Boeing 737 Quick Reference Handbook
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Boeing 737 Quick Reference Handbook

Boeing 737 Quick Reference Handbook

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Quick Reference Handbook
QA.Index Non-Normal Checklists-Index
ABORTED ENGINE START . . . . . . . . . . . . . . . 7.1
AIRSPEED UNRELIABLE . . . . . . . . . . . . . . . 10.1
APU FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.2
DEPRESSURIZATION . . . . . . . . . . . . . . . . . . . 2.4
EMERGENCY DESCENT . . . . . . . . . . . . . . . . . 2.6
SEPARATION . . . . . . . . . . . . . . . . . . . . . . . . . 8.6
ENGINE LIMIT/SURGE/STALL . . . . . . . . . . . . 7.12
ENGINE OVERHEAT . . . . . . . . . . . . . . . . . . . . . 8.8
ENGINE TAILPIPE FIRE . . . . . . . . . . . . . . . . . . 8.9
EVACUATION . . . . . . . . . . . . . . . . . Back Cover.2
OVERSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . 15.1
RUNAWAY STABILIZER . . . . . . . . . . . . . . . . . . 9.9
ROLL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9.25
WARNING HORN - CABIN ALTITUDE
OR CONFIGURATION . . . . . . . . . . . . . . . . . 15.2
June 9, 2006
737
Quick Action Index
D6-27370-73V-EZY(3V)
QA.Index.1

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  • Page 1: Table Of Contents

    Quick Reference Handbook Quick Action Index QA.Index Non-Normal Checklists-Index ABORTED ENGINE START ....7.1 AIRSPEED UNRELIABLE ....10.1 APU FIRE .

  • Page 2: Intentionally Blank

    Non-Normal Checklists - Index Intentionally Blank QA.Index.2 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 3 ENG OVERHEAT ........7.15,8.8 Copyright © The Boeing Company. See title page for details.
  • Page 4 LOCK FAIL ..........1.4 Copyright © The Boeing Company. See title page for details.
  • Page 5 YAW DAMPER ......... 9.27 Copyright © The Boeing Company. See title page for details.
  • Page 6 Annunciated Index - Lights List 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. ANN.Index.4 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 7 Non–Normal Checklist Use ......CI.2.3 Copyright © The Boeing Company. See title page for details.
  • Page 8 Checklist Introduction - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. CI.TOC.0.2 D6-27370-73V-EZY(3V) March 28, 2005...

  • Page 9: Normal Checklists

    If it becomes apparent that an entire procedure was not done: • stop the checklist • complete the entire procedure • do the checklist from the start Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) CI.1.1...

  • Page 10: Checklist Content

    • needed to meet regulatory requirements, or • items needed to maintain fleet commonality between the 737, 747-400, 757, 767, and 777, or • items that enhance safety of flight and are not monitored by an alerting system (for example autobrakes), or •...

  • Page 11: Non-Normal Checklists

    Approach or Landing checklist. Flight patterns for some non–normal situations are located in the Maneuvers chapter and show the sequence of configuration changes. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) CI.2.1...
  • Page 12 The NORMAL position of the oxygen regulator is used if prolonged use is needed and the situation allows. Normal boom mic operation is restored when oxygen use is no longer needed Copyright © The Boeing Company. See title page for details. CI.2.2 D6-27370-73V-EZY(3V)

  • Page 13: Non-Normal Checklist Use

    • the flight path is under control • the airplane is not in a critical stage of flight (such as takeoff or landing) • all recall items are complete. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 14 The following symbol shows that the checklist is complete. Each checklist has a checklist complete symbol at the end. Copyright © The Boeing Company. See title page for details. CI.2.4 D6-27370-73V-EZY(3V)
  • Page 15 “___CHECKLIST COMPLETE EXCEPT FOR DEFERRED ITEMS.” Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 16 Checklist Introduction - Non-Normal Checklists 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. CI.2.6 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 17 WINDOW DAMAGE ........0.38 Copyright © The Boeing Company. See title page for details.

  • Page 18: Unannunciated Checklists Section

    Non-Normal Checklists - Unannunciated Checklists 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.0.2 D6-27370-73V-EZY(3V) June 9, 2006...

  • Page 19: Aborted Engine Start

    ENGINE START switch ......OFF Note: MOC and Engineering should be contacted before attempting subsequent start, even if no limits have been exceeded. <EZY> Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 20: Air Conditioning Smoke/Fumes

    L PACK switch ......AUTO Plan to land at nearest suitable airport. Accomplish the SMOKE/FUMES REMOVAL checklist, if needed. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 21: Airspeed Unreliable

    PROBE HEAT .......Check ON MACH/AIRSPEED indicators ....Cross check Copyright © The Boeing Company. See title page for details. March 28, 2005...

  • Page 22: Auto Fail/Unscheduled Pressurization

    OUTFLOW VALVE switch ....As needed Operate the outflow valve to maintain proper cabin altitude and cabin rate of change. At traffic pattern altitude, position the outflow valve to full open. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 23 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 24: Bomb Threat

    • Move the passengers to a position at least 200m upwind of the aircraft. • Consult Ops Man Part A, section 10.1.6. Continued on next page Copyright © The Boeing Company. See title page for details. D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 25 Turbulent air penetration speed is usually a good compromise. • Upon landing, follow the same procedures as for taxiing. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 26: Cabin Altitude Warning Or Rapid Depressurization

    Accomplish the EMERGENCY DESCENT checklist if the airplane is above 14,000 feet MSL and control of cabin pressure is not possible, or cabin pressure is lost. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)

  • Page 27: Ditching

    Plan to touch down on the windward side and parallel to waves and swells. Plan a flaps 40 landing unless other configuration is needed. Continued on next page Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 28 Final position ....... . Transmit Transmit all pertinent information regarding final ditching position. Continued on next page Copyright © The Boeing Company. See title page for details. 0.10 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 29 At flare, rotate smoothly to touchdown attitude of 10-12 degrees, maintaining desired airspeed and rate of descent with thrust. At touchdown, reduce thrust to idle. Copyright © The Boeing Company. See title page for details. 0.11 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 30 • turn on cabin reading lights • turn on galley attendants work lights. [Prepares cabin lighting prior to depowering cabin fluorescent lights.] Continued on next page Copyright © The Boeing Company. See title page for details. 0.12 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 31 • turn off IFE and PC power switches (as installed). Plan to land at the nearest suitable airport. Accomplish the SMOKE/FUMES REMOVAL checklist, if needed. Copyright © The Boeing Company. See title page for details. 0.13 December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 32: Emergency Descent

    ENGINE START switches ....As needed The new course of action is based on weather, oxygen, fuel remaining and available airports. Use of long range cruise may be appropriate. Copyright © The Boeing Company. See title page for details. 0.14 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 33 An increase in fuel imbalance of approximately 230 kgs or more in 30 minutes should be considered an engine fuel leak. Conditions permitting, visually check for an engine fuel leak. Continued on next page Copyright © The Boeing Company. See title page for details. 0.15 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 34 TRANSPONDER MODE selector ....TA [Prevents climb commands which can exceed single engine performance capability. Continued on next page Copyright © The Boeing Company. See title page for details. 0.16 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 35 CROSSFEED selector ......OPEN Apply thrust changes slowly and smoothly. If a climb is needed, maintain the minimum pitch attitude needed for safe flight. Copyright © The Boeing Company. See title page for details. 0.17 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 36 DUCT PRESSURE ....Minimum 30 PSI If needed, advance the thrust lever to increase duct pressure. Continued on next page Copyright © The Boeing Company. See title page for details. 0.18 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 37: After Engine Start

