ATA26 防火
ATA章节中英对照
Chapter 1 –Brief History of AviationChapter 2 –DeregulationChapter 3 –Structure of the IndustryChapter 4 –Airline EconomicsChapter 5 –How Aircraft FlyChapter 6 –SafetyChapter 7 –SecurityChapter 8 –AirportsChapter 9 –Air Traffic ControlChapter 10 –Airlines and the Environment5章时间限制、维修检查(Time Limits,Maint. Checks) 6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage) 11章标牌和铭记(Placards and Markings)12章勤务(Servicing)20章标准施工---机体(Standard Practices---Airframe) 21章空调（Air Conditioning）22章自动飞行（Auto Flight）23章通讯（Communications）24章电源（Electrical Power）25章设备/装饰（Equipment/Furnishings）26章 .防火(Fire Protection)27章飞行操纵（Flight Controls）28章燃油（Fuel）29章液压源（Hydraulic Power）30章防冰和排雨（Ice and Rain Protection）31章指示/记录系统（Indicating/Recording system）32章起落架(Landing Gear)33章灯光（Lights）34章导航（Navigation）35章氧气(Oxygen)36章气源(Pneumatic)37章真空（Vacuum）38章水/污水（Water/waste）45章中央维护系统（Central maintenance System）49章机载辅助动力装置(Airborne Auxiliary Power)51章结构与标准施工(Structures & Standard Practices) 52章舱门(Doors)53章机身(Fuselage)54章发动机吊舱/吊架(Nacelles/Pylons)55章稳定装置 (Stabilizers)安定面56章窗户(Windows)57章机翼(Wings)70章标准施工—发动机(Standard Practices—Engines)71章动力装置(Power Plant( Package))72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))01 INTRODUCTION05 PERIODIC INSPECTIONS06 DIMENSIONS AND AREAS07 LIFTING AND SHORING08 LEVELING AND WEIGHING09 TOWING AND TAXIING10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE11 PLACARDS AND MARKINGS12 SERVICING - ROUTINE MAINTENANCE18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)20 STANDARD PRACTICES - AIRFRAME21 AIR CONDITIONING22 AUTO FLIGHT23 COMMUNICATIONS24 ELECTRICAL POWER25 EQUIPMENT / FURNISHINGS26 FIRE PROTECTION27 FLIGHT CONTROLS28 FUEL29 HYDRAULIC POWER30 ICE AND RAIN PROTECTION31 INDICATING / RECORDING SYSTEMS32 LANDING GEAR33 LIGHTS34 NAVIGATION35 OXYGEN36 PNEUMATIC37 VACUUM38 WATER / WASTE39 ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS 41 WATER BALLAST45 CENTRAL MAINTENANCE SYSTEM (CMS)46 INFORMATION SYSTEMS49 AIRBORNE AUXILIARY POWER51 STANDARD PRACTICES AND STRUCTURES - GENERAL52 DOORS53 FUSELAGE54 NACELLES / PYLONS55 STABILIZERS56 WINDOWS57 WINGS60 STANDARD PRACTICES - PROPELLER / ROTOR61 PROPELLERS / PROPULSORS62 MAIN ROTOR(S)63 MAIN ROTOR DRIVE(S)64 TAIL ROTOR65 TAIL ROTOR DRIVE66 ROTOR BLADE AND TAIL PYLON FOLDING67 ROTORS FLIGHT CONTROL70 STANDARD PRACTICES - ENGINE71 POWER PLANT - GENERAL72 ENGINE72(T) ENGINE - TURBINE / TURBOPROP, DUCTED FAN / UNDUCTED FAN72(R) ENGINE - RECIPROCATING73 ENGINE - FUEL AND CONTROL74 IGNITION75 BLEED AIR76 ENGINE CONTROLS77 ENGINE INDICATING78 EXHAUST79 OIL80 STARTING81 TURBINES (RECIPROCATING ENGINES)82 WATER INJECTION83 ACCESSORY GEAR BOXES (ENGINE DRIVEN)84 PROPULSION AUGMENTATION91 CHARTS5章时间限制、维修检查(Time Limits,Maint. Checks)6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage)11章标牌和铭记(Placards and Markings)12章勤务(Servicing)BMS3-33润滑脂的介绍/posts/35/topic-0045-359438.html20章标准施工---机体(Standard Practices---Airframe)21章空调(Air Conditioning)空调出口温度高/posts/35/topic-0045-359394.html[原创]关于737-300/500的空调/posts/35/topic-0045-356247.htmlPACK空中超温，会有那些原因引起呢？（专业贴）/posts/35/topic-0045 -359163.html22章自动飞行(Auto Flight)737NG的Y/D故障分析供大家参考/posts/72/topic-0045-729542.html 23章通讯(Communications)24章电源(Electrical Power)IDG和GEN /posts/35/topic-0045-358102.html737-300 B2972电源及APU自动关车排故思路之分析/posts/182/topic-0 045-1827865.html25章设备/装饰(Equipment/Furnishings)26章防火(Fire Protection)有关737灭火瓶...... /posts/35/topic-0045-357937.htmlAPU火警探测/posts/35/topic-0045-357662.html27章飞行操纵(Flight Controls)28章燃油(Fuel)737飞机燃油浮子电门/posts/35/topic-0045-359544.html29章液压源(Hydraulic Power)液压问题/posts/35/topic-0045-359382.html关于液压保险在液压管路的作用和位置？