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The FIDEEX system includes fire detector assemblies, sensing elements, smoke detectors, fire extinguishing containers and a FIDEEX control unit.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
FIRE PROTECTION
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:
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MASTER warning lights (2).
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Aural warning.
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EICAS messages.
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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. Indication and test function is provided in the flight compartment.
FIRE AGENT DISCHARGE INDICATION
The fire extinguisher bottle is fitted with a low pressure switch. The switch provides an annunciation in the flight compartment when pressure drops below a predetermined pressure setting.
SMOKE DETECTION
The FIDEEX system can provide smoke detection capability for the baggage compartment, forward and aft lavatories, up to four cabin closets and avionics bay.
PORTABLE FIRE EXTINGUISHERS
Portable fire extinguishers are located throughout the airplane. One halon type fire extinguisher is installed in the flight crew compartment. Refer to the EMERGENCY EQUIPMENT Chapter for additional information on the portable fire extinguishers.
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
SYSTEM OVERVIEW SCHEMATIC
1
1 Fire Control Handles.
2 Master WARNING/CAUTION LIGHTS. 2
3 4 5 PRIMARY EICAS Page Displays, Warnings, Cautions, Advisory and Status Messages. Avionics Bay (2). Avionics Rack. ROLL SEL WARNING CAUTION TOTAL FUEL (LBS) 41550 1.541.54 73.373.3 789789 14600 1460010000 2350 ND STAB NU RUDDERNL LWD RWD NR TRIMS 7.2 N2 FF (PPH) OIL TEMP OIL PRESS 93.4 5750 115 81 93.4 5750 115 81 EPR N1 ITT AIL 1.651.65 CRZ SYNC APU FIRE R ENG FIRE L ENG FIRE 3 WARNING CAUTION ROLL SEL
6 Left Main Wheel Well Overheat Detection. IAC
7 Right Main Wheel Well Overheat Detection. 6 4 DAU 5 7
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