CL_604-FIRE_PROTECTION庞巴迪挑战者防火

航空发表于 2010-5-16 10:09:11

CL_604-FIRE_PROTECTION
 
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航空发表于 2010-5-16 10:09:24

Table of Contents For Training Purposes Only May 03 9-i P I LOT T R A I N I N G GU I D E FIRE PROTECTION Introduction .........................................................................................................................9-1 Engine Fire/Overheat Protection.........................................................................................9-2 Description ....................................................................................................................9-2 Components and Operation..........................................................................................9-2 Heat-Sensing Elements ..........................................................................................9-2 Fire Detection Control Units ....................................................................................9-4 Engine Fire Extinguisher Bottles .............................................................................9-4 LH (RH) ENG FIRE PUSH Switch/Lights................................................................9-6 BOTTLE 1 (2) ARMED PUSH TO DISCH Switch/Lights ........................................9-6 Miscellaneous Test Panel .......................................................................................9-6 Auxiliary Power Unit Fire Protection ...................................................................................9-8 Description ....................................................................................................................9-8 Components and Operation..........................................................................................9-8 Heat-Sensing Element ............................................................................................9-8 Fire Detection Control Unit......................................................................................9-9 APU Fire Extinguishing Bottle .................................................................................9-9 APU FIRE PUSH Switch/Light .............................................................................. 9-10 APU BOTTLE ARMED PUSH TO DISCH Switch/Light ........................................ 9-10 Miscellaneous Test Panel ..................................................................................... 9-10 Baggage Compartment Fire Protection ............................................................................ 9-11 Description .................................................................................................................. 9-11 Components and Operation........................................................................................ 9-11 Smoke Detector .................................................................................................... 9-11 Smoke Detector Test ............................................................................................ 9-11 Lavatory Fire Protection.................................................................................................... 9-12 Description .................................................................................................................. 9-12 Components and Operation........................................................................................ 9-12 Smoke Detector .................................................................................................... 9-12 Automatic Fire Extinguisher .................................................................................. 9-12 Galley Overheat Protection (Optional) .............................................................................. 9-13 Description .................................................................................................................. 9-13 Components and Operation........................................................................................ 9-13 Galley Overheat Detector...................................................................................... 9-13 Portable Fire Extinguishers............................................................................................... 