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Boeing 787 Quick Reference Handbook
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Boeing 787 Quick Reference Handbook

Boeing 787 Quick Reference Handbook

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787
Quick Reference Handbook
Quick Action Index
QA.Index Quick Action Index-Index
ABORTED ENGINE START L, R . . . . . . . . 0.1,7.1
CABIN ALTITUDE . . . . . . . . . . . . . . . . . . . . . . . 2.1
DUAL ENG FAIL/STALL . . . . . . . . . . . . . . . 0.4,7.2
ENG AUTOSTART L, R . . . . . . . . . . . . . . . . . 7.3,8
ENG AUTOSTART L, R . . . . . . . . . . . . . . . . 7.9,14
ENG AUTOSTART L, R . . . . . . . . . . . . . . . . . . 7.15
ENG SVR DAMAGE/SEP L, R . . . . . . . . . 0.8,7.15
EVACUATION . . . . . . . . . . . . . . . . . Back Cover.1
FIRE APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.2
FIRE ENG L, R . . . . . . . . . . . . . . . . . . . . . . . . . 8.4
STABILIZER . . . . . . . . . . . . . . . . . . . . . . . . . . 9.11
December 15, 2006
D615Z003 Boeing Proprietary
QA.Index.1

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Summary of Contents for Boeing 787

  • Page 1 FIRE ENG L, R ......8.4 STABILIZER ......9.11 December 15, 2006 D615Z003 Boeing Proprietary QA.Index.1...

  • Page 2: Intentionally Blank

    Quick Action Index - Index Intentionally Blank QA.Index.2 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 3 Airplane number is supplied by the operator. Registry number is supplied by the national regulatory agency. Serial and tabulation numbers are supplied by Boeing. Airplane Number Registry Number...
  • Page 4 QRH Revision Record - Model Identification 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 QRR.ModID.2 D615Z003 Boeing Proprietary...
  • Page 5 Section RevRec QRR.RevRec QRH Revision Record-Revision Record Revision Transmittal Letter To: All holders of The Boeing Company 787 Flight Crew Operations Manual, Boeing Document Number D615Z003 Boeing Proprietary. Subject: Quick Reference Handbook Revision. This revision reflects the most current information available to The Boeing Company 45 days before the subject revision date.

  • Page 6: Revision Highlights

    Pages may also be republished without revision bars due to slight changes in the flow of the document. Copyright © The Boeing Company. See title page for details. December 15, 2006 QRR.RevRec.2...

  • Page 7: List Of Effective Pages

    December 15, 2006 * TOC.11.1-2 December 15, 2006 * 2.1-10 December 15, 2006 * 11.1-12 December 15, 2006 * = Revised, Added, or Deleted Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary QRR.LEP.1 December 15, 2006...
  • Page 8 December 15, 2006 Index (tab) * NNC.Index.1-8 December 15, 2006 Evacuation (tab) * Back Cover.1-2 December 15, 2006 * = Revised, Added, or Deleted Copyright © The Boeing Company. See title page for details. December 15, 2006 QRR.LEP.2 D615Z003 Boeing Proprietary...
  • Page 9 BRAKES ..........14.2 Copyright © The Boeing Company. See title page for details.
  • Page 10 DOORS ..........1.3 Copyright © The Boeing Company. See title page for details.
  • Page 11 ENG SHUTDOWN L, R ........7.14 Copyright © The Boeing Company. See title page for details.
  • Page 12 FMC RUNWAY DISAGREE ....... . 11.2 Copyright © The Boeing Company. See title page for details.
  • Page 13 GPWS TERR OVRD ........15.2 Copyright © The Boeing Company. See title page for details.
  • Page 14 LIQUID COOLING L ........2.5 Copyright © The Boeing Company. See title page for details.
  • Page 15 ROLL LEFT AUTHORITY ........9.7 Copyright © The Boeing Company. See title page for details.
  • Page 16 T/O THRUST DISAGREE ........4.2 Copyright © The Boeing Company. See title page for details.
  • Page 17 WING ANTI–ICE OFF ........3.7 Copyright © The Boeing Company. See title page for details.

  • Page 18: Intentionally Blank

    Annunciated Index - EICAS Messages 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 ANN.Index.10 D615Z003 Boeing Proprietary...

  • Page 19: Normal Checklists

    Ground equipment - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Clear Copyright © The Boeing Company. See title page for details.

  • Page 20: Before Takeoff

    Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ___ Copyright © The Boeing Company. See title page for details.
  • Page 21 Packs - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -Off Copyright © The Boeing Company. See title page for details.
  • Page 22 Normal Checklists 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 NC.4 D615Z003 Boeing Proprietary...

  • Page 23: Table Of Contents

    Non–Normal Checklist Use ......CI.2.4 Copyright © The Boeing Company. See title page for details.
  • Page 24 Checklist Introduction - Table of Contents 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 CI.TOC.0.2 D615Z003 Boeing Proprietary...

  • Page 25: Normal Checklists

    If the airplane configuration does not agree with the needed configuration: • stop the checklist • complete the respective procedure steps • continue the checklist Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary CI.1.1...

  • Page 26: Electronic Checklist Operation

    (for example autobrakes), or • during shutdown and secure, items that could result in injury to personnel or damage to equipment if not done Copyright © The Boeing Company. See title page for details. December 15, 2006 CI.1.2 D615Z003 Boeing Proprietary...

  • Page 27: Checklist Construction

    When a checklist challenge ends with “switch or lever”, then the challenge refers to the position of the switch or lever. For example, “FUEL CONTROL switches...CUTOFF” refers to the position of the switches. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 28 Checklist Introduction - Normal Checklists 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 CI.1.4 D615Z003 Boeing Proprietary...
  • Page 29 Information in brackets is also used to identify the checklist from which an item originated. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 30: Non-Normal Checklists

    It must be stressed that for persistent smoke or a fire that cannot be positively confirmed to be completely extinguished, the earliest possible descent, landing, and evacuation must be done. Copyright © The Boeing Company. See title page for details. December 15, 2006 CI.2.2...
  • Page 31 • Flight crew cycling (pulling and resetting) of circuit breakers to clear non-normal conditions is not recommended unless directed by a non-normal checklist Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary CI.2.3...

  • Page 32: Non-Normal Checklist Use

    • an engine or APU fire switch or cargo fire arming switch • a generator drive disconnect switch This does not apply to the DUAL ENG FAIL/STALL checklist Copyright © The Boeing Company. See title page for details. December 15, 2006 CI.2.4...
  • Page 33 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. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 34 “______ CHECKLIST COMPLETE EXCEPT FOR DEFERRED ITEMS.” Copyright © The Boeing Company. See title page for details. December 15, 2006 CI.2.6...
  • Page 35 WINDOW DAMAGE L, R ......0.30 Copyright © The Boeing Company. See title page for details.