    APU ........As needed TRANSPONDER MODE selector ....TA/RA Copyright © The Boeing Company. See title page for details. 0.19...
  • Page 38 Comply with demands without surrendering Avoid conflict on the airplane Do not attempt to overpower the hijackers Do not open the flight deck door under any circumstances. Copyright © The Boeing Company. See title page for details. 0.20 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 39 A maximum two-pilot effort on the controls will not cause a cable or system failure. Do not turn off any flight control switches. Continued on next page Copyright © The Boeing Company. See title page for details. 0.21 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 40 10° C. Note: When VREF ICE is needed, the wind additive should not exceed 10 knots. Continued on next page Copyright © The Boeing Company. See title page for details. 0.22 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 41 Flaps ........15, green light Copyright © The Boeing Company. See title page for details.
  • Page 42 APU BLEED AIR switch ......OFF Continued on next page Copyright © The Boeing Company. See title page for details. 0.24...
  • Page 43 The microphone/interphone with the stuck switch continuously transmits on flight interphone. The associated audio selector panel should remain on flight interphone. All other audio selector panels may be used normally. Copyright © The Boeing Company. See title page for details. 0.25 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 44 10,000 feet, whichever is higher At 14,000 feet or below: PRESSURIZATION MODE selector ... MAN Continued on next page Copyright © The Boeing Company. See title page for details. 0.26 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 45 [High airspeed may prevent opening the window.] First officer's sliding window ....Open Copyright © The Boeing Company. See title page for details. 0.27...
  • Page 46 10° C. Note: When VREF ICE is needed, the wind additive should not exceed 10 knots. Establish landing configuration early. Continued on next page Copyright © The Boeing Company. See title page for details. 0.28 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 47 Flaps ........15, Green light Copyright © The Boeing Company. See title page for details.
  • Page 48 Hold outflow valve switch in the OPEN position until outflow VALVE position indicator shows valve full open. Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 0.30 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 49 YAW DAMPER ....... . . OFF Continued on next page Copyright © The Boeing Company. See title page for details. 0.31...
  • Page 50 Note: Consider checking rudder freedom of movement at a safe altitude using slow rudder inputs while in the landing configuration and at approach speed. Continued on next page Copyright © The Boeing Company. See title page for details. 0.32 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 51 AUTOTHROTTLE ......ENGAGE Accomplish the normal DESCENT, APPROACH and LANDING checklists. Copyright © The Boeing Company. See title page for details. 0.33 December 2, 2005...
  • Page 52 • Engine malfunctions, increasing EGT, engine stall or flameout • Decrease or loss of airspeed indications • Equipment Cooling OFF light. Continued on next page Copyright © The Boeing Company. See title page for details. 0.34 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 53 If N2 is steadily increasing, and EGT remains within limits, the start is progressing normally. Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 0.35 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 54 If an intermittent horn sounds on the ground: Assure proper airplane takeoff configuration. If a steady horn sounds in flight: Assure proper airplane landing configuration. Copyright © The Boeing Company. See title page for details. 0.36 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 55 0.37 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 0.37 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 56 Sustained flight below 10,000 feet is not recommended due to the greater risk of bird strike. Continued on next page Copyright © The Boeing Company. See title page for details. 0.38 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 57 No crew action is needed. Shoulder harnesses may be removed. If a delamination only condition exists on any window: No crew action is needed. Shoulder harnesses may be removed. Copyright © The Boeing Company. See title page for details. 0.39 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 58 0.40 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 0.40 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 59 WINDOW DAMAGE ........1.6 Copyright © The Boeing Company. See title page for details.

  • Page 60: Intentionally Blank

    Non-Normal Checklists - Airplane General, Emer. Equip., Doors, Windows 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.1.2 D6-27370-73V-EZY(3V) December 2, 2005...

  • Page 61: Nnc.1 Non-Normal Checklists-Airplane General, Emer. Equip., Doors, Windows

    FLIGHT DECK DOOR selector ....DENY Rotate and hold for 1 second. [Prohibits unauthorized access to the flight deck.] Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 62: Door Annunciator

    If EQUIP, FWD/AFT CARGO or AIRSTAIR light is illuminated and pressurization is normal: Proceed normally. If EQUIP, FWD/AFT CARGO or AIRSTAIR light is illuminated and pressurization is not normal: Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 63: Elt

    ELT switch ......ON then ARM [Resets the ELT.] Copyright © The Boeing Company. See title page for details. December 2, 2005...

  • Page 64: Emergency Exit Lights Not Armed

    Note: The door can be locked with the dead bolt. PASSENGER OXYGEN ON The PASS OXY ON light illuminated indicates the Condition: passenger oxygen system is activated. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 65: Tailstrike On Takeoff

    OUTFLOW VALVE switch ......OPEN Hold outflow valve switch in the OPEN position until outflow VALVE position indicator shows valve full open. Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 66 LAND ALT ....... . 13,000 FT Continued on next page Copyright © The Boeing Company. See title page for details. June 9, 2006...
  • Page 67 No crew action is needed. Shoulder harnesses may be removed. If a delamination only condition exists on any window: No crew action is needed. Shoulder harnesses may be removed. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 68 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 69: Air Systems

    WING-BODY OVERHEAT ......2.10 Copyright © The Boeing Company. See title page for details.
  • Page 70 Non-Normal Checklists - Air Systems 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.2.2 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 71 L PACK switch ......AUTO Plan to land at the nearest suitable airport. Accomplish the SMOKE/FUMES REMOVAL checklist, if needed. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 72 OUTFLOW VALVE switch ....As needed Operate the outflow valve to maintain proper cabin altitude and cabin rate of change. At traffic pattern altitude, position the outflow valve to full open. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 73 WING ANTI-ICE ......As needed CAUTION: Use of wing anti-ice above approximately FL350 may cause bleed trip off and possible loss of cabin pressure. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 74 Accomplish the EMERGENCY DESCENT checklist if the airplane is above 14,000 feet MSL and control of cabin pressure is not possible, or cabin pressure is lost. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 75 TEMPERATURE selector ....MANUAL Adjust the air mix valve position as needed. Copyright © The Boeing Company. See title page for details. March 28, 2005...
  • Page 76 ENGINE START switches ....As needed The new course of action is based on weather, oxygen, fuel remaining and available airports. Use of long range cruise may be appropriate. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 77 FLIGHT ALTITUDE indicator ....Reset Reset to actual airplane altitude. Copyright © The Boeing Company. See title page for details. December 2, 2005...
  • Page 78 ......Closed Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005...
  • Page 79 GALLEY power ......OFF Copyright © The Boeing Company. See title page for details.
  • Page 80 LEFT PACK switch ..... . . AUTO WING ANTI-ICE switch ....As needed Copyright © The Boeing Company. See title page for details. 2.10...
  • Page 81 WING ANTI-ICE VALVE OPEN ......3.3 Copyright © The Boeing Company. See title page for details.
  • Page 82 Non-Normal Checklists - Anti-Ice, Rain 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.3.2 D6-27370-73V-EZY(3V) March 28, 2005...

  • Page 83: Nnc.3 Non-Normal Checklists-Anti-Ice, Rain

    Valve Open: If total air temperature is above 10°C, limit thrust on the affected engine to 80% N1 if possible. Valve Closed: Avoid icing conditions. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 84: Probe Heat

    Windshield air controls......Pull [Vents conditioned air to the inside of the windshield for defogging.] Copyright © The Boeing Company. See title page for details. March 28, 2005...
  • Page 85 WING ANTI–ICE switch ......OFF Avoid icing conditions. Copyright © The Boeing Company. See title page for details. March 28, 2005...
  • Page 86 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 87 AUTOTHROTTLE DISENGAGE ......4.1 Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) TOC.4.1...
  • Page 88 Non-Normal Checklists - Automatic Flight 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.4.2 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 89 Fly the airplane manually or re–engage an autopilot. AUTOTHROTTLE DISENGAGE The flashing red A/T light illuminated indicates the Condition: autothrottle has disengaged. Control thrust manually or re–engage the autothrottle. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 90 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 91 MICROPHONE SWITCH) ......5.1 Copyright © The Boeing Company. See title page for details.
  • Page 92 Non-Normal Checklists - Communications, Datalink 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.5.2 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 93 The microphone/interphone with the stuck switch continuously transmits on flight interphone. The associated audio selector panel should remain on flight interphone. All other audio selector panels may be used normally. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 94 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 95 TRANSFER BUS OFF ........6.6 Copyright © The Boeing Company. See title page for details.
  • Page 96 Non-Normal Checklists - Electrical 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.6.2 D6-27370-73V-EZY(3V) March 28, 2005...