9-14 Description .................................................................................................................. 9-14 Components and Operation........................................................................................ 9-14 Flight Compartment Fire Extinguisher................................................................... 9-14 Cabin Fire Extinguisher......................................................................................... 9-14 FIRE PROTECTION 9-ii For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E Main Landing Gear Bay Overheat Detection System ....................................................... 9-15 Description .................................................................................................................. 9-15 Components and Operation........................................................................................ 9-15 Heat-Sensing Element .......................................................................................... 9-15 Overheat Detection Control Unit ........................................................................... 9-16 MLG BAY Overheat Test ...................................................................................... 9-16 Controls and Indicators ..................................................................................................... 9-17 General ....................................................................................................................... 9-17 Engine and APU Fire/Overheat Protection ................................................................. 9-17 Fire Detection and FIREX Monitor Test ...................................................................... 9-18 MLG Bay Overheat Test ............................................................................................. 9-18 Baggage Smoke Detector Test................................................................................... 9-19 EICAS Messages........................................................................................................ 9-20 List of Figures Graphic Title Figure For Training Purposes Only May 03 9-iii P I LOT T R A I N I N G GU I D E FIRE PROTECTION Engine Fire Detection .........................................................................................................9-1 Jet Pipe / Pylon Overheat Sensing Element .......................................................................9-2 Engine and APU Fire Extinguishing System.......................................................................9-3 Glareshield Panels..............................................................................................................9-4 Miscellaneous Test Panel ...................................................................................................9-5 APU Fire Detection .............................................................................................................9-6 Copilot’s Glareshield Panel.................................................................................................9-7 Smoke Detector Test Button...............................................................................................9-8 Main Landing Gear Bay Overheat Heat-Sensing Element .................................................9-9 LDG GEAR CONTROL Panel........................................................................................... 9-10 Glareshield Panels............................................................................................................9-11 Miscellaneous Test Panel ................................................................................................. 9-12 Landing Gear Control Panel ............................................................................................. 