1.- In the event a lavatory smoke detector detects smoke: A.- Warnings will be generated only in the cockpit. B.- Warnings will be generated only on the flight deck. C.- Warnings will be generated in the cockpit and in the cabin.
2.- What systems are affected when the guarded red ENGINE FIRE push button
is pushed and released? A.- The Master Warning and the chime will be canceled and the AGENT pb's will
be armed. B.- All fluids, pneumatics and electrics relating to that engine are shut off. C.- Both are correct.
3.- Will an APU fire test shut sown the APU? A.- Yes. B.- No.
4.- In the event and aft cargo compartment smoke detector detects smoke: A.- Extinguishing is automatic. B.- Extinguishing is automatic only while on the ground. C.- The crew must depress the appropriate DISCH switch.
5.- The APU provides for automatic fire extinguishing: A.- On the ground only. B.- On the ground and in flight. C.- Only when selected to automatic by ground personnel.
6.- If you perform the APU FIRE TEST with only DC power available, you get
the MASTER WARN on the ECAM. A.- True. B.- False.
7.- Engine fire loops are installed in the: A.- Pylon nacelle. B.- Core. C.- Fan. D.- All the above.
8.- When the aircraft is on the ground and the APU is started on bettery power
only, is fire protection available? A.- Yes, the APU will initiate an auto shutdown and discharge the extinguishing
agent. B.- No, but the APU will initiate an auto shutdown. C.- No, automatic fire protection is only available if AC power is available.
9.- How many fire extinguishing bottles are available for fighting an APU fire? A.- One. B.- Two. C.- One cylinder shared with the aft cargo compartment. D.- Two cylinders shared with the aft cargo compartment.
10.- APU fire detection is accomplished by: A.- A two channel SDCU located in the APU compartment. B.- Two parallel fire detection loops. C.- One fire detection loop. D.- A three channel SDCU located in the APU compartment.
11.- After an APU fire has been detected how long will the chime continue to
sound? A.- Until the crew pushes the red MASTER WARN push button. B.- Until the crew pushes and releases the guarded red APU FIRE push button. C.- Both are correct.
12.- STATUS page: INOP SYS indicates ENG 1 LOOP B. A.- One fire detection loop has failed. Fire detection for both engines is not
available. B.- One detection loop for engine 1 has failed. Fire detection for both engines is
still available. C.- One fire detection loop of engine 1 has failed. Fire detection for engine 1 is
inoperative. D.- Both fire detection loops of engine 1 have failed. Fire detection for engine 1 is
inoperative.
13.- The aft cargo compartment smoke detection system consists of: A.- A dual loop smoke detector. B.- Four smoke detectors and a two channel smoke detection control unit. C.- One smoke detector, one smoke detection control unit and two automatically
discharging fire extinguishers. D.- Three smoke detectors, one smoke detection control unit and two
automatically discharging fire extinguishers.
14.- How long will the red APU FIRE pb on the overhead be illuminated? A.- Until the crew pushes and releases the guarded red APU FIRE push button. B.- For as long as the fire warning is present. C.- Until the crew pushes the red MASTER WARN push button.
15.- The A-320 has dual fire detector loops to ensure that a fault in one fire loop
will not affect fire detection capabilities. A.- True. B.- False.
16.- If there is an APU fire in flight the APU: A.- Will automatically shut down and the fire bottle will discharge. B.- Must be shut down manually and the agent manually descharged. C.- Must be shut down manually but the fire bottle will discharge automatically.
17.- The engine extinguishing agent switch is armed when: A.- The DISCH light is on. B.- The engine fire switch illuminates. C.- The engine fire switch is released out.
18.- Which of the following have automatic fire extinguishing systems? A.- APU on ground and lavatory waste bins. B.- APU on ground, lavatory waste bins and avionics bay. C.- APU on ground, aft cargo, forward cargo, lavatory waste bins and avionics
bay. D.- Lavatory waste bins.
