This quiz titled 'A320 FIRE PROTECTION' assesses knowledge on fire safety protocols specific to the A320 aircraft. It covers components of the fire triangle, automatic fire extinguishing systems, and procedures for APU fires, enhancing safety and maintenance skills.
APU , and lavatory waste bins.
APU, lavatory waste bins and avionics bay .
APU , aft cargo . forward cargo, lavatory waste bins and avionics bay .
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On the ground and in flight .
On the ground
Only when selected to automatic by ground personel.
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No, APU fire indications are only present in the cockpit .
Yes , the flames .
Yes , the external fire warning horn will sound and the APU red fire light will illuminate.
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For as long as the fire warning is present.
Until the crew pushes and release the guarded red APU FIRE push button.
Until the crew pushes the red MASTER WARNING push button.
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Until the crew pushes the red MASTER WARN push button .
Until the crew pushes and releases the guarded red APU FIRE push button.
Both A and B
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Yes , the APU will initiate an auto shutdown and discharge the extinguishing agent.
No, but the APU will initiate an auto shutdown.
None of the above
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A two channel SDCU located in the APU compartment.
Two parallel fire detection loops.
One fire detection loop .
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One
Two
One cylinder shared with the aft cargo compartment.
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There is no difference.
While on battery power , only the red APU FIRE and AGENT/DISC push button will illuminate.
It is not posible to test the APU fire protection while on battery power.
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Two fire detection loops .
Two smoke detectors and two fire detection loops.
A single fire detection loop.
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Each engine has it´s own dedicated fire extinguisher and has the capability to share the other engine´s cylinder
Each engine has two fire extinguishers.
None of the above .
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Only after the fire warning no longer exist .
When the crew pushes and releases the guarded red ENG FIRE push button .
When the crew pushes the red MASTER WARN push button.
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When the crew pushes the red MASTER WARN push button.
Only after the fire warning no longer exist.
Only after the crew selects the adjacent ENG MASTER switch to off .
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The Aircraft's Engine Fire Detection System
The Cargo Smoke Detection and Fire Suppression System
The APU Fire Detection and Extinguishing System
The Hydraulic Fire Protection System
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E/WD red 1 (2) ENG FIRE warning , lower ECAM engine page , red FIRE push button and AGENT SQUIB/DISC.
Lower ECAM engine page , pedestal mounted red FIRE annunciator , red ENG FIRE push button and the AGENT SQUIB/DISC lights illuminate.
The CRC and red MASTER WARNING light indicate a good engine fire test .
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A smoke detector , smoke detection unit and one halon cylinder .
A smoke detector and smoke detection control unit .
A smoke detector , heat detector , smoke detection control unit and one halon cylinder .
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A satisfactory test of the avionics compartment smoke detection control unit :
Smoke has been detected in the avionics compartment ventilation duct :
A fire has been detected in the avionics compartment.
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The BLOWER and EXTRACT push button FAULT lighs will be illuminated.
Only the BLOWER FAULT light will be illuminated .
Only the EXTRACT FAULT light will be illuminated.
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The avionics fire bottle automatically discharge
The cargo fire bottle automatically fires .
The aircraft will be in the Emergency Electrical Configuration.
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Two smoke detectors and one smoke detection control unit .
One smoke detector and one smoke detector unit.
One smoke detector and 4 lavatory waste bins , an automatically discharging fire extinguisher.
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Warnings will be generated only on the flight deck
Warnings will be generated only in the cabin.
Warnings will be generated in the cockpit and in the cabin.
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A dual loop smoke detector .
Four smoke detectors and two channel smoke detection control unit .
One smoke detector , one smoke detection control unit and two automatically discharging fire extinguishers.
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Only an ECAM message will be generated.
Only a MASTER WARN and CRC will be generated
A MASTER WARN CRC and an ECAM message will be generated .
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Extinguishing is automatic.
Extinguishing is automatic only while on the ground .
The crew must depress the appropriate DISCH switch
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Two complete cycles with associated warnings.
Not needed as this system self test during the first engine start.
One complete cycle with associated warnings .
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This is normal indication , the red APU thermal plug only appears if the APU Halon cylinder is Low.
An APU fire agent thermal discharge has occurred .
An external fire discharge has been activated .
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