9-13 Annunciator Panel.............................................................................................................9-14 9-iv For Training Purposes Only May 03 FIRE PROTECTION P I LOT T R A I N I N G GU I D E Page Intentionally Left Blank FIRE PROTECTION For Training Purposes Only May 03 9-1 P I LOT T R A I N I N G GU I D E CHAPTER 9: FIRE PROTECTION Introduction The fire protection system is divided into two separate subsystems: • Fire and overheat detection system • Fire extinguishing system The fire and overheat detection system includes components which detect fire, overheat, or smoke conditions. Fire and overheat detection is provided in the following areas: • engines • jet pipe and pylons • APU • main landing gear Smoke detection is provided in the baggage compartment and the lavatory. Provisions are also made for an optional galley overheat detection system. The fire extinguishing system delivers an extinguishing agent to protected areas of the aircraft; zone A of the engines and the APU enclosure. The detection and extinguishing systems can be tested and monitored from the cockpit. Portable fire extinguishers are provided in the cockpit and cabin. FIRE PROTECTION 9-2 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E Engine Fire/Overheat Protection Description The engine fire and overheat protection system detects fire and/or overheat conditions in the nacelle, jet pipe, and pylon areas of the engine. The engine fire and overheat protection system is divided in two zones, Zone A and Zone B: • Zone A includes the combustion area of the engine. Overheat/fire detection and extinguishing is provided • Zone B consists of the jet pipe and pylon area. Only overheat/fire detection is provided for this zone Each zone produces a distinctive aural and visual warning when an overheat and/or fire condition is detected. The extinguishing system consists of two fire extinguisher bottles. Either or both bottles can be discharged into the zone A area of the engines. Components and Operation Heat-Sensing Elements Each zone of the engine is protected by a single continuous heat-sensing element (loop) connected to its respective fire detection control unit. Each sensing element is a coaxial cable which has an inner conductor surrounded by an insulator material. The resistance of the insulating material decreases with an increase in temperature. The outer metal sheathing is permanently grounded. The loop resistance information is fed to the corresponding fire detection control unit. The Zone A sensing element is used to detect an overheat/fire condition in the combustion area of the engine. The Zone B sensing element is used to detect an overheat/fire condition in the area where electrical harnesses and plumbing go through the engine pylon. In addition, this sensing element is used to detect an overheat condition in the exhaust nozzle area of the engine. FIRE PROTECTION For Training Purposes Only May 03 9-3 P I LOT T R A I N I N G GU I D E Engine Fire Detection Figure 9-1 Jet Pipe / Pylon Overheat Sensing Element Figure 9-2 * NOTE: Only ZONE A can receive Fire Extinguishant ZONE A P604_09_001 Engine Fire Detection Sensing Elements (Zone A) Aft Mount Ring Fire Zone A (Engine Fire Detection) Fire Zone B (Engine Jet Pipe/ Pylon Overheat) P604_09_004 Pylon Sensing Element Engine Jet Pipe (Exhaust Nozzle) Sensing Element FIRE PROTECTION 9-4 For Training Purposes Only Sept 04 P I LOT T R A I N I N G GU I D E Fire Detection Control Units Each heat-sensing element has its own fire detection control unit which monitors the resistance of its loop. When the electrical resistance decreases to the warning trip point, the fire detection control unit prompts EICAS messages as well as aural and visual warnings to alert the flight crew of a fire and/or overheat condition. For Zone A, the fire warning signal causes the following aural and visual warnings to occur: • L (R) ENG FIRE warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • applicable red LH (RH) FIRE PUSH switch/light illuminates • fire bell sounds For Zone B, the fire warning signal causes the following aural and visual warnings to occur: • L (R) JETPIPE OVHT warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • “JETPIPE OVERHEAT” aural warning sounds The aural warnings can be silenced by pressing either MASTER WARNING switch/ light. The EICAS warning message will remain displayed and ENG FIRE PUSH switch/light will remain illuminated until the fire/overheat condition is corrected. The fire detection control units can discriminate between a true fire/overheat and a short in the heat sensing element. In the event of fire detector loop failure, the applicable L(R) FIRE FAIL or L(R) JETPIPE OVHT FAIL caution EICAS message will be displayed. Engine Fire Extinguisher Bottles Two engine