General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 12000 FT...
  • Page 458 Performance Inflight 737-8/LEAP-1B27 General CATB 737 Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. FINAL APPROACH (1500 FT) Gear Down, Set Thrust for 3° Glideslope Airport Altitude = 14000 FT...
  • Page 459 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI All Engine Section 11 All Engine Long Range Cruise Maximum Operating Altitude All Engine File Highlight All Engine Max Cruise Thrust ISA + 10°C and Below MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
  • Page 460 Performance Inflight 737-8/LEAP-1B27 All Engine CATB 737 Flight Crew Operations Manual Long Range Cruise Control All Engine File Highlight PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 80.4 81.8 83.4 84.7 86.2 88.1 MACH .737 .762 .787 .796 .797 .789 KIAS...
  • Page 461 737-8/LEAP-1B27 Performance Inflight All Engine CATB 737 Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - Low Altitudes File Highlight Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND HEADWIND COMPONENT (KTS)
  • Page 462 Performance Inflight 737-8/LEAP-1B27 All Engine CATB 737 Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - Low Altitudes Table 3 of 3: Fuel Required Adjustment (1000 KG) WEIGHT AT CHECK POINT (1000 KG) REFERENCE FUEL REQUIRED (1000 KG) -0.1...
  • Page 463 737-8/LEAP-1B27 Performance Inflight All Engine CATB 737 Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - High Altitudes File Highlight Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND HEADWIND COMPONENT (KTS)
  • Page 464 Performance Inflight 737-8/LEAP-1B27 All Engine CATB 737 Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - High Altitudes Table 2 of 3: Reference Fuel And Time Required at Check Point PRESSURE ALTITUDE (1000 FT) DIST FUEL TIME...
  • Page 465 737-8/LEAP-1B27 Performance Inflight All Engine CATB 737 Flight Crew Operations Manual Long Range Cruise Wind-Altitude Trade File Highlight CRUISE WEIGHT (1000 KG) PRESSURE ALTITUDE (1000 FT) The above wind factor table is for calculation of wind required to maintain present range capability at new pressure altitude, i.e., break-even wind.
  • Page 466 Performance Inflight 737-8/LEAP-1B27 All Engine CATB 737 Flight Crew Operations Manual Descent at .78/280/250 KIAS All Engine File Highlight DISTANCE (NM) PRESSURE TIME FUEL ALTITUDE LANDING WEIGHT (1000 KG) (MIN) (KG) (FT) 41000 39000 37000 35000 33000 31000 29000 27000...
  • Page 467 737-8/LEAP-1B27 Performance Inflight All Engine CATB 737 Flight Crew Operations Manual Holding File Highlight Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 25000 30000 35000 41000 57.8 60.4 64.2 68.4 73.2 78.1 82.6 KIAS FF/ENG...
  • Page 468 Performance Inflight 737-8/LEAP-1B27 All Engine CATB 737 Flight Crew Operations Manual Intentionally Blank October 26, 2021 PI.11.10 MN-FLT-OH-201...
  • Page 469 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI Advisory Information Section 12 Advisory Information File Highlight ADVISORY INFORMATION Advisory Information Runway Surface Condition Correlation Advisory Information RUNWAY REPORTED CONDITION RUNWAY SURFACE CONDITION DESCRIPTION BRAKING CODE ACTION Wet (Smooth, Grooved or PFC) or Frost Good 3 mm (0.12 inches) or less of: Water, Slush, Dry Snow or Wet Snow...
  • Page 470 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 471 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 472 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 473 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 474 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 475 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 476 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Non-Normal Configuration Landing Distance Airspeed Unreliable (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 477 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Airspeed Unreliable (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 478 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Airspeed Unreliable (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 479 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance All Flaps Up Landing VREF40 + 55 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 480 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance ANTISKID INOPERATIVE (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 481 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance ANTISKID INOPERATIVE (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 482 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance ANTISKID INOPERATIVE (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 483 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Jammed or Restricted Flight Controls (Flaps 15) VREF15 + 10 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 484 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LEADING EDGE FLAPS TRANSIT (Flaps 15) VREF15 + 15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 485 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 486 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 487 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 488 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 489 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 490 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 491 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A AND SYSTEM B (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 492 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM B (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 493 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance MANUAL REVERSION (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 494 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance One Engine Inoperative Landing (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 495 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance One Engine Inoperative Landing (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 496 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance SPOILERS (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING...
  • Page 497 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance SPOILERS (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING...
  • Page 498 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance SPOILERS (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING...
  • Page 499 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Stabilizer Trim Inoperative (Flaps 15) VREF15 + 10 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 500 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Asymmetry (1 ≤ Flap Lever < 15) VREF40 + 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST...
  • Page 501 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Asymmetry (Flap Lever 15 or 25) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 502 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Asymmetry (Flap Lever 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 503 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Disagree (1 ≤ Indicated Flaps < 15) VREF40 + 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST...
  • Page 504 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Disagree (15 ≤ Indicated Flaps < 30) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 505 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Disagree (30 ≤ Indicated Flaps < 40) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 506 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flaps Up Landing VREF40 + 40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 507 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Recommended Brake Cooling Schedule Reference Brake Energy (Millions of Foot Pounds) Table 1(a) of 3: Sea Level to 10000 ft Pressure Altitude BRAKES ON SPEED (KIAS)
  • Page 508 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Recommended Brake Cooling Schedule Reference Brake Energy (Millions of Foot Pounds) Table 1(b) of 3: 10000 ft to 14500 ft Pressure Altitude BRAKES ON SPEED (KIAS) PRESSURE ALTITUDE (1000 FT)
  • Page 509 737-8/LEAP-1B27 Performance Inflight Advisory Information CATB 737 Flight Crew Operations Manual ADVISORY INFORMATION Recommended Brake Cooling Schedule Event Adjusted Brake Energy (Millions of Foot Pounds) Table 2(a) of 3: No Reverse Thrust REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
  • Page 510 Performance Inflight 737-8/LEAP-1B27 Advisory Information CATB 737 Flight Crew Operations Manual Intentionally Blank October 26, 2021 PI.12.42 MN-FLT-OH-201...
  • Page 511 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI Engine Inoperative Section 13 Engine Inoperative file Highlight ENGINE INOP Engine Inoperative Initial Max Continuous %N1 Engine Inoperative Based on .79M, A/C high and anti-ice off PRESSURE ALTITUDE (1000 FT) TAT (°C)
  • Page 512 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 37000 FT Pressure Altitude TAT (°C) KIAS 87.9 88.8 89.8 90.8 91.8 91.9...
  • Page 513 737-8/LEAP-1B27 Performance Inflight Engine Inoperative CATB 737 Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 27000 FT Pressure Altitude TAT (°C) KIAS 89.0 90.0 90.9 91.8 92.7 93.5 93.1 91.8...
  • Page 514 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE -0.9 -0.9 -0.8 -0.9 -0.8 ENGINE & WING ANTI-ICE -3.4...
  • Page 515 737-8/LEAP-1B27 Performance Inflight Engine Inoperative CATB 737 Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 18000 FT Pressure Altitude TAT (°C) KIAS 86.6 87.4 88.3 89.1 89.9 90.7 90.2 89.2...
  • Page 516 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 10000 FT Pressure Altitude TAT (°C) KIAS 87.0 87.8 88.7 89.5 90.3 91.1 91.9 91.9...
  • Page 517 737-8/LEAP-1B27 Performance Inflight Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Driftdown Speed/Level Off Altitude 100 ft/min residual rate of climb WEIGHT (1000 KG) OPTIMUM LEVEL OFF PRESSURE ALTITUDE DRIFTDOWN START ISA + 10°C...
  • Page 518 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Driftdown/LRC Cruise Range Capability Table 1 of 2: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND HEADWIND COMPONENT (KTS)
  • Page 519 737-8/LEAP-1B27 Performance Inflight Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Altitude Capability 100 ft/min residual rate of climb PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) ISA + 10°C & BELOW ISA + 15°C...
  • Page 520 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Control PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 87.8 91.7 93.4 MACH .545 .587 .599 KIAS FF/ENG 2674 2647 2625 86.1...
  • Page 521 737-8/LEAP-1B27 Performance Inflight Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Diversion Fuel and Time Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM)
  • Page 522 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Holding Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 25000 30000 35000 75.8 79.2 84.0 88.9 KIAS...
  • Page 523 737-8/LEAP-1B27 Performance Inflight Engine Inoperative CATB 737 Flight Crew Operations Manual File Highlight ENGINE INOP ADVISORY INFORMATION Gear Down Landing Rate of Climb Available Flaps 15 RATE OF CLIMB (FT/MIN) PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000...
  • Page 524 Performance Inflight 737-8/LEAP-1B27 Engine Inoperative CATB 737 Flight Crew Operations Manual ENGINE INOP ADVISORY INFORMATION Gear Down Landing Rate of Climb Available Flaps 30 RATE OF CLIMB (FT/MIN) PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500...
  • Page 525 737-8/LEAP-1B27 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Alternate Mode EEC Section 14 Alternate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Alternate Mode EEC Limit Weight Alternate Mode EEC NORMAL MODE PERFORMANCE LIMIT WEIGHT (1000 KG)
  • Page 526 Performance Inflight 737-8/LEAP-1B27 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Alternate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Max Takeoff %N1 Based on engine bleeds for packs on and anti-ice off AIRPORT PRESSURE ALTITUDE (1000 FT) AIRPORT OAT (°C)
  • Page 527 737-8/LEAP-1B27 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Alternate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Max Climb %N1 Based on engine bleed for packs on and anti-ice off PRESSURE ALTITUDE (1000 FT) / SPEED (KIAS OR MACH) (°C)
  • Page 528 Performance Inflight 737-8/LEAP-1B27 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Alternate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Go-Around %N1 Based on engine bleed for packs on and anti-ice off REPORTED AIRPORT PRESSURE ALTITUDE (1000 FT) (°C)
  • Page 529 737-8/LEAP-1B27 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Alternate Mode EEC Section 15 Alternate Mode EEC, Engine Inoperative file Highlight ALTERNATE MODE EEC ENGINE INOP Alternate Mode EEC Initial Max Continuous %N1 Alternate Mode EEC, Engine Inoperative Based on .79M, A/C high and anti-ice off...
  • Page 530 Performance Inflight 737-8/LEAP-1B27 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Alternate Mode EEC file Highlight ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Alternate Mode EEC Max Continuous %N1 Based on A/C high and anti-ice off 37000 FT Pressure Altitude TAT (°C)
  • Page 531 737-8/LEAP-1B27 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE -2.0 -1.8 -1.5 -1.2...
  • Page 532 Performance Inflight 737-8/LEAP-1B27 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 27000 FT Pressure Altitude TAT (°C) KIAS 89.0 90.0 90.9...
  • Page 533 737-8/LEAP-1B27 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 20000 FT Pressure Altitude TAT (°C) KIAS 86.4 87.3 88.2...
  • Page 534 Performance Inflight 737-8/LEAP-1B27 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 18000 FT Pressure Altitude TAT (°C) KIAS 86.6 87.4 88.3...
  • Page 535 737-8/LEAP-1B27 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 10000 FT Pressure Altitude TAT (°C) KIAS 87.0 87.8 88.7...
  • Page 536 Performance Inflight 737-8/LEAP-1B27 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Intentionally Blank October 26, 2021 PI.15.8 MN-FLT-OH-201...
  • Page 537 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI Gear Down Section 16 GearDown File Highlight GEAR DOWN Gear Down Long Range Cruise Altitude Capability Gear Down Max Cruise Thrust, 100 ft/min residual rate of climb PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) ISA + 10°C &...
  • Page 538 Performance Inflight 737-8/LEAP-1B27 Gear Down CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN Long Range Cruise Control PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 79.7 MACH .466 KIAS FF/ENG 1909 77.8 88.0 MACH .453 .559 KIAS FF/ENG 1789 1834 75.7...
  • Page 539 737-8/LEAP-1B27 Performance Inflight Gear Down CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN Long Range Cruise Enroute Fuel and Time Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND HEADWIND COMPONENT (KTS)
  • Page 540 Performance Inflight 737-8/LEAP-1B27 Gear Down CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN Descent VREF40+70 KIAS PRESSURE ALTITUDE TIME (MIN) FUEL (KG) DISTANCE (NM) (FT) 41000 20.8 39000 20.1 37000 19.3 35000 18.6 33000 17.9 31000 17.2 29000 16.4...
  • Page 541 737-8/LEAP-1B27 Performance Inflight Gear Down CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN Holding Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 25000 30000 35000 69.2 72.3 77.1 82.0 86.9 KIAS FF/ENG 1820...
  • Page 542 Performance Inflight 737-8/LEAP-1B27 Gear Down CATB 737 Flight Crew Operations Manual Intentionally Blank October 26, 2021 PI.16.6 MN-FLT-OH-201...
  • Page 543 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI Gear Down, Engine Inop Section 17 Gear Down, Engine Inop File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Gear Down, Engine Inop Driftdown Speed/Level Off Altitude Gear Down, Engine Inoperative...
  • Page 544 Performance Inflight 737-8/LEAP-1B27 Gear Down, Engine Inop CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Altitude Capability 100 ft/min residual rate of climb PRESSURE ALTITUDE (FT) WEIGHT ISA + 10°C (1000 KG) ISA + 15°C...
  • Page 545 737-8/LEAP-1B27 Performance Inflight Gear Down, Engine Inop CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Control PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 89.7 91.8 MACH .386 .400 KIAS FF/ENG...
  • Page 546 Performance Inflight 737-8/LEAP-1B27 Gear Down, Engine Inop CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Diversion Fuel and Time Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM)
  • Page 547 737-8/LEAP-1B27 Performance Inflight Gear Down, Engine Inop CATB 737 Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Holding Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 89.9 KIAS FF/ENG 3730 87.8...
  • Page 548 Performance Inflight 737-8/LEAP-1B27 Gear Down, Engine Inop CATB 737 Flight Crew Operations Manual Intentionally Blank October 26, 2021 PI.17.6 MN-FLT-OH-201...
  • Page 549 737-8/LEAP-1B27 CATB 737 Flight Crew Operations Manual Performance Inflight Chapter PI Text Section 18 Text Text Text File Highlgiht Introduction This chapter contains information to supplement performance data from the Flight Management Computer (FMC). In addition, sufficient inflight data is provided to complete a flight with the FMC inoperative. In the event...
  • Page 550 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual Takeoff speeds are determined as follows: 1. Determine V1, VR, and V2 from the Takeoff Speeds table (Table 1) with brake release weight. 2. Adjust V1, VR, and V2 for temperature and pressure altitude from the V1, VR, V2 Adjustments table (Table 2).
  • Page 551 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual Flap Maneuver Speeds This table provides flap maneuver speeds for various flap settings. During flap retraction, selection of the next flap position is initiated when reaching the maneuver speed for the existing flap position. During flap retraction, at least adequate maneuver capability of 30°...
  • Page 552 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual 4. Enter the V1(MCG) Limit Weight table (Table 2) with the adjusted field length and pressure altitude to obtain the slush/standing water limit weight with respect to minimum field length required for V1(MCG) speed.
  • Page 553 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual One Thrust Reverser Inoperative Wet runway takeoff performance presented for all brakes operating is based on the use of one thrust reverser during deceleration. When operating with a thrust reverser inoperative, the runway/obstacle limited takeoff weight and V1 speed must be reduced to account for the reduced deceleration capability.