  • Page 36: Unannunciated Checklists Section

    Non-Normal Checklists - Unannunciated Checklists 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.0.2 D615Z003 Boeing Proprietary...

  • Page 37: Aborted Engine Start L, R

    START selector....... . . NORM Copyright © The Boeing Company. See title page for details.

  • Page 38: Ditching

    GND PROX GEAR OVRD ......OVRD Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary...
  • Page 39 • OUTFLOW VLV L • OUTFLOW VLV R • PACK L • PACK R • CABIN ALTITUDE AUTO • PACK L+R Continued on next page Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 40 Flaps........20 or 30 Advise the cabin to brace for touchdown. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary...

  • Page 41: Dual Eng Fail/Stall

    [Restores flight control normal mode following reversion to secondary mode caused by loss of pitot heat.] Autopilot can be re–engaged when flight control normal mode is restored. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 42 TRANSPONDER MODE selector....TA/RA U ENG LIM/SURGE/STALL L, R (TBD) Condition: Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 43 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 44 Note: Use flaps 20 and VREF20 for landing and flaps 5 for go–around. If landing using flaps 30 (performance permitting): Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 45: Fire Eng Tailpipe L, R

    Continue to motor until the tailpipe fire is extinguished. START selector (Affected engine)....NORM Copyright © The Boeing Company. See title page for details. December 15, 2006...
  • Page 46 FUEL JETTISON NOZZLE switches (Both)..OFF FUEL JETTISON ARM switch..... OFF Copyright © The Boeing Company. See title page for details. 0.10...
  • Page 47 0.11 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 0.11 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 48: Fuel Leak

    Destination fuel estimate..... . Check Verify adequate fuel available in left and right main tanks to complete flight. Continued on next page Copyright © The Boeing Company. See title page for details. 0.12 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 49 If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Continued on next page Copyright © The Boeing Company. See title page for details. 0.13 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 50: Gear Lever Locked Dn

    Landing gear lever....... . . UP Copyright © The Boeing Company. See title page for details.
  • Page 51 0.15 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 0.15 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 52: Loss Of All Displays

    HDG REF switch......TRUE [TCP backup navigation uses a true track reference.] Continued on next page Copyright © The Boeing Company. See title page for details. 0.16 D615Z003 Boeing Proprietary...
  • Page 53 ALTN GEAR switch....DOWN and hold Push and hold for 1 second. Copyright © The Boeing Company. See title page for details. 0.17...

  • Page 54: Overweight Landing

    GND PROX FLAP OVRD..... . . OVRD Note: Use flaps 20 and VREF20 for landing and flaps 5 for go–around. Copyright © The Boeing Company. See title page for details. 0.18 D615Z003 Boeing Proprietary...
  • Page 55 0.19 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 0.19 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 56 Left PACK switch......AUTO [Restores left side of the air conditioning system.] Continued on next page Copyright © The Boeing Company. See title page for details. 0.20 D615Z003 Boeing Proprietary...
  • Page 57 Do not accomplish the following checklists: PACK R TRIM AIR R If smoke/fumes are persistent: Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 0.21 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 58 CABIN/UTILITY power switch..... OFF Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 0.22...
  • Page 59 0.23 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 0.23 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 60 [Concentrates smoke/fumes in the forward part of the airplane and attempts to remove it through the forward outflow valve.] Do not accomplish the following checklist: OUTFLOW VALVE AFT Continued on next page Copyright © The Boeing Company. See title page for details. 0.24 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 61 [Concentrates smoke/fumes in the aft part of the airplane and attempts to remove it through the aft outflow valve.] Do not accomplish the following checklist: OUTFLOW VALVE FWD Copyright © The Boeing Company. See title page for details. 0.25 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 62: Tat Probe Icing

    • Reference/Target N1 and Reference N1 may be temporarily unreliable • Observe EGT caution limits • Maximum N1 may be temporarily unreliable. Continued on next page Copyright © The Boeing Company. See title page for details. 0.26 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 63 • Reference/Target N1 and Reference N1 are displayed • TAT is not near 0 degrees C. Do not accomplish the following checklists: ENG EEC MODE L ENG EEC MODE R Copyright © The Boeing Company. See title page for details. 0.27 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 64 • decrease or loss of airspeed indications • EQUIP COOLING OVRD indications • FIRE CARGO FWD or AFT indications. Continued on next page Copyright © The Boeing Company. See title page for details. 0.28 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 65 Autopilot can be re–engaged when flight control normal mode is restored. Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 0.29 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 66 Sustained flight below 10,000 feet is not recommended due to greater risk of bird strike. Copyright © The Boeing Company. See title page for details. 0.30 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 67: Window Damage L, R

    WINDOW DAMAGE L, R ....... 1.6 Copyright © The Boeing Company. See title page for details.

  • Page 68: Intentionally Blank

    Non-Normal Checklists - Airplane General, Emer. Equip., Doors, Windows 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.1.2 D615Z003 Boeing Proprietary...

  • Page 69: Automatic Unlock

    FLIGHT DECK DOOR ACCESS selector... . . DENY Rotate and hold for 1 second. [Prohibits unauthorized access to flight deck.] CREW OXYGEN LOW Crew oxygen pressure is low. Condition: Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 70: []Door Aft, Fwd Cargo

    Note: The door is in a safe configuration as long as cabin pressurization is normal. [Positive cabin differential pressure ensures door remains in place.] Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 71: []Door Bulk Cargo

    [Positive cabin differential pressure ensures door remains in place.] DOORS Two or more doors are not closed and latched and Condition: locked. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 72: Elt On

    [Removes electrical power to prevent possible lock overheat.] Door can be locked with deadbolt. FD DOOR OPEN Flight deck security door is open. Condition: Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 73: Lock Fail

    (Conditions permitting)......OFF [Removes electrical power to prevent possible lock overheat.] Door can be locked with deadbolt. PASS OXYGEN ON Passenger oxygen system is activated. Condition: Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 74 Sustained flight below 10,000 feet is not recommended due to greater risk of bird strike. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 75 VENTILATION ALTN ....... . . 2.10 Copyright © The Boeing Company. See title page for details.
  • Page 76 Non-Normal Checklists - Air Systems 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.2.2 D615Z003 Boeing Proprietary...