Firex bottles are installed in the aft equipment bay under the APU enclosure. The bottles are charged with Halon 1301 and pressurized with dry nitrogen (600 to 625 psi). Each bottle is equipped with a left and right squib (electrically actuated discharge cartridges), thermal discharge port, pressure gauge and a left and right discharge line. The discharge lines are interconnected to allow discharge of both bottles (if needed) into one engine. The selection of the LH or RH ENG FIRE PUSH switch/light will determine which squibs are fired. The thermal discharge port provides overpressure relief for each Firex bottle. Should the pressure in a Firex bottle exceed 1400 psi, the thermal discharge port will discharge the extinguishing agent in the immediate vicinity of the bottle. FIRE PROTECTION For Training Purposes Only Sept 04 9-5 P I LOT T R A I N I N G GU I D E Engine and APU Fire Extinguishing System Figure 9-3 APU Firex Bottle Thermal Discharge Tube Pressure Switch Connection Discharge Port APU FIREX Discharge Tube APU FIREX Bottle 1 Bottle APU Enclosure VIEW LOOKING FORWARD P604_09_003 2 Bottle Left Engine Right Engine Squib (Dual Firing Elements) Gauge FIRE PROTECTION 9-6 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E LH (RH) ENG FIRE PUSH Switch/Lights The engine fire extinguishing system is controlled by the LH (RH) ENG FIRE PUSH switch/lights. When the LH (RH) ENG FIRE PUSH switch/light is pressed, the following occurs: • the Firex bottle squibs are armed, both BOTTLE 1 (2) ARMED PUSH TO DISCH switch/lights illuminate • engine generator shuts down • fuel shutoff valve (SOV) closes • hydraulic shutoff valve (SOV) closes • bleed air shutoff valve (SOV) closes • associated engine igniters disabled BOTTLE 1 (2) ARMED PUSH TO DISCH Switch/Lights When an illuminated BOTTLE 1(2) ARMED PUSH TO DISCH switch/light is pressed, electrical current fires the squibs in the associated bottle and pressurized Halon is directed into the engine nacelle. The selection of the LH or RH ENG FIRE PUSH switch/light will determine which engine nacelle will receive the extinguishing agent. Glareshield Panels Figure 9-4 Miscellaneous Test Panel The Engine Fire/Overheat Protection System may be tested from the Miscellaneous Test Panel located on the forward pedestal. The FIRE DET WARN/FAIL switch provides the means of testing the fire/overheat detection system by selectively simulating fire/overheat conditions and fail conditions. LH ENG FIRE PUSH GPWS TERR INHB MASTER WARNING BOTTLE 1 ARMED PUSH TO DISCH STALL MASTER CAUTION PULL UP GND PROX ATS N2 SYNC ATS N1 TO FAIL ATS N1 TO FAIL APU FIRE PUSH RH ENG FIRE PUSH GPWS TERR INHB MASTER BOTTLE 2 WARNING ARMED PUSH TO DISCH BOTTLE ARMED PUSH TO DISCH STALL MASTER CAUTION PULL UP GND PROX LH ENG FIRE PUSH Switch/Light BOTTLE 1 ARMED PUSH TO DISCH Switch/Light RH ENG FIRE PUSH Switch/Light BOTTLE 2 ARMED PUSH TO DISCH Switch/Light P604_09_009 FIRE PROTECTION For Training Purposes Only May 03 9-7 P I LOT T R A I N I N G GU I D E Selecting the switch to the WARN position verifies the continuity of all the sensing elements and bottle charge status. Selecting the switch to the FAIL position verifies the ability of the detection control units to discriminate between an actual overheat/fire and false fire (shorted) loops. The FIREX MONITOR 1 (2) (APU) TEST switches provide a means for the flight crew to test the respective squib circuitry continuity. Miscellaneous Test Panel Figure 9-5 TEST TEST TEST TEST TEST WARN TEST FIRE DET 1 2 APU BOTTLE FAIL SPS TEST FIREX MONITOR AURAL WARN TEST LAMP TEST OVSP TEST 1 2 ENG BOTTLE FIREX MONITOR 1 (2) (APU) TEST Switches FIRE DET WARN/FAIL Switch P604_09_008 FIRE PROTECTION 9-8 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E Auxiliary Power Unit Fire Protection Description The APU fire detection system is used to detect an overheat/fire condition within the APU enclosure. The fire detection system continuously monitors the APU. If a fire or overheat condition is detected, the APU will automatically shut down and an EICAS message as well as an aural and visual warning will occur. The APU fire extinguishing system consists of one fire extinguisher bottle. Components and Operation Heat-Sensing Element The APU is protected by one continuous heat-sensing element installed within the