DESCRIPTION
General 09−10−1
Flight Compartment Fire Warning 09−10−2
Fire Detecting System 09−10−2
Wheel Well Overheat Warning 09−10−2
Fire Agent Discharge Indication 09−10−2
Smoke Detection 09−10−2
Portable Fire Extinguishers 09−10−2
System Overview Schematic 09−10−3
Fire Control Handles 09−10−4
Engine Fire Control Handle 09−10−5
APU Fire Control Handle 09−10−5
Synoptic Pages 09−10−6
Fire Extinguisher assembly 09−10−7
Fire Extinguisher Discharge Squibs 09−10−7
Fire Extinguisher Gauges 09−10−8
Fire Zone Discharge Schematic 09−10−8
FIDEEX Control Unit 09−10−9
Main Engine Fire Detection 09−10−10
Main Engine FIDEEX Control 09−10−12
Engine FIDEEX Control Schematic 09−10−13
APU Compartment Fire Detection 09−10−14
APU FIDEEX Control Schematic 09−10−15
APU FIDEEX/FADEC Interface 09−10−16
APU FIDEEX/FADEC Control Schematic 09−10−16
Main Wheel Well (MWW) Overheat Detection 09−10−17
Smoke Detection 09−10−18
Pilot Initiated Test 09−10−20
EICAS Messages 09−10−22
EMS CIRCUIT PROTECTION
CB − Fire System 09−20−1
FIRE PROTECTION
TABLE OF CONTENTS
CHAPTER 9
09−00−1
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
09−00−1
Page
TABLE OF CONTENTS
FIRE PROTECTION
TABLE OF CONTENTS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
09−00−2
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL
A Fire Detection and Extinguishing (FIDEEX) system with fault discrimination is installed with fire
detectors located in each engine nacelle and in the APU compartment.
The FIDEEX system interfaces with numerous airplane equipment and provides the following
capabilities:
· Monitor zones for fire/overheat/smoke events and FIDEEX system health and status.
· Automatic detection and reporting of fire events for each of the two power plants and the
Auxiliary Power Unit (APU).
· Fire extinguishing for each of the power plant and APU upon receipt of pilot initiated arming
and discharging commands.
· Automatic detection and reporting of overheat events for the two Main Wheel Wells (MWWs).
· Automatic detection and reporting of smoke events for each of the lavatories (fwd/aft),
baggage compartment, up to four cabin closets (requires installation of optional smoke
detectors) and avionics bay.
BAGGAGE COMPARTMENT
SMOKE DETECTION
(OPTIONAL)
MAIN LANDING GEAR
OVERHEAT DETECTION
APU FIRE DETECTION/
EXTINGUISHING SYSTEM
POWER PLANT FIRE
DETECTION/EXTINGUISHING
AFT CLOSET
OPTIONAL
LAVATORY SMOKE
DETECTION
(OPTIONAL)
FORWARD LEFT AND RIGHT
CLOSET (OPTIONAL SMOKE
DETECTION)
AFT
LAVATORY
(OPTIONAL)
AVIONICS BAY
SMOKE DETECTION
FGF0910_001a
AVIONICS RACK
SMOKE DETECTION
The FIDEEX system includes fire detector assemblies, sensing elements, smoke detectors, fire
extinguishing containers and a FIDEEX control unit.
FIRE PROTECTION
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
09−10−1
FLIGHT COMPARTMENT FIRE WARNING
The fire protection system provides the means to detect and extinguish a fire in the engine nacelles
and in the Auxiliary Power Unit (APU) compartment. Engine/APU fire warning is provided by:
· MASTER warning lights (2).
· Aural warning.
· EICAS messages.
· Three red warning lights (one for each engine nacelle and one for the APU compartment),
installed in the flight compartment fire handles.
Both the detection systems and extinguishing systems permit testing and/or monitoring for system
faults from the flight compartment. A fire warning and extinguisher pre−flight test of the system is
provided in the flight compartment.
FIRE DETECTING SYSTEM
An overheat detection system, installed in the pylon area for each engine, permits the flight crew to
monitor any overheat condition in this area. A similar overheat detection system is installed in each
main landing gear wheel well.
WHEEL WELL OVERHEAT WARNING
An element in the wheel well area warns of an overheat condition in either of the main wheel wells.
　
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