  • Page 77: []Cabin Altitude

    VMO/MMO. Level off at lowest safe altitude or 10,000 feet, whichever is higher. If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 78: []Cabin Altitude Auto

    Push and hold for 30 seconds or until outflow valve positions indicate fully open. CABIN TEMPERATURE Flight deck or cabin temperature zone(s) are or may Condition: become dangerously hot or cold. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 79: []Cargo A/C Fwd

    Aft equipment cooling system is inoperative. Condition: Plan to land at the nearest suitable airport. Note: After 30 minutes, non-critical electronic equipment may fail. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 80: []Equip Cooling Fwd

    Landing altitude selector....PULL, set manually LIQUID CLG QTY L, R Liquid cooling system quantity is low. Condition: Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 81: []Liquid Cooling L

    Leave all controls in the normal positions. Do not accomplish the following checklists: PACK R FUEL PUMP CTR R HYD PRESS C2 HYD PRESS DEM L Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 82: []Outflow Valve Aft, Fwd

    Air conditioning RESET switch....PUSH Push and hold for 1 second. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary...
  • Page 83 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 84 Flight deck sunshades/sunvisors....Install [Reduces flight deck heating during daylight operations.] Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 85 Instruct flight attendants to adjust cabin windows to full dark during daylight operations. Do not accomplish the following checklist: CABIN ALTITUDE AUTO DOOR AJAR Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 86: []Pack Mode L, R

    Air conditioning RESET switch....PUSH Push and hold for 1 second. VENTILATION ALTN Ventilation system is in the alternate mode. Condition: Copyright © The Boeing Company. See title page for details. 2.10 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 87 WING ANTI–ICE OFF ........3.8 Copyright © The Boeing Company. See title page for details.
  • Page 88 Non-Normal Checklists - Anti-Ice, Rain 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.3.2 D615Z003 Boeing Proprietary...

  • Page 89: []Anti-Ice Det Wing

    [Enables display of ICING ENG message if encountering icing conditions.] Note: Avoid icing conditions. [Anti-ice is not available to affected engine because the engine anti-ice system has failed.] Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 90: []Anti-Ice Leak Eng L, R

    GND PROX FLAP OVRD ....OVRD Note: Use flaps 20 and VREF20 for landing and flaps 5 for go–around. Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 91: Anti-Ice Loss Eng L, R

    [Enables ICING WING message to be displayed if icing conditions are encountered.] []HEAT PITOT C Center pitot probe heat is inoperative. Condition: Note: Standby air data is unreliable in icing conditions. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 92: []Heat Pitot L

    Condition: Note: Operate engine and wing anti–ice systems manually. ICING ENG Ice is detected and one or both engine anti–ice Condition: selectors are OFF. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 93: []Overheat Wing

    WING ANTI–ICE selector......OFF Note: Avoid icing conditions. [Anti-ice is not available to the wing because the wing anti-ice system has failed.] Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 94: Tat Probe Icing

    EEC MODE switches (Both)......OFF Push one switch at a time. [Ensures both engines operate in alternate mode.] Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 95: Window Heat

    Do not accomplish the following checklists: ENG EEC MODE L ENG EEC MODE R WINDOW HEAT Two or more window heats are off. Condition: Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 96: []Window Heat L, R Fwd

    SIDE WINDOW HEAT switch..... OFF [Removes power to prevent arcing.] WING ANTI–ICE OFF Wing anti-ice selector is in the off position. Condition: Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 97 T/O THRUST DISAGREE ....... . 4.2 Copyright © The Boeing Company. See title page for details.
  • Page 98 Non-Normal Checklists - Automatic Flight 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.4.2 D615Z003 Boeing Proprietary...

  • Page 99: Autopilot

    NO AUTOLAND GLS Autoland is not available for a GLS approach. Condition: NO AUTOLAND ILS Autoland is not available for an ILS approach. Condition: Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 100: Land 3

    Autoland system does not have redundancy for triple Condition: channel autoland. T/O THRUST DISAGREE Thrust management takeoff thrust calculation Condition: disagrees with EEC takeoff thrust calculation. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 101 VHF DATALINK ........5.2 Copyright © The Boeing Company. See title page for details.
  • Page 102 Non-Normal Checklists - Communications 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.5.2 D615Z003 Boeing Proprietary...

  • Page 103: Datalink Lost

    The affected audio control panel transmitter selectors should remain on FLT. SATCOM SATCOM system has failed. Condition: SATCOM DATALINK SATCOM datalink has failed. Condition: Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 104: Satcom Voice

    SATCOM VOICE SATCOM voice communication has failed. Condition: SATVOICE LOST SATCOM voice communication is temporarily lost. Condition: VHF DATALINK VHF datalink has failed. Condition: Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 105 MAIN BATTERY DISCH ....... . 6.3 Copyright © The Boeing Company. See title page for details.
  • Page 106 Non-Normal Checklists - Electrical 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.6.2 D615Z003 Boeing Proprietary...

  • Page 107: Nnc.6 Non-Normal Checklists-Electrical

    [Provides an additional source of electrical power for wing anti-ice.] Do not accomplish the following checklist: ELEC BATTERY OFF Battery switch is OFF. Condition: ELEC CABIN/UTIL OFF Cabin/utility power switch is OFF. Condition: Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 108: []Elec Gen Off Apu L, R

    (If APU available)..... START, then ON [Provides an additional source of electrical power.] ELEC IFE/SEATS OFF In-flight entertainment system/passenger seats Condition: power switch is OFF. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 109: Elec Standby Sys

    A fault is detected in the standby power system. Condition: MAIN BATTERY DISCH Main battery is discharging or hot battery bus is Condition: unpowered. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 110 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 111 [] ENG START CUTOUT L, R ......7.14 Copyright © The Boeing Company. See title page for details.
  • Page 112 VOLCANIC ASH ........7.18 Copyright © The Boeing Company. See title page for details.
  • Page 113 APU selector......START, then ON Copyright © The Boeing Company. See title page for details.

  • Page 114: Dual Eng Fail/Stall

    [Restores flight control normal mode following reversion to secondary mode caused by loss of pitot heat.] Autopilot can be re–engaged when flight control normal mode is restored. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 115: []Eng Autostart L, R

    Note: Maximum thrust limiting is not available with autothrottle disconnected. Alternate thrust setting information is displayed on N1 indications. Do not accomplish the following checklist: ENG EEC MODE (for other engine) Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 116: []Eng Fail L, R

    FUEL CONTROL switch....CUTOFF Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 117 If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Do not accomplish the following checklist: AUTOTHROTTLE Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 118: []Eng Fuel Filter L, R

    [Prevents possibility of not being able to shutdown the engine if both valves subsequently fail open.] ENG IDLE DISAGREE One engine is at approach idle and the other engine is Condition: at minimum idle. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...
  • Page 119 GND PROX FLAP OVRD......OFF TRANSPONDER MODE selector....TA/RA Copyright © The Boeing Company. See title page for details. December 15, 2006...