请教/posts/35/topic-0045-3592 99.html液压系统故障/posts/35/topic-0045-359411.html30章防冰和排雨(Ice and Rain Protection)31章指示/记录系统(Indicating/Recording system)32章起落架(Landing Gear)如何延长飞机轮胎的使用寿命/posts/35/topic-0045-358979.html前轮磨损/posts/35/topic-0045-359232.html谁能说说金属刹车片和碳刹车片的优缺点？/posts/35/topic-0045-358669. html请问哪位对防滞刹车结构熟悉的，简单介绍一下，谢谢那里有资料，网上有吗？http://bbs. /posts/35/topic-0045-359091.html请教:飞机换轮子的时候为什么要转动轮子? /posts/177/topic-0045-177 5484.html一起B737-300飞机使用自动速度刹车时，AUTO SPEED BRAKE 跳开关跳开http://bbs.fee /posts/103/topic-0045-1038900.html33章灯光(Lights)34章导航(Navigation)35章氧气(Oxygen)36章气源(Pneumatic)一起引气故障导致的增压故障（B737NG）/posts/103/topic-0045-1035067. html37章真空(Vacuum)38章水/污水(Water/waste)45章中央维护系统(Central maintenance System)49章机载辅助动力装置(Airborne Auxiliary Power)APU启动不起来了! /posts/35/topic-0045-357370.htmlAPU维护灯亮/posts/35/topic-0045-357331.html51章结构与标准施工(Structures & Standard Practices)52章舱门(Doors)53章机身(Fuselage)54章发动机短舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)56章窗户(windows)[讨论]玻璃上裂纹深度的测量？？/posts/35/topic-0045-350765.html57章机翼(wings)70章标准施工---发动机(Standard Practices---Engines)71章动力装置(Power Plant (Package))IAEV2500系列发动机试车总结/posts/85/topic-0045-850361.html72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)737反推故障/posts/35/topic-0045-357397.html79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))ATA Specification 22001 *Reserved for Airline Use2 *Reserved for Airline Use3 *Reserved for Airline Use4 *Reserved for Airline Use5 TIME LIMITS/ MAINTENANCE CHECKS-00 General-10 Time Limits-20 Scheduled Maintenance Checks-30 & -40 Reserved-50 Unscheduled Maintenance checks6 DIMENSIONS AND AREAS7 LIFTING & SHORING-00 General-10 Jacking-20 Shoring8 LEVELING & WEIGHING-00 General-10 Weighing and Balancing-20 Leveling9 TOWING & TAXIING-00 General-10 Towing-20 Taxiing10 PARKING, MOORING, STORAGE & RETURN TO SERVICE -00 General-10 Parking/Storage-20 Mooring-30 Return to Service11 PLACARDS AND MARKINGS-00 General-10 Exterior Color Schemes and Markings-20 Exterior Placards and Markings-30 Interior Placards12 SERVICING-00 General-10 Replenishing-20 Scheduled Servicing-30 Unscheduled Servicing13 *Unassigned14 *Unassigned15 *Unassigned16 *Unassigned17 *Unassigned18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY) -00 GENERAL --10 VIBRATION ANALYSIS-20 NOISE ANALYSIS19 *Unassigned20 STANDARD PRACTICES-AIRFRAME-90 *Reserved for Airline Use21 AIR CONDITIONING-00 General-10 Compression-20 Distribution-30 Pressurization Control-40 Heating-50 Cooling-60 Temperature Control-70 Moisture/Air Contaminant22 AUTO FLIGHT-00 General-10 Autopilot-20 Speed-Attitude Correction-30 Auto Throttle-40 System Monitor-50 Aerodynamic Load Alleviating23 COMMUNICATIONS-00 General-10 Speech Communications-15 SATCOM-20 Data Transmission and Automatic Calling -30 Comfort-40 Interphone-50 Audio Integrating-60 Static Discharging-70 Audio & Video Monitoring-80 Integrated Automatic24 ELECTRICAL POWER-00 General-10 Generator Drive-20 AC Generation-30 DC Generation-40 External Power-50 AC Electrical Load Distribution-60 DC Electrical Load Distribution25 EQUIPMENT/FURNISHINGS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Galley-40 Lavatories-50 Additional Compartments-60 Emergency-70 Available-80 Insulation26 FIRE PROTECTION-00 General-10 Detection-20 Extinguishing-30 Explosion Suppression27 FLIGHT CONTROLS-00 General-10 Aileron & Tab-20 Rudder & Tab-30 