Fire Protection Flashcards
There is no difference between APU fire detection/extinguishing whether in flight or on the ground with either engine running. [8.80.10]
A. True.
A. True.
A “BOTTLE DISCH APU” displayed on EICAS indicates: [8.80.30, 8.80.10]
B. The APU fire extinguisher bottle is low.
B. The APU fire extinguisher bottle is low
What is indicated by the BOTTLE 1 DISCH ENG EICAS message during preflight? [8.80.10]
C. Fire bottle 1 has discharged or pressure is low.
C. Fire bottle 1 has discharged or pressure is low.
Which of the following will unlock the engine fire switch? [8.80.20]
A. Pushing the lock override button beneath the fire switch.
B. A fire signal from the respective engine.
C. Placing the fuel cutoff switch to the cutoff position.
D. Any of the above.
A. Pushing the lock override button beneath the fire switch.
B. A fire signal from the respective engine.
C. Placing the fuel cutoff switch to the cutoff position.
D. Any of the above.
On the ground, after the FWD CARGO FIRE ARM switch is selected to ARM, all seven bottles discharge immediately. [8.80.10]
B. False.
B. False.
There is no flight deck indication of lavatory smoke. [8.80.10]
B. False.
B. False.
When the engine fire switch is pulled up, rotating the switch in either direction discharges one extinguisher bottle into the associated engine, and then 30 seconds later discharges the remaining bottle into the same engine. [8.80.10]
B. False.
B. False
In regard to the hydraulic system, pulling an engine fire handle: [8.80.20]
A. Will shut off fluid to the associated pump.
C. Depressurizes the engine driven pump.
D. A and C are correct.
A. Will shut off fluid to the associated pump.
C. Depressurizes the engine driven pump.
D. A and C are correct.
Failure of a single channel of an engine fire detection assembly will only be indicated by a status message and may have no accompanying EICAS caution or warning
message. [8.80.10]
A. True.
A. True
Selecting ARM on the FWD cargo fire arm switch will: [8.80.20]
A. Configure the FWD equipment cooling system to OVERRIDE mode.
B. Shut down the forward cargo heat.
C. Command the air conditioning packs to provide minimum flow rate consistent with pressurization demands.
D. All the above.
A. Configure the FWD equipment cooling system to OVERRIDE mode.
B. Shut down the forward cargo heat.
C. Command the air conditioning packs to provide minimum flow rate consistent with pressurization demands.
D. All the above.
Which of the following are indication(s) of an engine fire? [8.80.10]
A. The fire bell sounds.
C. The engine FUEL CONTROL (L or R) switch fire warning light
illuminates.
D. A and C are correct.
A. The fire bell sounds.
C. The engine FUEL CONTROL (L or R) switch fire warning light
illuminates.
D. A and C are correct.
An EICAS message BOTTLE DISCH CARGO will illuminate when both rapid discharge extinguisher bottle pressure’s are low. [8.80.10, 8.80.30]
A. True.
A. True.
Arming the AFT Cargo Fire Arm switch: [8.80.20]
A. Shuts down the Lavatory / Galley vent fans.
A. Shuts down the Lavatory / Galley vent fans
EICAS fire warning messages can always be removed using the CANC/RCL button. [8.150.10]
B. False.
B. False.
Which of the following statements are TRUE regarding the Cargo Compartment Fire Protection? [8.80.10]
A. Cargo fire suppression is provided for up to 330 minutes.
B. Seven fire extinguisher bottles are available to either the FWD or AFT cargo compartment.
C. Normally at least two detectors in the same compartment must detect smoke to cause a Warning to be generated.
D. All the above.
A. Cargo fire suppression is provided for up to 330 minutes.
B. Seven fire extinguisher bottles are available to either the FWD or AFT cargo compartment.
C. Normally at least two detectors in the same compartment must detect smoke to cause a Warning to be generated.
D. All the above.
The flight deck crew rest compartment has a smoke detection system, but no built-in automatic fire extinguishing system. [8.80.10]
A. True.
A. True
With a loss of either channel of the dual channel engine detector assembly: [8.80.10]
C. Overheat and Fire detection continues operating normally on one detector.
C. Overheat and Fire detection continues operating normally on one detector.
The APU is equipped with 2 independent fire bottles. [8.80.10]
B. False.
B. False
The indication of smoke in the overhead flight crew rest compartment is: [8.80.10]
A. Caution beeper and an EICAS caution message SMOKE REST UPR DR 1.
A. Caution beeper and an EICAS caution message SMOKE REST UPR DR 1.
What provisions are there for testing the fire and overheat detection system? [8.80.10]
C. The fire and overheat detection system has both manual and automatic fault
testing.
C. The fire and overheat detection system has both manual and automatic fault
testing.
The main wheel well has fire and overheat detection as well as fire extinguishing. [8.80.10]
B. False.
B. False
In the event of a fire, Halon from five of the cargo fire bottles is metered into the selected cargo compartment. This allows a steady flow of Halon into the cargo compartment to keep the fire suppressed for a minimum of 400 minutes. [8.80.10]
B. False.
B. False
What are the indications on the flight deck when cargo fire extinguisher bottle discharge is initiated? [8.80.10]
A. The cargo fire discharge switch light illuminates when the first extinguisher bottles begin to discharge.
C. The CARGO FIRE FWD/AFT warning message is likely to remain after the fire is extinguished due to smoke in the cargo compartment.
D. A and C are correct
A. The cargo fire discharge switch light illuminates when the first extinguisher bottles begin to discharge.
C. The CARGO FIRE FWD/AFT warning message is likely to remain after the fire is extinguished due to smoke in the cargo compartment.
D. A and C are correct
Pushing the FWD or AFT cargo fire arm switch (ARMED visible) discharges the extinguishers. [8.80.20]
B. False.
B. False.