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TOC.8.1
Table of Contents
NNAC.I8R N oCn-ONoNrmDalI TChIeOckNlisItNs-FGir eS PMrotOectKioEn /FUMES . . . . . . . . . . . . . . . . . . . . 8.1
APU DET INOP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.2
APU FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.2
CARGO FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.3
CARGO FIRE DETECTOR FAULT . . . . . . . . . . . . . . . . . . . . . . . . 8.3
ELECTRICAL SMOKE/FUMES OR FIRE . . . . . . . . . . . . . . . . . . 8.4
ENGINE FIRE/OVERHEATDETECTOR FAULT . . . . . . . . . . . . . 8.5
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION . . . . . 8.6
ENGINE OVERHEAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.8
ENGINE TAILPIPE FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.9
SMOKE/FUMES REMOVAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.10
WHEEL WELL FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.12
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
TOC.8.2
Non-Normal Checklists -
Fire Protection
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
8.1
8.1
NNC.8 Non-Normal Checklists-Fire Protection
Condition: A concentration of air conditioning smoke/fumes is
identified.
OXYGEN MASKS AND SMOKE GOGGLES
(if required) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
CREW COMMUNICATIONS
(if required) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ESTABLISH
RECIRCULATION FAN SWITCH . . . . . . . . . . . . . . . . . . . . .OFF
[Eliminates possible source of smoke/fumes.]
If smoke/fumes stop:
Continue flight with the recirculation fan switch OFF.
If smoke/fumes continue:
ISOLATION VALVE SWITCH . . . . . . . . . . . . . . . . . . . CLOSE
R PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If smoke/fumes stop:
Continue flight with the R PACK switch OFF and
ISOLATION VALVE switch CLOSE.
If smoke/fumes continue:
R PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
L PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If smoke/fumes stop:
Continue flight with the L PACK switch OFF and
ISOLATION VALVE switch CLOSE.
If smoke/fumes continue:
L PACK SWITCH. . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Plan to land at nearest suitable airport.
Continued on next page
AIR CONDITIONING SMOKE/FUMES
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
8.2
8.2
Continued from previous page
Accomplish the SMOKE/FUMES REMOVAL checklist, if
required.
Condition: The APU DET INOP light illuminated indicates the
APU fire detection loop has failed.
APU SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
CAUTION: Do not operate the APU. An APU fire would not
be detected and the APU would continue to run.
Condition: Fire is detected in the APU.
APU fire switch. . . . . . . . . . . . . . . . . . . . . Pull, rotate and hold
Rotate to the stop and hold for 1 second.
APU switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Plan to land at the nearest suitable airport.
[Fire damage my have occurred.]
When on the ground:
STANDBY POWER switch . . . . . . . . . . . . . . . . . . . . . . . BAT
APU DET INOP
APU FIRE
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
8.3
8.3
Condition: Fire is detected in the related cargo compartment.
CARGO FIRE ARM SWITCH (FWD/AFT). . . . . . . . . . . .ARMED
CARGO FIRE DISCHARGE SWITCH. . . . . . . . . . . . . . . . PUSH
Push and hold for 1 second.
Note: DISCH light may require up to 30 seconds to
illuminate.
RECIRCULATION FAN SWITCH . . . . . . . . . . . . . . . . . . . . .OFF
ONE PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
Plan to land at the nearest suitable airport.
WARNING: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: The DETECTOR FAULT light illuminated indicates
both loops in one or both cargo compartments have
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