  • Page 120: []Eng Limit Exceed L, R

    GND PROX FLAP OVRD..... . . OVRD Note: Use flaps 20 and VREF20 for landing and flaps 5 for go–around. Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 121: []Eng Limit Prot L, R

    Retard until N1 remains within appropriate limits. U ENG LIM/SURGE/STALL L, R (TBD) Condition: []ENG LPC ANTI-ICE L, R Engine anti-ice capability is degraded. Condition: Note: Avoid icing conditions. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 122: []Eng Oil Filter L, R

    If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Do not accomplish the following checklist: AUTOTHROTTLE Copyright © The Boeing Company. See title page for details. 7.10 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 123: []Eng Oil Press L, R

    If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Do not accomplish the following checklist: AUTOTHROTTLE Copyright © The Boeing Company. See title page for details. 7.11 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 124: []Eng Oil Temp L, R

    If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Do not accomplish the following checklist: AUTOTHROTTLE Copyright © The Boeing Company. See title page for details. 7.12 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 125: Eng Rev Air/Gnd

    N1, N2 or N3 from exceeding the RPM operating limit. ENG SHUTDOWN Both engines were shutdown on the ground by the Condition: fuel control switches or fire switches. Copyright © The Boeing Company. See title page for details. 7.13 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 126: Eng Shutdown L, R

    START selector....... . . NORM Engine starters are inhibited for a 30 minute cooldown period. Do not accomplish the following checklist: ENG AUTOSTART Copyright © The Boeing Company. See title page for details. 7.14 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 127 [Prevents engine from unexpectedly rotating if starter function is regained.] Increase airspeed until X-START is no longer displayed. [Assures sufficient air flow for windmill start.] []ENG SURGE L, R (TBD) Condition: Copyright © The Boeing Company. See title page for details. 7.15 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 128 TRANSPONDER MODE selector....TA ONLY [Prevents climb commands which can exceed single engine performance capability.] Continued on next page Copyright © The Boeing Company. See title page for details. 7.16 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 129 Do not accomplish the following checklist: AUTOTHROTTLE ENG THRUST L, R Engine is producing greater than or less than Condition: commanded thrust. Copyright © The Boeing Company. See title page for details. 7.17 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 130 • decrease or loss of airspeed indications • EQUIP COOLING OVRD indications • FIRE CARGO FWD or AFT indications. Continued on next page Copyright © The Boeing Company. See title page for details. 7.18 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 131 Autopilot can be re–engaged when flight control normal mode is restored. Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 7.19 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 132: Intentionally Blank

    7.20 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 7.20 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 133: Fire Protection

    SMOKE REST UPR DR 4 ....... 8.16 Copyright © The Boeing Company. See title page for details.
  • Page 134 Non-Normal Checklists - Fire Protection 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.8.2 D615Z003 Boeing Proprietary...

  • Page 135: Bottle 1, 2 Disch Eng

    A fault is detected in the engine fire detection system. Condition: Note: Engine fire detection may not be available. An engine fire warning which occurs is valid. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 136: []Fire Apu

    Landing altitude selector..... . PUSH [Restores automatic selection of the FMC landing altitude.] Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 137: []Fire Cargo Fwd

    Note: After landing, inform ground personnel NOT to open the cargo door until all passengers and crew have exited the airplane and fire fighting equipment is nearby. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 138: Engine Fire

    GND PROX FLAP OVRD..... . . OVRD Note: Use flaps 20 and VREF20 for landing and flaps 5 for go–around. Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 139: Fire Eng Tailpipe L, R

    Continue to motor until the tailpipe fire is extinguished. START selector (Affected engine)....NORM Copyright © The Boeing Company. See title page for details. December 15, 2006...

  • Page 140: []Fire Wheel Well

    Landing gear lever......UP Copyright © The Boeing Company. See title page for details.
  • Page 141 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 142 If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Continued on next page Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 143: []Smoke Equip Clg Aft

    Plan to land at the nearest suitable airport. Note: After 30 minutes of operation at low altitude and low cabin differential pressure, non-critical electronic equipment may fail. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 144: Smoke Equip Clg Misc

    [Removes left side of the trim air system as a possible source of smoke/fumes.] Do not accomplish the following checklists: PACK L TRIM AIR L Continued on next page Copyright © The Boeing Company. See title page for details. 8.10 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 145 Do not accomplish the following checklists: PACK R TRIM AIR R If smoke/fumes are persistent: Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 8.11 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 146 CABIN/UTILITY POWER switch....OFF Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 8.12...
  • Page 147 8.13 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 8.13 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 148 [Concentrates smoke/fumes in the forward part of the airplane and attempts to remove it through the forward outflow valve.] Do not accomplish the following checklist: OUTFLOW VALVE AFT Continued on next page Copyright © The Boeing Company. See title page for details. 8.14 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 149: Smoke Lavatory

    Cabin crew communications....Establish If smoke is persistent: Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 8.15 December 15, 2006...
  • Page 150 Cabin crew communications....Establish If smoke is persistent: Plan to land at the nearest suitable airport. Copyright © The Boeing Company. See title page for details. 8.16 D615Z003 Boeing Proprietary...
  • Page 151 [] STALL PROTECTION ....... . . 9.12 Copyright © The Boeing Company. See title page for details.

  • Page 152: Intentionally Blank

    Non-Normal Checklists - Flight Controls 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.9.2 D615Z003 Boeing Proprietary...

  • Page 153: []Auto Speedbrake

    Note: Use current flaps and VREF30 + 20 for landing. If flap position 20 or greater: Note: Use current flaps and VREF20 for landing. Do not accomplish the following checklist: FLAPS PRIMARY FAIL Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 154 Alternate FLAPS selector......EXT Monitor airspeed during extension. [Extends flaps to flaps 20 position.] Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 155: []Flight Control Mode

    [From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight extension.] Note: Manually extend speedbrakes after landing. [From AUTO SPEEDBRAKE checklist.] Do not accomplish the following checklists: AUTO SPEEDBRAKE Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 156: []Flight Controls

    [Airplane is approaching its nose down pitch control limit.] Note: Avoid speedbrake use and rapid thrust increases. [Only limited elevator authority is available to counter nose up pitching.] Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 157: []Pitch Up Authority

    If flap position 20 or greater: Note: Use flaps 20 and VREF30 + 20 for landing. [Higher approach speeds provide better pitch up control authority.] Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 158: []Pri Flight Computers

    [From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight extension.] Note: Manually extend speedbrakes after landing. [From AUTO SPEEDBRAKE checklist.] Do not accomplish the following checklists: AUTO SPEEDBRAKE Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 159: []Roll Left Authority

    Note: Crosswind limit for landing is 10 knots. [Maintains sufficient control authority for de-crab maneuver.] Note: Left control wheel may be required after landing to control roll asymmetry. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 160: []Roll Right Authority

    Plan to land at the nearest suitable airport. [Unknown drag condition may decrease range.] Note: Use LRC speed for diversion. Do not use FMC fuel predictions. Copyright © The Boeing Company. See title page for details. D615Z003 Boeing Proprietary December 15, 2006...

