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┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃l FIRE ENGTANDIAPU ┃SEQ 001 1 ┃I REV 26 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
EXTINGUISHING
Each engine has two extinguisher bottles equipped with electrically operated squibs to
discharge their contents. Each squib has a dual electric supply. The flight crew controls the
discharge from the ENG FIRE panel in the cockpit.
The APU has one fire extinguisher bottle that has an electrically operated squib to
discharge its agent. The flight crew controls the discharge from the APU FIRE panel in the
cockpit. This bottle also discharges automatically if there is an APU fire when the aircraft
is on the ground.
FIRE WARNINGS AND LOOP CAUTIONS
Fire detection units process all the warnings and cautions originating in the sensing
elements :
- The fire warning appears in case of :
~ a fire signal from both loop A and B or,
~ a fire signal from one loop when the other is faulty, or
~ breaks in both loops occuring within 5 seconds of each other (flame effect), or
~ a test performed on the control panel.
- The loop-fault cautions appear if :
one loop is faulty or,
both loops are faulty or,
the fire detection unit fails
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃FIRE PROTECTION ┃1.26.20 P 3 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 100 I ┃I REV 33 ┃
┃ A~7-~'M" A321 ┃ ENG AND APU ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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AIRBUS A320 Flight Crew Operating Manual3(55)
