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OPERATIONS MANUAL

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Fire Protection<br />

Fire Warnings:<br />

When a fire is detected, the fire bell on the flight deck rings every five<br />

seconds. The first ring is louder than the subsequent rings. In case<br />

of an APU fire, the APU fire warning horn sounds also; the horn is<br />

installed in the right body gear wheel well. Both the bell and the horn<br />

can be silenced by extinguishing the APU fire, or by pulling the APU<br />

fire switch. In any case of a fire—in the APU, engine, cargo, or wheel<br />

well—, pushing a master warning reset switch silences the flight deck<br />

fire bell and turns off the master warning lights. Fire warnings are<br />

entirely reset when the respective fire is extinguished.<br />

Fire warnings are inhibited during part of the takeoff: the inhibit starts<br />

at V1 if the FMC provides a valid V1 speed, else when the aircraft pitch<br />

rises through 5°. The inhibit ends after 25 seconds or when climbing<br />

through 400 ft.<br />

Squibs and Fire Extinguisher Bottles:<br />

Squibs are small, electrically triggered explosive devices mounted on the<br />

sealed outlets of the fire extinguisher bottles. When a squib detonates,<br />

it tears the outlet open, and pressurized halon gas in the bottle will<br />

discharge through a duct system into the area where the fire is located.<br />

The main hot battery bus provides the trigger power; the power may be<br />

routed to a squib using the respective fire switch. Using a test switch on<br />

the maintenance panel, the power can be routed to the squib through<br />

a test lamp; the lamp acts as a resistor and reduces the current so that<br />

the squib will not explode during the test. Lights that do not illuminate<br />

during the test will indicate the respective power line to the squib is<br />

broken, or not powered, or the squib has been fired.<br />

Each test switch refers to the squibs on the A or B engine bottles and the<br />

APU bottle,—or to cargo bottle squibs,—or to both. For example, on a<br />

non-ER passenger aircraft, test switch 1 refers to all A bottle squibs and<br />

all cargo bottle forward squibs; and test switch 2 refers to all B bottle<br />

squibs and all cargo bottle aft squibs. Other aircraft include two more<br />

test switches that refer to the cargo bottle squibs only.<br />

The test light itself incorporates another switch; when that switch is<br />

pushed and the light does not illuminate, the test lamp is broken, or<br />

power is removed. That is a plain lamp test and cannot be influenced by<br />

a failed squib.<br />

— Page 240 —<br />

For preview only. Not for sale. Many pages are intentionally removed.

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