Elevator & Tab-40 Horizontal Stabilizer-50 Flaps-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -70 Gust Lock & Dampener-80 Lift Augmenting28 FUEL-00 General-10 Storage-20 Distribution-30 Dump-40 Indicating29 HYDRAULIC POWER-00 General-10 Main-20 Auxiliary-30 Indicating30 ICE AND RAIN PROTECTION-00 General-10 Airfoil-20 Air Intakes-30 Pitot and Static-40 Windows, Windshields and Doors-50 Antennas and Radomes-60 Propellers/Rotors-70 Water Lines-80 Detection31 INDICATING/RECORDING SYSTEMS-00 General-10 Instrument & Control Panels-20 Independent Instruments-30 Recorders-40 Central Computers-50 Central Warning Systems-60 Central Display Systems-70 Automatic Data Reporting Systems 32 LANDING GEAR-00 General-10 Main Gear and Doors-20 Nose Gear and Doors-30 Extension and Retraction-40 Wheels and Brakes-50 Steering-60 Position and Warning-70 Supplementary Gear33 LIGHTS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Cargo and Service Compartments -40 Exterior-50 Emergency Lighting34 NAVIGATION-00 General-10 Flight Environment-20 Attitude & Direction-30 Landing and Taxiing Aids-40 Independent Position Determining -50 Dependent Position Determining -60 Flight Management Computing35 OXYGEN-00 General-10 Crew-20 Passenger-20 Passenger-30 Portable36 PNEUMATIC-00 General-10 Distribution-20 Indicating37 VACUUM-00 General-10 Distribution-20 Indicating38 WATER/WASTE-00 General-10 Potable-20 Wash-30 Waste Disposal-40 Air Supply39 *Unassigned40 *Unassigned41 WATER BALLAST-00 General-10 Storage-20 Dump-30 Indication42 *Unassigned43 *Unassigned44 CABIN SYSTEMS-00 General-10 Cabin Core System-20 Inflight Entertainment System-30 External Communication System-40 Cabin Mass Memory System-50 Cabin Monitoring System-60 Miscellaneous Cabin System45 CENTRAL MAINTENANCE SYSTEM-00 General-5 thru -19 CMS/Aircraft General-20 thru -49 CMS/Airframe Systems-45 Central Maintenance System-50 thru -59 CMS/Structures-60 thru -69 CMS/Propellers-70 thru -89 CMS/Power Plant45INFORMATION SYSTEMS-00 General-10 Airplane General Information Systems -20 Flight Deck Information Systems-30 Maintenance Information Systems-40 Passenger Cabin Information Systems -50 Miscellaneous Information Systems47 *Unassigned48 *Unassigned49 AIRBORNE AUXILIARY POWER-00 General-10 Power Plant-20 Engine-30 Engine Fuel and Control-40 Ignition/Starting-50 Air-60 Engine Controls .-70 Indicating-80 Exhaust-90 Oil50 Cargo and Accessory Compartments-00 General-10 Cargo Compartments-20 Cargo Loading Systems-30 Cargo Related Systems-40 Available-50 Accessory-60 Insulation51 Standard Practices, General-00 General-10 Investigation, Cleanup and Aerodynamic Smoothness-20 Processes-30 Materials-40 Fasteners-50 Support of Airplane for Repair and Alignment Check Procedures -60 Control-Surface Balancing-70 Repairs-80 Electrical Bonding52 DOORS-00 General-10 Passenger/Crew-20 Emergency Exit-30 Cargo-40 Service and Miscellaneous-50 Fixed Interior-60 Entrance Stairs-70 Monitoring and Operation-80 Landing Gear53 FUSELAGE-00 General-10 thru -90 (As Required) Fuselage Sections54 NACELLES/PYLONS-00 General-10 thru -40 (As Required) Nacelle Section-50 thru -80 (As Required) Pylon55 STABILIZERS-00 General-10 Horizontal Stabilizer or Canard-20 Elevator-30 Vertical Stabilizer-40 Rudder56 WINDOWS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Door-40 Inspection and Observation57 WINGS-00 General-10 Center Wing-20 Outer Wing-30 Wing Tip-40 Leading Edge and Leading Edge Devices -50 Trailing Edge Trailing Edge