  • Page 554 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual Assumed Temperature Reduced Thrust Regulations permit the use of up to 25% takeoff thrust reduction for operation with assumed temperature reduced thrust. Use of assumed temperature reduced thrust is not allowed with anti-skid inoperative or on runways contaminated with standing water, ice, slush, or snow.
  • Page 555 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual Pitch attitude and power setting are shown in bold type to emphasize pilot action. Altitude and/or vertical speed indications may also be unreliable. All Engines Long Range Cruise Maximum Operating Altitude These tables provide the maximum operating altitude in the same manner as the FMC.
  • Page 556 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual To determine remaining fuel and time required, first enter the Ground to Air Miles Conversion table (Table 1) to convert ground distance and enroute wind to an equivalent still air distance. Next, enter the Reference Fuel and Time table (Table 2) with air distance from Table 1 and the desired altitude and read reference fuel and time required.
  • Page 557 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual Normal Configuration Landing Distance Tables are provided as advisory information for normal configuration landing distances on dry runways and runways with good, good to medium, medium, medium to poor, and poor reported braking action. Landing distances (reference distances plus adjustments) are 115% of the actual landing distance.
  • Page 558 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual Tables for Non-Normal Configuration Landing Distance in this section are similar in format and used in the same manner as tables for the Normal Configuration Landing Distance previously described. For an engine inoperative landing, check the rate of climb capability shown in Gear Down Landing Rate of Climb Available tables to ensure adequate climb performance.
  • Page 559 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual Engine Inoperative Initial Max Continuous %N1 The Initial Max Continuous %N1 setting for use following an engine failure is shown. The table is based on the typical all engine cruise speed of .79 Mach to provide a target %N1 setting at the start of driftdown.
  • Page 560 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual To determine fuel required, enter the Ground to Air Miles Conversion table (Table 1) with the desired ground distance and correct for anticipated winds to obtain air distance to destination. Then enter the Driftdown/Cruise Fuel and Time table (Table 2) with air distance and weight at start of driftdown to determine fuel and time required.
  • Page 561 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual Holding Single engine holding data is provided in the same format as the all engine holding data and is based on the same assumptions. Gear Down Landing Rate of Climb Available Rate of climb data is provided as guidance information in the event an engine inoperative landing (manual or autoland) is planned.
  • Page 562 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual Takeoff Speed Adjustment Takeoff speeds computed for the reduced weight need no further adjustment. Max Takeoff %N1 To find alternate mode EEC Max Takeoff %N1 based on normal engine bleed for air conditioning packs on, enter the Alternate Mode EEC Max Takeoff %N1 table with airport pressure altitude and airport OAT and read %N1.
  • Page 563 737-8/LEAP-1B27 Performance Inflight Text CATB 737 Flight Crew Operations Manual Max Continuous %N1 Power setting is based on one engine operating with one A/C pack operating and all anti-ice bleeds off. Enter the table with pressure altitude, TAT, and IAS or Mach to read %N1. Power settings may be interpolated for intermediate airspeeds.
  • Page 564 Performance Inflight 737-8/LEAP-1B27 Text CATB 737 Flight Crew Operations Manual Tables for gear down, engine inoperative performance in this section are identical in format and used in the same manner as tables for the gear up, engine inoperative configuration previously described.
  • Page 565 737-8 TS2 L EAP-1B28 KG C M FAA CATB TO1-10% TO2-20% ALT -AB (FMC Model 737-8.2) AOA-DIAL Section 737-8 TS2 LEAP-1B28 KG C M FAA CATB TO1-10% TO2-20% AL T-AB (FMC Model 737-8.2) AOA-DIAL 737 MAX Flight Crew Operations Manual...
  • Page 566 Performance Inflight - Table of Contents 737 MAX Flight Crew Operations Manual TO2 Dry Snow Takeoff ......PI.30.46 TO2 Wet Snow Takeoff.
  • Page 567 Performance Inflight - Table of Contents 737 MAX Flight Crew Operations Manual ANTISKID INOPERATIVE (Flaps 30) ... . . PI.32.13 ANTISKID INOPERATIVE (Flaps 40) ... . . PI.32.14 Jammed or Restricted Flight Controls (Flaps 15) .
  • Page 568 Performance Inflight - Table of Contents 737 MAX Flight Crew Operations Manual Driftdown/LRC Cruise Range Capability ....PI.33.8 Long Range Cruise Altitude Capability ....PI.33.9 Long Range Cruise Control .
  • Page 569 Performance Inflight - Table of Contents 737 MAX Flight Crew Operations Manual Advisory Information ....... PI.38.8 Engine Inoperative .
  • Page 570 Performance Inflight - Table of Contents 737 MAX Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.TOC.30.6 MN-FLT-OH-201 March 1, 2021...
  • Page 571 Pk g Mod el Id entification File high ligh t Pk g Mod el Id entification General Performance Inflight number 30 package was chosen to represent all 737 MAX 8 28K CATB from GOL’s fleet. March 1, 2021 MN-FLT-OH-201 PI.ModID.30.1...
  • Page 572 Performance Inflight - Pkg Model Identification 737 MAX Flight Crew Operations Manual Intentionally Blank PI.ModID.30.2 MN-FLT-OH-201 March 1, 2021...
  • Page 573 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI General Section 30 Flight Crew Requirements for Chemical Passenger Oxygen System General General File Highlight General Required Pressure (PSI) for 114/115 Cubic Ft. Cylinder BOTTLE NUMBER OF CREW USING OXYGEN TEMPERATURE °C...
  • Page 574 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Table 2 of 4: V1, VR, V2 Adjustments* TAKEOFF SPEEDS ADJUSTMENTS (KIAS) TEMP (°C) PRESS ALT (1000 FT) PRESS ALT (1000 FT) PRESS ALT (1000 FT) -2 0 2 4 6 8 10 12 14.5 -2 0 2 4 6 8 10 12 14.5 -2 0 8 10 12 14.5...
  • Page 575 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Takeoff Speeds - Dry Runway General Max Takeoff Thrust Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500...
  • Page 576 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Intentionally Blank PI.30.4 MN-FLT-OH-201 March 1, 2021...
  • Page 577 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Takeoff Speeds - Wet Runway File Highlight Max Takeoff Thrust Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 578 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Takeoff Speeds - Wet Runway Max Takeoff Thrust Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 579 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Stabilizer Trim Setting File Highlight Max Takeoff Thrust Flaps 1 and 5 STABILIZER TRIM SETTING (UNITS) WEIGHT C.G. (%MAC) (1000 KG) 8 1/2 8 1/4 7 3/4 7 1/4...
  • Page 580 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual VREF File Highlight Based on 14500 ft reference pressure altitude VREF (KIAS) WEIGHT FLAPS (1000 KG) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 581 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Flap Maneuver Speeds File Highlight FLAP POSITION MANEUVER SPEED VREF40 + 70 VREF40 + 50 VREF40 + 30 VREF40 + 30 VREF40 + 20 VREF40 + 10 VREF30 VREF40 Boeing Proprietary.
  • Page 582 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Slush/Standing Water Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH 3 mm (0.12 INCHES) 6 mm (0.25 INCHES) 13 mm (0.50 INCHES)
  • Page 583 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Slush/Standing Water Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH 3 mm (0.12 INCHES) 6 mm (0.25 INCHES) 13 mm (0.50 INCHES)
  • Page 584 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Dry Snow Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH 30 mm (1.18 INCHES) 60 mm (2.36 INCHES) 100 mm (4.00 INCHES)
  • Page 585 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Dry Snow Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH 30 mm (1.18 INCHES) 60 mm (2.36 INCHES) 100 mm (4.00 INCHES)
  • Page 586 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Wet Snow Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH 5 mm (0.20 INCHES) 13 mm (0.50 INCHES) 30 mm (1.18 INCHES)
  • Page 587 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Wet Snow Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH 5 mm (0.20 INCHES) 13 mm (0.50 INCHES) 30 mm (1.18 INCHES)
  • Page 588 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Slippery Runway Takeoff Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION GOOD MEDIUM POOR FIELD/OBSTACLE LIMIT WEIGHT PRESS ALT (FT)
  • Page 589 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Slippery Runway Takeoff No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION GOOD MEDIUM POOR FIELD/OBSTACLE LIMIT WEIGHT PRESS ALT (FT) PRESS ALT (FT)
  • Page 590 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Slippery Runway Takeoff No Reverse Thrust Table 3 of 3: V1 Adjustment (KIAS) REPORTED BRAKING ACTION GOOD MEDIUM POOR WEIGHT (1000 KG) PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT) S.L.
  • Page 591 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Takeoff %N1 File Highlight Max Takeoff Thrust Based on engine bleed for packs on and anti-ice off AIRPORT AIRPORT PRESSURE ALTITUDE (1000 FT) 14 14.5 (°C) 85.2 85.7 86.2 86.2 86.3 86.3 86.3 86.3 86.3 86.3 86.1 85.7 85.3 84.4 83.4 82.3 81.1 80.5 86.7 87.1 87.5 87.5 87.6 87.6 87.6 87.6 87.6 87.6 87.4 87.0 86.7 85.7 84.8 83.6 82.5 81.9...
  • Page 592 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Assumed Temperature Reduced Thrust File Highlight Maximum Assumed Temperature (Table 1 of 3) Based on 25% Takeoff Thrust Reduction AIRPORT PRESSURE ALTITUDE (1000 FT) OAT (°C) 14 14.5 -5 & BELOW 59...
  • Page 593 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Assumed Temperature Reduced Thrust %N1 Adjustment for Temperature Difference (Table 3 of 3) ASSUMED OUTSIDE AIR TEMPERATURE (°C) TEMP MINUS OAT (°C) 1. Determine Maximum Assumed Temperature allowed from Table 1.
  • Page 594 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO1 Takeoff Speeds - Dry Runway File Highlight 10% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 595 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO1 Takeoff Speeds - Dry Runway 10% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 Boeing Proprietary.
  • Page 596 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO1 Takeoff Speeds - Wet Runway File Highlight 10% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 597 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO1 Takeoff Speeds - Wet Runway 10% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 Boeing Proprietary.
  • Page 598 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO1 Stabilizer Trim Setting File Highlight 10% Thrust Reduction Flaps 1 and 5 STABILIZER TRIM SETTING (UNITS) WEIGHT C.G. (%MAC) (1000 KG) 8 1/2 8 1/2 8 1/2 8 1/4 7 3/4 7 1/2...
  • Page 599 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Slush/Standing Water Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO1 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES)
  • Page 600 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO1 Slush/Standing Water Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO1 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES)
  • Page 601 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Dry Snow Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO1 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES)
  • Page 602 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO1 Dry Snow Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO1 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES)
  • Page 603 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Wet Snow Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO1 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES)
  • Page 604 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO1 Wet Snow Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO1 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES)
  • Page 605 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO1 Slippery Runway Takeoff 10% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO1 DRY GOOD MEDIUM...
  • Page 606 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO1 Slippery Runway Takeoff 10% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO1 DRY GOOD MEDIUM POOR FIELD/OBSTACLE...
  • Page 607 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO1 Slippery Runway Takeoff 10% Thrust Reduction No Reverse Thrust Table 3 of 3: V1 Adjustment (KIAS) REPORTED BRAKING ACTION GOOD MEDIUM POOR WEIGHT (1000 KG) PRESS ALT (FT)
  • Page 608 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO1 Takeoff %N1 File Highlight 10% Thrust Reduction Based on engine bleed for packs on and anti-ice off AIRPORT AIRPORT PRESSURE ALTITUDE (1000 FT) 14 14.5 (°C) 81.6 82.0 82.5 82.6 82.6 82.6 82.6 82.6 82.6 82.6 82.4 82.0 81.7 80.7 79.8 78.7 77.5 76.9 83.0 83.4 83.8 83.9 83.9 83.9 83.9 83.9 83.9 83.9 83.7 83.3 83.0 82.0 81.1 80.0 78.9 78.3...
  • Page 609 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO1 Assumed Temperature Reduced Thrust File Highlight Maximum Assumed Temperature (Table 1 of 3) Based on 25% Takeoff Thrust Reduction AIRPORT PRESSURE ALTITUDE (1000 FT) OAT (°C) 14 14.5 -5 &...
  • Page 610 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO1 Assumed Temperature Reduced Thrust %N1 Adjustment for Temperature Difference (Table 3 of 3) ASSUMED OUTSIDE AIR TEMPERATURE (°C) TEMP MINUS OAT (°C) 1. Determine Maximum Assumed Temperature allowed from Table 1.
  • Page 611 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO2 Takeoff Speeds - Dry Runway File Highlight 20% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 612 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO2 Takeoff Speeds - Dry Runway 20% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 Boeing Proprietary.
  • Page 613 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO2 Takeoff Speeds - Wet Runway File Highlight 20% Thrust Reduction Table 1 of 4: V1, VR, V2 FLAPS 1 FLAPS 5 FLAPS 10 FLAPS 15 FLAPS 25 WEIGHT (1000 KG) Check V1(MCG).
  • Page 614 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO2 Takeoff Speeds - Wet Runway 20% Thrust Reduction Table 4 of 4: V1(MCG) V1(MCG) (KIAS) TEMP PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000 14500 Boeing Proprietary.
  • Page 615 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO2 Stabilizer Trim Setting File Highlight 20% Thrust Reduction Flaps 1 and 5 STABILIZER TRIM SETTING (UNITS) WEIGHT C.G. (%MAC) (1000 KG) 8 1/2 8 1/2 8 1/2 8 1/2 8 1/4...
  • Page 616 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Slush/Standing Water Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO2 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES)
  • Page 617 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO2 Slush/Standing Water Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) SLUSH/STANDING WATER DEPTH TO2 DRY 3 mm (0.12 INCHES) 6 mm (0.25 INCHES)
  • Page 618 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Dry Snow Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO2 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES)
  • Page 619 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO2 Dry Snow Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) DRY SNOW DEPTH TO2 DRY 30 mm (1.18 INCHES) 60 mm (2.36 INCHES)
  • Page 620 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Wet Snow Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO2 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES)
  • Page 621 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO2 Wet Snow Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) WET SNOW DEPTH TO2 DRY 5 mm (0.20 INCHES) 13 mm (0.50 INCHES)
  • Page 622 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION TO2 Slippery Runway Takeoff 20% Thrust Reduction Maximum Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO2 DRY GOOD MEDIUM...
  • Page 623 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO2 Slippery Runway Takeoff 20% Thrust Reduction No Reverse Thrust Table 1 of 3: Weight Adjustment (1000 KG) REPORTED BRAKING ACTION TO2 DRY GOOD MEDIUM POOR FIELD/OBSTACLE...
  • Page 624 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION TO2 Slippery Runway Takeoff 20% Thrust Reduction No Reverse Thrust Table 3 of 3: V1 Adjustment (KIAS) REPORTED BRAKING ACTION GOOD MEDIUM POOR WEIGHT (1000 KG) PRESS ALT (FT)
  • Page 625 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO2 Takeoff %N1 File Highlight 20% Thrust Reduction Based on bleed packs on and anti-ice off AIRPORT AIRPORT PRESSURE ALTITUDE (1000 FT) 14 14.5 (°C) 77.5 77.9 78.4 78.5 78.5 78.5 78.5 78.5 78.5 78.5 78.3 77.9 77.6 76.7 75.8 75.4 75.5 75.5 79.0 79.3 79.7 79.8 79.9 79.9 79.8 79.9 79.9 79.9 79.7 79.3 78.9 78.0 77.1 76.0 74.9 74.9...