  • Page 161: []Slats Drive

    Condition: between 15 and 800 feet, or when the flap lever is in a landing position, or when either thrust lever is not closed. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 162: []Spoiler Drag

    One or more spoiler panels are inoperative. Condition: Note: Roll rate may be reduced in flight. Speedbrake effectiveness may be reduced in flight and during landing. Copyright © The Boeing Company. See title page for details. 9.10 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 163: []Stab Greenband

    [Provides sufficient elevator authority for landing.] Do not accomplish the following checklist: FLIGHT CONTROLS STABILIZER CUTOUT Both stabilizer cutout switches are in CUTOUT. Condition: Copyright © The Boeing Company. See title page for details. 9.11 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 164: []Stabilizer L2

    Note: Right control wheel pitch trim switches may be inoperative. []STALL PROTECTION Some stall protection functions are inoperative. Condition: Note: Any stall indications should be considered valid. Copyright © The Boeing Company. See title page for details. 9.12 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 165 SINGLE SOURCE FD ........10.6 Copyright © The Boeing Company. See title page for details.

  • Page 166: Intentionally Blank

    Non-Normal Checklists - Flight Instruments, Displays 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.10.2 D615Z003 Boeing Proprietary...

  • Page 167: []Airspeed Unreliable

    Note: Control of the EFIS/DSP panel is accessed from the MFD system display, using the PANEL BACKUP key. Copyright © The Boeing Company. See title page for details. 10.1 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 168: []Hud Single Operation

    [Captain’s] [First Officer’s] HUD has failed. Condition: []HUD TAKEOFF HUD takeoff guidance is unavailable. Condition: Visibility is acceptable for takeoff without HUD guidance: Continue normal operation. Copyright © The Boeing Company. See title page for details. 10.2 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 169 10.3 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 10.3 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 170 HDG REF switch......TRUE [TCP backup navigation uses a true track reference.] Continued on next page Copyright © The Boeing Company. See title page for details. 10.4 D615Z003 Boeing Proprietary...

  • Page 171: Sgl Source Approach

    ALTN GEAR switch....DOWN and hold Push and hold for 1 second. SGL SOURCE APPROACH Both PFDs are using the same source for ILS Condition: information. Copyright © The Boeing Company. See title page for details. 10.5 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 172: []Sgl Source Attitude

    Both PFDs are using the same source for radio Condition: altimeter information. SINGLE SOURCE FD Both PFDs are using the same source for flight Condition: director information. Copyright © The Boeing Company. See title page for details. 10.6 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 173 WEATHER RADAR SYS ......11.11 Copyright © The Boeing Company. See title page for details.
  • Page 174 Non-Normal Checklists - Flight Management, Navigation 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.11.2 D615Z003 Boeing Proprietary...

  • Page 175: []Fmc

    The FMC calculated holding pattern exceeds the Condition: maximum protected airspace limits. Decrease airspeed or advise ATC you are unable to comply with required holding airspace limits. Copyright © The Boeing Company. See title page for details. 11.1 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 176: Fmc Intercept Hdg

    FMC VERIFY POSITION The FMC calculation of airplane position is based on Condition: conflicting data. GPS has failed. Condition: Copyright © The Boeing Company. See title page for details. 11.2 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 177: []Insufficient Fuel

    Airplane must be stopped to allow IRS alignment to complete. When IRS ALIGN MODE memo message is no longer displayed: Continue normal operation. Copyright © The Boeing Company. See title page for details. 11.3 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 178: []Lnav Bank Angle Lim

    [From FLIGHT CONTROL MODE checklist.] Note: Manual control inputs are required to compensate for asymmetric thrust conditions. [From FLIGHT CONTROL MODE checklist.] Continued on next page Copyright © The Boeing Company. See title page for details. 11.4 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 179 [From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight extension.] Note: Manually extend speedbrakes after landing. [From AUTO SPEEDBRAKE checklist.] Do not accomplish the following checklists: AUTO SPEEDBRAKE FLIGHT CONTROL MODE Copyright © The Boeing Company. See title page for details. 11.5 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 180: []Nav Airspeed Data

    Note: Do not arm speedbrake lever. [From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight extension.] Note: Manually extend speedbrakes after landing. [From AUTO SPEEDBRAKE checklist.] Continued on next page Copyright © The Boeing Company. See title page for details. 11.6 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 181 11.7 787 Flight Crew Operations Manual Continued from previous page Do not accomplish the following checklist: AUTO SPEEDBRAKE FLIGHT CONTROL MODE Copyright © The Boeing Company. See title page for details. 11.7 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 182: []Nav Inertial Sys

    Note: VOR course deviation is available in the ND VOR mode. ILS localizer and glideslope deviation raw data is available on both the PFD and ND. Continued on next page Copyright © The Boeing Company. See title page for details. 11.8 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 183: []Nav Unable Rnp

    If on procedure or airway without RNP: Verify position. If on the ground: Message may display with GPS disabled. PILOT RESPONSE Recent pilot activity has not been detected. Condition: Copyright © The Boeing Company. See title page for details. 11.9 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 184: []Rwy/App Crs Error

    Only a single FMC is operating. Condition: SGL SOURCE APPROACH Both PFDs are using the same source for ILS Condition: information. TRANSPONDER Transponders have failed. Condition: Copyright © The Boeing Company. See title page for details. 11.10 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 185: []Transponder Panel

    Note: TCP control of the glideslope inhibit, transponder mode, and aural cancel controls is accessed from the TCP menu page. WEATHER RADAR SYS Weather radar system is inoperative. Condition: Copyright © The Boeing Company. See title page for details. 11.11 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 186 11.12 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 11.12 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 187 [] FUEL VALVE APU ........12.15 Copyright © The Boeing Company. See title page for details.
  • Page 188 Non-Normal Checklists - Fuel 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.12.2 D615Z003 Boeing Proprietary...

  • Page 189: []Fuel Auto Jettison

    FUEL JETTISON ARM switch ..... . . OFF [Disarms fuel jettison system and removes FUEL TO REMAIN quantity from EICAS.] Copyright © The Boeing Company. See title page for details. 12.1 December 15, 2006...

  • Page 190: []Fuel Balance Sys

    CROSSFEED switch......OFF [Restores main tank–to–engine fuel feed.] Copyright © The Boeing Company. See title page for details. 12.2...

  • Page 191: []Fuel Crossfeed

    [Takes away command for crossfeed valve to open, which would cause unwanted crossfeed if it opened later in flight.] Do not complete the following checklist: FUEL BALANCE SYS Copyright © The Boeing Company. See title page for details. 12.3 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 192: []Fuel Disagree

    PROGRESS page 2......Select TOTALIZER or CALCULATED....Select use Select the most accurate value. Copyright © The Boeing Company. See title page for details. 12.4 D615Z003 Boeing Proprietary...