APU enclosure. This sensing element is connected to the APU Fire Detection Control Unit. Operation of the sensing element is identical to the engine fire detection system. APU Fire Detection Figure 9-6 APU Enclosure Sensing Element (450°F) APU COMPARTMENT VIEW LOOKING FORWARD P604_09_002 APU Enclosure FIRE PROTECTION For Training Purposes Only May 03 9-9 P I LOT T R A I N I N G GU I D E Fire Detection Control Unit The APU has a dedicated fire detection control unit which continuously monitors the resistance of its own loop. When the electrical resistance decreases to the warning trip point, the unit produces a fire warning signal to the EICAS which causes the following aural and visual warnings to occur: • APU FIRE warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • fire bell sounds • APU FIRE PUSH switch/light illuminates The APU will also shut down automatically. The aural warnings can be silenced by pressing either MASTER WARNING switch/ light. However, the EICAS warning message will remain displayed and APU FIRE PUSH switch/light will remain illuminated until the fire/overheat condition is corrected. As with the engine fire-sensing elements, the APU fire detection control unit can discriminate between an actual fire/overheat and a false fire (i.e., short in the sensing element). In the event of APU fire detector loop failure, the APU FIRE FAIL caution EICAS message will be displayed. APU Fire Extinguishing Bottle APU fire extinguishing is provided by one Firex bottle located adjacent to the APU compartment in the aft equipment bay. The bottle is charged with Halon 1301 and pressurized with dry nitrogen (600 to 625 psi). The APU Firex bottle is equipped with a pressure gauge and a thermal discharge port and is connected by a single tube to the APU compartment. The pressurized extinguishing agent is discharged by a squib with dual firing cartridges, for redundancy. The thermal discharge port provides overpressure relief. Operation is identical to the engine Firex bottles. FIRE PROTECTION 9-10 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E APU FIRE PUSH Switch/Light The APU fire extinguishing system is controlled by the APU FIRE PUSH switch/light. When the APU FIRE PUSH switch/light is pressed, the following occurs: • the bottle squibs are armed, APU BOTTLE ARMED PUSH TO DISCH switch/ light illuminates • APU shuts down (if not already shut down) • APU fuel shutoff valve (SOV) closes • APU negative-G shutoff valve (SOV) closes • APU LCV closes • APU generator shuts down APU BOTTLE ARMED PUSH TO DISCH Switch/Light When an illuminated APU BOTTLE ARMED PUSH TO DISCH switch/light is pressed, electrical current fires the squibs in the APU bottle and pressurized Halon is directed into the APU enclosure. Copilot’s Glareshield Panel Figure 9-7 Miscellaneous Test Panel The APU Fire Protection System is tested simultaneously with the Engine Fire Protection System, via the Miscellaneous Test Panel. Refer to the Engine Fire and Overheat Protection, Miscellaneous Test Panel section for additional information. ATS N1 TO FAIL APU FIRE PUSH RH ENG FIRE PUSH GPWS TERR INHB MASTER BOTTLE 2 WARNING ARMED PUSH TO DISCH BOTTLE ARMED PUSH TO DISCH STALL MASTER CAUTION PULL UP GND PROX APU FIRE PUSH Switch/Light APU BOTTLE ARMED PUSH TO DISCH Switch/Light P604_09_017 FIRE PROTECTION For Training Purposes Only May 03 9-11 P I LOT T R A I N I N G GU I D E Baggage Compartment Fire Protection Description Fire protection for the baggage compartment consists of an electronic smoke detector that interfaces with the EICAS to provide aural and visual warnings. Components and Operation Smoke Detector The aircraft is equipped with a smoke detection system for the baggage compartment. When the smoke density reaches a predetermined level, the smoke detector produces a fire warning signal which causes the following aural and visual warnings to occur: • SMOKE BAGGAGE BAY warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • “SMOKE” aural warning sounds The aural warning can be silenced by pressing either MASTER WARNING switch/ light. However, the EICAS warning message will remain displayed until the unit resets itself. Smoke Detector Test The baggage compartment smoke detector can be tested by the pushing in and holding the SMK DET test button located on the ANNUNCIATOR