  • Page 626 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual TO2 Assumed Temperature Reduced Thrust File Highlight Maximum Assumed Temperature (Table 1 of 3) Based on 25% Takeoff Thrust Reduction AIRPORT PRESSURE ALTITUDE (1000 FT) OAT (°C) 14 14.5 -5 &...
  • Page 627 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual TO2 Assumed Temperature Reduced Thrust %N1 Adjustment for Temperature Difference (Table 3 of 3) ASSUMED OUTSIDE AIR TEMPERATURE (°C) TEMP MINUS OAT (°C) 1. Determine Maximum Assumed Temperature allowed from Table 1.
  • Page 628 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Max Climb %N1 File Highlight Based on engine bleed for packs on and anti-ice off PRESSURE ALTITUDE (1000 FT) / SPEED (KIAS OR MACH) (°C) 0.78 0.78 0.78 0.78 0.78...
  • Page 629 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Go-Around %N1 File Highlight Based on engine bleed for packs on and anti-ice off REPORTED AIRPORT PRESSURE ALTITUDE (1000 FT) (°C) 14 14.5 (°C) 60 85.5 86.0 86.4 86.5 86.6 86.6 86.6 86.6 86.6 86.7 86.4 86.1 85.7 84.8 83.8 82.7 81.6 81.0 55 87.0 87.4 87.8 87.8 87.9 87.9 87.9 87.9 87.9 88.0 87.7 87.4 87.0 86.1 85.2 84.0 82.9 82.3...
  • Page 630 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration File Highlight Altitude and/or vertical speed indications may also be unreliable. CLIMB (280/.76) Flaps Up, Set Max Climb Thrust PRESSURE WEIGHT (1000 KG)
  • Page 631 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. CRUISE (.76/280) Flaps Up, Set Thrust for Level Flight PRESSURE WEIGHT (1000 KG)
  • Page 632 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. DESCENT (.76/280) Flaps Up, Set Idle Thrust PRESSURE WEIGHT (1000 KG) ALTITUDE (FT) PITCH ATT -1.0...
  • Page 633 737-8/LEAP-1B28 Performance Inflight General CATB 737 MAX Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. TERMINAL AREA (5000 FT) Set Thrust for Level Flight WEIGHT (1000 KG) FLAP/GEAR POSITION...
  • Page 634 Performance Inflight 737-8/LEAP-1B28 General CATB 737 MAX Flight Crew Operations Manual Flight With Unreliable Airspeed/ Turbulent Air Penetration Altitude and/or vertical speed indications may also be unreliable. GO-AROUND Flaps 15, Gear Up, Set Go-Around Thrust WEIGHT (1000 KG) PRESSURE ALTITUDE (FT) PITCH ATT 22.5...
  • Page 635 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI All Engine Section 31 Long Range Cruise Maximum Operating Altitude All Engine All Engine File Highlight All Engine Max Cruise Thrust ISA + 10°C and Below MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE)
  • Page 636 Performance Inflight 737-8/LEAP-1B28 All Engine CATB 737 MAX Flight Crew Operations Manual Long Range Cruise Control All Engine File Highlight PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 80.4 81.8 83.4 84.7 86.2 88.1 MACH .737 .762 .787 .796 .797 .789...
  • Page 637 737-8/LEAP-1B28 Performance Inflight All Engine CATB 737 MAX Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - Low Altitudes File Highlight Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND...
  • Page 638 Performance Inflight 737-8/LEAP-1B28 All Engine CATB 737 MAX Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - Low Altitudes Table 3 of 3: Fuel Required Adjustment (1000 KG) WEIGHT AT CHECK POINT (1000 KG) REFERENCE FUEL REQUIRED (1000 KG) -0.1...
  • Page 639 737-8/LEAP-1B28 Performance Inflight All Engine CATB 737 MAX Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - High Altitudes File Highlight Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND...
  • Page 640 Performance Inflight 737-8/LEAP-1B28 All Engine CATB 737 MAX Flight Crew Operations Manual Long Range Cruise Enroute Fuel and Time - High Altitudes Table 2 of 3: Reference Fuel And Time Required at Check Point PRESSURE ALTITUDE (1000 FT) DIST FUEL...
  • Page 641 737-8/LEAP-1B28 Performance Inflight All Engine CATB 737 MAX Flight Crew Operations Manual Long Range Cruise Wind-Altitude Trade File Highlight CRUISE WEIGHT (1000 KG) PRESSURE ALTITUDE (1000 FT) The above wind factor table is for calculation of wind required to maintain present range capability at new pressure altitude, i.e., break-even wind.
  • Page 642 Performance Inflight 737-8/LEAP-1B28 All Engine CATB 737 MAX Flight Crew Operations Manual Descent at .78/280/250 KIAS All Engine File Highlight DISTANCE (NM) PRESSURE TIME FUEL ALTITUDE LANDING WEIGHT (1000 KG) (MIN) (KG) (FT) 41000 39000 37000 35000 33000 31000 29000...
  • Page 643 737-8/LEAP-1B28 Performance Inflight All Engine CATB 737 MAX Flight Crew Operations Manual Holding File Highlight Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 25000 30000 35000 41000 57.8 60.4 64.2 68.4 73.2 78.1 82.6 KIAS...
  • Page 644 Performance Inflight 737-8/LEAP-1B28 All Engine CATB 737 MAX Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.31.10 MN-FLT-OH-201 March 1, 2021...
  • Page 645 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Advisory Information Section 32 Advisory Information File Highlight ADVISORY INFORMATION Runway Surface Condition Correlation Advisory Information Advisory Information RUNWAY REPORTED CONDITION RUNWAY SURFACE CONDITION DESCRIPTION BRAKING CODE ACTION...
  • Page 646 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 647 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 648 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 649 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 650 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 651 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Normal Configuration Landing Distance Flaps 40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C BRAKING 5000 KG...
  • Page 652 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Non-Normal Configuration Landing Distance Airspeed Unreliable (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 653 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Airspeed Unreliable (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 654 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Airspeed Unreliable (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 655 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance All Flaps Up Landing VREF40 + 55 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 656 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance ANTISKID INOPERATIVE (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 657 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance ANTISKID INOPERATIVE (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 658 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance ANTISKID INOPERATIVE (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 659 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Jammed or Restricted Flight Controls (Flaps 15) VREF15 + 10 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 660 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LEADING EDGE FLAPS TRANSIT (Flaps 15) VREF15 + 15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 661 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 662 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 663 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF BOTH ENGINE DRIVEN GENERATORS (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 664 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 665 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 666 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 667 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM A AND SYSTEM B (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 668 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance LOSS OF SYSTEM B (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 669 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance MANUAL REVERSION (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 670 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance One Engine Inoperative Landing (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 671 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance One Engine Inoperative Landing (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 672 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance SPOILERS (Flaps 15) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 673 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance SPOILERS (Flaps 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 674 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance SPOILERS (Flaps 40) VREF40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 675 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Stabilizer Trim Inoperative (Flaps 15) VREF15 + 10 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 676 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Asymmetry (1 ≤ Flap Lever < 15) VREF40 + 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP...
  • Page 677 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Asymmetry (Flap Lever 15 or 25) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1%...
  • Page 678 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Asymmetry (Flap Lever 30) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 679 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Disagree (1 ≤ Indicated Flaps < 15) VREF40 + 30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP...
  • Page 680 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Disagree (15 ≤ Indicated Flaps < 30) VREF15 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST...
  • Page 681 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flap Disagree (30 ≤ Indicated Flaps < 40) VREF30 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST...
  • Page 682 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Non-Normal Configuration Landing Distance Trailing Edge Flaps Up Landing VREF40 + 40 LANDING DISTANCE AND ADJUSTMENTS (M) REVERSE WIND SLOPE TEMP THRUST DIST PER 1% 65000 KG 10 KTS 10°C...
  • Page 683 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual File Highlight ADVISORY INFORMATION Recommended Brake Cooling Schedule Reference Brake Energy (Millions of Foot Pounds) Table 1(a) of 3: Sea Level to 10000 ft Pressure Altitude BRAKES ON SPEED (KIAS)
  • Page 684 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Recommended Brake Cooling Schedule Reference Brake Energy (Millions of Foot Pounds) Table 1(b) of 3: 10000 ft to 14500 ft Pressure Altitude BRAKES ON SPEED (KIAS)
  • Page 685 737-8/LEAP-1B28 Performance Inflight Advisory Information CATB 737 MAX Flight Crew Operations Manual ADVISORY INFORMATION Recommended Brake Cooling Schedule Event Adjusted Brake Energy (Millions of Foot Pounds) Table 2(a) of 3: No Reverse Thrust REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
  • Page 686 Performance Inflight 737-8/LEAP-1B28 Advisory Information CATB 737 MAX Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.32.42 MN-FLT-OH-201 March 1, 2021...
  • Page 687 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Engine Inoperative Section 33 Engine Inoperative file Highlight ENGINE INOP Initial Max Continuous %N1 Engine Inoperative Engine Inoperative Based on .79M, A/C high and anti-ice off PRESSURE ALTITUDE (1000 FT) TAT (°C)
  • Page 688 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 37000 FT Pressure Altitude TAT (°C) KIAS 87.9 88.9 89.9 90.8 91.8...
  • Page 689 737-8/LEAP-1B28 Performance Inflight Engine Inoperative CATB 737 MAX Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 27000 FT Pressure Altitude TAT (°C) KIAS 89.0 89.9 90.8 91.8 92.7 93.5 93.1...
  • Page 690 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE -0.8 -0.8 -0.9 -1.0 -1.1 ENGINE & WING ANTI-ICE -3.4...
  • Page 691 737-8/LEAP-1B28 Performance Inflight Engine Inoperative CATB 737 MAX Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 18000 FT Pressure Altitude TAT (°C) KIAS 88.5 89.3 90.1 90.9 91.8 92.7 92.1...
  • Page 692 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 10000 FT Pressure Altitude TAT (°C) KIAS 89.8 90.7 91.5 92.3 93.2 94.0 94.8...
  • Page 693 737-8/LEAP-1B28 Performance Inflight Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Driftdown Speed/Level Off Altitude 100 ft/min residual rate of climb WEIGHT (1000 KG) OPTIMUM LEVEL OFF PRESSURE ALTITUDE DRIFTDOWN START ISA + 10°C...
  • Page 694 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Driftdown/LRC Cruise Range Capability Table 1 of 2: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND HEADWIND COMPONENT (KTS)
  • Page 695 737-8/LEAP-1B28 Performance Inflight Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Altitude Capability 100 ft/min residual rate of climb PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) ISA + 10°C & BELOW ISA + 15°C...
  • Page 696 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Control PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 87.8 91.7 93.4 MACH .545 .587 .599 KIAS FF/ENG 2674...
  • Page 697 737-8/LEAP-1B28 Performance Inflight Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Diversion Fuel and Time Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM)
  • Page 698 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP MAX CONTINUOUS THRUST Holding Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 25000 30000 35000 75.8 79.2 84.0 88.9...
  • Page 699 737-8/LEAP-1B28 Performance Inflight Engine Inoperative CATB 737 MAX Flight Crew Operations Manual File Highlight ENGINE INOP ADVISORY INFORMATION Gear Down Landing Rate of Climb Available Flaps 15 RATE OF CLIMB (FT/MIN) PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000...
  • Page 700 Performance Inflight 737-8/LEAP-1B28 Engine Inoperative CATB 737 MAX Flight Crew Operations Manual ENGINE INOP ADVISORY INFORMATION Gear Down Landing Rate of Climb Available Flaps 30 RATE OF CLIMB (FT/MIN) PRESSURE ALTITUDE (FT) (°C) -2000 2000 4000 6000 8000 10000 12000...
  • Page 701 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Alternate Mode EEC Section 34 Altern ate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Limit Weight Altern ate Mode EEC Altern ate Mode EEC NORMAL MODE PERFORMANCE LIMIT WEIGHT (1000 KG)
  • Page 702 Performance Inflight 737-8/LEAP-1B28 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Altern ate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Max Takeoff %N1 Based on engine bleeds for packs on and anti-ice off AIRPORT PRESSURE ALTITUDE (1000 FT) AIRPORT OAT (°C)
  • Page 703 737-8/LEAP-1B28 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Altern ate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Max Climb %N1 Based on engine bleed for packs on and anti-ice off PRESSURE ALTITUDE (1000 FT) / SPEED (KIAS OR MACH) (°C)
  • Page 704 Performance Inflight 737-8/LEAP-1B28 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Altern ate Mode EEC file Highlight ALTERNATE MODE EEC Alternate Mode EEC Go-Around %N1 Based on engine bleed for packs on and anti-ice off REPORTED AIRPORT PRESSURE ALTITUDE (1000 FT) (°C)
  • Page 705 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Alternate Mode EEC Section 35 Altern ate Mode EEC, Engine Inoperative file Highlight ALTERNATE MODE EEC ENGINE INOP Alternate Mode EEC Initial Max Continuous %N1 Altern ate Mode EEC, Engine Inoperative Based on .79M, A/C high and anti-ice off...
  • Page 706 Performance Inflight 737-8/LEAP-1B28 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Altern ate Mode EEC file Highlight ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Alternate Mode EEC Max Continuous %N1 Based on A/C high and anti-ice off 37000 FT Pressure Altitude TAT (°C)
  • Page 707 737-8/LEAP-1B28 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE -2.0 -1.8 -1.3 -1.0...
  • Page 708 Performance Inflight 737-8/LEAP-1B28 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 27000 FT Pressure Altitude TAT (°C) KIAS 89.0 89.9 90.8...
  • Page 709 737-8/LEAP-1B28 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 20000 FT Pressure Altitude TAT (°C) KIAS 89.2 90.0 90.8...
  • Page 710 Performance Inflight 737-8/LEAP-1B28 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 18000 FT Pressure Altitude TAT (°C) KIAS 88.5 89.3 90.1...
  • Page 711 737-8/LEAP-1B28 Performance Inflight Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual ALTERNATE MODE EEC ENGINE INOP MAX CONTINUOUS THRUST Max Continuous %N1 Based on A/C high and anti-ice off 10000 FT Pressure Altitude TAT (°C) KIAS 89.8 90.7 91.5...
  • Page 712 Performance Inflight 737-8/LEAP-1B28 Alternate Mode EEC CATB 737 MAX Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.35.8 MN-FLT-OH-201 March 1, 2021...
  • Page 713 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Gear Down Section 36 GearDown File Highlight GEAR DOWN Long Range Cruise Altitude Capability Gear Down Gear Down Max Cruise Thrust, 100 ft/min residual rate of climb PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) ISA + 10°C &...
  • Page 714 Performance Inflight 737-8/LEAP-1B28 Gear Down CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN Long Range Cruise Control PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 79.7 MACH .466 KIAS FF/ENG 1909 77.8 88.0 MACH .453 .559 KIAS FF/ENG...
  • Page 715 737-8/LEAP-1B28 Performance Inflight Gear Down CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN Long Range Cruise Enroute Fuel and Time Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM) AIR DISTANCE (NM) GROUND HEADWIND COMPONENT (KTS)
  • Page 716 Performance Inflight 737-8/LEAP-1B28 Gear Down CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN Descent VREF40+70 KIAS PRESSURE ALTITUDE TIME (MIN) FUEL (KG) DISTANCE (NM) (FT) 41000 20.8 39000 20.1 37000 19.3 35000 18.6 33000 17.9 31000 17.2 29000 16.4...
  • Page 717 737-8/LEAP-1B28 Performance Inflight Gear Down CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN Holding Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 25000 30000 35000 69.2 72.3 77.1 82.0 86.9 KIAS FF/ENG...