  • Page 193: []Fuel Imbalance

    Push and hold for 1 second. [Initiates automatic fuel balancing.] FUEL IN CENTER Both center fuel pump switches are OFF with fuel in Condition: the center tank. Copyright © The Boeing Company. See title page for details. 12.5 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 194: Fuel Jett Nozzle L, R

    FUEL JETTISON NOZZLE switches (Both)..OFF FUEL JETTISON ARM switch..... OFF Copyright © The Boeing Company. See title page for details. 12.6...

  • Page 195: []Fuel Jettison Sys

    FUEL JETTISON ARM switch..... . . OFF [Disarms fuel jettison system and removes TO REMAIN quantity from EICAS.] Do not complete the following checklist: FUEL JETTISON Copyright © The Boeing Company. See title page for details. 12.7 December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 196 Destination fuel estimate..... CHECK Verify adequate fuel available in left and right main tanks to complete flight. Continued on next page Copyright © The Boeing Company. See title page for details. 12.8 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 197 If landing using flaps 30 (performance permitting): Note: Use flaps 30 and VREF30 for landing and flaps 20 for go–around. Continued on next page Copyright © The Boeing Company. See title page for details. 12.9 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 198: Fuel Low Center

    Do not complete the following checklist: FUEL QTY LOW FUEL LOW CENTER Center tank is empty and one or both center fuel Condition: pump switches are ON. Copyright © The Boeing Company. See title page for details. 12.10 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 199: []Fuel Press Eng L, R

    [Prevents fuel imbalance by feeding both engines from the same center fuel pump.] FUEL PUMP switch (Affected pump)....OFF Copyright © The Boeing Company. See title page for details. 12.11 December 15, 2006...

  • Page 200: []Fuel Pump Ctr L+R

    Right aft or forward fuel pump output pressure is low. Condition: FUEL PUMP switch (Affected pump)....OFF Copyright © The Boeing Company. See title page for details. 12.12 D615Z003 Boeing Proprietary...

  • Page 201: []Fuel Qty Low

    Note: Avoid high nose up attitude and excessive acceleration or deceleration. [Prevents forward pumps from uncovering.] Copyright © The Boeing Company. See title page for details. 12.13 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 202: []Fuel Temp High

    Main tank fuel pump switches should remain ON. Do not accomplish the following checklists: FUEL PUMP L AFT FUEL PUMP L FWD FUEL PUMP R AFT FUEL PUMP R FWD Copyright © The Boeing Company. See title page for details. 12.14 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 203: []Fuel Temp Low

    Do not start the APU. [Prevents a potential fire hazard.] Note: APU is not available for remainder of flight. Do not accomplish the following checklist: APU SHUTDOWN Copyright © The Boeing Company. See title page for details. 12.15 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 204: Intentionally Blank

    12.16 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 12.16 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 205 RAT UNLOCKED ........13.16 Copyright © The Boeing Company. See title page for details.
  • Page 206 Non-Normal Checklists - Hydraulics 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.13.2 D615Z003 Boeing Proprietary...

  • Page 207: Nnc.13 Non-Normal Checklists-Hydraulics

    [Attempts to eliminate source of overheat.] Note: Thrust reverser on the affected side may be inoperative. Do not accomplish the following checklist: HYD PRESS PRI Copyright © The Boeing Company. See title page for details. 13.1 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 208: []Hyd Press Dem L, R

    PRIMARY PUMP switch......OFF Copyright © The Boeing Company. See title page for details.
  • Page 209 13.3 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 13.3 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 210: []Hyd Press Sys C

    Note: Do not arm speedbrake lever. [From AUTO SPEEDBRAKE checklist. Prevents inadvertent inflight extension.] Note: Manually extend speedbrakes after landing. [From AUTO SPEEDBRAKE checklist.] Continued on next page Copyright © The Boeing Company. See title page for details. 13.4 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 211 [Releases gear uplocks and gear door locks allowing gear to free fall.] Do not accomplish the following checklists: FLAPS PRIMARY FAIL SLATS PRIMARY FAIL GEAR DOOR Copyright © The Boeing Company. See title page for details. 13.5 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 212: []Hyd Press Sys L

    Note: Roll rate may be reduced in flight. Speedbrake effectiveness may be reduced in flight and during landing. [From SPOILERS checklist.] Do not accomplish the following checklist: ENG REVERSER L SPOILERS Copyright © The Boeing Company. See title page for details. 13.6 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 213 13.7 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 13.7 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 214: []Hyd Press Sys L+C

    Note: Plan additional time for slower slat and flap operation. [From FLAPS PRIMARY FAIL and SLATS PRIMARY FAIL checklists.] Continued on next page Copyright © The Boeing Company. See title page for details. 13.8 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 215 Note: For go–around, observe gear EXTEND limit speed (270K/.82M). [From GEAR DOOR checklist.] Do not accomplish the following checklists: AUTO SPEEDBRAKE FLIGHT CONTROLS SPOILERS Continued on next page Copyright © The Boeing Company. See title page for details. 13.9 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 216: Hyd Press Sys L+C+R

    Do not accomplish the following checklists: FLAPS PRIMARY FAIL SLATS PRIMARY FAIL GEAR DOOR HYD PRESS SYS L+C+R All hydraulic system pressures are low. Condition: Copyright © The Boeing Company. See title page for details. 13.10 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 217 13.11 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. 13.11 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 218: []Hyd Press Sys L+R

    Note: Use flaps 20 and VREF30 + 20 for landing. [From FLIGHT CONTROLS checklist. Higher approach speeds improve airplane maneuvering characteristics.] Continued on next page Copyright © The Boeing Company. See title page for details. 13.12 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 219: []Hyd Press Sys R

    Note: Roll rate may be reduced in flight. Speedbrake effectiveness may be reduced in flight and during landing. [From SPOILERS checklist.] Do not accomplish the following checklist: ENG REVERSER R SPOILERS Copyright © The Boeing Company. See title page for details. 13.13 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 220: []Hyd Press Sys R+C

    Note: Plan additional time for slower slat and flap operation. [From FLAPS PRIMARY FAIL and SLATS PRIMARY FAIL checklists.] Continued on next page Copyright © The Boeing Company. See title page for details. 13.14 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 221 Note: For go–around, observe gear EXTEND limit speed (270K/.82M). [From GEAR DOOR checklist.] Do not accomplish the following checklists: AUTO SPEEDBRAKE FLIGHT CONTROLS SPOILERS Continued on next page Copyright © The Boeing Company. See title page for details. 13.15 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 222: Hyd Qty Low C, L, R

    GEAR DOOR HYD QTY LOW C, L, R Hydraulic quantity is low. Condition: RAT UNLOCKED Ram air turbine is not stowed and locked. Condition: Copyright © The Boeing Company. See title page for details. 13.16 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 223: Landing Gear

    TIRE PRESS ......... . 14.6 Copyright © The Boeing Company. See title page for details.

  • Page 224: Intentionally Blank

    Non-Normal Checklists - Landing Gear 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.14.2 D615Z003 Boeing Proprietary...