  • Page 97: Nnc.6 Non-Normal Checklists-Electrical

    ELEC The ELEC light illuminated indicates a fault exists in Condition: the DC or standby power system. Note: The ELEC light only illuminates on the ground. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 98 • turn on cabin reading lights • turn on galley attendants work lights. [Prepares cabin lighting prior to depowering cabin fluorescent lights.] Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 99 • turn off cabin fluorescent light switches • turn off IFE and PC power switches (as installed). Plan to land at the nearest suitable airport. Accomplish the SMOKE/FUMES REMOVAL checklist, if needed. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 100: Loss Of Both Engine Driven Generators

    (STBY power control unit, P6) ....Reset if tripped Continued on next page Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 101: Source Off

    If SOURCE OFF light remains illuminated: APU (if available) ....START & ON BUS Copyright © The Boeing Company. See title page for details. December 2, 2005...

  • Page 102: Standby Power Off

    If TRANSFER BUS OFF light remains illuminated: APU (if available) ....START & ON BUS Copyright © The Boeing Company. See title page for details. March 28, 2005...
  • Page 103 VOLCANIC ASH ........7.26 Copyright © The Boeing Company. See title page for details.
  • Page 104 Non-Normal Checklists - Engines, APU 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.7.2 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 105 APU switch ........OFF CAUTION: Do not operate the APU. An APU fire would not be detected and the APU would continue to run. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 106: Apu Fault

    APU switch ........OFF [The LOW OIL PRESSURE light extinguishes in 5 minutes.] Copyright © The Boeing Company. See title page for details. December 2, 2005...

  • Page 107: Apu Overspeed

    Note: Maximum thrust limiting is available with autothrottle engaged. Observe engine limits. [Alternate mode will not provide the same engine limit protections as the normal mode.] Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 108: Engine Control

    TRANSPONDER MODE selector ..... . TA [Prevents climb commands which can exceed single engine performance capability. Continued on next page Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 109 ISOLATION VALVE switch ..... AUTO Plan to land at the nearest suitable airport. Accomplish the ONE ENGINE INOPERATIVE LANDING checklist. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 110: Engine Fire, Severe Damage Or Separation

    If high vibration returns and further airspeed reduction and descent are not practicable, increasing airspeed may reduce vibration. Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 111 DETECTOR FAULT The FAULT light illuminated indicates both loops on Condition: an engine have failed. The fire detection system in one or both engines is inoperative. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)

  • Page 112: Engine High Oil Temperature

    Retard until engine oil temperature is within normal operating range or thrust lever is closed. If temperature is in the amber band for more than 45 minutes: Accomplish the ENGINE FAILURE /SHUTDOWN checklist. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 113 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 114: Engine In-Flight Start

    DUCT PRESSURE ....Minimum 30 PSI If needed, advance the thrust lever to increase duct pressure. Continued on next page Copyright © The Boeing Company. See title page for details. 7.10 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 115 APU ........As needed TRANSPONDER MODE selector ....TA/RA Copyright © The Boeing Company. See title page for details. 7.11...

  • Page 116: Engine Limit/Surge/Stall

    Plan to land at the nearest suitable airport. Accomplish the ONE ENGINE INOPERATIVE LANDING checklist. If indications are stabilized and EGT decreases: Continued on next page Copyright © The Boeing Company. See title page for details. 7.12 June 9, 2006 D6-27370-73V-EZY(3V)

  • Page 117: Engine Low Oil Pressure

    If engine oil pressure is in the amber band with takeoff thrust set: Do not takeoff. If engine oil pressure is at or below the redline: Accomplish the ENGINE FAILURE/SHUTDOWN checklist. Copyright © The Boeing Company. See title page for details. 7.13 December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 118: Engine Oil Filter Bypass

    If the OIL FILTER BYPASS alert extinguishes: Operate the engine at reduced thrust to keep the alert extinguished. If the OIL FILTER BYPASS alert remains illuminated: Accomplish the ENGINE FAILURE/SHUTDOWN checklist. Copyright © The Boeing Company. See title page for details. 7.14 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 119: Engine Overheat

    Accomplish the ENGINE FIRE, SEVERE DAMAGE OR SEPARATION checklist. If the ENG OVERHEAT light extinguishes: Operate the engine at reduced thrust to keep the light extinguished. Copyright © The Boeing Company. See title page for details. 7.15 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 120: Engine Tailpipe Fire

    Continue to motor until the tailpipe fire is extinguished. ENGINE START switch (affected engine) ... OFF Copyright © The Boeing Company. See title page for details. 7.16 June 9, 2006...
  • Page 121 80% N1. If vibration does not decrease: Accomplish the procedure for “If not in icing conditions.” Copyright © The Boeing Company. See title page for details. 7.17 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 122: Loss Of Thrust On Both Engines

    APU BLEED AIR switch ......OFF Continued on next page Copyright © The Boeing Company. See title page for details. 7.18...
  • Page 123 APU ........As needed Copyright © The Boeing Company. See title page for details.

  • Page 124: One Engine Inoperative Landing

    Maintain VREF 15 + 5 or VREF ICE + 5 minimum on final approach to assure adequate maneuver margin and speed for go-around. Continued on next page Copyright © The Boeing Company. See title page for details. 7.20 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 125 + 15 knots or VREF ICE + 5 knots or minimum maneuver speed • Accelerate to flaps 1 maneuvering speed prior to flap retraction. Continued on next page Copyright © The Boeing Company. See title page for details. 7.21 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 126 A REVERSER light illuminated indicates a fault is Condition: detected in the related engine reverser system. Note: Additional system failures may cause in-flight deployment. Expect normal reverser operation after landing. Copyright © The Boeing Company. See title page for details. 7.22 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 127 Operate the engine normally. If the engine does not respond to forward thrust lever movement or buffet or yaw exists: Accomplish the ENGINE FAILURE /SHUTDOWN checklist. Copyright © The Boeing Company. See title page for details. 7.23 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 128 Ground air source (if in use) ... . . Disconnect ENGINE START lever ..... CUTOFF Copyright © The Boeing Company. See title page for details. 7.24...
  • Page 129 7.25 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 7.25 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 130 • Engine malfunctions, increasing EGT, engine stall or flameout. • Decrease or loss of airspeed indications. • Equipment Cooling OFF light. Continued on next page Copyright © The Boeing Company. See title page for details. 7.26 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 131 If N2 is steadily increasing, and EGT remains within limits, the start is progressing normally. Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 7.27 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 132 7.28 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 7.28 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 133: Fire Protection

    WHEEL WELL FIRE ........8.12 Copyright © The Boeing Company. See title page for details.