  • Page 718 Performance Inflight 737-8/LEAP-1B28 Gear Down CATB 737 MAX Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.36.6 MN-FLT-OH-201 March 1, 2021...
  • Page 719 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Gear Down, Engine Inop Section 37 Gear Down, Engine Inop File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Driftdown Speed/Level Off Altitude Gear Down, Engine Inop Gear Down, Engine Inoperative...
  • Page 720 Performance Inflight 737-8/LEAP-1B28 Gear Down, Engine Inop CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Altitude Capability 100 ft/min residual rate of climb PRESSURE ALTITUDE (FT) WEIGHT ISA + 10°C (1000 KG) ISA + 15°C...
  • Page 721 737-8/LEAP-1B28 Performance Inflight Gear Down, Engine Inop CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Control PRESSURE ALTITUDE (1000 FT) WEIGHT (1000 KG) 89.7 91.8 MACH .386 .400 KIAS...
  • Page 722 Performance Inflight 737-8/LEAP-1B28 Gear Down, Engine Inop CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Long Range Cruise Diversion Fuel and Time Table 1 of 3: Ground to Air Miles Conversion AIR DISTANCE (NM)
  • Page 723 737-8/LEAP-1B28 Performance Inflight Gear Down, Engine Inop CATB 737 MAX Flight Crew Operations Manual File Highlight GEAR DOWN ENGINE INOP MAX CONTINUOUS THRUST Holding Flaps Up PRESSURE ALTITUDE (FT) WEIGHT (1000 KG) 1500 5000 10000 15000 20000 89.9 KIAS FF/ENG 3730 87.8...
  • Page 724 Performance Inflight 737-8/LEAP-1B28 Gear Down, Engine Inop CATB 737 MAX Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.37.6 MN-FLT-OH-201 March 1, 2021...
  • Page 725 737-8/LEAP-1B28 CATB 737 MAX Flight Crew Operations Manual Performance Inflight Chapter PI Text Section 38 Text Text Text File Highlgiht Introduction This chapter contains information to supplement performance data from the Flight Management Computer (FMC). In addition, sufficient inflight data is provided to complete a flight with the FMC inoperative. In the event...
  • Page 726 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual Takeoff speeds are determined as follows: 1. Determine V1, VR, and V2 from the Takeoff Speeds table (Table 1) with brake release weight. 2. Adjust V1, VR, and V2 for temperature and pressure altitude from the V1, VR, V2 Adjustments table (Table 2).
  • Page 727 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual Flap Maneuver Speeds This table provides flap maneuver speeds for various flap settings. During flap retraction, selection of the next flap position is initiated when reaching the maneuver speed for the existing flap position. During flap retraction, at least adequate maneuver capability of 30°...
  • Page 728 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual 4. Enter the V1(MCG) Limit Weight table (Table 2) with the adjusted field length and pressure altitude to obtain the slush/standing water limit weight with respect to minimum field length required for V1(MCG) speed.
  • Page 729 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual One Thrust Reverser Inoperative Wet runway takeoff performance presented for all brakes operating is based on the use of one thrust reverser during deceleration. When operating with a thrust reverser inoperative, the runway/obstacle limited takeoff weight and V1 speed must be reduced to account for the reduced deceleration capability.
  • Page 730 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual Assumed Temperature Reduced Thrust Regulations permit the use of up to 25% takeoff thrust reduction for operation with assumed temperature reduced thrust. Use of assumed temperature reduced thrust is not allowed with anti-skid inoperative or on runways contaminated with standing water, ice, slush, or snow.
  • Page 731 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual Pitch attitude and power setting are shown in bold type to emphasize pilot action. Altitude and/or vertical speed indications may also be unreliable. The pitch attitude is provided to the nearest half degree.
  • Page 732 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual To determine remaining fuel and time required, first enter the Ground to Air Miles Conversion table (Table 1) to convert ground distance and enroute wind to an equivalent still air distance. Next, enter the Reference Fuel and Time table (Table 2) with air distance from Table 1 and the desired altitude and read reference fuel and time required.
  • Page 733 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual Normal Configuration Landing Distance Tables are provided as advisory information for normal configuration landing distances on dry runways and runways with good, good to medium, medium, medium to poor, and poor reported braking action. Landing distances (reference distances plus adjustments) are 115% of the actual landing distance.
  • Page 734 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual Tables for Non-Normal Configuration Landing Distance in this section are similar in format and used in the same manner as tables for the Normal Configuration Landing Distance previously described.
  • Page 735 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual Engine Inoperative Initial Max Continuous %N1 The Initial Max Continuous %N1 setting for use following an engine failure is shown. The table is based on the typical all engine cruise speed of .79 Mach to provide a target %N1 setting at the start of driftdown.
  • Page 736 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual To determine fuel required, enter the Ground to Air Miles Conversion table (Table 1) with the desired ground distance and correct for anticipated winds to obtain air distance to destination. Then enter the Driftdown/Cruise Fuel and Time table (Table 2) with air distance and weight at start of driftdown to determine fuel and time required.
  • Page 737 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual Holding Single engine holding data is provided in the same format as the all engine holding data and is based on the same assumptions. Gear Down Landing Rate of Climb Available Rate of climb data is provided as guidance information in the event an engine inoperative landing (manual or autoland) is planned.
  • Page 738 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual Takeoff Speed Adjustment Takeoff speeds computed for the reduced weight need no further adjustment. Max Takeoff %N1 To find alternate mode EEC Max Takeoff %N1 based on normal engine...
  • Page 739 737-8/LEAP-1B28 Performance Inflight Text CATB 737 MAX Flight Crew Operations Manual Max Continuous %N1 Power setting is based on one engine operating with one A/C pack operating and all anti-ice bleeds off. Enter the table with pressure altitude, TAT, and IAS or Mach to read %N1. Power settings may be interpolated for intermediate airspeeds.
  • Page 740 Performance Inflight 737-8/LEAP-1B28 Text CATB 737 MAX Flight Crew Operations Manual Tables for gear down, engine inoperative performance in this section are identical in format and used in the same manner as tables for the gear up, engine inoperative configuration previously described.
  • Page 741 Volume 2 1 Airplane General, Emergency Equipment, Doors, Windows Airplane General, Emergency Equipment, Doors, Windows Systems Description 1-Airplane General, Emergency Equipment, Doors, Windows Table Of Contents 737 MAX Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Table of Contents Section TOC Dimensions .
  • Page 742 Airplane General, Emergency Equipment, Doors, Windows - Table of Contents 737 MAX Flight Crew Operations Manual Exterior Lighting ........1.30.5 LED - Landing, Taxi and Runway Turnoff Lights .
  • Page 743 Emergency Equipment Symbols ......1.40.25 Emergency Equipment Locations – 737-8 Series Airplanes ..1.40.27 Doors and Windows.
  • Page 744 Airplane General, Emergency Equipment, Doors, Windows - Table of Contents 737 MAX Flight Crew Operations Manual Intentionally Blank 1.TOC.4 MN-FLT-OH-201 October 26, 2021...
  • Page 745 (35.92m) 47'-1” (14.35m) 18’-9” (5.72m) 40'-10” (12.45m) 51’-2” (15.60m) 128’-4” (39.12m) 129’-6” (39.47m) NOTE: * Clearance is nominal. Add plus or minus 3 inches (.08m) to account for variations in conditions during routine servicing. 737-8 March 1, 2021 MN-FLT-OH-201 1.10.1...
  • Page 746 No differential braking.) CAUTION: Do not attempt to make a turn away from an obstacle within 15 feet (4.57 meters) of the wing tip or within 23 feet (7.1 meters) of the nose. 737-8 1.10.2 MN-FLT-OH-201 March 1, 2021...
  • Page 747 737 MAX Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Instrument Panels Section 20 20 Instrument Panels Instrument Panels File Highlight Panel Arrangement AFT OVERHEAD PANEL FORWARD OVERHEAD PANEL GLARESHIELD PANEL MAIN PANEL- FIRST MAIN OFFICER PANEL- CAPTAIN FIRST...
  • Page 748 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Aft Flight Deck Overview WHITE DOME LIGHT P6-1 NAV, INST, & COMM OBSERVER OXYGEN MASK WHITE DOME LIGHT P6-2 SYSTEMS P18-1 NAV P6-3 FUEL SYSTEM, COAT LIGHTING &...
  • Page 749 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Main Panel - Captain LIGHTS TEST TEST STAB OUT OF BELOW G/S TAKEOFF CABIN P/RST P/RST P/RST P-INHIBIT CONFIG ALTITUDE TRIM MAIN PANEL BACKGROUND AFDS FLOOD PFD/MFD NORM INBD...
  • Page 750 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Main Panel - First Officer TEST P/RST P/RST P/RST SPEED BRAKE CABIN TAKEOFF BELOW G/S EXTENDED ALTITUDE CONFIG P-INHIBIT GROUND PROXIMITY MAIN PANEL PFD/MFD NORM GPWS FLAP GEAR...
  • Page 751 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual October 26, 2021 MN-FLT-OH-201 1.20.5...
  • Page 752 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Glareshield Panel MINS BARO MTRS RADIO BARO FIRE MASTER FLT CONT ELEC VOR MAP RANGE WARN CAUTION VOR 2 BELL CUTOUT PUSH TO RESET FUEL OVHT/DET ADF 2 CLOCK...
  • Page 753 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Main Panel - Center ISFD HEADING FROM LEFT IRS ONLY HP/IN 29.92 IN 5400 5200 4800 ATT RST BARO NOSE GEAR LEFT RIGHT NOSE GEAR GEAR GEAR LEFT...
  • Page 754 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Forward Electronic Panel FUEL FLOW AUTO BRAKE RESET AUTO BRAKE DISARM INFO RATE USED ENG TFR SELECTOR SELECTOR ANTISKID BRAKE PRESS ANTISKID INOP INIT INIT VNAV -BRT+ VNAV...
  • Page 755 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual File Highlight Forward Overhead Panel FLT CONTROL STANDBY OVERHEAT OVERHEAT OVERHEAT OVERHEAT QUANTITY STBY STBY PRESSURE AIR TEMP PASS STBY WINDOW HEAT RUD ON A ON B ON OVHT SIDE...
  • Page 756 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Aft Overhead Panel VHF-1 VHF-2 VHF-3 HF-1 HF-2 INT CABIN IRS DISPLAY 1-NAV-2 1-ADF-2 SPKR DSPL SEL RADIO S AT 1 SAT 2 PPOS WIND TK/GS HDG/STS TEST...
  • Page 757 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Control Stand DOWN FLAP ARMED FLAP STAB STAB TRIM TRIM FLIGHT NOSE NOSE DOWN DOWN DETENT PARKING BRAKE NOSE PULL NOSE UP FLAP DOWN DISENGAGE DISENGAGE IDLE STAB TRIM...
  • Page 758 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Aft Electronic Panel OVHT DET OVHT DET BELL CUTOUT WHEEL L BOTTLE R BOTTLE WELL DISCHARGED DISCHARGED ENGINES FAULT DISCH NORMAL DISCH DISCH NORMAL ENG 1 ENG 2 APU DET OVERHEAT...
  • Page 759 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual File Highlight Auxiliary Panels (TYPICAL) SPARE BULB STOWAGE SUN VISOR STOWAGE NOSE WHEEL ESCAPE STRAP STANDBY SPEAKER STEERING STOWAGE MAGNETIC COMPASS MAP LIGHT CHART LIGHT CHART AND MAP LIGHT CONTROLS OXYGEN MASK...
  • Page 760 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Attendant Control Panels Forward Attendant Control Panel General Lighting Layout Passenger Seating Area GROUND SERVICE Boarding/ Take Off/ Night Meal/ Lighting Deplane Landing Cruise Cruise Beverage EMERGENCY EVACUATION Sunrise/...
  • Page 761 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Aft Attendant Control Panel General Lighting Layout EMERGENCY Passenger Seating Area EXIT LIGHTS Boarding/ Take Off/ Night Meal/ Lighting Deplane Landing Cruise Cruise Beverage Sunrise/ White White Sunset...
  • Page 762 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 MAX Flight Crew Operations Manual Attendant Handset LIFT HANDSET PILOT ATTENDANT PILOT ALERT PASSENGER ADDRESS PUSH TO TALK RESET CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND 1.20.16 MN-FLT-OH-201 March 1, 2021...
  • Page 763 737 MAX Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Controls and Indicators Section 30 30 Con trols and Ind icators Controls and Indicators File Highlight Flight Deck Lighting Map and Chart Light Controls CHART SIDEWALL PANELS MAP Light Control Rotate –...
  • Page 764 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual MAIN PANEL Light Control Rotate – • Captain – controls brightness of Captain’s panel and instrument lighting, center instrument panel, and AFDS panel displays and edge lighting •...
  • Page 765 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual FLOOD Light Control Rotate – controls overhead spotlight brightness directed at the control stand and aft electronic panel. PANEL Light Control Rotate – controls forward and aft electronic control panel lights brightness. Overhead/Circuit Breaker Panel Light Controls CIRCUIT BREAKER PANEL...
  • Page 766 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Dome Light Control DOME WHITE BRIGHT AFT OVERHEAD PANEL DOME Light Control DIM – sets overhead dome lights to low brightness. OFF – overhead dome lights are extinguished. BRIGHT –...
  • Page 767 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Exterior Lighting LED - Landing, Taxi and Runway Turnoff Lights The Landing, Taxi and Runway Turnoff Lights are located in each wing root strakelet and provide the lighting necessary for airplane operation. RUNWAY TAXI LANDING...
  • Page 768 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Miscellaneous Exterior Lights POSITION ANTI WHEEL LOGO COLLISION WING WELL STROBE & STEADY STEADY FORWARD OVERHEAD PANEL LOGO Light Switch OFF – logo lights on each side of vertical fin extinguished. ON –...
  • Page 769 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Emergency Lighting and Passenger Signs Flight Deck 1B402 - 1B786, 1B806 - 1J594 EMER EXIT LIGHTS ARMED FASTEN INOP BELTS AUTO FORWARD OVERHEAD PANEL 1B401, 1B801 - 1B805 EMER EXIT LIGHTS ARMED...
  • Page 770 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual ARMED – (guarded position) all emergency lights illuminate automatically if airplane electrical power to DC bus No. 1 fails or AC power is turned off. ON –...
  • Page 771 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Emergency Locator Transmitter AFT OVERHEAD PANEL 1B785, 1B786, 1J585 - 1J594 Emergency Locator Transmitter Light Illuminated (amber) – ELT has been activated and is simultaneously transmitting tone and position data (as installed) on 121.5, 243.0 and 406.0 MHz.
  • Page 772 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Doors Flight Deck Door FOR GROUND USE ONLY DEADBOLT POSITIONS UNLOCKED LOCKED KEY OPERABLE LOCKED KEY INOPERABLE FLIGHT DECK DOOR Deadbolt and Deadbolt Placard Release Pins Pull pins inward - manually separates decompression panel from a jammed door to allow panel opening and egress.
  • Page 773 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Flight Deck Emergency Access Panel PASSENGER SIDE DOOR POST Keypad Push - enters 3 to 8 digit emergency access code by pressing numeric then “ENT” keys.
  • Page 774 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Flight Deck Access System Switch FLIGHT DECK ACCESS SYSTEM NORM FLIGHT DECK SIDE DOOR POST Flight Deck Access System Switch OFF - removes electrical power from door lock. NORM (Normal) - flight deck access system configured for flight.