  • Page 225: []Antiskid

    LANDING GEAR lever......UP If on the ground: Refer to Brake Cooling Schedule table in Performance–Inflight chapter for required cooling time. Copyright © The Boeing Company. See title page for details. 14.1 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 226: []Brakes

    [Releases gear uplocks and gear door locks allowing gear to free fall.] Do not accomplish the following checklist: GEAR DOOR Wait 30 seconds. Continued on next page Copyright © The Boeing Company. See title page for details. 14.2 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 227 FUEL PRESS ENG L FUEL PRESS ENG R []GEAR DOOR One or more gear doors are not closed. Condition: Note: Observe gear EXTEND limit speed (270K/.82M). Copyright © The Boeing Company. See title page for details. 14.3 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 228: []Gear Drag Brace L, R

    Landing gear lever....... . . UP Copyright © The Boeing Company. See title page for details.

  • Page 229: []Gear Side Brace L, R

    Condition: Note: Do not taxi with loss of steering. TILLER L Tiller is inoperative on the affected side. Condition: TILLER R (TBD) Condition: Copyright © The Boeing Company. See title page for details. 14.5 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 230: Tire Press

    14.6 787 Flight Crew Operations Manual TIRE PRESS Tire pressures are not normal. Condition: Copyright © The Boeing Company. See title page for details. 14.6 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 231: Warning Systems

    [] WINDSHEAR SYS ........15.4 Copyright © The Boeing Company. See title page for details.
  • Page 232 Non-Normal Checklists - Warning Systems 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 TOC.15.2 D615Z003 Boeing Proprietary...

  • Page 233: Airspeed Low

    CONFIG PARKING BRAKE Parking brake is set when either engine's thrust is in Condition: the takeoff range on the ground. Copyright © The Boeing Company. See title page for details. 15.1 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 234: Config Rudder

    GPWS GEAR OVRD GPWS GEAR OVERRIDE is in the OVRD position. Condition: GPWS TERR OVRD GPWS TERR OVERRIDE is in the OVRD position. Condition: Copyright © The Boeing Company. See title page for details. 15.2 D615Z003 Boeing Proprietary December 15, 2006...

  • Page 235: []Gnd Prox Sys

    Plan to land at the nearest suitable airport. Do not accomplish the following checklist: CABIN ALTITUDE AUTO TCAS TCAS has failed. Condition: TCAS OFF TCAS is in standby mode. Condition: Copyright © The Boeing Company. See title page for details. 15.3 December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 236: Tcas Ra Captain, F/O

    Windshear alerts may not be provided. Condition: Note: Some or all windshear alerts are not available. Windshear alerts which occur are still valid. Copyright © The Boeing Company. See title page for details. 15.4 D615Z003 Boeing Proprietary December 15, 2006...
  • Page 237 Visual Traffic Pattern ....... MAN.2.6 Go–Around and Missed Approach ....MAN.2.7 Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.TOC.0.1...
  • Page 238 Maneuvers - Table of Contents 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.TOC.0.2 D615Z003 Boeing Proprietary...

  • Page 239: Approach To Stall Recovery

    If the first officer is making the takeoff, the first officer must maintain control of the airplane until the captain makes a positive input to the controls. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 240 • if the airplane is unsafe or unable to fly. During the takeoff, the crew member observing the non-normal situation will immediately call it out as clearly as possible. Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.1.2...
  • Page 241 • 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. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 242: Terrain Avoidance

    Accomplish the following maneuver for any of these conditions: • activation of the “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. December 15, 2006 MAN.1.4 D615Z003 Boeing Proprietary...

  • Page 243: Traffic Avoidance

    Immediately accomplish the following by recall whenever a TCAS traffic advisory (TA) or resolution advisory (RA) occurs. WARNING: Comply with RA if there is conflict between RA and air traffic control. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.1.5...
  • Page 244 If traffic is sighted, maneuver as required. WARNING: A DESCEND (fly down) RA issued below 1000 feet AGL should not be followed. Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.1.6 D615Z003 Boeing Proprietary...

  • Page 245: Upset Recovery

    • pitch attitude greater than 10 degrees nose down, or • bank angle greater than 45 degrees, or • within above parameters but flying at airspeeds inappropriate for the conditions. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.1.7...
  • Page 246 • Complete the recovery: • when approaching the horizon, roll to wings level • check airspeed and adjust thrust • establish pitch attitude. Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.1.8 D615Z003 Boeing Proprietary...

  • Page 247: Windshear

    Predictive windshear warning during takeoff roll: (“WINDSHEAR AHEAD, WINDSHEAR AHEAD” aural) • Prior to V1, reject takeoff. • After V1, perform the Windshear Escape Maneuver. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.1.9...
  • Page 248 • 5 degrees 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. December 15, 2006 MAN.1.10 D615Z003 Boeing Proprietary...

  • Page 249: Manual Flight

    • Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°. • Retract speedbrakes. • Follow flight director TO/GA guidance (if available). Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.1.11...
  • Page 250 WARNING: *** Severe windshear may exceed the performance capability of the AFDS. The pilot flying must be prepared to disconnect the autopilot and autothrottle(s) and fly manually. Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.1.12 D615Z003 Boeing Proprietary...
  • Page 251 787 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. December 15, 2006 D615Z003 Boeing Proprietary MAN.2.1...

  • Page 252: Flight Patterns

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual ILS Approach Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.2.2 D615Z003 Boeing Proprietary...

  • Page 253: Instrument Approach Using Vnav

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual Instrument Approach Using VNAV Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.2.3...

  • Page 254: Instrument Approach Using V/S Or Fpa

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual Instrument Approach Using V/S or FPA Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.2.4 D615Z003 Boeing Proprietary...

  • Page 255: Circling Approach

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual Circling Approach Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.2.5...

  • Page 256: Visual Traffic Pattern

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual Visual Traffic Pattern Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.2.6 D615Z003 Boeing Proprietary...

  • Page 257: Go-Around And Missed Approach

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual Go–Around and Missed Approach Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary MAN.2.7...

  • Page 258: Intentionally Blank

    Maneuvers - Flight Patterns 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 MAN.2.8 D615Z003 Boeing Proprietary...
  • Page 259 VREF ......... PI.A12.1 Copyright © The Boeing Company. See title page for details.
  • Page 260 Performance Inflight A - Table of Contents 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.TOC.A.2 D615Z003 Boeing Proprietary...

