Systems - Fire Protection Flashcards
The APU fire protection system automatically shuts down the APU and extinguishes the fire (FM 8.80.10.1)
On the ground.
A warning horn heard on the ground may be an indication of (FM 8.80.10.1)
An APU fire.
How many fire extinguishers are associated with the avionics smoke detection system? (FM 8.80.10.2)
None
Placing the BLOWER and EXTRACT switches in OVRD causes the avionics ventilation system to go into the ____ configuration. (FM 8.80.20.9)
Smoke
The AVIONICS SMOKE ECAM is associated with what fault lights? (FM 8.80.10.2)
GEN 1 LINE SMOKE, BLOWER & EXTRACT FAULT lights.
How many fuel pumps are operating in the avionics smoke configuration? (FM 8.60.20.5)
One pump in each wing tank.
The SMOKE light indicates (FM 8.80.20.9)
Smoke is detected in avionics ventilation system.
The cargo compartments on the 320 are protected by (FM 8.80.10.3)
Two fire bottles.
How does the cargo fire extinguishing system on the 319 differ from the 320? (FM 8.80.10.3)
The 319 (and 320 N4902U and N4901U) have one fire bottle that can be discharged into either the forward or aft cargo compartment.
In the 320, the second cargo fire extinguisher bottle can be discharged (FM 8.80.20.7)
Only to the same cargo compartment as the first.
When pressed, the 320 CARGO SMOKE test button (FM 8.80.20.7)
Tests SMOKE lights twice with associated ECAM.
When does the DISCH AGENT 2 light illuminate on the 320 CARGO SMOKE panel? (FM 8.80.20.7)
60 minutes after AGENT 1 is discharged.
What occurs when the ENG 1 FIRE switch is released out? (FM 8.80.20.1)
Both fire extinguisher agents arm but do not discharge.
The engine fire detection system consists of a dual loop system. What occurs when one of the loops fail? (FM 8.80.10.3)
The remaining loop can detect a fire and generate a fire warning.
An engine fire warning appears when (FM 8.80.10.3)
Both loops break within 5 seconds of each other.
In the event of an engine fire, the associated ENG FIRE switch and ENG START and IGN panel FIRE lights remain illuminated until the (FM 8.80.20.1)
Respective fire warning is no longer active.
What occurs if the engines are running and the ENG 1 FIRE switch is released out? (FM 8.80.20.1)
Engine 1 will shutdown.
What occurs to the pneumatic system if the ENG FIRE switch is released out? (FM 8.80.20.1)
Closes both the engine bleed valve and the pack flow control valve.
Each lavatory is equipped with what type of fire detection and extinguishing equipment? (FM 8.80.10.4)
An automatic waste bin extinguisher and a smoke detector.
How is the lavatory trash bin fire extinguishing system activated? (FM 8.80.10.4)
Completely automatic.
When smoke is detected in a lavatory a chime sounds (FM 8.80.10.4)
Through all flight attendant loudspeakers.