Panel. Smoke Detector Test Button Figure 9-8 ANNUNCIATOR PANEL P604_09_010 RESET CALL SMK LAV CAB FIRE PROTECTION 9-12 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E Lavatory Fire Protection Description Fire protection for the lavatory consists of an electronic smoke detector that interfaces with the EICAS to provide aural and visual warnings and an independent fire extinguisher that operates automatically in the waste container. Components and Operation Smoke Detector The aircraft is equipped with a smoke detection system in the lavatory. When the smoke density reaches a predetermined level, the smoke detector produces a signal to the EICAS to alert the crew and sounds an aural alarm in the lavatory. The lavatory smoke warning signal causes the following aural and visual warnings to occur: • SMOKE TOILET warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • “SMOKE” aural warning sounds The aural warning can be silenced by pressing either MASTER WARNING switch/ light. However, the EICAS warning message will remain displayed until the unit resets itself. Automatic Fire Extinguisher In the event of a fire in the lavatory waste container, automatic fire extinguishing is provided. The bottle is mounted on a bracket beside the waste container. Once the temperature reaches a predetermined level, two heat-sensitive capsules melt and release Halon 1211 into the waste container. (Individual aircraft installations may vary, consult Completion Center documentation for aircraft-specific information.) FIRE PROTECTION For Training Purposes Only May 03 9-13 P I LOT T R A I N I N G GU I D E Galley Overheat Protection (Optional) Description Overheat protection for the galley consists of an optional overheat detection system that interfaces with the EICAS to provide aural and visual warnings. Components and Operation Galley Overheat Detector When the temperature reaches a predetermined level, the overheat detector provides a signal to the EICAS to alert the crew of a galley overheat. The galley overheat alert signal causes the following aural and visual warnings to occur: • GALLEY OVHT warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • a triple attenson sounds The aural warning can be silenced by pressing either MASTER WARNING switch/ light. However, the EICAS warning message will remain displayed until the unit resets itself. FIRE PROTECTION 9-14 For Training Purposes Only Jan 04 P I LOT T R A I N I N G GU I D E Portable Fire Extinguishers Description Portable Halon 1211 fire extinguishers are provided in both the flight compartment and the cabin to fight a fire occurring inside the aircraft. Halon 1211 is effective in fighting Class A, B and C fires. Components and Operation Flight Compartment Fire Extinguisher The flight compartment fire extinguisher is installed behind the copilot’s seat. Discharging of the Halon is effected by squeezing a spring-loaded lever. IF A FIRE EXTINGUISHER IS TO BE DISCHARGED IN THE FLIGHT COMPARTMENT, ALL FLIGHT CREW MUST WEAR OXYGEN MASKS WITH EMERGENCY SELECTED (100% OXYGEN). CREW EXPOSURE TO HIGH LEVELS OF HALON VAPORS MAY RESULT IN DIZZINESS, IMPAIRED COORDINATION, AND REDUCED MENTAL SHARPNESS. Cabin Fire Extinguisher The cabin fire extinguisher is installed during completion and its location may vary depending on the interior configuration. Consult the aircraft Completion Center manual for the specific location(s). Operation is identical to the Flight Compartment fire extinguisher. WARNING FIRE PROTECTION For Training Purposes Only Sept 04 9-15 P I LOT T R A I N I N G GU I D E Main Landing Gear Bay Overheat Detection System Description The Main Landing Gear (MLG) is protected by a continuous-loop overheat detection system in each wheel bin. The loops are monitored for resistance by the overheat detection control unit which, through EICAS, provides aural and visual warnings of an overheat condition in the main wheel bins. Components and Operation Heat-Sensing Element The main landing gear bay heat-sensing elements (loops) are installed around the top inner surface of the main wheel bins. Operation is identical to the engine and APU fire-sensing elements. The loops are connected to the MLG overheat detection control unit. Main Landing Gear Bay Overheat Heat-Sensing Element Figure 9-9 P604_09_011 Wheel Bins Detection