Fire Protection Flashcards

1
Q

Pushing either illuminated Master FIRE WARN light”,” in flight”,” _____.

A

silences the Fire Warning Bell
extinguishes both FIRE WARN lights
resets the system for future warnings

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2
Q

Pushing the _____ provides the same function as pushing either Master FIRE WARN light for an engine fire warning

A

Fire Warning BELL CUTOUT switch

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3
Q

The _____ Bus powers the Engine Overheat and Fire Detection. The _____ Bus powers the Engine Fire Extinguishing.

A

Battery / Hot Battery

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4
Q

If illuminated”,” the ENG OVERHEAT light and Engine Fire Switch remain illuminated until ________.

A

the temperature drops below the onset temperature

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5
Q

With the OVHT DET switch in the A position”,” _____ can initiate an overheat or fire warning.

A

only the A detector loop

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6
Q

With the OVHT DET switch selected to “A” during an Overheat/Fire Test”,” a FAULT light (amber) indications means_____.

A

there is a fault in loop A

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7
Q

If one overheat/fire detector loop fails with the OVHT DET switch on NORMAL”, “the _____.

A

remaining loop functions as a single loop detector

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8
Q

Rotating an Engine Fire Switch in one direction _____.

A

electrically fires a squib on one bottle”,” discharging the extinguisher

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9
Q

The _____ Bus powers the APU Fire Detection and the _____ Bus powers the APU Fire Extinguishing.

A

Battery / Hot Battery

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10
Q

Select the two events that will unlock the APU Fire Switch ______. (Select ALL correct answers.)

A

using the Fire Switch Override

the Fire Switch illuminates

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11
Q

Pressing the HORN CUTOUT switch on the APU Fire Control Panel (main wheel well) silences the _____ and the APU Fire Warning Light _____.

A

Fire Warning Bell and APU Fire Warning Horn / stops flashing but remains illuminated

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12
Q

Placing the Overheat/Fire Protection Panel Test Switch to OVHT/FIRE checks ______.

A

engine”,” APU and wheel well overheat and fire detection circuitry

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13
Q

Placing the Overheat/Fire Protection Panel Test Switch to FAULT/INOP checks _____ and related Flight Deck indicators.

A

engine and APU module fault detection circuitry

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14
Q

A FAULT light (amber) illuminates during an OVHT FIRE test. This indicates a failure of ______.

A

at least one loop on an engine

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15
Q

Setting the ENGINES APU EXT/TEST switch to position _____ tests the APU Fire Bottle _____.

A

1 or 2 / circuit continuity

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16
Q

Complete this statement: Main wheel well fire _____.

A

detection requires AC power

17
Q

When TEST is pushed and held on the Boeing Cargo Fire Panel”,” a DETECTOR FAULT light (amber) illuminated indicates ______.

A

a fault (failure) in one or more detectors in the loop(s)

18
Q

The second fire bottle”,” on the Boeing Lower Cargo Compartment Fire Suppression Dual Bottle system”,” discharges _____.

A

automatically by a timer for a total of 195 minutes saturation