Fire Protection Flashcards

1
Q

What areas have fire extinguishing protection?

A
  • cargo compartments
  • engines
  • APU
  • lavatories
  • cockpit and cabin via portable extinguishers
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2
Q

How many fire sensing elements on the aircraft?

A

‐ Three or four (as installed) engine fire sensing elements, in the pylon nacelle, in the engine core, and in the engine fan section

‐ One fire sensing element in the APU compartment

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3
Q

How many fire extinguishing bottles?

A
  • 4 engine bottles (2 per engine)
  • 1 APU bottle
  • 1 or 2 cargo compartment bottles
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4
Q

What happens when ENG 1(2) FIRE pb is pressed?

A
‐ Silences the aural fire warning 
‐ Arms the fire extinguisher squibs 
‐ Closes the low-pressure fuel valve 
‐ Closes the hydraulic fire shut off valve 
‐ Closes the engine bleed valve 
‐ Closes the pack flow control valve 
‐ Cuts off the FADEC power supply 
‐ Deactivates the IDG
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5
Q

When the APU FIRE pb is pressed

A

‐ Shuts down the APU
‐ Silences the aural warning
‐ Arms the squib on the APU fire extinguisher
‐ Closes the low-pressure fuel valve
‐ Shuts off the APU fuel pump
‐ Closes the APU bleed valve and X bleed valve
- deactivate the APU gen

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6
Q

What happens when Smoke is detected in the avionics?

A

When smoke is detected for more than 5 s:
‐ The Single Chime (SC) sounds
‐ The MASTER CAUTION lights flash
‐ The ECAM AVIONICS SMOKE alert triggers
‐ SMOKE light of the GEN 1 LINE pb-sw comes on
‐ FAULT lights of the BLOWER pb-sw and the EXTRACT pb-sw come on

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7
Q

How many smoke detectors in the cargo compartments?

A
  • Two smoke detectors that are in the forward cargo compartment ceiling panel
  • Four smoke detectors that are in the aft cargo compartment ceiling panel
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8
Q

When is the 2nd bottle discharge in the cargo compartment?

A
  • 60 min after the discharge of AGENT 1, the DISCH AGENT 2 light comes on to indicate that the flight crew has to discharge AGENT 2
  • A flow metering system controls the discharge of bottle 2 over 90 mins
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9
Q

How is SMOKE detected in the Avionics Bay?

A

Via one smoke detector in the extraction duct of the avionics ventilation system

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