  • Page 134: Intentionally Blank

    Non-Normal Checklists - Fire Protection 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.8.2 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 135 L PACK switch ......AUTO Plan to land at nearest suitable airport. Accomplish the SMOKE/FUMES REMOVAL checklist, if needed. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 136 APU switch ........OFF If the APU fire switch remains illuminated: Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 137 The DETECTOR FAULT light illuminated indicates Condition: both loops in one or both cargo compartments have failed. The fire detection system in one or both cargo compartments is inoperative. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 138 • turn on cabin reading lights • turn on galley attendants work lights. [Prepares cabin lighting prior to depowering cabin fluorescent lights.] Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 139 DETECTOR FAULT The FAULT light illuminated indicates both loops on Condition: an engine have failed. The fire detection system in one or both engines is inoperative. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 140 If high vibration returns and further airspeed reduction and descent are not practicable, increasing airspeed may reduce vibration. Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 141 ....... . AUTO Plan to land at the nearest suitable airport. Accomplish the ONE ENGINE INOPERATIVE LANDING checklist when appropriate. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 142 Accomplish the ENGINE FIRE, SEVERE DAMAGE OR SEPARATION checklist. If the ENG OVERHEAT light extinguishes: Operate the engine at reduced thrust to keep the light extinguished. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 143 Continue to motor until the tailpipe fire is extinguished. ENGINE START switch (affected engine) ... OFF Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 144 At 14,000 feet or below: PRESSURIZATION MODE selector ... MAN Continued on next page Copyright © The Boeing Company. See title page for details. 8.10 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 145 [High airspeed may prevent opening the window.] First officer's sliding window ....Open Copyright © The Boeing Company. See title page for details. 8.11...
  • Page 146 (235 KNOTS maximum) ....UP & OFF Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 8.12...
  • Page 147 YAW DAMPER ........9.27 Copyright © The Boeing Company. See title page for details.

  • Page 148: Intentionally Blank

    Non-Normal Checklists - Flight Controls 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.9.2 D6-27370-73V-EZY(3V) December 2, 2005...

  • Page 149: Nnc.9 Non-Normal Checklists-Flight Controls

    Altimeters ........___ Continued on next page Copyright © The Boeing Company. See title page for details. March 28, 2005...

  • Page 150: Feel Differential Pressure

    FLIGHT CONTROL switch ....STBY RUD Copyright © The Boeing Company. See title page for details. March 28, 2005...

  • Page 151: Jammed Or Restricted Flight Controls

    A maximum two-pilot effort on the controls will not cause a cable or system failure. Do not turn off any flight control switches. Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 152 10° C. Note: When VREF ICE is needed, the wind additive should not exceed 10 knots. Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 153 Flaps ........15, Green light Copyright © The Boeing Company. See title page for details.

  • Page 154: Leading Edge Flaps Transit

    Flaps ..... . . Extend to flaps 1 then retract to flaps up Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 155 Set VREF 15 + 15. Limit bank angle to 15° until reaching flaps up maneuvering speed. Continue checklist at DEFERRED ITEMS, DESCENT. Continued on next page Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 156 G-EZJA - G-EZJN Note: Due to minimum speed reversion, V/S and VNAV PTH modes may revert to LVL CHG mode. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 157: Runaway Stabilizer

    Stabilizer ......Trim manually Anticipate trim requirements. Complete the normal DESCENT, APPROACH and LANDING checklists. Establish proper airspeed and in-trim condition early on final approach. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 158: Speed Brake Do Not Arm

    SPEED BRAKE lever ... . . ARMED/DOWN DETENT If light is illuminated on the ground: Do not takeoff. Copyright © The Boeing Company. See title page for details. 9.10 December 2, 2005...
  • Page 159 Stabilizer trim ......As needed If the stabilizer fails to respond to electric trim inputs: Accomplish the STABILIZER TRIM INOPERATIVE checklist. Copyright © The Boeing Company. See title page for details. 9.11 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 160 10° C. Note: When VREF ICE is needed, the wind additive should not exceed 10 knots. Establish landing configuration early. Continued on next page Copyright © The Boeing Company. See title page for details. 9.12 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 161 Flaps ........15, Green light Copyright © The Boeing Company. See title page for details.
  • Page 162 No crew action needed in flight. If the STBY RUD ON light is illuminated with no other flight deck indications: Avoid large or abrupt rudder pedal inputs. Copyright © The Boeing Company. See title page for details. 9.14 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 163 9.15 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 9.15 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 164 Check the appropriate Non–Normal Configuration Landing Distance table in the ADVISORY INFORMATION section of the Performance–Inflight chapter. Continue checklist at DEFERRED ITEMS, DESCENT. Continued on next page Copyright © The Boeing Company. See title page for details. 9.16 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 165 Flaps ......____, Green/amber light [The light may be green or amber depending on the cause of the failure.] Copyright © The Boeing Company. See title page for details. 9.17...
  • Page 166 Plan to extend flaps to 15 using alternate flap extension. Note: The drag penalty with the leading edge devices extended may make it impossible to reach an alternate field. Continued on next page Copyright © The Boeing Company. See title page for details. 9.18 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 167 Approach briefing ......Completed Continued on next page Copyright © The Boeing Company. See title page for details. 9.19...
  • Page 168 1, after the ALTERNATE FLAPS position switch is held down: Accomplish the TRAILING EDGE FLAPS UP LANDING checklist. Continued on next page Copyright © The Boeing Company. See title page for details. 9.20 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 169 Flaps ....... . . ___, Green light Copyright © The Boeing Company. See title page for details.
  • Page 170 Performance–Inflight chapter. Maintain flaps up maneuvering speed until on final. Limit bank angle to 15° until reaching flaps up maneuvering speed. Continued on next page Copyright © The Boeing Company. See title page for details. 9.22 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 171 Altimeters ........___ Continued on next page Copyright © The Boeing Company. See title page for details. 9.23...
  • Page 172 FASTEN BELTS switch ......ON Copyright © The Boeing Company. See title page for details.

  • Page 173: Uncommanded Rudder/Yaw Or

    YAW DAMPER ....... . . OFF Continued on next page Copyright © The Boeing Company. See title page for details. 9.25...
  • Page 174 Note: Consider checking rudder freedom of movement at a safe altitude using slow rudder inputs while in the landing configuration and at approach speed. Continued on next page Copyright © The Boeing Company. See title page for details. 9.26 December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 175: Yaw Damper

    If turbulence is encountered and passenger comfort becomes affected, reduce airspeed and/or descend to a lower altitude. Do not exceed flaps 30 if the crosswind exceeds 30 knots. Copyright © The Boeing Company. See title page for details. 9.27 December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 176: Intentionally Blank

    9.28 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 9.28 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 177 IAS DISAGREE ........10.4 Copyright © The Boeing Company. See title page for details.
  • Page 178 Non-Normal Checklists - Flight Instruments, Display 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.10.2 D6-27370-73V-EZY(3V) December 2, 2005...

  • Page 179: Nnc.10 Non-Normal Checklists-Flight Instruments, Display

    PROBE HEAT .......Check ON MACH/AIRSPEED indicators ....Cross check Copyright © The Boeing Company. See title page for details. 10.1...

  • Page 180: Alt Disagree

    The CDS FAULT annunciation indicates a CDS fault. Condition: Note: CDS FAULT annunciates on the ground only, prior to the second engine start. Dispatch is not authorized. Copyright © The Boeing Company. See title page for details. 10.2 December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 181: Display Failure

    ..... . . BOTH ON 1 or BOTH ON 2 Select side corresponding to the operating control panel. Verify DISPLAYS CONTROL PANEL annunciation and ALT flag extinguish. Copyright © The Boeing Company. See title page for details. 10.3 December 2, 2005 D6-27370-73V-EZY(3V)

  • Page 182: Dsply Source

    The IAS DISAGREE alert indicates the captain’s and Condition: first officer’s airspeed indications disagree by more than 5 knots for 5 continuous seconds. Accomplish the AIRSPEED UNRELIABLE checklist. Copyright © The Boeing Company. See title page for details. 10.4 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 183 UNABLE REQD NAV PERF - RNP ..... . . 11.4 Copyright © The Boeing Company. See title page for details.
  • Page 184 Non-Normal Checklists - Flight Management, Navigation 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.11.2 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 185 Note: Look-ahead terrain alerting and display are unavailable due to position uncertainty. No crew action is needed in flight if ANP meets the requirements for phase of flight. Copyright © The Boeing Company. See title page for details. 11.1 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 186 If the FAULT light illuminates again, notify maintenance. In flight: Note: The IRS ATT and/or NAV mode(s) may be inoperative. Continued on next page Copyright © The Boeing Company. See title page for details. 11.2 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 187 An IRS ON DC light illuminated indicates the related Condition: IRS is operating from the switched hot battery bus. Power to the right IRS is removed after 5 minutes. Copyright © The Boeing Company. See title page for details. 11.3 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 188 If flying an approach that has an RNP alerting requirement: Initiate a go-around unless suitable visual references can be established and maintained. If flying an approach without an RNP alerting requirement: Verify position. Copyright © The Boeing Company. See title page for details. 11.4 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 189 LOW ..........12.9 Copyright © The Boeing Company. See title page for details.
  • Page 190 Non-Normal Checklists - Fuel 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.12.2 D6-27370-73V-EZY(3V) December 2, 2005...