  • Page 775 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Flight Deck (FLT DK) Door Lock Selector Spring loaded to AUTO. Selector must be pushed in to rotate from AUTO to UNLKD. Selector must not be pushed in to rotate from AUTO to DENY. UNLKD - door unlocked while selector in UNLKD.
  • Page 776 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Exterior Door Annunciator Lights ENTRY SERVICE LEFT FWD RIGHT FWD OVERWING OVERWING CARGO LEFT AFT RIGHT AFT EQUIP OVERWING OVERWING CARGO ENTRY SERVICE FORWARD OVERHEAD PANEL RIGHT AFT RIGHT FWD OVERWING...
  • Page 777 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Passenger Entry/Galley Service Doors CONTROL HANDLE INSTRUCTION PLACARD ASSIST HANDLE SLIDE COMPARTMENT SLIDE PRESSURE GAUGE VIEWER STOWAGE HOOKS FLOOR BRACKETS GIRT GIRT BAR PASSENGER CABIN Oxygen Oxygen Panel CREW...
  • Page 778 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual ON – activates system and drops masks if automatic function fails. Passenger Oxygen On Light Illuminated (amber) – passenger oxygen system is operating and masks have dropped.
  • Page 779 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Regulator and Inflation Lever (Hidden) Grasp Regulator and pull up – 1B401, 1B402, 1B801 - 1J594 • allows mask removal from stowage box • activates oxygen and microphone when stowage box doors open Squeeze Inflation Lever –...
  • Page 780 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Inflation Lever Squeeze – 1B401, 1B4 02, 1B801 - 1J594 • inflates mask harness • flow indicator shows a colored cross momentarily as harness inflates. •...
  • Page 781 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Tank Drain Valve Handle Open - drains water from tank. Closed - normal position. Access Panel Cannot be closed unless the Fill and Overflow Valve and Tank Drain Valve Handles are in the closed position.
  • Page 782 Airplane General, Emergency Equipment, Doors, Windows - Controls and Indicators 737 MAX Flight Crew Operations Manual Water Supply Selector Valve Each lavatory has a Water Supply Selector Valve. The Water Supply Selector Valve has four positions, and is located in the cabinet below the sink. SUPPLY ON –...
  • Page 783 737 MAX Flight Crew Operations Manual Airplane General, Emergency Chapter 1 Equipment, Doors, Windows Systems Description Section 40 40 Systems Description Systems Description File Highlight Introduction This chapter describes miscellaneous airplane systems, including: • lighting systems • emergency egress • oxygen systems •...
  • Page 784 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Strobe Lights Four high intensity white strobe lights are installed on the left forward winglet, right forward winglet, and both sides of the tailcone. Anti–collision Lights Two red anti–collision strobe lights are located on the top and bottom of the fuselage.
  • Page 785 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Exterior Lighting Locations WING ILLUMINATION LIGHTS (WHITE) WING ILLUMINATION LIGHTS (WHITE) TAXI LIGHT TAXI LIGHT (WHITE) (WHITE) RUNWAY TURNOFF RUNWAY TURNOFF LIGHTS (WHITE) LIGHTS (WHITE) LANDING LANDING LIGHTS (WHITE)
  • Page 786 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Passenger Cabin Lighting Passenger cabin lighting is supplied by incandescent and fluorescent lights. General cabin lighting is provided by window lights, ceiling lights, and entry lights.
  • Page 787 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Interior Emergency Lighting Interior emergency exit lights are located: • in the lower inboard corner of stowage bins to illuminate the aisle. • over the entry/service and overwing emergency doors to indicate the door exits.
  • Page 788 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual First Flight of the Day with Additional Steps to Bin Doors Closed Maximum Duration Follow for charging Allowed (Hours) (Crossbin/COS/Direct W1/W2 credit High) 15 minute charge a) Close overhead bin doors during charging.
  • Page 789 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Quick Turn with Bin Doors Open and Passengers in Seats (White BRIGHT) 10 minute charge a) Charging must begin prior to 15 minute charge previous discharge duration ending b) Bin doors can be open during charging...
  • Page 790 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual In-Flight Charging Taxi/Take off Charging must begin 10 minute charge prior to previous discharge duration Meal/Beverage ending. Strips are 15 minute charge assumed to be Day Cruise shadowed during 15 minute charge...
  • Page 791 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual First Flight of the Day with Additional Steps to Bin Doors Closed Maximum Duration Follow for charging Allowed (Hours) (Crossbin/COS/Direct W1/W2 credit High) 15 minute charge a) Close overhead bin doors during charging.
  • Page 792 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Quick Turn with Bin Doors Open and Passengers in Seats (White BRIGHT) 10 minute charge a) Charging must begin prior to 15 minute charge 12.5 previous discharge duration ending b) Bin doors can be...
  • Page 793 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual In-Flight Charging Taxi/Take off Charging must begin 10 minute charge prior to previous discharge duration Meal/Beverage ending. Strips are 15 minute charge assumed to be Day Cruise shadowed during 15 minute charge...
  • Page 794 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Continuous Flight No limit if ceiling and If the Attendant sidewall light stays on Control Panel loses communication with the ceiling and sidewall lights these lights will change to a default medium white.
  • Page 795 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Emergency Exit Lighting INTEGRAL SLIDE LIGHTING EXIT LOCATOR SIGNS - LOCATED IN THE ESCAPE SLIDE PASSENGER CABIN LIGHTING CEILING. PHOTOLUMINESCENT STRIP LIGHTING EXTERIOR EMERGENCY LIGHTING AISLE LIGHTS EMERGENCY EXIT SIGNS - LOCATED IN THE FORWARD...
  • Page 796 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Oxygen System Schematic OXYGEN MASK PRESSURE REDUCER THERMAL DISCHARGE PORT CREW OXYGEN CREW PASS OXYGEN CYLINDER OXYGEN NORMAL PASS OXY OXY PRESS PS1 X 100 BAROMETRIC PRESSURE SWITCH...
  • Page 797 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Flight Crew Oxygen System The flight crew oxygen system uses quick-donning, diluter-demand masks/regulators located at each crew station. Oxygen is supplied by a single cylinder. Oxygen pressure is displayed on the Oxygen Pressure indicator located on the aft overhead panel when the battery switch is ON.
  • Page 798 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual MASK DONNING Stowing Instructions To stow the oxygen mask accomplish the following: • Set the regulator to “100%.” • Ensure that the cloth liner is secured at the top of the stowage box and is laying flat against all interior sides of the box.
  • Page 799 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual CAUTION: Do not push the harness “cross” straps into or behind the nose piece. Doing this may cause the cross straps to hang up on the mask during inflation.
  • Page 800 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual TEST RESET MASK STOWING Portable Protective Breathing Equipment Protective Breathing Equipment (PBE/Smoke Hood) devices for crew use (for combating fires and/or entering areas of smoke or fume accumulation) may be stowed throughout the airplane;...
  • Page 801 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual The system is activated automatically by a pressure switch at a cabin altitude of 14,000 feet or when the Passenger Oxygen Switch on the aft overhead panel is positioned to ON.
  • Page 802 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Passenger Portable Oxygen First aid and supplemental portable oxygen cylinders are installed at suitable 1B785, 1B7 86, 1J5 85 - 1J594 locations in the passenger cabin. The cylinders are fitted with a pressure gage, pressure regulator and on–off valve.
  • Page 803 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Water Fire Extinguishers Water fire extinguishers contain a solution of water mixed with antifreeze. The container is pressurized by a CO2 cartridge when the extinguisher handle is rotated fully clockwise.
  • Page 804 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Chemical Fire Extinguisher (BCF/BTP) LEVER RING SAFETY DISCHARGE NOZZLE PRESSURE GAUGE HANDLE 1.40.22 MN-FLT-OH-201 March 1, 2021...
  • Page 805 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Fire Extinguisher Usage Each class of fire calls for specialized action. Using the wrong extinguisher may do more harm than good. For your own protection, you should know these basic types, how to use them, and why.
  • Page 806 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual EUROPEAN/AUSTRALIAN CLASS OF FIRES EXTINGUISHER TYPE There are three common classes of fire: Water (H2O) COMBUSTIBLE MATERIALS TYPE CLASS paper, wood, fabric, rubber, saturates material certain plastics, etc., where and prevents quenching by water is effective.
  • Page 807 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Intentionally Blank March 1, 2021 MN-FLT-OH-201 1.40.25...
  • Page 808 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual 1.40.26 MN-FLT-OH-201 March 1, 2021...
  • Page 809 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual File Highlight Emergency Equipment Symbols WATER DRY CHEMICAL EXTINGUISHER EXTINGUISHER EXTINGUISHER EXTINGUISHER EXTINGUISHER PORTABLE PORTABLE DISPOSABLE FULL FACE PROTECTIVE OXYGEN BOTTLE OXYGEN BOTTLE OXYGEN MASK OXYGEN MASK BREATHING WITH SMOKE...
  • Page 810 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Intentionally Blank 1.40.28 MN-FLT-OH-201 March 1, 2021...
  • Page 811 Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual 40 Systems Description File Highlight Emergency Equipment Locations – 737-8 Series Airplanes 1B401, 1B402, 1B801 - 1B824 A = ATTENDANT SEAT L = LAVATORY G = GALLEY Additional...
  • Page 812 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual 1J 585 A = ATTENDANT SEAT L = LAVATORY G = GALLEY C = CLOSET In Ovhd Bin UNDER EACH PASSENGER SEAT (10) In Ovhd Bin SPARE In Ovhd Bin At Each Attendant Seat...
  • Page 813 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual 1B785, 1B786 A = ATTENDANT SEAT L = LAVATORY G = GALLEY C = CLOSET On Fwd Face of Class Divider In Ovhd Bin UNDER EACH PASSENGER SEAT (10) In Ovhd Bin...
  • Page 814 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual 1J 590 - 1J5 94 A = ATTENDANT SEAT L = LAVATORY G = GALLEY C = CLOSET On Fwd Face of Class Divider In Ovhd Bin UNDER EACH PASSENGER SEAT (10)
  • Page 815 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual File Highlight Doors and Windows The airplane has two passenger entry doors, one cabin door (the flight deck/passenger cabin entry), two service doors and two cargo doors. There is also a center electrical and electronic (E/E) equipment access door and an equipment compartment access door on the bottom of the airplane.
  • Page 816 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual The emergency access code is used to gain access to the flight deck in case of pilot incapacitation. A flight deck chime and illumination of the amber AUTO UNLK light indicates the correct emergency access code has been entered and the door is programmed to unlock after a time delay.
  • Page 817 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual The flight deck number two windows can be opened on the ground or in flight and can be used for emergency evacuation. To open the window, depress the trigger and turn the handle back and inboard.
  • Page 818 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Emergency Evacuation Routes Emergency evacuation may be accomplished through four entry/service doors and four overwing escape hatches. Flight deck crew members may evacuate the airplane through two sliding flight deck windows. Emergency Evacuation Routes Flight Deck Window Emergency Egress If the flight deck number two windows must be used for emergency egress, use...
  • Page 819 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual The above illustrated method of departure would probably be the easiest for most crewmembers. This technique is difficult and should be used only in extreme emergency.
  • Page 820 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Escape Slide Detachment Handle TO RELEASE SLIDE FOR DITCHING ONLY 1. LIFT FLAP 2. PULL HANDLE DETACHMENT HANDLE PULL PULL FLOOR BRACKETS GIRT GIRT BAR MANUAL INFLATION HANDLE 1.40.38 MN-FLT-OH-201...
  • Page 821 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Escape Straps Escape straps are installed above each aft emergency exit door frame. The escape doors must be opened to expose the straps. One end of the strap is attached to the door frame.
  • Page 822 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Emergency Exit Doors Four Type III emergency exits are located in the passenger cabin over the wings. These are canopy-type doors and are held in place by mechanical locks and airplane cabin pressure.
  • Page 823 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual EMERGENCY EXIT WARNING ONLY DOOR SWINGS OUT AND UP PUSH TO OPEN HOLD YOUR DOOR OPENS OUT AND UP KNEE AGAINST AUTOMATICALLY DOOR WHILE OPENING OR SERIOUS INJURY CAN OCCUR...
  • Page 824 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Flight Deck Seats The flight deck has three seat types: 1B401, 1B4 02, 1B801 - 1B824 • pilot seats (captain and first officer) • first observer seat •...
  • Page 825 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Four units hold the base of the seat to the aircraft seat tracks. A spring-loaded track lock lever mechanism sets fore and aft movement on the seat tracks. ARMREST HEIGHT ADJUSTMENT KNOB LUMBAR...
  • Page 826 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual EYE REFERENCE POSITION 1.40.44 MN-FLT-OH-201 March 1, 2021...
  • Page 827 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual First Observer Seat FIRST OBSERVER SEAT The first observer seat folds into the flight compartment wall when not in use. To use the seat, push the release latch. Then lower the seat into position. Raise the seat back to the detents in the doorway sidewall brackets.
  • Page 828 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual RELEASE HANDLE ON BACK OF SEAT RETRACTABLE SHOULDER HARNESS SEAT BOTTOM CUSHION LAP BELT RETRACTABLE HINGE CROTCH STRAP NOTE: THE SEAT FOLDS INTO THE WALL WITH VERY CLOSE TOLERANCES. USE CAUTION NOT TO PINCH YOUR FINGERS WHEN YOU STOW THE SEAT.
  • Page 829 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Second Observer Seat 1B401, 1B402, 1B801 - 1B824 SECOND OBSERVER SEAT The second observer seat is located behind the captain’s seat and is not adjustable. The seat has: •...
  • Page 830 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual SHOULDER HARNESS LAP BELT Galleys Galleys are located in the passenger cabin to provide convenient and rapid service to the passengers. Generally, they are installed in the cabin adjacent to the forward and aft galley service doors.
  • Page 831 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Electrical Power Electricity for the galleys is 115V AC supplied from the airplane transfer buses and controlled by a switch on the overhead panel. Circuit breakers are located in the lower E/E bay as part of the power distribution panels.
  • Page 832 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 MAX Flight Crew Operations Manual Hot Water Hot and cold water is available in all lavatories. The water heater is located below the lavatory sink. When emptied, it heats a new water charge in four minutes. An amber light is ON when the heater is operating normally.
  • Page 833 Air Systems 2 Air Systems 2-Air Systems Table Of Contents 737 MAX Flight Crew Operations Manual Air Systems Chapter 2 Table of Contents Section TOC Controls and Indicators ....... . . 2.10 Bleed Air Controls and Indicators .
  • Page 834 Air Systems - Table of Contents 737 MAX Flight Crew Operations Manual Zone Temperature Control ....... 2.30.5 Zone Temperature Control Modes .
  • Page 835 737 MAX Flight Crew Operations Manual Air Systems Chapter 2 Controls and Indicators Section 10 10 Controls and Indicators Controls and Indicators File Highlight Bleed Air Controls and Indicators DUAL BLEED L RECIRC FAN R RECIRC FAN AUTO AUTO OVHT DUCT PRESS TEST...
  • Page 836 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual OPEN – opens isolation valve. WING–BODY OVERHEAT Light Illuminated (amber) – • left light indicates overheat from bleed air duct leak in left engine strut, left inboard wing leading edge, left air conditioning bay, keel beam or APU bleed air duct •...
  • Page 837 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Illuminated (amber) – an incorrect bleed air configuration after takeoff or go-around • turning either BLEED switch ON will extinguish both BLEED lights if lights illuminated because of a configuration problem. TRIP RESET Switch Push (if fault condition is corrected) –...
