Fire Protection Flashcards
During preflight, you notice the BOTTLE DISCH APU message displayed on EICAS. What does this mean?
• The APU fire bottle pressure is low.
• This is a normal indication prior to APU start.
• The APU fire bottle squibs are inoperative.
• An APU Fire has been fought using one of the 2 APU fire bottles.
• The APU fire bottle pressure is low.
During preflight, you notice the BOTTLE 1 DISCH ENG message displayed on EICAS. What does this mean?
• Ground maintenance is servicing fire bottle 1.
• The fire bottle squibs are inoperative.
• Fire bottle 1 has discharged or pressure is low.
• This is a normal indication prior to APU start.
• Fire bottle 1 has discharged or pressure is low.
What action should you take if the fire switch remains locked after a fire is detected?
• Push the fire override switch, then pull the fire switch.
• Pull fire switch to override the lock.
• Rotate the fire switch.
• Wait until the fire light extinguish
• Push the fire override switch, then pull the fire switch.
What happens when an APU fire is detected on the ground and the engines are running?
• The APU shuts down automatically but the fire bottle must be manually discharged.
• The APU does NOT shut down automatically but the fire bottle discharges automatically.
• The APU does NOT shut down automatically and the fire bottle must be discharged manually.
• The APU shuts down automatically and the fire bottle automatically discharges after a 15 second delay.
• The APU shuts down automatically and the fire bottle automatically discharges after a 15 second delay.
On the ground, if the FWD CARGO FIRE ARM switch is armed, what happens when the CARGO FIRE DISCH switch is pushed?
• All 5 fire bottles arm and airflow around the cargo compartment is reduced.
• All 7 bottles discharge into the forward cargo compartment.
• One of the metered bottles discharges into the forward cargo compartment.
• Two rapid dump bottles and one metered bottle discharge into the forward cargo compartment.
• Two rapid dump bottles and one metered bottle discharge into the forward cargo compartment.
What happens when an APU fire is detected on the ground and the engines are shut down?
• The APU shuts down automatically but the fire bottle must be discharged manually.
• The APU shuts down automatically and the fire bottle discharges automatically.
• The APU does NOT shut down automatically but the fire bottle discharges automatically.
• The APU does NOT shut down automatically and the fire bottle must be discharged manually.
• The APU shuts down automatically and the fire bottle discharges automatically.
Which of the following statements is TRUE concerning a wheel well fire?
• There is NO built-in fire extinguishing system for the wheel well.
• Fires are detected by two smoke detection units in the wheel well.
• Two fire bottles protect the wheel well from fires.
• There is only a single loop available for wheel well fire detection.
• There is NO built-in fire extinguishing system for the wheel well.
Which of the following statements is TRUE concerning a lavatory fire?
A. The EICAS message SMOKE LAVATORY is displayed.
B. The lavatory extinguisher activates when the smoke detector senses smoke.
C. If smoke is detected, an aural alert sounds and the respective lavatory call
light illuminates.
D. Both A and C are correct.
D. Both A and C are correct.
When the engine fire switch is pulled out, rotating the switch in either direction discharges both extinguisher bottles into the associated engine.
A. True.
B. False.
B. False.
When inflight, and a fire is sensed, the CARGO FIRE protection system automatically discharges two bottles immediately. The remaining metered bottles discharge ___ minutes later.
• 5
• 20
• 10
• 15
• 15
The FIRE CARGO FWD/AFT warning message is likely to remain after the fire is extinguished due to smoke in the cargo compartment.
A. True.
B. False.
A. True.
When the airplane is on the ground with both engines shut down, a fire signal from either APU fire loop will cause:
• An EICAS message DET FIRE APU to display.
• The APU to shutdown after a 90 second cool down period.
• The APU to automatically shutdown and the fire bottle to discharge.
• The OVERHEAT APU EICAS message to display.
• The APU to automatically shutdown and the fire bottle to discharge.
In regards to the hydraulic system, pulling an engine fire handle:
A. Will shut off fluid to the associated pump.
B. Depressurizes the engine driven pump.
C. Removes power from the thrust reverser isolation valve.
D. All of the above
D. All of the above
Failure of a single channel of an engine fire detection assembly will:
• Be indicated by a DET FIRE ENG LIR EICAS message.
• Cause loss of the OVERHEAT protection for the associated engine.
• Cause the system to switch to a single channel operation.
• Automatically unlock the fire switch.
• Cause the system to switch to a single channel operation.
Placing the FWD cargo fire arm switch in the ARM position will:
• Put the equipment cooling system into the OVERRIDE mode.
• Shut down the lav galley vent fan.
• Shut down the bulk cargo ventilation system.
• Command the air conditioning packs to provide maximum flow.
• Put the equipment cooling system into the OVERRIDE mode.