Fire Protection Flashcards

1
Q

Describe what to do if the Engine or APU Fire switch cannot be pulled in the event of a fire or emergency evacuation.

A

Push the fire override switch located beneath the fire switch.

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2
Q

What happens when the Engine Fire switch is pulled?

A

Shuts off: Fuel, Bleed Air, Generator, Hydraulics and arms the Fire Bottle.

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3
Q

With an engine fire, what three ways can the fire bell be silenced?

A

Depressing either Master Warning switch or pulling the appropriate fire switch, extinguishing the fire.

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4
Q

What is the meaning of an L/R ENG OVHT light and EICAS caution message?

A

Engine overheat is detected.

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5
Q

How many fire bottles are available for engine fires?

A

Two

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6
Q

Describe what happens when a Cargo Compartment ARM switch is pushed.

A

Arms respective bottles (2), turns off the left recirculation fan.

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7
Q

What would you expect to see illuminated after pushing the AFT Cargo Compartment ARM switch?

A

The “ARMED” and “AFT” lights illuminate.

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8
Q

How many bottles are available for cargo fires?

A

2

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9
Q

What happens when the APU fire switch is pulled?

A

Shuts Off: Fuel, Generator, Air and Arms Fire Bottle

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10
Q

Why does the APU Shutdown switch on the Ground Control Panel have to be pushed before discharging the fire bottle?

A

It arms the fire bottle.

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11
Q

Describe what happens on the outside of the aircraft when an APU fire occurs on the ground?

A

The fire horn sounds in the nose wheel and the fire warning light illuminates.

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12
Q

How many fire bottles are available for the APU?

A

1

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13
Q

What type of fire protection is provided for the main gear wheel well?

A

One fire detection loop.

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14
Q

How long will the main gear wheel well fire warning lights remain illuminated?

A

Until the fire is extinguished.

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15
Q

Describe when the Engine and APU Fire Detection Systems are tested?

A

The system will automatically test the detection system when power is initially applied. The system can be tested manually also.

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16
Q

What are the cockpit indications of a failure of an Engine Fire Detection System?

A

EICAS will display SYS FAIL. This can be reset allowing for single system monitoring.

17
Q

Why is it important to push the System Fail Reset switch after a FAIL P-RESET light illuminates?

A

Resets the monitor for the other systems.

18
Q

Where are overheat detections systems installed.

A

Engines, struts, and pneumatic ducts in the wing and body areas.

19
Q

Where on the engines are the Fire/Overheat loops located?

A

Nacelle.