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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. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier_Global_000-Fire_Protection