19.- Are there any warnings to alert ground personnel when there is a fire in the
APU compartment? A.- YES, but only if previously selected to automatic by the ground personnel. B.- No, APU fire indications are only present in the cockpit. C.- Yes, the flames. D.- Yes, the external fire warning horn will sound and the APU red fire light will
illuminate.
20.- A DISH light on either the engine or APU fire agent witches indicates: A.- The APU or engine FIRE switch has been pushed. B.- The extinguisher bottle has been discharged. C.- A fault has occurred in the respective fire bottle.
21.- If a break in both engine fire loops occurs within __________ seconds of
each other a __________ will occur. A.- 10 sec. a FIRE warning. B.- 5 sec. a FIRE DET FAULT message on ECAM. C.- 5 sec. a FIRE warning.
22.- The avionics compartment is the only area where there is no fire
extinguishing system installed. A.- True. B.- False.
23.- When the APU FIRE SWITCH is released out: A.- Shuts down the APU. B.- Arms the squib on the APU fire extinguisher. C.- The APU bleed and cross bleed valves are closed. D.- All the above.
24.- Can the APU FIRE test be performe during bettery power only? A.- Yes. B.- No.
25.- With reference to cargo compartment fire extinguishing, which statement is
true? A.- There are two fire bottles, one fr the FWD compartment and one for the AFT. B.- There is only one fire bottle, pressing either DISCH push button discharges it
into both compartements. C.- There is only one fire bottle, when it is discharged both amber DISCH lights
come on. D.- There are two fire bottles, when the DISCH pushbutton is pressed, they are
both discharged into the appropriate compartment.
26.- If an engine fire is detected, when will the guarded red ENG FIRE push
button light extinguish? A.- Only after the fire warning no longer exists. B.- When the crew pushes and releases the guarded red ENGINE FIRE
pushbutton. C.- When the crew pushes the red MASTER WARN pushbutton. D.- When the crew pushes the red MASTER WARN pushbutton and then
releases the guarded ENGINE FIRE pushbutton.
27.- How many halon fire extinguishing cylinders are per engine? A.- Each engine has two fire extinguishers. B.- Each engine has it\'s own dedicated fire extinguisher and has the capability to
share the other engine\'s cylinder. C.- Each engine has it's own dedicated fire extinguisher and has the capability to
share one centrally located halon cylinder. D.- Each engine has one fire extinguisher.
28.- In the event that the aft cargo compartment smoke detector, detects smoke: A.- Only an ECAM message will be generated. B.- Only a MASTER WARN and a CRC will be generated. C.- A MASTER WARN, CRC and an ECAM message will be generated. D.- A CRC and an ECAM message will be generated.
29.- How does the APU fire test on battery power differ from the APU fire test
with all busses powered? A.- There is no difference. B.- While on battery power, only the red APU FIRE and AGENT/DISC push
button will illuminate. C.- It is not possible to test the APU fire protection while on battery power.
30.- Each lavatory is equipped with: A.- Two smoke detectors and one smoke detection control unit. B.- One smoke detector and one smoke detection control unit. C.- One smoke detector, and for lavatory waste bins, an automatically
discharging fire extinguisher. D.- Two smoke detectors and two automatically discharging fire extinguishers.
31.- Each engine nacelle and pylon area is equipped with: A.- Two fire detection loops. B.- A single fire detection loop. C.- Two smoke detectors and two fire detection loops. D.- A single fire detection loop and a single smoke detector.
32.- In addition to the CRC and red MASTER WARN light, a good engine fire test
will display which of the following (AC power available)? A.- The CRC and red MASTER WARN light indicate a positive engine fire test. B.- Lower ECAM engine page, pedestal mounted red FIRE annunciator, red ENG
FIRE push button and the AGENT SWUIB/DISC lights illuminate. C.- E/WD red 1 (2) ENG FIRE WARNING, lower ECAM engine page, red FIRE
annunciator, red ENG FIRE push button, and AGENT SQUIB/DISC.
33.- If an APU fire is detected on the ground, the APU shuts down automatically
and the agent is discharged _____ after the warning is activated. A.- Immediately. B.- 1 seconds. C.- 3 seconds. D.- 6 seconds.
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