曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 100 I ┃I REV 34 ┃
┃ A~7-~'M" A321 ┃ GENERAL ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━━┻━━━━━┛
Aircraft Fire Protection Systems are comprised of :
- Fire and overheat detection and extinguishing systems for the
~ Engines
~ APU
- Smoke detection and extinguishing systems for the :
~ Cargo compartments
~ Lavatories
- Smoke detection for the :
~ Avionic bay
- Portable fire extinguishers for the :
~ Flight compartment
~ Passenger cabin
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I ~-~ A318 ┃FIRE PROTECTION ┃1.26.20 P 1 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 005 I ┃I REV 24 ┃
┃ A~7-~'M" A321 ┃ ENG AND APU ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━━┻━━━━━┛
DETECTION
The engines and the APU each have a fire and overheat detection system consisting of :
- Two identical gas detection loops (A and B) mounted in parallel.
- A Fire Detection Unit (FDU).
The gas detection loops consist of :
- Three sensing elements for each engine, one in the pylon nacelle, one in the engine core
and one in the engine fan section.
- One sensing element in the APU compartment.
When a sensing element is subjected to heat, it sends a signal to the fire detection unit.
As soon as loops A and B detect temperature at a preset level, they trigger the fire warning
system.
A fault in one loop (break or loss of electrical supply) does not affect the warning system.
The unaffected loop still protects the aircraft.
If the system detects an APU fire while the aircraft is on the ground, it shuts down the APU
automatically and discharges extinguishing agent.
RASTER
WARNING
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.26.20 P 2 ┃
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(54)