  • Page 261: Advisory Information

    (Alt Mode %N1) (65.1) (68.0) (71.2) (74.8) PITCH ATT 15000 0.976 0.996 1.025 1.060 (270 KIAS) (Alt Mode %N1) (61.7) (64.3) (67.6) (71.1) Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A10.1...
  • Page 262 (Alt Mode %N1) (51.1) (57.3) (62.8) (67.3) KIAS PITCH ATT 0.999 1.010 1.021 1.030 5000 (Alt Mode %N1) (47.3) (53.1) (58.5) (63.3) KIAS Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.2 D615Z003 Boeing Proprietary...
  • Page 263 (57.7) (62.2) KIAS PITCH ATT -0.5 1.050 1.070 1.090 1.120 FLAPS 30 (VREF30 + 10) (Alt Mode %N1) (50.3) (57.9) (63.8) (68.3) KIAS Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A10.3...

  • Page 264: Normal Configuration Landing Distance

    Autobrake data valid for both auto and manual speedbrakes. Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold (1000 ft of air distance). Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.4...
  • Page 265 Autobrake data valid for both auto and manual speedbrakes. Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold (1000 ft of air distance). Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 266 Autobrake data valid for both auto and manual speedbrakes. Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold (1000 ft of air distance). Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.6...

  • Page 267: Non-Normal Configuration Landing Distance

    Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold to stop (1000 ft of air distance). Assumes maximum manual braking and maximum available reverse thrust. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 268 Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold to stop (1000 ft of air distance). Assumes maximum manual braking and maximum available reverse thrust. Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.8...
  • Page 269 Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold to stop (1000 ft of air distance). Assumes maximum manual braking and maximum available reverse thrust. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 270 Actual (unfactored) distances are shown. Includes distance from 50 ft above threshold to stop (1000 ft of air distance). Assumes maximum manual braking and maximum available reverse thrust. Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.10...

  • Page 271: Recommended Brake Cooling Schedule

    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. December 15, 2006 D615Z003 Boeing Proprietary...
  • Page 272 (When inflight with gear extended, the BTMS indications may vary between individual brakes, due to air- stream effects.) Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.12...

  • Page 273: Landing Climb Limit Weight

    With engine and wing anti-ice on, decrease weight by 3400 lb. When operating in icing conditions during any part of the flight with forecast landing temperature below 10°C, decrease weight by 45400 lb. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary...

  • Page 274: Intentionally Blank

    Performance Inflight A 777-200ER/TRENT892 Advisory Information Category A Brakes 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A10.14 D615Z003 Boeing Proprietary...

  • Page 275: Initial Max Continuous Epr

    1.467 1.465 1.364 1.402 1.439 1.473 1.506 1.523 1.523 1.521 1.518 -20 & 1.364 1.402 1.439 1.473 1.506 1.523 1.523 1.521 1.518 BELOW Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A11.1...

  • Page 276: Max Continuous Epr

    -0.014 -0.013 -0.012 -0.012 ENGINE & WING** -0.026 -0.024 -0.022 -0.021 -0.020 * Wing anti-ice on, packs on. **Wing anti-ice on, packs off. Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A11.2 D615Z003 Boeing Proprietary...
  • Page 277 -0.012 -0.012 -0.013 -0.012 ENGINE & WING** -0.019 -0.019 -0.019 -0.019 -0.018 * Wing anti-ice on, packs on. **Wing anti-ice on, packs off. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A11.3...
  • Page 278 -0.019 -0.018 -0.012 ENGINE & WING** -0.021 -0.024 -0.024 -0.023 -0.022 -0.014 * Wing anti-ice on, packs on. **Wing anti-ice on, packs off. Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A11.4 D615Z003 Boeing Proprietary...

  • Page 279: Driftdown Speed/Level Off Altitude

    17900 16400 21000 19700 18200 22900 21600 20100 24800 23500 22100 26500 25400 24200 28400 27300 26100 30400 29200 28100 33200 31600 30200 Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A11.5...

  • Page 280: Driftdown/Lrc Cruise Range Capability

    45.1 49.9 54.9 59.9 64.9 70.0 75.2 80.2 85.5 4:27 APU fuel included. Driftdown at optimum driftdown speed and cruise at LRC speed. Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A11.6 D615Z003 Boeing Proprietary...

  • Page 281: Long Range Cruise Altitude Capability

    23500 22100 25900 24700 23300 27100 25800 24600 28300 27000 25800 29500 28200 26900 30800 29500 28100 32400 30800 29400 34100 32500 30700 Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A11.7...

  • Page 282: Long Range Cruise Control

    1.162 1.185 1.213 1.244 MACH .434 .474 .492 .510 .530 .550 .570 .591 KIAS FF/ENG 9133 9031 9011 8995 8976 8955 8938 8918 Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A11.8 D615Z003 Boeing Proprietary...

  • Page 283: Long Range Cruise Diversion Fuel And Time

    -14.5 -7.1 10.9 22.3 -15.7 -7.7 11.7 24.0 -16.9 -8.3 12.5 25.8 -18.1 -9.0 13.3 27.5 -19.4 -9.6 14.1 29.1 APU fuel included. Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A11.9...

  • Page 284: Holding

    1.102 1.141 1.201 KIAS FF/ENG 8290 8200 8010 7920 7900 7810 This table includes 5% additional fuel for holding in a racetrack pattern. Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A11.10 D615Z003 Boeing Proprietary...

  • Page 285: Max Climb Epr

    -0.012 -0.014 -0.021 -0.025 -0.018 -0.019 -0.020 -0.024 -0.029 -0.033 *Wing anti-ice on, packs on. **Wing anti-ice on, single bleed source and both packs off. VREF FLAPS WEIGHT (1000 LB) Copyright © The Boeing Company. See title page for details. December 15, 2006 D615Z003 Boeing Proprietary PI.A12.1...
  • Page 286 Performance Inflight A 777-200ER/TRENT892 General Category A Brakes 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. December 15, 2006 PI.A12.2 D615Z003 Boeing Proprietary...
  • Page 287 BOTTLE 1, 2 DISCH ENG ....... . . 8.1 Copyright © The Boeing Company. See title page for details.
  • Page 288 DUAL ENG FAIL/STALL ....... . 0.4,7.2 Copyright © The Boeing Company. See title page for details.
  • Page 289 ENG SVR DAMAGE/SEP L, R ......8.5,10.3 Copyright © The Boeing Company. See title page for details.
  • Page 290 FUEL PRESS ENG L, R ....... . . 12.10 Copyright © The Boeing Company. See title page for details.
  • Page 291 HYD PRESS SYS R+C ........13.12 Copyright © The Boeing Company. See title page for details.
  • Page 292 PRI FLIGHT COMPUTERS ....... . . 9.6 Copyright © The Boeing Company. See title page for details.
  • Page 293 TERR POS ..........15.4 Copyright © The Boeing Company. See title page for details.
  • Page 294 WINDSHEAR SYS ........15.4 Copyright © The Boeing Company. See title page for details.

  • Page 295: Back Cover

    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.1...
  • Page 296 Back Cover.2 787 Flight Crew Operations Manual Intentionally Blank Copyright © The Boeing Company. See title page for details. Back Cover.2 December 15, 2006 D615Z003 Boeing Proprietary...
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