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* det - detector
* DV - Distinguished Visitor
* E/E - electronic equipment
* ENG - engine
* ext - extinguish
* HMU - hydro-mechanical unit
* hyd - hydraulic
* inop - inoperable
* LED - light emitting diodes
* LOC - local
* lts - lights
* maint - maintenance
* MD&T - master dim and test
* mem - memory
* MLG - main landing gear
* ovht - overheat
* PA - passenger address
* ref - reference
* rev - reverser
* typ - typical
* vlv - valve
* warn - warning
* W/W - wheel well
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Purpose
The fire alarms provide visual and aural indication to the flight
crew about a fire in any of these systems:
* Engine 1
* Engine 2
* APU
* Forward cargo compartment
* Aft cargo compartment
* Main wheel well.
Visual and Aural Indications
When there is a fire, these are the visual and aural indications:
* Two red FIRE WARN lights on the P7 panel come on
* Bell in the aural warning unit comes on
* Red light and horn on alternatly in the right main wheel well
come on (APU fire only). (The horn does not come on in
flight.)
Functional Description
When there is a fire in the engine, the engine and APU fire
detection module provides a ground for the two red FIRE WARN
lights and the bell.
When there is a fire in the APU, the engine and APU fire
detection module provides a ground for the two red FIRE WARN
lights and the bell. The same module provides power for the red
light and horn on the P28 panel.
When there is a fire in the main wheel well, the compartment
overheat detection controller provides a ground for the two red
FIRE WARN lights and the bell.
When there is smoke in the forward or aft cargo compartment,
the cargo electronic unit provides a ground for the two red FIRE
WARN lights and the bell.
The two red FIRE WARN lights, bell, and horn are reset by
removal of the ground. The reset is done by a momentary push
on one of these:
* Left FIRE WARN light
* Right FIRE WARN light
* Bell cutout switch on P8
* Horn cutout switch on the P28 panel.
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EFFECTIVITY
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Purpose
The engine overheat and fire detection system uses detectors
on the engine. The detectors monitor engines for overheat and
fire conditions. When the system senses an overheat or a fire
condition, alarm indications operate in the flight compartment.
The indications are on the P7 glareshield panel and on the
engine and APU fire control panel. A bell also operates in the
flight compartment for an engine fire.
FIRE PROTECTION - ENGINE FIRE DETECTION - INTRODUCTION
EFFECTIVITY
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