  • Page 191: Nnc.12 Non-Normal Checklists-Fuel

    PUMP switches ........ON Verify the LOW PRESSURE lights extinguish and position both switches OFF when both LOW PRESSURE lights illuminate. Copyright © The Boeing Company. See title page for details. 12.1 June 9, 2006 D6-27370-73V-EZY(3V)

  • Page 192: Crossfeed Selector Inoperative

    Flight conditions permitting, vary thrust to maintain fuel balance. If unable to maintain acceptable balance, land as soon as possible. Valve Open: Maintain fuel balance with selective use of fuel pumps. Copyright © The Boeing Company. See title page for details. 12.2 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 193: Engine Fuel Leak

    An increase in fuel imbalance of approximately 230 kgs or more in 30 minutes should be considered an engine fuel leak. Conditions permitting, visually check for an engine fuel leak. Continued on next page Copyright © The Boeing Company. See title page for details. 12.3 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 194 TRANSPONDER MODE selector ....TA [Prevents climb commands which can exceed single engine performance capability. Continued on next page Copyright © The Boeing Company. See title page for details. 12.4 June 9, 2006 D6-27370-73V-EZY(3V)

  • Page 195: Fuel Filter Bypass

    A fuel FILTER BYPASS light illuminated indicates Condition: impending fuel filter bypass due to a contaminated filter. Note: Erratic engine operation and flameout may occur due to fuel contamination. Copyright © The Boeing Company. See title page for details. 12.5 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 196 CROSSFEED selector ..... CLOSE Continued on next page Copyright © The Boeing Company. See title page for details. 12.6 December 2, 2005...

  • Page 197: Fuel Quantity Indication Inoperative

    FMC FUEL WEIGHT ......Enter Enter and periodically update manually calculated fuel weight on the FMC PERF INIT page. Copyright © The Boeing Company. See title page for details. 12.7 December 2, 2005...

  • Page 198: Imbal

    Fuel ........Balance Copyright © The Boeing Company. See title page for details.

  • Page 199: Low

    Apply thrust changes slowly and smoothly. If a climb is needed, maintain the minimum pitch attitude needed for safe flight. [Minimizes the possibility of uncovering the fuel pumps.] Copyright © The Boeing Company. See title page for details. 12.9 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 200 12.10 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 12.10 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 201 STANDBY HYDRAULIC LOW PRESSURE ....13.11 STANDBY HYDRAULIC LOW QUANTITY ....13.11 Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) TOC.13.1...
  • Page 202 Non-Normal Checklists - Hydraulics 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.13.2 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 203 ELECTRIC HYDRAULIC PUMP switch ....OFF [One pump provides adequate pressure for normal system operation.] Copyright © The Boeing Company. See title page for details. 13.1...
  • Page 204 Altimeters ........___ Continued on next page Copyright © The Boeing Company. See title page for details. 13.2...
  • Page 205 Flaps ....... . ___ , Green light Copyright © The Boeing Company. See title page for details.
  • Page 206 Plan to extend flaps to 15 using alternate flap extension. Note: Alternate flap extension time to flaps 15 is approximately 2 minutes. Continued on next page Copyright © The Boeing Company. See title page for details. 13.4 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 207 10 position. Note: Operation within the lower amber airspeed band may be needed until the LE FLAPS TRANSIT light extinguishes. Continued on next page Copyright © The Boeing Company. See title page for details. 13.5 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 208 Flaps ........15, green light Copyright © The Boeing Company. See title page for details.
  • Page 209 13.7 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 13.7 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 210 10° C. Note: When VREF ICE is needed, the wind additive should not exceed 10 knots. Plan for manual gear extension. Continued on next page Copyright © The Boeing Company. See title page for details. 13.8 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 211 • Advance thrust to go-around smoothly and slowly to avoid excessive pitch-up • Prepare to trim • Limit bank angle to 15 degrees until minimum maneuver speed. Continued on next page Copyright © The Boeing Company. See title page for details. 13.9 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 212 10 position. Note: Operation within the lower amber airspeed band may be needed until the LE FLAPS TRANSIT light extinguishes. Continued on next page Copyright © The Boeing Company. See title page for details. 13.10 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 213 Note: With a loss of hydraulic system A and B, the rudder is inoperative. STANDBY HYDRAULIC LOW QUANTITY The standby hydraulic LOW QUANTITY light Condition: illuminated indicates low quantity in the standby hydraulic reservoir. Copyright © The Boeing Company. See title page for details. 13.11 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 214 13.12 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 13.12 March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 215: Landing Gear

    WHEEL WELL FIRE ........14.8 Copyright © The Boeing Company. See title page for details.

  • Page 216: Intentionally Blank

    Non-Normal Checklists - Landing Gear 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.14.2 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 217 BRAKE PRESSURE INDICATOR ZERO PSI The brake accumulator has no nitrogen precharge. Condition: Accumulator braking is not available. Note: If hydraulic systems indications are normal, brake operation is unaffected. Copyright © The Boeing Company. See title page for details. 14.1 December 2, 2005 D6-27370-73V-EZY(3V)
  • Page 218 Plan to land at the nearest suitable airport. CAUTION: Do not operate the speed brakes in flight. CAUTION: Do not operate the speed brakes in flight. Continued on next page Copyright © The Boeing Company. See title page for details. 14.2 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 219 Flaps ......___ , Green light Manually deploy the speed brakes immediately upon touchdown. Copyright © The Boeing Company. See title page for details. 14.3 December 2, 2005...
  • Page 220 If all landing gear indicate down and locked: Land normally. If all landing gear do not indicate down and locked: Accomplish the PARTIAL OR GEAR UP LANDING checklist. Copyright © The Boeing Company. See title page for details. 14.4 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 221 14.5 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 14.5 March 28, 2005 D6-27370-73V-EZY(3V)
  • Page 222 Approach briefing ......Completed Continued on next page Copyright © The Boeing Company. See title page for details. 14.6...
  • Page 223 Flaps ........40, Green light Copyright © The Boeing Company. See title page for details.
  • Page 224 (235 knots maximum) ..... . UP & OFF Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 14.8...

  • Page 225: Warning Systems

    CONFIGURATION ....... . . 15.2 Copyright © The Boeing Company. See title page for details.
  • Page 226 Non-Normal Checklists - Warning Systems 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. TOC.15.2 D6-27370-73V-EZY(3V) June 9, 2006...

  • Page 227: Altitude Alert

    If PSEU light does not extinguish when the Master Caution system is reset: Do not takeoff. Note: The PSEU light illuminates on the ground only. Copyright © The Boeing Company. See title page for details. 15.1 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 228 If an intermittent horn sounds on the ground: Assure proper airplane takeoff configuration. If a steady horn sounds in flight: Assure proper airplane landing configuration. Copyright © The Boeing Company. See title page for details. 15.2 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 229 Visual Traffic Pattern ....... MAN.2.7 Go–Around and Missed Approach ....MAN.2.8 Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) MAN.TOC.0.1...
  • Page 230 Maneuvers - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. MAN.TOC.0.2 D6-27370-73V-EZY(3V) December 2, 2005...