  • Page 838 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Air Conditioning Controls and Indicators PASS AIR TEMP TEMP. °C CONT TRIM AIR ZONE ZONE ZONE TEMP TEMP TEMP CONT CAB FWD CAB AFT CAB AUTO AUTO AUTO DUAL BLEED L RECIRC FAN...
  • Page 839 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual ZONE TEMP Lights Illuminated (amber) – • CONT CAB indicates a duct temperature overheat or failure of the flight deck primary and standby temperature control • FWD CAB or AFT CAB indicates duct temperature overheat. Temperature Selector AUTO –...
  • Page 840 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual AUTO – • in-flight – •the left recirculation fan operates if both packs are operating unless either PACK switch is in HIGH •the right recirculation fan operates if both packs are operating unless both PACK switches are in HIGH.
  • Page 841 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Equipment Cooling Panel EQUIP COOLING EXHAUST SUPPLY NORM ALTN EQUIP SMOKE FORWARD OVERHEAD PANEL Equipment Cooling Supply OFF Light Illuminated (amber) – no airflow from selected cooling supply fan. Equipment (EQUIP) COOLING SUPPLY Switch NORM –...
  • Page 842 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Cabin Altitude Panel HORN CUTOUT CABIN X 1000 FEET PRESS DIFF LIMIT:TAKE- OFF & LDG .125 PSI FORWARD OVERHEAD PANEL CABIN Altimeter (ALT)/Differential Pressure (DIFF PRESS) Indicator Inner Scale – indicates cabin altitude in feet. Note: The CABIN ALT indicator can show a cabin altitude of less than 0 feet and reach the upper end of the cabin altitude scale.
  • Page 843 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Altitude (ALT) HORN CUTOUT Switch Push – • cuts out intermittent cabin altitude warning horn • altitude warning horn sounds when cabin exceeds 10,000 feet altitude. Cabin Pressurization Panel AUTO OFF SCHED ALTN...
  • Page 844 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Flight Altitude (FLT ALT) Indicator • indicates selected cruise altitude • set before takeoff. Note: A panel failure detected after a DC power interruption will result in the display of “88888”...
  • Page 845 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Outflow VALVE Position Indicator • indicates position of outflow valve • operates in all modes. Outflow Valve Switch (spring–loaded to center) CLOSE – closes outflow valve electrically with pressurization mode selector in MAN position.
  • Page 846 Air Systems - Controls and Indicators 737 MAX Flight Crew Operations Manual Intentionally Blank 2.10.12 MN-FLT-OH-201 March 1, 2021...
  • Page 847 737 MAX Flight Crew Operations Manual Air Systems Chapter 2 Bleed Air System Description Section 20 20 Bleed Air System Description Bleed Air System Description File Highlight Introduction Air for the bleed air system can be supplied by the engines, APU, or an external air cart/source.
  • Page 848 Air Systems - Bleed Air System Description 737 MAX Flight Crew Operations Manual Bleed Sensors Bleed sensors illuminate the respective BLEED light when engine bleed air temperature or pressure exceeds a predetermined limit. The respective engine bleed air valve closes automatically. The BLEED light also illuminates with a failure within the bleed air system, and both BLEED lights illuminate if an incorrect bleed configuration is present after takeoff or go-around.
  • Page 849 Air Systems - Bleed Air System Description 737 MAX Flight Crew Operations Manual APU Bleed Air Valve The APU bleed air valve permits APU bleed air to flow to the bleed air duct. The valve closes automatically when the APU is shut down. The APU bleed air valve is DC controlled and pressure operated.
  • Page 850 Air Systems - Bleed Air System Description 737 MAX Flight Crew Operations Manual Bleed Air System Schematic L RECIRC FAN R RECIRC FAN AUTO AUTO OVHT DUCT PRESS TEST L PACK R PACK ISOLATION VALVE AUTO AUTO CLOSE HIGH HIGH LEFT AUTO WING...
  • Page 851 Air Systems - Bleed Air System Description 737 MAX Flight Crew Operations Manual Wing-Body Overheat A wing-body overheat condition is caused by a bleed air duct leak. It is sensed by the overheat sensors located as shown. Wing-Body Overheat Ducts and Lights L PACK R PACK ISOLATION...
  • Page 852 Air Systems - Bleed Air System Description 737 MAX Flight Crew Operations Manual Intentionally Blank 2.20.6 MN-FLT-OH-201 March 1, 2021...
  • Page 853 737 MAX Flight Crew Operations Manual Air Systems Chapter 2 Air Conditioning System Description Section 30 30 Air Conditioning System Description Air Co nditioning System Descrip tion File Highlight Introduction The air conditioning system provides temperature controlled air by processing bleed air from the engines, APU, or a ground air source in air conditioning packs.
  • Page 854 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual When the aircraft is on the ground or the flaps are down, and both air conditioning pack switches are set to AUTO, and engine bleed switches are both set to ON, if one pack fails or one engine fails or a pack switch is selected to OFF, the remaining pack will not automatically transfer to high air flow.
  • Page 855 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual If a primary pack control fails, the affected pack is controlled by the standby pack control in the opposite controller. A primary or standby pack control failure causes the MAINT, MASTER CAUTION, and OVERHEAD System Annunciator lights to illuminate after landing.
  • Page 856 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual Air Conditioning Pack Schematic TO MIX MANIFOLD CONT CAB FWD CAB AFT CAB AUTO AUTO AUTO WATER ELECTRONIC ELECTRONIC SEPARATOR CONTROLLER CONTROLLER L PRIMARY R PRIMARY PACK CONTROL PACK CONTROL L RAM R RAM...
  • Page 857 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual Zone Temperature Control There are three zones: flight deck, forward cabin and aft cabin. Desired zone temperature is set by adjusting the individual Temperature Selectors. The selector range is approximately 65°F (18°C) to 85°F (30°C).
  • Page 858 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual Unbalanced Pack Temperature Control Mode Any failure affecting the supply of trim air will cause the temperature control system to control both packs independently. If flight deck trim air is lost, the left pack will provide conditioned air to the flight deck at the selected temperature and the right pack will satisfy the demand of the passenger zone which requires the most cooling.
  • Page 859 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual There is also a dual purpose valve behind the rudder pedal of each pilot. These valves provide air for warming the pilots' feet and for defogging the inside of the No.
  • Page 860 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual Loss of airflow due to failure of an equipment cooling fan results in illumination of the related equipment cooling OFF light. Selecting the alternate fan should restore airflow and extinguish the OFF light within approximately 5 seconds. In the event of a forward cargo fire warning, the equipment cooling exhaust fan is shut off and the equipment cooling exhaust OFF light is inhibited.
  • Page 861 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual Air Conditioning Distribution Schematic TRIM AIR ZONE ZONE ZONE TEMP TEMP TEMP CONT CAB FWD CAB AFT CAB RECIRC FANS ELECTRONIC ELECTRONIC CONTROLLER CONTROLLER FWD CAB AFT CAB ZONE TEMP ZONE TEMP CONTROL...
  • Page 862 Air Systems - Air Conditioning System Description 737 MAX Flight Crew Operations Manual Intentionally Blank 2.30.10 MN-FLT-OH-201 March 1, 2021...
  • Page 863 737 MAX Flight Crew Operations Manual Air Systems Chapter 2 Pressurization System Description Section 40 40 Pressurization System Description Pressu rization System Descrip tion File Highlight Introduction Cabin pressurization is controlled during all phases of airplane operation by the cabin pressure control system. The cabin pressure control system includes two identical automatic controllers available by selecting AUTO or ALTN and a manual (MAN) pilot–controlled mode.
  • Page 864 Air Systems - Pressurization System Description 737 MAX Flight Crew Operations Manual Cabin Pressure Control System Schematic BARO BARO ADIRU ADIRU STATIC PORT STATIC PORT AUTO OFF SCHED ALTN FAIL DESCENT AUTO FLT ALT CABIN MANUAL CABIN SENSE SENSE PORT PORT LAND ALT STALL...
  • Page 865 Air Systems - Pressurization System Description 737 MAX Flight Crew Operations Manual Outflow Valve The outflow valve is the overboard exhaust exit for the majority of the air circulated through the passenger cabin. Passenger cabin air is drawn through foot level grills, down around the aft cargo compartment, where it provides heating, and is discharged overboard through the outflow valve.
  • Page 866 Air Systems - Pressurization System Description 737 MAX Flight Crew Operations Manual Auto Mode Operation The AUTO system consists of two identical controllers, with one controller alternately sequenced as the primary operational controller for each new flight. The other automatic controller is immediately available as a backup. In the AUTO or ALTN mode, the pressurization control panel is used to preset two altitudes into the auto controllers: •...
  • Page 867 Air Systems - Pressurization System Description 737 MAX Flight Crew Operations Manual Selected FLT ALT Differential Pressure Limit At or below 28,000 feet 7.45 psid 28,000 feet to 37,000 feet 7.80 psid Above 37,000 feet 8.35 psid The descent mode is activated when the airplane descends 0.25 psi below the selected FLT ALT.
  • Page 868 Air Systems - Pressurization System Description 737 MAX Flight Crew Operations Manual Flight Path Events – Auto Mode CONSTANT FLT ALT SETTING AIRPLANE ALT .25 psid .25 psid *Note CRUISE MODE DESCENT MODE ACTIVATES ACTIVATES NORMAL ( P = 7.45 psid at or below 28,000 ft.) ( P = 7.80 psid above 28,000 ft.
  • Page 869 Anti-Ice, Rain 3 Anti-Ice, Rain 3-Anti-Ice, Rain Table Of Contents 737 MAX Flight Crew Operations Manual Anti-Ice, Rain Chapter 3 Table of Contents Section TOC Controls and Indicators ....... . . 3.10 Window Heat Panel .
  • Page 870 Anti-Ice, Rain - Table of Contents 737 MAX Flight Crew Operations Manual Intentionally Blank 3.TOC.2 MN-FLT-OH-201 March 1, 2021...
  • Page 871 737 MAX Flight Crew Operations Manual Anti-Ice, Rain Chapter 3 Controls and Indicators Section 10 10 Controls and Indicators Controls and Indicators File Highlight Window Heat Panel OVERHEAT OVERHEAT OVERHEAT OVERHEAT WINDOW HEAT OVHT SIDE SIDE PWR TEST FORWARD OVERHEAD PANEL Window OVERHEAT Lights Illuminated (amber) –...
  • Page 872 Anti-Ice, Rain - Controls and Indicators 737 MAX Flight Crew Operations Manual PWR TEST – provides a confidence test. Note: Refer to Supplementary Normal Procedures for Window Heat Test procedures. Windshield/Foot Air Controls WIND WIND FOOT FOOT SHIELD SHIELD BELOW MAIN PANEL - BELOW MAIN PANEL - CAPTAIN FIRST OFFICER...
  • Page 873 Anti-Ice, Rain - Controls and Indicators 737 MAX Flight Crew Operations Manual Probe Heat Panel PROBE CAPT PITOT PITOT AUTO L ELEV R ELEV PITOT PITOT L ALPHA R ALPHA VANE VANE HEAT TEMP PROBE PITOT FORWARD OVERHEAD PANEL Probe Heat Lights Illuminated (amber) –...
  • Page 874 Anti-Ice, Rain - Controls and Indicators 737 MAX Flight Crew Operations Manual ENG ANTI–ICE Lights Illuminated (amber) – indicates cowl thermal anti-ice system has been inhibited due to a system failure or when an engine core anti-ice valve fails closed. COWL ANTI–ICE Lights Illuminated (amber) –...
  • Page 875 Anti-Ice, Rain - Controls and Indicators 737 MAX Flight Crew Operations Manual Thermal Anti–Ice Indications Illuminated – • Green – cowl anti–ice valve(s) open • Amber – cowl anti–ice valve is not in position indicated by related engine anti–ice switch. Wing Anti–Ice Panel L VALVE R VALVE...
  • Page 876 Anti-Ice, Rain - Controls and Indicators 737 MAX Flight Crew Operations Manual ON (on the ground) – • wing anti–ice control valves open if thrust on both engines is below takeoff warning setting and temperature inside both distribution ducts is below thermal switch activation temperature •...
  • Page 877 737 MAX Flight Crew Operations Manual Anti-Ice, Rain Chapter 3 System Description Section 20 20 System Description Sy stem Description File Highlight Introduction Thermal anti-icing (TAI), electrical anti-icing, and windshield wipers are the systems provided for ice and rain protection. The anti-ice and rain systems include: •...
  • Page 878 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Flight Deck Window Heat Flight deck window numbers 1 and 2 consist of glass panes laminated to each side of a vinyl core. Flight deck window number 3 consists of two acrylic panes separated by an air space.
  • Page 879 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Flight Deck Window Heat Schematic OVERHEAT WINDOW HEAT OVHT SIDE SIDE PWR TEST TEMPERATURE CONTROLLER TEMPERATURE CONTROLLER FROM WIND WIND AIR CONDITIONING SHIELD SHIELD SYSTEM CONDITION: WINDOW HEAT ON R SIDE OVERHEATED Windshield Wipers The rain removal system for the forward windows consists of windshield wipers...
  • Page 880 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Probe and Sensor Heat Pitot probes, the total air temperature probe and the alpha vanes are electrically heated. Static ports are not heated. When operating on standby power, only the captain’s pitot probe is heated, however, the CAPT PITOT light does not illuminate for a failure.
  • Page 881 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Flap Setting Engine Idle Speed Icing Idle Less than 15 Degrees Approach Idle 15 Degrees or Greater Approach Idle Note: Stall warning logic adjusts stick shaker and minimum maneuver speed bars on the airspeed indicator.
  • Page 882 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Engine Anti–Ice System Schematic ENGINE COWL ANTI-ICE (TAI) ANTI-ICE ANTI-ICE COWL COWL ANTI-ICE ANTI-ICE COWL VALVE COWL VALVE ANTI-ICE BLEED AIR ENGINE DUCT BLEED VALVE COWL ANTI-ICE 10th VALVE MODULATING &...
  • Page 883 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Both valves close if either engine thrust is above the takeoff warning setting or either temperature sensor senses a duct overtemperature. The valves automatically reopen if thrust on both engines is reduced and both temperature sensors are cool. If either engine is above the takeoff warning setting and the WING ANTI–ICE switch is ON, the L VALVE and R VALVE lights are inhibited.
  • Page 884 Anti-Ice, Rain - System Description 737 MAX Flight Crew Operations Manual Wing Anti–Ice System Schematic L VALVE R VALVE WING ANTI-ICE THRUST LEVERS ABOVE T.O. WARNING BELOW T.O. WARNING GROUND HIGH THERMAL SWITCH TEMP TEMP AIR-GROUND SAFETY SENSORS BLEED AIR DUCT WING ANTI-ICE LEADING EDGE CONTROL VALVE...
  • Page 885 Automatic Flight 4 Automatic Flight 4-Automatic Flig ht Table Of Contents 737 MAX Flight Crew Operations Manual Automatic Flight Chapter 4 Table of Contents Section TOC Controls and Indicators ....... . . 4.10 Mode Control Panel (MCP) .
  • Page 886 Automatic Flight - Table of Contents 737 MAX Flight Crew Operations Manual Automatic Flight Approach and Landing ....4.20.17 Automatic Flight Approach Profile..... 4.20.22 Go–Around .