Loop FIRE PROTECTION 9-16 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E Overheat Detection Control Unit The overheat detection control unit continuously monitors the loop resistance of the sensing element (loop). When the electrical resistance decreases to the warning trip point, the unit produces an overheat warning signal to the EICAS, which causes the following aural and visual warnings to occur: • MLG BAY OVHT warning EICAS message is displayed • MASTER WARNING switch/lights illuminate flashing • “GEAR BAY OVERHEAT” aural warning sounds The overheat detection control unit can discriminate between an actual overheat and a false overheat (i.e., short in the sensing element). In the event of main landing gear overheat detector failure, the MLG BAY OVHT FAIL caution EICAS message will be displayed. MLG BAY Overheat Test The MLG BAY overheat detection system can be tested from the LDG GEAR CONTROL panel located on the center forward pedestal. The OVHT test switch is used to verify the continuity of the heat-sensing element by simulating an overheat/fire condition. The FAIL test switch is used to verify the ability of the detection control unit to discriminate between an actual overheat/fire and false overheat/fire (shorted) loop. LDG GEAR CONTROL Panel Figure 9-10 MUTED OFF TEST MLG BAY OVHT TEST OVHT FAIL UP DN LDG GEAR DN LCK REL ANTI-SKID ARMED NOSE STEER ARMED HORN OFF OVHT TEST Switch FAIL TEST Switch P604_09_012 FIRE PROTECTION For Training Purposes Only May 03 9-17 P I LOT T R A I N I N G GU I D E Controls and Indicators General The controls for the various fire protection systems are located on the glareshield; the systems advisory, caution and warning messages are displayed on EICAS, and the test switches are located on the MISCELLANEOUS TEST Panel and LDG GEAR control panel. Engine and APU Fire/Overheat Protection Glareshield Panels Figure 9-11 ATS N1 TO FAIL APU FIRE PUSH RH ENG FIRE PUSH GPWS TERR INHB MASTER BOTTLE 2 WARNING ARMED PUSH TO DISCH BOTTLE ARMED PUSH TO DISCH STALL MASTER CAUTION PULL UP GND PROX LH ENG FIRE PUSH GPWS TERR INHB MASTER WARNING BOTTLE 1 ARMED PUSH TO DISCH STALL MASTER CAUTION PULL UP GND PROX ATS N2 SYNC ATS N1 TO FAIL LH ENGINE FIRE PUSH Switch/Light (guarded, alternate-action) Push: Illuminated arms Firex bottle 1 and 2, BOTTLE 1 (2) ARMED PUSH TO DISCH switch/lights illuminate green closes left fuel shutoff valve (SOV) closes left hydraulic shutoff valve (SOV) shuts down generator 1 closes left 10th- and 14th-stage bleed air shutoff valves (SOVs) disables left engine ignition – Indicates a left engine overheat/fire condition. BOTTLE 1 ARMED PUSH TO DISCH Switch/Light (momentary-action) Push Illuminated – Fires squib to discharge Firex bottle 1 agent into applicable engine. – Indicates Firex bottle 1 is armed for discharge. : Switch/light will extinguish after agent is discharged. NOTE BOTTLE 2 ARMED PUSH TO DISCH Switch/Light (momentary-action) Push Illuminated – Fires squib to discharge Firex bottle 2 agent into the applicable engine. – Indicates Firex bottle 2 is armed for discharge. : Switch/light will extinguish after agent is discharged. NOTE RH ENGINE FIRE PUSH Switch/Light (guarded, alternate-action) Push: arms Firex bottle 1 and 2, BOTTLE 1 (2) ARMED PUSH TO DISCH switch/lights illuminate green closes right fuel shutoff valve (SOV) closes right hydraulic shutoff valve (SOV) shuts down generator 2 closes right 10th- and 14th-stage bleed air shutoff valves (SOVs) disables right engine ignition P604_09_013 APU ENGINE FIRE PUSH Switch/Light (guarded, alternate-action) Push: Illuminated commands an APU shutdown. arms APU Firex bottle, APU BOTTLE ARMED PUSH TO DISCH switch/light illuminates green. closes APU Fuel Shutoff Valve and Negative-G Shutoff Valve closes APU LCV shuts down APU generator – Indicates an APU overheat/fire condition. APU BOTTLE ARMED PUSH TO DISCH Switch/Light (momentary-action) Push Illuminated – Fires squib to discharge APU Firex bottle agent into the APU enclosure. – Indicates APU Firex bottle is armed for discharge. : Switch/light will extinguish after agent is discharged. NOTE LEFT GLARESHIELD RIGHT GLARESHIELD FIRE PROTECTION 9-18 For Training Purposes Only May 03 P I LOT T R A I N I N G GU I D E Fire Detection and FIREX Monitor Test Miscellaneous Test Panel Figure 