  • Page 231: Non-Normal Maneuvers

    Prior to 80 knots, the takeoff should be rejected for any of the following: • activation of the master caution system • system failure(s) • unusual noise or vibration • tire failure Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) MAN.1.1...
  • Page 232 Note: During a rejected takeoff below 90 knots, autobraking is not initiated and the AUTO BRAKE DISARM light does not illuminate. Copyright © The Boeing Company. See title page for details. MAN.1.2 D6-27370-73V-EZY(3V)
  • Page 233 Advising the ground crew of the hot brake hazard Advising passengers of the need to remain seated or evacuate Completion of Non-Normal checklist (if appropriate) for conditions which caused the RTO. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) MAN.1.3...

  • Page 234: Terrain Avoidance

    Accomplish the following maneuver for any of these conditions: • Activation of “PULL UP” or “TERRAIN TERRAIN PULL UP” warning. • Other situations resulting in unacceptable flight toward terrain. Copyright © The Boeing Company. See title page for details. MAN.1.4 D6-27370-73V-EZY(3V)
  • Page 235 VMC conditions prior to a terrain or obstacle warning, the alert may be regarded as cautionary and the approach may be continued. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 236: Traffic Avoidance

    RA command. Follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action. Attempt to establish visual contact. Call out any conflicting traffic. Copyright © The Boeing Company. See title page for details. MAN.1.6 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 237 After positive rate of climb Position gear lever up. established, call for GEAR UP. Attempt to establish visual contact. Call out any conflicting traffic. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) MAN.1.7...

  • Page 238: Upset Recovery

    If the airplane is stalled, recovery from the stall must be accomplished first by applying and maintaining nose down elevator until stall recovery is complete and stick shaker activation ceases. Copyright © The Boeing Company. See title page for details. MAN.1.8 D6-27370-73V-EZY(3V)

  • Page 239: Roll

    WARNING: * Excessive use of pitch trim or rudder may aggravate an upset situation or may result in loss of control and/or high structural loads. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) MAN.1.9...

  • Page 240: Windshear

    1000 feet AGL, in excess of any of the following: • 15 knots indicated airspeed • 500 fpm vertical speed Copyright © The Boeing Company. See title page for details. MAN.1.10 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 241 737 Flight Crew Operations Manual • 5° pitch attitude • 1 dot displacement from the glideslope • unusual thrust lever position for a significant period of time. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V) MAN.1.11...
  • Page 242 EEC’s are in the normal mode. If terrain contact is imminent, advance thrust levers full forward. Note: ** If TO/GA is not available, disconnect autopilot and autothrottle and fly manually. Copyright © The Boeing Company. See title page for details. MAN.1.12 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 243 WARNING: *** Severe windshear may exceed the performance of the AFDS. The pilot flying must be prepared to disconnect the autopilot and autothrottle and fly manually. Copyright © The Boeing Company. See title page for details. March 28, 2005 D6-27370-73V-EZY(3V)

  • Page 244: Intentionally Blank

    Maneuvers - Non-Normal Maneuvers 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. MAN.1.14 D6-27370-73V-EZY(3V) March 28, 2005...
  • Page 245 737 Flight Crew Operations Manual Maneuvers Chapter MAN Flight Patterns Section 2 MAN.2 Maneuvers-Flight Patterns Takeoff Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) MAN.2.1...
  • Page 246 Maneuvers Flight Patterns 737 Flight Crew Operations Manual ILS Approach - Fail Passive Copyright © The Boeing Company. See title page for details. MAN.2.2 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 247 Maneuvers Flight Patterns 737 Flight Crew Operations Manual Non-Precision Approach < EZY > Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) MAN.2.3...
  • Page 248 Maneuvers Flight Patterns 737 Flight Crew Operations Manual Instrument Approach Using VNAV Copyright © The Boeing Company. See title page for details. MAN.2.4 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 249 Maneuvers Flight Patterns 737 Flight Crew Operations Manual Instrument Approach Using V/S Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) MAN.2.5...
  • Page 250 Maneuvers Flight Patterns 737 Flight Crew Operations Manual Circling Approach Copyright © The Boeing Company. See title page for details. MAN.2.6 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 251 Maneuvers Flight Patterns 737 Flight Crew Operations Manual Visual Traffic Pattern Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) MAN.2.7...
  • Page 252 Maneuvers Flight Patterns 737 Flight Crew Operations Manual Go–Around and Missed Approach Copyright © The Boeing Company. See title page for details. MAN.2.8 D6-27370-73V-EZY(3V) December 2, 2005...
  • Page 253 Altitudes ........PI.11.3 Copyright © The Boeing Company. See title page for details.
  • Page 254 Advisory Information ......PI.16.8 Copyright © The Boeing Company. See title page for details.
  • Page 255 Gear Down ........PI.16.12 Copyright © The Boeing Company. See title page for details.
  • Page 256 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.TOC.0.4 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 257 WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) Max Takeoff Thrust TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.1...
  • Page 258 WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) Max Takeoff Thrust TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. PI.10.2 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 259 WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) Max Takeoff Thrust TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.3...
  • Page 260 WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) Max Takeoff Thrust TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. PI.10.4 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 261 5 3/4 4 3/4 3 1/4 35-45 7 1/4 6 1/2 6 1/2 5 1/4 4 1/2 3 1/2 2 3/4 VREF FLAPS WEIGHT (1000 KG) Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.5...
  • Page 262 Flap Maneuver Speeds FLAP POSITION MANEUVER SPEED VREF40 + 70 VREF40 + 50 VREF40 + 30 VREF40 + 30 VREF40 + 20 VREF40 + 10 Copyright © The Boeing Company. See title page for details. PI.10.6 D6-27370-73V-EZY(3V) June 9, 2006...