  • Page 887 737 MAX Flight Crew Operations Manual Automatic Flight Chapter 4 Controls and Indicators Section 10 10 Controls and Indicators Controls and Indicators File Highlight Mode Control Panel (MCP) A/P ENGAGE COURSE IAS/MACH HEADING ALTITUDE VERT SPEED COURSE V NAV L NAV VORLOC INTV INTV...
  • Page 888 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual OFF – disengages A/T and prevents A/T engagement. Changeover (C/O) Switch Push – • changes IAS/MACH display between IAS and MACH • automatic changeover occurs at approximately FL260. MCP Speed Condition Symbols Overspeed or underspeed limiting symbol appears when commanded speed cannot be reached.
  • Page 889 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual N1 Mode • A/T maintains thrust at N1 limit selected from FMC CDU. N1 mode engaged manually by pushing N1 switch if N1 mode is compatible with existing AFDS modes. N1 mode engages automatically when: •engaging LVL CHG in climb (except during inhibit period for 2 1/2 minutes after lift-off) •engaging VNAV in climb.
  • Page 890 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Speed Intervention (SPD INTV) Switch Push (when VNAV engaged) – • IAS/MACH display alternately shows selected IAS/Mach and blanks • when IAS/MACH display is unblanked, FMC speed intervention is active, FMC target speed is displayed, and IAS/MACH Selector may be used to set desired speed •...
  • Page 891 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Climb – • autothrottle holds FMC thrust limit • AFDS holds FMC target speed • automatic level-off occurs at MCP altitude or VNAV altitude, whichever is reached first •MCP constrained altitude annunciates VNAV ALT •VNAV constrained altitude annunciates VNAV PTH.
  • Page 892 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual ALTITUDE Display Displays selected altitude • displayed altitude is reference for altitude alerting and automatic level–offs • altitude range is 0 to 50,000 feet in 100 foot increments •...
  • Page 893 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual A LVL CHG climb or descent is initiated by: • selecting a new altitude • pushing LVL CHG switch • setting desired airspeed. Climb – • autothrottle holds limit thrust •...
  • Page 894 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual • uncorrected barometric altitude at which ALT HLD switch was pressed if not at MCP selected altitude •pitch mode annunciates ALT HOLD •ALT HLD switch light illuminates. When in ALT HOLD at selected MCP altitude: •...
  • Page 895 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual V/S mode automatically engages if ALT ACQ mode is engaged and a new MCP altitude is selected which is more than 100 feet different from previously selected altitude. •...
  • Page 896 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Lateral Navigation COURSE IAS/MACH HEADING V NAV L NAV VORLOC INTV SPEED LVLCHG HDGSEL GLARESHIELD COURSE Display Displays course set by course selector. Note: Different courses and frequencies on two VHF NAV receivers can cause disagreement between Captain and FO F/D displays and affect A/P operation.
  • Page 897 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual LNAV arming criteria on the ground: • origin runway in flight plan • active route entered in FMC • track of first leg within 5 degrees of runway heading •...
  • Page 898 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual The capture point is variable and depends on intercept angle and closure rate. Localizer capture occurs not later than 1/2 dot deviation. Course capture is indicated when VOR/LOC annunciation changes from armed to engaged. While engaged in VOR or LOC modes: •...
  • Page 899 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Heading Select (HDG SEL) Switch Push – • engages HDG SEL command mode • commands roll to follow selected heading • annunciates HDG SEL as FMA roll mode and illuminates HDG SEL switch light.
  • Page 900 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual • SINGLE CH annunciates in A/P Status Display after localizer capture •for single autopilot approach, SINGLE CH remains annunciated for entire approach •for dual autopilot approach, SINGLE CH annunciation extinguishes 1B785, 1J585 - 1 J594 when second autopilot engages and ROLLOUT (as installed) armed and FLARE armed are annunciated...
  • Page 901 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Autopilot / Flight Director Pushing a CMD or CWS switch engages related A/P in CMD or CWS and illuminates switch lights. A/P can operate in CMD, CWS, or a combination of CMD and CWS.
  • Page 902 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Control Wheel Steering Engage (CWS ENGAGE) Switch (A or B): Push – • engages A/P • engages pitch and roll modes in CWS. Other pitch and roll modes not enabled •...
  • Page 903 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual • command bars are displayed if command pitch and/or roll modes are engaged • on ground, arms pitch and roll modes for engagement in TO/GA and 1B401, 1B402, 1B801 - 1B824 wings level when TO/GA switch is pushed.
  • Page 904 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Takeoff/Go–Around (TO/GA) Switches Push – engages AFDS and A/T in takeoff or go–around mode if previously armed. Autopilot / Autothrottle Indicators TEST P/RST P/RST P/RST MAIN PANEL - CAPTAIN/FIRST OFFICER STAB OUT OF...
  • Page 905 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Autothrottle (A/T) Disengage Light Illuminated (red) – • flashing – autothrottle has disengaged • steady – disengage light test switch held in position 2. Illuminated (amber) – • steady – disengage light test switch held in position 1 •...
  • Page 906 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Thrust Mode Display 96.0 96.0 87.7 87.7 ENGINE DISPLAY A/T LIM 96.0 96.0 87.7 87.7 ENGINE DISPLAY Thrust Mode Display N1 limit reference is the active N1 limit for autothrottle and manual thrust control. N1 limit reference is also displayed by N1 reference bugs with N1 SET control in AUTO position.
  • Page 907 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual • CON – continuous • ––– – FMC not computing thrust limit. Autothrottle Limit (A/T LIM) Indication Illuminated (white) – the FMC is not providing the A/T system with N1 limit values.
  • Page 908 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Roll Armed Mode • VOR/LOC (white) • LNAV FAC (white) (as 1B785, 1B786, 1J585 - 1J594 • LNAV VOR/LOC (white) installed) • LNAV (white) • LNAV B/CRS (white) (as 1B785, 1B786, 1J585 - 1J594 installed) •...
  • Page 909 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Pitch Armed Mode • G/S (white) • FLARE (white) • V/S (white) • G/S V/S (white) • VNAV (white) • G/P V/S (white) (as installed) 1B785, 1B786, 1J585 - 1J594 •...
  • Page 910 Automatic Flight - Controls and Indicators 737 MAX Flight Crew Operations Manual Intentionally Blank 4.10.24 MN-FLT-OH-201 March 1, 2021...
  • Page 911 737 MAX Flight Crew Operations Manual Automatic Flight Chapter 4 System Description Section 20 20 System Description Sy stem Description File Highlight General The automatic flight system (AFS) consists of the autopilot flight director system (AFDS) and the autothrottle (A/T). The flight management computer (FMC) provides N1 limits and target N1 for the A/T and command airspeeds for the A/T and AFDS.
  • Page 912 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Autopilot Engagement Criteria Each A/P can be engaged by pushing a separate CMD or CWS engage switch. A/P engagement in CMD or CWS is inhibited unless both of the following pilot–controlled conditions are met: •...
  • Page 913 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual • activating either pilot’s control wheel trim switch (except with LAND 3 1B785, 1J585 - 1J594 or LAND 2 annunciated) • moving either STAB TRIM PRI or the STAB TRIM B/U cutout switch to the CUTOUT position •...
  • Page 914 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual • the F/D has no landing flare capability. F/D command bars retract from view at approximately 50 feet RA on an ILS approach. • During a Fail Operational autoland flare with FLARE engaged and 1B785, 1J585 - 1J594 LAND 3 annunciated, F/D command bars center (as installed).
  • Page 915 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual AFDS Status Annunciation The following AFDS status annunciations are displayed in the A/P status display located above the attitude indicator on the outboard display unit: • CMD (one or both autopilots are engaged) •...
  • Page 916 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual AFDS Flight Mode Annunciations The flight mode annunciations are displayed just above the attitude indicator on the outboard display unit. The mode annunciations, from left to right, are: • autothrottle •...
  • Page 917 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual • TO/GA – Go–around Engaged for go–around by pushing the TO/GA switch under the following conditions: •inflight below 2000 feet radio altitude •inflight above 2000 feet radio altitude with flaps not up or G/S captured •not in takeoff mode •either F/D ON or OFF.
  • Page 918 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual • FLARE (armed) – during a dual A/P ILS approach, FLARE is displayed after LOC and G/S capture and below 1500 feet RA. The second A/P couples with the flight controls and A/P go–around mode arms •...
  • Page 919 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual With CWS engaged, the A/P maneuvers the airplane in response to control pressures applied by either pilot. The control pressure is similar to that required for manual flight. When control pressure is released, the A/P holds existing attitude.
  • Page 920 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual The A/T system operates properly with the EECs ON or in ALTN. In either case, the A/T uses the FMC N1 limits. During A/T operation, it is recommended that both EECs be ON or both be in ALTN, as this produces minimum thrust lever separation.
  • Page 921 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Automatic Flight Operations The phases of flight for automatic flight operations are: • Takeoff and climb • Approach and landing • Enroute • Go–around Automatic Flight Takeoff and Climb Takeoff is a flight director only function of the TO/GA mode.
  • Page 922 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual After LIFT-OFF: • if an engine failure occurs, the pitch command target speed is: •V2, if airspeed is below V2 •existing speed, if airspeed is between V2 and V2 + 20 •V2 + 20, if airspeed is above V2 + 20.
  • Page 923 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Automatic Flight Takeoff Profile 1B401, 1B4 02, 1B801 - 1B824 Engage A/P LNAV MCP SPD • A/P engages in • Pitch mode engages in MCP SPD LNAV TO/GA Thrust Reduction •...
  • Page 924 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual 1B401, 1B4 02, 1B801 - 1B824 Engage A/P LNAV VNAV SPD • A/P engages in LNAV VNAV SPD Thrust Reduction • A/T N1 mode engages at CLB power LNAV VNAV SPD 800 ft above field...
  • Page 925 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual 1B785, 1B7 86, 1J585 - 1J594 Engage A/P HDG SEL MCP SPD • A/P engages in • Pitch mode engages in MCP SPD HDG SEL TO/GA Thrust Reduction • A/T N1 mode engages at CLB power HDG SEL...
  • Page 926 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual 1B785, 1B7 86, 1J585 - 1J594 Engage A/P LNAV VNAV SPD • A/P engages in LNAV VNAV SPD Thrust Reduction • A/T N1 mode engages at CLB power LNAV VNAV SPD 800 ft above field...
  • Page 927 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Other pitch modes available are: • altitude hold (ALT HOLD) • level change (MCP SPD) • vertical speed (V/S). Automatic Flight Approach and Landing The AFDS provides guidance for single A/P non–precision approaches. The VOR/LOC switch arms the AFDS for VOR or localizer tracking.
  • Page 928 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Localizer and Glideslope Armed After setting the localizer frequency and course, pushing the APP switch selects the APP mode. The APP switch illuminates and VOR/LOC and G/S annunciate armed. The APP mode permits selecting the second A/P to engage in CMD. This arms the second A/P for automatic engagement after LOC and G/S capture and when descent below 1500 RA occurs.
  • Page 929 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual • the SINGLE CH annunciation extinguishes • A/P go–around mode arms but is not annunciated. Note: During a dual autopilot approach and after FLARE ARM annunciation, any attempted manual override of the autopilots may result in an autopilot disengage.
  • Page 930 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Flare The A/P flare maneuver starts at approximately 50 feet RA and is completed at touchdown: • FLARE engaged is annunciated and with LAND 3 annunciated (as 1B785, 1J585 - 1J594 installed), F/D command bars center.
  • Page 931 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual ILS Beam Anomaly/Ground Station Failure Detection For a single channel or F/D only approach, the autopilot will disengage and/or the F/D bars will be removed if a persistent localizer/glideslope beam anomaly or ground station failure is detected.
  • Page 932 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Automatic Flight Approach Profile 1B401, 1B4 02, 1B786 - 1B824 ILS APPROACH 4.20.22 MN-FLT-OH-201 March 1, 2021...
  • Page 933 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual 1B785, 1B7 86, 1J585 - 1J594 IAN APPROACH March 1, 2021 MN-FLT-OH-201 4.20.23...
  • Page 934 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual 1B785, 1J585 - 1J594 FAIL-OPERATIONAL APPROACH 4.20.24 MN-FLT-OH-201 March 1, 2021...
  • Page 935 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Go–Around Go–Around (GA) mode is engaged by pushing either TO/GA switch. An A/P go–around requires dual A/P operation and is armed when FLARE armed is annunciated. If both A/Ps are not operating, a manual F/D go–around is available. With the A/T Arm switch at ARM, the A/T go–around mode is armed: •...
  • Page 936 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual TO/GA mode termination from A/P go–around: • below 400 feet RA, the AFDS remains in the go–around mode unless both A/Ps and F/Ds are disengaged • if the A/P is compensating for asymmetric thrust during the go-around, 1B785, 1J585 - 1J594 autopilot rudder control is disabled when a new pitch or roll mode is selected...
  • Page 937 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual • not in takeoff mode • if the TO/GA switches are activated after touchdown (wheel spin-up). With the first push of either TO/GA switch: • A/T (if armed) engages in GA and advances thrust toward the reduced go–around N1 to produce 1000 to 2000 fpm rate of climb.
  • Page 938 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Single Engine F/D Go–Around With a push of either TO/GA switch: • F/D roll commands hold current ground track at or below 50 feet AGL. Above 50 feet AGL, LNAV will engage. The Roll Mode annunciation will display LNAV engaged above 50 feet AGL •...
  • Page 939 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual During an approach without FLARE arm or FLARE engage displayed, if TO/GA is pressed with LNAV arm annunciated on the FMA, the flight director LNAV mode will engage when the airplane is above 50 feet. Below that altitude the mode will be track hold.
  • Page 940 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Automatic Flight Go–Around Profile Missed Approach altitude MCP SPD LNAV ALT HOLD • Pitch mode engages in ALT HOLD Approaching Missed Approach altitude - MCP SPD LNAV ALT ACQ •...
  • Page 941 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Takeoff or Go–Around If windshear is encountered during F/D takeoff or go–around, the F/D pitch command bar provides commands to maintain the target speed until vertical speed decreases to approximately +600 fpm. At this point, the F/D pitch bar commands a 15 degree nose–up pitch attitude.
  • Page 942 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Speeds greater than Vmo/Mmo cannot be selected from the MCP. Speeds can be selected which exceed flap and gear placards or are less than minimum speed. Minimum speed is based on angle of attack and is approximately 1.3 Vs for the current flap configuration.
  • Page 943 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual Minimum Speed Reversion The AFDS and A/T do not control to a speed which is less than minimum speed for the current flap configuration. This speed is approximately 1.3 Vs. Minimum speed, FMC speed, or selected speed, whichever is higher, becomes the AFS commanded speed.
  • Page 944 Automatic Flight - System Description 737 MAX Flight Crew Operations Manual In the above modes with the autopilot engaged, the autopilot disengages and the F/D command bars (both pitch and roll) are removed one second after stick shaker activation. When airspeed increases to the top of the minimum maneuver speed (amber) bar, the F/D command bars (both pitch and roll) return and the autopilot can be re-engaged.
  • Page 945 Communications 5 Communications 5-Communications Table Of Contents 737 MAX Flight Crew Operations Manual Communications Chapter 5 Table of Contents Section TOC Controls and Indicators ....... . . 5.10 Radio Tuning Panel .
  • Page 946 Communications - Table of Contents 737 MAX Flight Crew Operations Manual Pre-Recorded Announcement Machine (PRAM)....5.20.4 Call System......... . . 5.20.6 VHF Communications .
