Fire Protection Flashcards

1
Q

How many smoke detectors are located in the forward cargo compartment?

A

3

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2
Q

How many smoke detectors are located in the aft cargo compartment?

A

2

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3
Q

True or False: The cargo compartment smoke detectors are monitored by the MAU.

A

True

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4
Q

Where is the lavatory fire extinguisher bottle located?

A

Inside each lavatory waste container

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5
Q

True or False: Due to the fact that both lavatories are continuously monitored by
the flight attendants, neither lavatory has a smoke detector.

A

False

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6
Q

The Engine fire protection system provides _______.

A

Engine fire detection,
engine fire extinguishing,
and continuous built-in tests to detect internal faults

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7
Q

Where are the engine fire bottles located?

A

Right hand wing to fuselage fairing

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8
Q

How could the aural warning be silenced in the event of an engine fire?

A

By pressing either master WARN switchlight

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9
Q

If an engine fire is detected, which of the following will occur?

A

Firebell aural sounds,
the FIRE handle illuminates,
the master WARN lights illuminate,
a warning message is displayed on EICAS,
a FIRE warning light illuminates on respective ITT

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10
Q

By pulling an engine Fire Handle, which of the following will occur?

A

Will cause following shutoff valves to close:
engine fuel shutoff valve,
engine hydraulic shutoff valve,
and engine bleed air shutoff valve

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11
Q

The APU fire protection system provides which of the following?

A

APU fire detection,
APU fire extinguishing,
and continuous built-in tests to detect internal faults

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12
Q

True or False: In the event of an APU fire, pressing either master WARN
switchlight silences the master WARN aural alert.

A

True

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13
Q

If an APU fire is detected, which of the following will occur?

A

A firebell aural sounds,
the red striped bar on the APU EMER STOP button illuminates,
the master WARN lights illuminate,
and the EICAS message APU FIRE is displayed

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14
Q

True or False: When the fire detectors no longer sense a fire in the APU, the APU
fire extinguisher button will still be illuminated.

A

FALSE

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15
Q

True or False: The cargo compartments are continuously being monitored for smoke.

A

True

[smoke detection is continuous - Built In Test is periodic]

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16
Q

If smoke is detected in the forward cargo compartment by a single smoke detector,
which of the following will occur?

A

The air circulation fan automatically turns off, and the ventilation outflow valve closes

17
Q

If a smoke condition is sensed in either cargo compartment, which of the following
will occur?

A

The high rate fire extinguishing bottle is automatically armed,
a firebell aural sounds,
the master WARN lights illuminate,
the associated cargo compartment extinguishing button illuminates,
the EICAS warning and advisory messages are displayed

18
Q

To extinguish a fire in the forward cargo compartment, pilots must _______.

A

Select the illuminated cargo fire extinguisher button

19
Q

In flight, the low rate fire bottle will discharge automatically after one minute,
providing protection from re-ignition for _______ minutes.

A

75 min.

20
Q

True or False: On the ground, the cargo compartment low-rate extinguisher fire
bottle will automatically discharge.

A

False

21
Q

True or False: The cargo fire extinguishing system CANNOT be used in the
absence of an alarm condition.

A

False

22
Q

In the event that there is an absence of a fire alarm condition, which of the
following is true about the forward and aft cargo compartments?

A

The alarm will be treated as a fault

23
Q

True or False: The forward and aft lavatories do not have any fire protection
Installed.

A

False

24
Q

True or False: The fire extinguishers that are installed in each lavatory will only
extinguish a fire located in the lavatory waste bin.

A

True

25
Q

True or False: The lavatory fire extinguishing system has flight deck controls.

A

False

26
Q

At what temperature will the lavatory fire extinguisher automatically discharge?

A

Exceeds 172 degrees Fahrenheit

27
Q

Lavatory fire extinguishing is accomplished how?

A

When the temperature inside the waste bin exceeds 172 degrees Fahrenheit the tip of each tube will melt causing the extinguishing agent to discharge in the waste bin

28
Q

The fire detection system TEST button in the flightdeck is used to test all the
following systems EXCEPT _______.

A

Engine fire detection,
APU fire detection,
and cargo smoke detection

“62522”

6 - lights on overhead panel
2 - master warning switchlights
5 - EICAS messages
2 - Reverse Video ITT FIRE indication
2 - triple chime fire bell, master warning chime

29
Q

There are a total of _______ bottles available to extinguish an engine fire and
_______ bottles available to extinguish an APU fire.

A

2, 1

30
Q

True or False: During normal operations, both engine overheat detector loops must
detect a fire before a warning is generated.

A

True

31
Q

Which of the following statements best describes the operation of the cargo fire
extinguisher system?

A

After the annunciation of smoke detection in the cargo compartment pressing the associated cargo compartment button causes:
The high rate bottle discharges immediately into the selected compartment and the CRG FIREX HI DISCH EICAS advisory message to display.
The low rate bottle discharges at a slower rate preventing reignition for 75 minutes [the low rate bottle discharges 1 minute later when in flight]

32
Q

On the ground, the APU will shut down automatically _______ seconds after a fire
condition is detected.

A

10 sec.

33
Q

What are the flight deck and cabin indications that the lavatory waste bin
extinguisher has discharged?

A

There are no flightdeck or cabin indications that the bottle has discharged