9-12 MLG Bay Overheat Test Landing Gear Control Panel Figure 9-13 TEST TEST TEST TEST TEST WARN TEST FIRE DET 1 2 APU BOTTLE FAIL L R G SWITCH SPS TEST FIREX MONITOR AURAL WARN TEST LAMP TEST OVSP TEST 1 2 1 2 1 2 ENG BOTTLE P604_09_018 FIREX MONITOR TEST Switches (spring-loaded to normal position) TEST – Tests applicable Firex bottle squib circuit continuity. FIRE DET Switch (spring-loaded to OFF) WARN FAIL – Tests engine (both engine and jet pipe/pylon) and APU fire detection loops for continuity by simulating an overheat/fire condition, verifies engine and APU bottle charge. – Tests engine (both engine and jet pipe/pylon) and APU fire detection units’ ability to discriminate between a shorted loop and an actual overheat/fire. MUTED OFF TEST MLG BAY OVHT TEST OVHT FAIL UP DN LDG GEAR DN LCK REL ANTI-SKID ARMED NOSE STEER ARMED HORN OFF P604_09_014 MLG BAY OVHT TEST Switch (spring-loaded to normal position) OVHT – Tests MLG Bay overheat loop continuity by simulating an overheat condition in the main landing gear bay. MLG BAY OVHT Warning FAIL TEST Switch (spring-loaded to normal position) FAIL – Tests MLG Bay overheat detection control units’ ability to discriminate between a shorted loop and an actual overheat. FIRE PROTECTION For Training Purposes Only May 03 9-19 P I LOT T R A I N I N G GU I D E Baggage Smoke Detector Test Annunciator Panel Figure 9-14 RESET CALL SMK LAV CAB P604_09_015 SMK DET Switch (momentary-action) Push – Tests the baggage compartment smoke detector unit. FIRE PROTECTION 9-20 For Training Purposes Only Jan 04 P I LOT T R A I N I N G GU I D E EICAS Messages The fire and overheat protection system messages are shown on the EICAS Primary and Status pages. The fire and overheat protection system messages and aural warnings are listed below. A brief explanation of each message is provided. MESSAGE MEANING AURAL WARNING (IF ANY) APU FIRE Fire detected in the APU enclosure. FIRE BELL L ENGINE FIRE Fire detected in the respective engine nacelle. FIRE BELL R ENGINE FIRE L JETPIPE OVHT Overheat detected in the respective jetpipe and/or pylon area. “JETPIPE OVERR JETPIPE OVHT HEAT” GALLEY OVHT Galley overheat detected (if galley overheat detector is installed). TRIPLE ATTENSON SMOKE BAGGAGE BAY Smoke detected in the baggage compartment. “SMOKE” SMOKE TOILET Smoke detected in the lavatory area. “SMOKE” APU BOTTLE LO APU firex bottle pressure is low. APU FIRE FAIL APU fire detection loop is failed (shorted out). APU NEG-G SOV APU negative-G shutoff valve is open after actuation of the APU FIRE PUSH switch/light, or the negative-G shutoff valve position does not match the APU PWR FUEL switch/light position within 5 seconds. APU SOV APU fuel shutoff valve is open after actuation of the APU FIRE PUSH switch/light, or the fuel shutoff valve position does not match the APU PWR FUEL switch/light position within 5 seconds. ENG BOTTLE 1 LO Respective engine firex bottle pressure is low. ENG BOTTLE 2 LO L ENG SOV Respective fuel shutoff valve is not closed after actuation of the ENG FIRE PUSH switch/ R ENG SOV light. L FIRE FAIL Respective fire detection loop is failed (shorted out). R FIRE FAIL HYD SOV 1 Hydraulic shutoff valve is not closed after actuation of the respective ENG FIRE PUSH HYD SOV 2 switch/light. L JETPIPE OVHT FAIL The respective jetpipe/pylon overheat detection loop is failed (shorted out). R JETPIPE OVHT FAIL APU SOV CLSD APU fuel shutoff and negative-G shutoff valves have closed after actuation of the APU FIRE PUSH switch/light. APU SQUIB 1 OK Respective squib has passed its self-test. APU SQUIB 2 OK L ENG SOV CLSD Respective engine fuel shutoff valve has closed after actuation of respective ENG FIRE R ENG SOV CLSD PUSH switch/light. L ENG SQUIB 1 OK Respective squib has passed its self-test. L ENG SQUIB 2 OK R ENG SQUIB 1 OK R ENG SQUIB 2 OK HYD SOV 1 CLSD Respective hydraulic shutoff valve has closed after actuation of the respective ENG FIRE HYD SOV 2 CLSD PUSH switch/light. EICAS Messages Table 9-1

shineixueche 发表于 2010-10-25 22:43:01

庞巴迪挑战者的资料好多啊。

dul 发表于 2011-2-11 13:17:10

yogeyoi

一节一节的下，好费劲啊

bocome 发表于 2011-7-31 11:21:32

庞巴迪挑战者防火

autofannuaa 发表于 2011-12-7 14:12:29

偶然经过，学习一下

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CL_604-FIRE_PROTECTION庞巴迪挑战者防火

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