  • Page 263: Advisory Information

    3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.7...
  • Page 264 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.8...
  • Page 265 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.9...
  • Page 266 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.10...
  • Page 267 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.11...
  • Page 268 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.12...
  • Page 269 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.13...
  • Page 270 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.14...
  • Page 271 %N1 Adjustments for Engine Bleed AIRPORT PRESSURE ALTITUDE (FT) BLEED CONFIGURATION -2000 -1000 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.15...
  • Page 272 87.5 88.5 89.6 90.4 91.5 91.9 92.3 92.9 93.4 93.7 94.3 MINIMUM ASSUMED TEMP (°C) With engine bleed for packs off, increase %N1 by 0.9. Copyright © The Boeing Company. See title page for details. PI.10.16 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 273 3. Use the difference between assumed temperature and OAT to determine the %N1 adjustment from Table 3. 4. Subtract %N1 adjustment from Maximum %N1 in Table 2. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 274 SLOPE (%) WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. PI.10.18 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 275 SLOPE (%) WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.19...
  • Page 276 SLOPE (%) WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. PI.10.20 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 277 SLOPE (%) WIND (KTS) WEIGHT (1000 KG) *V1 not to exceed VR V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.21...
  • Page 278 7 1/2 7 1/4 6 1/2 5 3/4 4 3/4 35-45 7 1/4 6 1/2 6 1/2 5 1/4 4 1/2 3 1/2 2 3/4 Copyright © The Boeing Company. See title page for details. PI.10.22 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 279 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.23...
  • Page 280 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.24...
  • Page 281 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.25...
  • Page 282 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.26...
  • Page 283 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.27...
  • Page 284 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.28...
  • Page 285 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.29...
  • Page 286 2. If V1(MCG) limited, set V1 = V1(MCG). If not V1(MCG) limited, enter V1 Adjustment table with the actual weight to obtain V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). Copyright © The Boeing Company. See title page for details. PI.10.30...
  • Page 287 %N1 Adjustments for Engine Bleeds AIRPORT PRESSURE ALTITUDE (FT) BLEED CONFIGURATION -2000 -1000 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.31...
  • Page 288 85.5 86.3 87.2 88.0 88.8 89.3 89.8 90.3 90.8 91.3 91.9 MINIMUM ASSUMED TEMP (°C) With engine bleed for packs off, increase %N1 by 0.9. Copyright © The Boeing Company. See title page for details. PI.10.32 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 289 3. Use the difference between assumed temperature and OAT to determine the %N1 adjustment from Table 3. 4. Subtract %N1 adjustment from Maximum %N1 in Table 2. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 290 PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE -0.6 -0.8 -0.9 -0.9 -0.8 -0.8 ENGINE & WING ANTI-ICE* -1.8 -2.1 -2.5 -2.7 -3.0 -3.0 *Dual bleed sources Copyright © The Boeing Company. See title page for details. PI.10.34 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 291 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF A/C HIGH -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 -0.2 Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.35...
  • Page 292 -1900 -1700 -1600 Holding (VREF40 + 70) Flaps Up, %N1 for Level Flight WEIGHT (1000 KG) PRESSURE ALTITUDE (FT) PITCH ATT 10000 PITCH ATT 5000 Copyright © The Boeing Company. See title page for details. PI.10.36 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 293 (VREF + INCREMENT) FLAPS 15 PITCH ATT (VREF 15 + 10) FLAPS 30 PITCH ATT (VREF 30 + 10) FLAPS 40 PITCH ATT (VREF 40 + 10) Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.10.37...
  • Page 294 Performance Inflight 737-700/CFM56-7B20 General JAA/JAROPS Category A Brakes 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.10.38 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 295 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 41000 *Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb. Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-73V-EZY(3V) PI.11.1...
  • Page 296 69.5 71.1 72.6 73.9 75.6 77.8 80.2 MACH .491 .513 .536 .561 .586 .611 .634 .657 .682 .713 KIAS FF/ENG Shaded area approximates optimum altitude. Copyright © The Boeing Company. See title page for details. PI.11.2 D6-27370-73V-EZY(3V) March 15, 2002...
  • Page 297 11.3 6:16 10.0 5:40 5:16 4:57 1900 12.9 7:04 11.9 6:38 10.6 6:00 5:35 5:14 2000 13.5 7:28 12.5 7:01 11.1 6:19 10.2 5:53 5:31 Copyright © The Boeing Company. See title page for details. March 15, 2002 D6-27370-73V-EZY(3V) PI.11.3...
  • Page 298 WEIGHT AT CHECK POINT (1000 KG) REFERENCE FUEL REQUIRED (1000 KG) -0.2 -0.1 -0.4 -0.3 -0.7 -0.4 -0.9 -0.6 -1.2 -0.7 -1.6 -0.8 -1.9 -0.9 Copyright © The Boeing Company. See title page for details. PI.11.4 D6-27370-73V-EZY(3V) March 15, 2002...
  • Page 299 4017 3853 3706 6754 6257 5813 5433 5100 4800 4580 4377 4190 4019 3864 7053 6530 6063 5664 5314 5000 4770 4558 4362 4184 4022 Copyright © The Boeing Company. See title page for details. March 15, 2002 D6-27370-73V-EZY(3V) PI.11.5...
  • Page 300 -0.3 -0.1 -0.6 -0.3 -1.0 -0.4 -1.4 -0.6 -1.8 -0.8 -2.2 -0.9 -2.6 -1.1 -3.0 -1.3 -3.5 -1.6 -4.0 -1.8 -4.5 -2.0 -5.0 -2.2 10.1 Copyright © The Boeing Company. See title page for details. PI.11.6 D6-27370-73V-EZY(3V) March 15, 2002...
  • Page 301 (FT) 41000 39000 37000 35000 33000 31000 29000 27000 25000 23000 21000 19000 17000 15000 10000 5000 1500 Allowances for a straight-in approach are included. Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.11.7...
  • Page 302 KIAS FF/ENG 44.1 46.4 49.9 53.6 57.5 61.8 66.1 70.4 77.6 KIAS FF/ENG This table includes 5% additional fuel for holding in a racetrack pattern. Copyright © The Boeing Company. See title page for details. PI.11.8 D6-27370-73V-EZY(3V) March 15, 2002...

  • Page 303: Advisory Information

    8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) PI.12.1...

  • Page 304: Intentionally Blank

    Performance Inflight 737-700/CFM56-7B20 Advisory Information JAA/JAROPS Category A Brakes 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.12.2 D6-27370-73V-EZY(3V) September 27, 2004...
  • Page 305 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Copyright © The Boeing Company. See title page for details. December 2, 2005 D6-27370-73V-EZY(3V) PI.12.3...
  • Page 306 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. PI.12.4 D6-27370-73V-EZY(3V)
  • Page 307 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 308 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. PI.12.6 D6-27370-73V-EZY(3V)
  • Page 309 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 310 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. PI.12.8 D6-27370-73V-EZY(3V)
  • Page 311 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 312 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. PI.12.10 D6-27370-73V-EZY(3V)
  • Page 313 *For landing distance above 8000 ft pressure altitude, first apply the STD altitude adjustment to derive new reference landing distance for 8000 ft, then apply applicable HIGH altitude adjustment between 8000 ft and 14000 ft to this new reference distance. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 314 *To correct for wind, enter table with the brakes on speed minus one half the headwind or plus 1.5 times the tailwind. If ground speed is used for brakes on speed, ignore wind and enter table with sea level, 15°C. Copyright © The Boeing Company. See title page for details. PI.12.12 D6-27370-73V-EZY(3V)
  • Page 315 Brake temperature monitor system (BTMS) indication on CDS systems page may be used 10 to 15 minutes after airplane has come to a complete stop or inflight with gear retracted to determine recommended cooling schedule. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 316 Performance Inflight 737-700/CFM56-7B20 Advisory Information JAA/JAROPS Category A Brakes 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.12.14 D6-27370-73V-EZY(3V) September 27, 2004...

