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[] SMOKE EQUIP CLG FWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.9
u SMOKE EQUIP CLG MISC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10
u SMOKE/FUMES AIR COND . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10
u SMOKE/FUMES/FIRE ELEC . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.12
u SMOKE/FUMES REMOVAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.14
SMOKE LAVATORY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.15
SMOKE LAV/COMPT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.15
u SMOKE REST UPR DR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.15
u SMOKE REST UPR DR 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.16
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.8.2 D615Z003 Boeing Proprietary
Non-Normal Checklists -
Fire Protection
Intentionally
Blank
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 8.1
8.1
NNC.8 Non-Normal Checklists-Fire Protection
Condition: Engine fire extinguisher bottle 1 or bottle 2 pressure
is low.
Condition: APU fire extinguisher bottle pressure is low.
Condition: Both rapid discharge cargo fire extinguisher bottle
pressures are low.
Condition: APU fire detection is inoperative.
If APU not running:
Note: Do not start the APU unless use is required.
If APU running:
Plan to shut down the APU as soon as practical.
Condition: Affected cargo compartment smoke detection is
inoperative.
Condition: A fault is detected in the engine fire detection system.
Note: Engine fire detection may not be available. An engine
fire warning which occurs is valid.
BOTTLE 1, 2 DISCH ENG
BOTTLE DISCH APU
BOTTLE DISCH CARGO
[]DET FIRE APU
DET FIRE CARGO AFT, FWD
[]DET FIRE ENG L, R
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary
8.2
8.2
Condition: Fire is detected in the APU.
APU fire switch. . . . . . . . . . . . . . . . . . . . .Pull, rotate, and hold
Rotate to the stop and hold for 1 second.
If the FIRE APU message stays shown:
Plan to land at the nearest suitable airport.
Do not accomplish the following checklist:
APU SHUTDOWN
Condition: Smoke is detected in the aft cargo compartment.
AFT CARGO FIRE ARM switch. . . . . . . . . . . . . . . . . . .ARMED
CARGO FIRE discharge switch. . . . . . . . . . . . . . . . . . . . PUSH
Push and hold for 1 second.
Landing altitude selector. . . . . . . . . . . . . . . . . .PULL, set 8000
[Minimizes extinguisher agent leakage out of the compartment.]
Plan to land at the nearest suitable airport.
Note: Aft equipment cooling normal mode is inoperative.
After 30 minutes of operation at low altitude and low
cabin differential pressure, non-critical electronic
equipment may fail.
[From EQUIP CLG OVRD AFT checklist.]
Do not accomplish the following checklist:
EQUIP CLG OVRD AFT
LANDING ALTITUDE
When at top of descent:
Landing altitude selector. . . . . . . . . . . . . . . . . . . . . . PUSH
[Restores automatic selection of the FMC landing altitude.]
Continued on next page
[]FIRE APU
[]FIRE CARGO AFT
December 15, 2006
787 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary 8.3
8.3
Continued from previous page
When at top of descent: (continued)
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.
Condition: Smoke is detected in the forward cargo compartment.
FORWARD CARGO FIRE ARM switch. . . . . . . . . . . . .ARMED
CARGO FIRE discharge switch. . . . . . . . . . . . . . . . . . . . PUSH
Push and hold for 1 second.
Landing altitude selector. . . . . . . . . . . . . . . . . .PULL, set 8000
[Minimizes extinguisher agent leakage out of the compartment.]
Plan to land at the nearest suitable airport.
Note: Forward equipment cooling normal mode is
inoperative. After 30 minutes of operation at low
altitude and low cabin differential pressure,
non-critical electronic equipment may fail.
[From EQUIP CLG OVRD FWD checklist.]
Do not accomplish the following checklists:
EQUIP CLG OVRD FWD
LANDING ALTITUDE
　
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