  • Page 947 737 MAX Flight Crew Operations Manual Communications Chapter 5 Controls and Indicators Section 10 10 Controls and Indicators Controls and Indicators File Highlight Radio Tuning Panel ACTIVE STANDBY TEST VHF1 VHF3 VHF2 HF SENS AFT ELECTRONIC PANEL Note: When a switch is labeled "INOP" that switch is not available and should not be used.
  • Page 948 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Radio Tuning Panel OFF Switch Push – • disconnects the panel from the communication radios • switch illuminates (white). HF Sensitivity Control Rotate – adjusts the sensitivity of the on–side HF receiver. Radio Tuning Light Illuminated (white) - indicates the selected radio.
  • Page 949 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Radio Tuning Panel Fail Modes ACTIVE STANDBY PANEL FAIL ACTIVE STANDBY FAIL FAIL AFT ELECTRONIC PANEL PANEL FAIL The radio tuning panel has failed. FAIL FAIL The selected radio has failed. Note: The selected frequencies may continue to be displayed in the frequency indicator when the radio is not available.
  • Page 950 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Audio Control Panel (ACP) 1B785, 1B786 MIC SELECTOR 1-HF-2 1-VHF-2-VHF-3 1-NAV-2 1-ADF-2 SPKR MASK BOOM NORM FLIGHT DECK CREW STATIONS Note: When a switch is labeled "INOP" that switch is not available and should not be used.
  • Page 951 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Transmitter Selector (MIC SELECTOR) Switches Illuminated – related switch is active Push – • selects related communication system for subsequent transmission • only one switch may be selected at a time; pushing a second switch deselects first switch •...
  • Page 952 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual 1B785, 1B786 Speaker (SPKR) Switch Illuminated (white) – SPKR switch is active. Push – audio from selected receiver is heard on overhead speaker. Rotate – adjusts overhead speaker volume. Push again –...
  • Page 953 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual SELCAL Panel 1B785, 1B786, 1J590 - 1J594 1B785, 1B786 SELCAL VHF 1 VHF 2 VHF 3 HF 1 HF 2 PRESS TO RESET AFT ELECTRONIC PANEL Note: When a switch is labeled "INOP" that switch is not available and should not be used.
  • Page 954 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual ACARS Printer October 26, 2021 5.10.8 MN-FLT-OH-201...
  • Page 955 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual October 26, 2021 MN-FLT-OH-201 5.10.9...
  • Page 956 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual The Printer Control Panel lights brightness is controlled by rotating the "PANEL" brightness switch on the Flood and Aft Electronics Lights Control Panel, see chapter 1.30, located on the AFT ELECTRONIC PANEL. SELF ALERT RESET...
  • Page 957 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Printer Busy (PTR BUSY) Light Illuminated - • printer is printing • flashes when printing is complete. Broadband System Switch 1B824 1B824 BROADBAND SYSTEM BROADBAND COMM XMIT INHIB AFT OVERHEAD PANEL Broadband System Power/Mode Selector OFF - removes power from the Broadband System.
  • Page 958 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Miscellaneous Communication Controls (Typical) OVERHEAD SPEAKER HAND MICROPHONE (AS INSTALLED) BOOM MICROPHONE/ HEADSET OXYGEN MASK MICROPHONE HEADPHONES BOOM MIC HEAD PHONE HAND MIC (VIEW FROM BELOW) FLIGHT DECK CREW STATIONS Overhead Speaker Monitors audio from related pilot’s ACP.
  • Page 959 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Communication Jacks Used for appropriate microphone or headphone plugs. Push–To–Talk Switch MIC (microphone) – • selects oxygen mask or boom microphone for transmission, as selected by ACP transmitter selector. •...
  • Page 960 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Interphone and Passenger Address Controls SERVICE INTER INTERPHONE PHONE FLIGHT AFT OVHD PANEL EXTERNAL POWER CONNECTOR PANEL INTERPHONE PASS ADDRESS CONTROL STAND FLIGHT DECK CREW/ ATTENDANT STATIONS (AS INSTALLED) SERVICE INTERPHONE Switch OFF –...
  • Page 961 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Passenger Address (PASS ADDRESS) Hand Microphone Jack With microphone installed: • used to make PA announcements • bypasses ACPs. INTERPHONE FLIGHT Jack Connects ground crew to flight interphone system. Flight Deck / Attendant PA Hand Microphone Used to make PA announcements.
  • Page 962 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual ERASE Switch (red) Push (2 seconds) – • all four channels are erased • operative only when airplane is on ground and parking brake is set. 1B401, 1B402, 1B801 - 1B824 TEST Switch Push –...
  • Page 963 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual VOICE RECORDER Switch AUTO - powers the cockpit voice recorder from first engine start until 5 minutes after last engine shutdown ON - powers the cockpit voice recorder until first engine start, then trips the switch to AUTO.
  • Page 964 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Ground Call (GRD CALL) Switch Push – sounds a horn in nose wheel well until released. Attendant Call (ATTEND) Switch Push – • sounds a two–tone chime in passenger cabin •...
  • Page 965 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Master Call Lights Lavatory Call Light Crew Call Light (amber) (pink) Passenger Call Light (blue) CALL LIGHT PANEL Call Light Illuminated – • pink – flight deck or other flight attendant station is calling. •...
  • Page 966 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual ATTENDANT Call Switch Push – • sounds a two–tone chime in passenger cabin • illuminates both pink master call lights. Call RESET Switch Push – • extinguishes both pink master call lights •...
  • Page 967 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual Pre-Recorded Announcement Machine (PRAM) The PRAM is typically located above the FA seats on the LAV A wall. ANNC VOLUME MUSIC FLIGHT START STOP READY PRE-RECORDED ANNOUNCEMENT MACHINE (PRAM) October 26, 2021 MN-FLT-OH-201 5.10.21...
  • Page 968 Communications - Controls and Indicators 737 MAX Flight Crew Operations Manual LCD Display Displays system status and announcement selection. Mode Control Select Switches Selectable Modes are: • ANNC-manual announcement selection mode. • MUSIC-music selection mode. • FLIGHT-Flight pattern auto announcement selection mode. Music Volume Press ▲...
  • Page 969 737 MAX Flight Crew Operations Manual Communications Chapter 5 System Description Section 20 20 System Description Sy stem Description File Highlight Introduction The communication system includes: • radio communication system • interphone communication system • cockpit voice recorder system • communication crew alerting system The communication systems are controlled using the: •...
  • Page 970 Communications - System Description 737 MAX Flight Crew Operations Manual The two flight compartment speakers are muted for the Captain’s and First Officer’s push-to-talk microphone operation. The speakers are not muted for oxygen mask microphone operation. Microphones Hand microphones and boom microphones may be plugged into the related jacks at the flight deck crew stations.
  • Page 971 Communications - System Description 737 MAX Flight Crew Operations Manual The ACP transmitter selectors are not functional. Any transmission from that 1B401, 1B402, 1B801 - 1J594 station must be from the radio shown on the chart below. The transmitter selector for the usable radio illuminates when a station is operating in the degraded mode.
  • Page 972 Communications - System Description 737 MAX Flight Crew Operations Manual Service (Attendant) Interphone System The service interphone system provides intercommunication between the flight deck, Flight Attendants, and ground personnel. Flight deck crewmembers communicate using either a separate handset (if installed) or their related ACP and any standard microphone.
  • Page 973 Communications - System Description 737 MAX Flight Crew Operations Manual The PRAM is typically located above the FA seats on the LAV A wall. When an announcement is selected, the PRAM micro-processor accesses the announcement and broadcasts the information. PRAM announcements can be selected using the PRAM key pad after pressing the ANNC button on the Mode Control Select Panel.
  • Page 974 Communications - System Description 737 MAX Flight Crew Operations Manual • MUSIC-music selection mode. To play music, press the MUSIC button. The MUSIC light illuminates and a music selection screen appears on the LCD, along with the corresponding codes. Enter the code for the desired music title, using the KEY pad.
  • Page 975 Communications - System Description 737 MAX Flight Crew Operations Manual 1B401, 1B402, 1B801 - 1J594 Location of Call Visual Signal at Aural Signal at Called Position Originator Called Position Called Position Flight deck Attendant station Pink master Two–tone chime call light Flight deck Nose wheel well Horn in nose...
  • Page 976 Communications - System Description 737 MAX Flight Crew Operations Manual The audio control panels are used to control voice transmission and receiver monitoring. When an HF transmitter is keyed after a frequency change, the antenna tunes. A steady or intermittent tone may be heard through the audio system.
  • Page 977 Communications - System Description 737 MAX Flight Crew Operations Manual The airborne system consists of a management unit in the E/E compartment, either an interactive display unit or multipurpose control display unit (MCDU), and frequently a printer. Data is entered and transmitted to the ground operations center.
  • Page 978 Communications - System Description 737 MAX Flight Crew Operations Manual Broadband System A dedicated broadband communications system provides passengers and crew 1B824 with real-time, high-speed internet connectivity in flight. Passengers and crew access the system with compatible personal electronic devices (PEDs) using the cabin wireless access points (WAP).
  • Page 979 Electrical 6 Electrical 6-Electrical Table Of Contents 737 MAX Flight Crew Operations Manual Electrical Chapter 6 Table of Contents Section TOC Controls and Indicators ....... . . 6.10 Electrical Panel .
  • Page 980 Electrical - Table of Contents 737 MAX Flight Crew Operations Manual DC Power System Schematic ......6.20.10 Standby Power System .
  • Page 981 737 MAX Flight Crew Operations Manual Electrical Chapter 6 Controls and Indicators Section 10 10 Controls and Indicators Controls and Indicators File Highlight Electrical Panel DC AMPS CPS FREQ DC VOLTS AC AMPS AC VOLTS TR UNIT ELEC DISCHARGE AC AND DC AC AND DC MAINT METERING PANEL...
  • Page 982 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual AC and DC Metering Panel DC AMPS CPS FREQ DC VOLTS AC AMPS AC VOLTS TR UNIT ELEC DISCHARGE MAINT AUX BAT APU GEN GEN2 GEN1 STBY STBY TEST TEST IFE/PASS CAB/UTIL...
  • Page 983 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual Frequency Meter Indicates frequency of source selected by AC meters selector. AC Voltmeter Indicates voltage of source selected by AC meters selector. Battery Discharge (BAT DISCHARGE) Light Illuminated (amber) – with BAT switch ON, excessive battery discharge detected. TR UNIT Light Illuminated (amber) –...
  • Page 984 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual AC Meters Selector Selects AC source for AC voltmeter, AC ammeter and frequency meter indications TEST – used by maintenance. CAB/UTIL Switch OFF – removes electrical power from galley and cabin equipment systems including: •...
  • Page 985 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual Generator Drive and Standby Power Panel STANDBY STANDBY PWR OFF PWR OFF DRIVE DRIVE STANDBY POWER DISCONNECT DISCONNECT AUTO FORWARD OVERHEAD PANEL Generator Drive (DRIVE) Lights Illuminated (amber) – Integrated drive generator (IDG) low oil pressure caused by one of the following: •...
  • Page 986 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual STANDBY POWER Switch AUTO (guarded position) – • In flight, or on the ground, and AC transfer buses powered: •AC standby bus is powered by AC transfer bus 1 •DC standby bus is powered by TR1, TR2 and TR3 •...
  • Page 987 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual Ground Power Available (GRD POWER AVAILABLE) Light Illuminated (blue) – ground power is connected and meets airplane power quality standards. Ground Power (GRD PWR) Switch Three position switch, spring–loaded to neutral OFF –...
  • Page 988 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual APU Generator Off Bus (GEN OFF BUS) Light Illuminated (blue) – APU is running and not powering a bus. APU Generator (GEN) Switches Three position switch, spring–loaded to neutral. OFF –...
  • Page 989 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual GROUND SERVICE Switch Momentary push–button switch. Provides manual control of ground service buses. Enables servicing airplane using external power without activating AC transfer buses. Illuminated (white) – • ON – connects external power to ground service buses •...
  • Page 990 Electrical - Controls and Indicators 737 MAX Flight Crew Operations Manual Intentionally Blank 6.10.10 MN-FLT-OH-201 March 1, 2021...
  • Page 991 737 MAX Flight Crew Operations Manual Electrical Chapter 6 System Description Section 20 20 System Description Sy stem Description File Highlight Introduction Dual Battery Primary electrical power is provided by two engine integrated drive generators (IDGs) which supply three-phase, 115 volt, 400 cycle alternating current. Each IDG supplies its own bus system in normal operation and can also supply essential and non-essential loads of the opposite side bus system when one IDG is inoperative.
  • Page 992 Electrical - System Description 737 MAX Flight Crew Operations Manual Ground Service For ground servicing, a ground service switch is on the forward attendant’s panel. The switch provides ground power directly to the AC ground service buses for utility outlets, cabin lighting and the battery charger without powering all airplane electrical buses.
  • Page 993 Electrical - System Description 737 MAX Flight Crew Operations Manual AC Power System Each AC power system consists of a transfer bus, a main bus, two galley buses, and a ground service bus. Transfer bus 1 also supplies power to the AC standby bus.
  • Page 994 Electrical - System Description 737 MAX Flight Crew Operations Manual Flight Deck Auxiliary Power System The system is composed of a power converter and AC outlets on the P6 and P18 1B401 - 1B785, 1B801 - 1J594 panels to provide power for Flight Deck Personal Electronic Devices (PEDs). A protective device is a part of the safety aspect of the outlets to prevent tampering with foreign objects.
  • Page 995 Electrical - System Description 737 MAX Flight Crew Operations Manual AC Power Schematic GRD POWER AVAILABLE DRIVE DRIVE GROUND SERVICE GEN 1 APU GEN GEN 2 TO GND FROM GND SVC BUS 2 SVC SWITCH AC TRANSFER BUS 1 AC TRANSFER BUS 2 BTB1 BTB2 SERVICE...
  • Page 996 Electrical - System Description 737 MAX Flight Crew Operations Manual The generator drive (DRIVE) amber caution light is illuminated when low oil pressure is sensed in the IDG. IDG low oil pressure is caused by one of the following: • IDG failure •...
  • Page 997 Electrical - System Description 737 MAX Flight Crew Operations Manual Electrical Power Controls and Monitoring Schematic DC AMPS CPS FREQ DRIVE DISCONNECT DC VOLTS AC AMPS AC VOLTS TR UNIT ELEC DISCHARGE MAINT AUX BAT APU GEN GEN2 GEN1 STBY STBY TEST TEST...
  • Page 998 Electrical - System Description 737 MAX Flight Crew Operations Manual Transformer Rectifier Units The TRs convert 115 volt AC to 28 volt DC, and are identified as TR1, TR2, and TR3. TR1 receives AC power from transfer bus 1. TR2 receives AC power from transfer bus 2.
  • Page 999 Electrical - System Description 737 MAX Flight Crew Operations Manual Battery Charger Transformer/Rectifier Dual Battery The purpose of the battery chargers is to restore and maintain the batteries at full electrical power. The main battery charger is powered through AC ground service bus 2.
  • Page 1000 Electrical - System Description 737 MAX Flight Crew Operations Manual DC Power System Schematic BUS TRANSFER AC TRANSFER BUS 2 AC TRANSFER BUS 1 115V AC GND 115V AC GND SERVICE BUS 1 SERVICE BUS 2 CROSS BUS TIE RELAY DC BUS 1 DC BUS 2 DC STANDBY BUS...

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