  • Page 317: Engine Inoperative

    BLEED CONFIGURATION ENGINE ANTI-ICE -1.2 -1.1 -1.0 -0.9 -0.8 -0.8 -0.8 -0.8 -0.8 ENGINE & WING ANTI-ICE -4.2 -4.4 -4.5 -4.7 -5.0 -4.8 -4.8 -4.8 -4.8 Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.13.1...
  • Page 318 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE ON -0.9 -0.9 -0.8 -0.8 -0.8 ENGINE & WING ANTI-ICE ON -4.1 -4.3 -4.5 -4.7 -4.7 Copyright © The Boeing Company. See title page for details. PI.13.2 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 319 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE ON -0.9 -0.9 -1.0 -1.0 -1.0 ENGINE & WING ANTI-ICE ON -3.6 -3.8 -3.8 -3.9 -4.0 Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.13.3...
  • Page 320 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE ON -0.9 -0.9 -0.9 -0.9 ENGINE & WING ANTI-ICE ON -3.2 -3.4 -3.4 -3.5 Copyright © The Boeing Company. See title page for details. PI.13.4 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 321 %N1 Adjustments for Engine Bleeds PRESSURE ALTITUDE (1000 FT) BLEED CONFIGURATION ENGINE ANTI-ICE ON -0.6 -0.8 -0.8 -0.8 ENGINE & WING ANTI-ICE ON -2.9 -3.0 -3.1 -3.2 Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.13.5...
  • Page 322 11600 23200 21100 17000 26000 24900 22900 28300 27300 26200 30500 29700 28600 32700 31900 31000 35000 34300 33400 37600 36900 36100 40700 39900 39100 Copyright © The Boeing Company. See title page for details. PI.13.6 D6-27370-73V-EZY(3V) March 15, 2002...
  • Page 323 10.4 4:33 1700 10.2 11.0 4:50 1800 10.0 10.8 11.6 5:07 Includes APU fuel burn. Driftdown at optimum driftdown speed and cruise at LRC speed. Copyright © The Boeing Company. See title page for details. March 29, 2004 D6-27370-73V-EZY(3V) PI.13.7...
  • Page 324 37500 With engine anti-ice on, decrease altitude capability by 5900 ft. With engine and wing anti-ice on, decrease altitude capability by 13000 ft (optional system). Copyright © The Boeing Company. See title page for details. PI.13.8 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 325 80.6 82.5 MACH .355 .382 .394 .407 .422 .438 .455 .474 .496 .520 KIAS FF/ENG 1173 1117 1097 1078 1059 1042 1037 1040 1048 1055 Copyright © The Boeing Company. See title page for details. September 26, 2003 D6-27370-73V-EZY(3V) PI.13.9...
  • Page 326 -0.3 -0.8 -0.4 -1.0 -0.5 -1.1 -0.6 -1.3 -0.6 -1.4 -0.7 -1.6 -0.8 -1.8 -0.9 -1.9 -1.0 -2.1 -1.0 -2.3 -1.1 Includes APU fuel burn. Copyright © The Boeing Company. See title page for details. PI.13.10 D6-27370-73V-EZY(3V) September 26, 2003...
  • Page 327 65.4 70.0 74.1 78.7 83.5 93.6 KIAS FF/ENG 1070 1050 1030 1010 1090 This table includes 5% additional fuel for holding in a racetrack pattern. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V) PI.13.11...
  • Page 328 Performance Inflight 737-700/CFM56-7B20 Engine Inoperative JAA/JAROPS Category A Brakes 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.13.12 D6-27370-73V-EZY(3V) June 9, 2006...
  • Page 329 5100 14400 11600 8600 25400 19300 12400 27900 26400 23300 30200 29100 27400 32400 31400 30200 34600 33600 32500 37000 36100 35000 39700 38800 37800 Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V) PI.14.1...
  • Page 330 1151 63.2 71.9 73.5 75.2 77.0 78.7 80.5 82.3 84.3 86.9 MACH .321 .392 .408 .425 .442 .461 .481 .503 .526 .547 KIAS FF/ENG 1044 Copyright © The Boeing Company. See title page for details. PI.14.2 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 331 REFERENCE FUEL REQUIRED (1000 KG) -0.3 -0.2 -0.7 -0.3 -1.0 -0.5 -1.4 -0.7 -1.8 -0.9 -2.1 -1.1 -2.5 -1.2 -2.8 -1.4 -3.2 -1.6 -3.6 -1.8 -3.9 -1.9 Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.14.3...
  • Page 332 (FT) 41000 39000 37000 35000 33000 31000 29000 27000 25000 23000 21000 19000 17000 15000 10000 5000 1500 Allowances for a straight-in approach are included. Copyright © The Boeing Company. See title page for details. PI.14.4 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 333 74.7 79.1 83.8 93.3 KIAS FF/ENG 1090 1070 1050 1030 1000 1000 1090 This table includes 5% additional fuel for holding in a racetrack pattern. Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.14.5...
  • Page 334 Performance Inflight 737-700/CFM56-7B20 Gear Down JAA/JAROPS Category A Brakes 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.14.6 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 335 89.4 92.7 MACH .296 .305 .313 .322 .331 .342 .354 .369 .384 .400 KIAS FF/ENG 1973 1943 1906 1877 1856 1838 1828 1832 1839 1872 Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.15.1...
  • Page 336 -0.2 -0.6 -0.3 -0.8 -0.4 -1.0 -0.5 -1.2 -0.6 -1.4 -0.7 -1.6 -0.8 -1.8 -0.9 -2.0 -1.0 -2.2 -1.1 -2.4 -1.2 Includes APU fuel burn. Copyright © The Boeing Company. See title page for details. PI.15.2 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 337 2160 2150 2160 72.1 75.0 79.1 83.6 KIAS FF/ENG 1960 1940 1920 1920 This table includes 5% additional fuel for holding in a racetrack pattern. Copyright © The Boeing Company. See title page for details. March 31, 2003 D6-27370-73V-EZY(3V) PI.15.3...
  • Page 338 Performance Inflight 737-700/CFM56-7B20 Gear Down, Engine Inop JAA/JAROPS Category A Brakes 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. PI.15.4 D6-27370-73V-EZY(3V) March 31, 2003...
  • Page 339 Slope and wind adjustments to V1 are obtained by entering the Slope and Wind V1 Adjustment table. Copyright © The Boeing Company. See title page for details. October 31, 2002 D6-27370-73V-EZY(3V) PI.16.1...
  • Page 340 Using VREF as the basis for the schedule makes it variable as a function of weight and will provide adequate maneuver margin above stall at all weights. Copyright © The Boeing Company. See title page for details. PI.16.2 D6-27370-73V-EZY(3V)
  • Page 341 1. Determine takeoff speeds V1, VR and V2 for actual brake release weight using the Dry Runway Takeoff Speeds table for the appropriate flap setting and thrust rating. Copyright © The Boeing Company. See title page for details. June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 342 The performance level used to calculate the “good” data is consistent with wet runway testing done on early Boeing jets. The performance level used to calculate the “poor” data reflects a runway covered with wet ice.
  • Page 343 OAT to obtain a %N1 adjustment. Subtract the %N1 adjustment from the maximum takeoff %N1 found previously to determine the assumed temperature reduced thrust %N1. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V) PI.16.5...
  • Page 344 As indicated by the shaded area, at optimum altitude .79M approximates the Long Range Cruise Mach schedule. Copyright © The Boeing Company. See title page for details. PI.16.6 D6-27370-73V-EZY(3V) September 27, 2004...
  • Page 345 Small variations in airspeed will not appreciably affect the overall endurance time. Enter the table with weight and pressure altitude to read %N1, IAS and fuel flow per engine. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 346 The performance level used to calculate the "good" data is consistent with wet runway testing done on early Boeing jets. The performance level used to calculate "poor" data reflects runways covered with wet ice.
  • Page 347 BTMS, use the hottest brake indication 10 to 15 minutes after the airplane has come to a complete stop, or inflight with gear retracted to determine recommended cooling schedule. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V) PI.16.9...
  • Page 348 If altitudes other than the level off altitude is used, fuel and time required may be obtained by using the Engine Inoperative Long Range Cruise Enroute Fuel and Time table. Copyright © The Boeing Company. See title page for details. PI.16.10 D6-27370-73V-EZY(3V)
  • Page 349 Flaps 15 and Flaps 30. Enter the table with TAT and pressure altitude to read rate of climb available. Apply adjustments shown to correct for weight. Copyright © The Boeing Company. See title page for details. September 27, 2004 D6-27370-73V-EZY(3V)
  • Page 350 Tables for gear down performance in this section are identical in format and used in the same manner as tables for the gear up configuration previously described. Copyright © The Boeing Company. See title page for details. PI.16.12 D6-27370-73V-EZY(3V) September 27, 2004...
  • Page 351 CDS FAULT ..........10.2 Copyright © The Boeing Company. See title page for details.
  • Page 352 EQUIPMENT COOLING OFF ....... 2.7 Copyright © The Boeing Company. See title page for details.
  • Page 353 LOSS OF SYSTEM B ........13.4 Copyright © The Boeing Company. See title page for details.
  • Page 354 STANDBY RUDDER ON ........9.14 Copyright © The Boeing Company. See title page for details.
  • Page 355 YAW DAMPER ......... 9.27 Copyright © The Boeing Company. See title page for details.
  • Page 356 Non-Normal Checklists - Index 737 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. NNC.Index.6 D6-27370-73V-EZY(3V) June 9, 2006...

  • Page 357: Back Cover

    Back Cover.1 737 Flight Crew Operations Manual NNC.Back Cover Evacuation Checklist-Evacuation Checklist Evacuation Checklist is on the reverse side of this page. Copyright © The Boeing Company. See title page for details. Back Cover.1 June 9, 2006 D6-27370-73V-EZY(3V)
  • Page 358 Related fire switch....Rotate and hold Rotate to the stop and hold for 1 second. Copyright © The Boeing Company. See title page for details. Back Cover.2...

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