Devices -60 Ailerons and Elevons-70 Spoilers-80 (as required)-90 Wing Folding System58 *Unassigned59 *Reserved for Airline Use60 STANDARD PRACTICES - PROPELLER/ROTOR61 PROPELLERS/PROPULSION-00 General-10 Propeller Assembly-20 Controlling-30 Braking-40 Indicating-50 Propulsor Duct62 ROTOR(S)-00 General-10 Rotor blades-20 Rotor head(s)-30 Rotor Shaft(s)/Swashplate Assy(ies) -4063 ROTOR DRIVE(S)-00 General-10 Engine/Gearbox couplings-20 Gearbox(es)-30 Mounts, attachments-40 Indicating64 TAIL ROTOR-00 General-10* Rotor blades-20* Rotor head-30 Available-40 Indicating65 TAIL ROTOR DRIVE-00 General-10 Shafts-20 Gearboxes-30 Available-40 Indicating66 FOLDING BLADES/PYLON-00 General-10 Rotor blades-20 Tail pylon-30 Controls and Indicating67 ROTORS FLIGHT CONTROL-00 General-10 Rotor-20 Anti-torque Rotor control (Yaw control)-30 Servo-control System68 *Unassigned69*Unassigned70 STANDARD PRACTICES - ENGINES71 POWER PLANT-00 General-10 Cowling-30 Fireseals-40 Attach Fittings-50 Electrical Harness-60 Air Intakes-70 Engine Drains72 ENGINE TURBINE/TURBO PROP DUCTED FAN/UNDUCTED FAN-00 General-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted Gear Driven Propulsor)-20 Air Inlet Section-30 Compressor Section-40 Combustion Section-50 Turbine Section-60 Accessory Drives-70 By-pass Section-80 Propulsor Section (Rear Mounted)73 ENGINE FUEL AND CONTROL-00 General-10 Distribution-20 Controlling-30 Indicating74 IGNITION-00 General-10 Electrical Power-20 Distribution-30 Switching75 AIR-00 General-10 Engine Anti-Icing-20 Cooling-30 Compressor Control-40 Indicating76 ENGINE CONTROLS-00 General-10 Power Control-20 Emergency Shutdown77 ENGINE INDICATING-00 General-10 Power-20 Temperature-30 Analyzers That-40 Integrated Engine Instrument Systems 78 EXHAUST-00 General-10 Collector/Nozzle-20 Noise Suppressor-30 Thrust Reverser-40 Supplementary Air79 OIL-00 General-10 Storage-20 Distribution-30 Indicating80 STARTING-00 General-10 Cranking81 TURBINES-00 General-10 Power Recovery-20 Turbo-Supercharger82 WATER INJECTION-00 General-10 Storage-20 Distribution-30 Dumping and Purging-40 Indicating83 ACCESSORY GEAR-BOXES-00 General-10 Drive Shaft Section-20 Gearbox Section84 Propulsion Augmentation-00 General-10 Jet Assist Takeoff85 *Unassigned86 *Unassigned87 *Unassigned88 *Unassigned89 *Unassigned90 *Unassigned91 CHARTS92 *Unassigned93 *Unassigned94 *Unassigned95 *Reserved for Airline Use96 *Reserved for Airline Use97 WIRING REPORTING-00-00 General-01-00 Zone 100 Fuselage Lower-02-00 Zone 200 Fuselage Top-03-00 Zone 300 Stabilizers-04-00 Zone 400 Nacelles-Pylons-05-00 Zone 500 Left Wing-06-00 Zone 600 Right Wing-07-00 Zone 700 Landing Gear Compartment -08-00 Zone 800 Doors-09-00 Zone 900 Lavatories & Galleys-20-00 Electrical Standard Items/Practices -21-00 Air Conditioning - General-21-10 Compression-21-20 Distribution-21-30 Pressurization Control-21-40 Heating-21-50 Cooling-21-60 Temperature Control-21-70 Moisture/Air Contaminant Control-22-00 Auto Flight - General-22-10 Autopilot-22-20 Speed - Attitude Correction-22-30 Auto Throttle-22-40 System Monitors-22-50 Aerodynamic Load Alleviating-23-00 Communications - General-23-10 Speech Communications-23-15 SATCOM-23-20 Data Transmission and Automatic Calling-23-30 Passenger Address, Entertainment and Comfort-23-40 Interphone-23-50 Audio Integrating-23-60 Static Discharging-23-70 Audio and Video Monitoring-23-80 Integrated Automatic Tuning-24-00 Electrical Power - General-24-10 Generator Drive-24-20 AC Generation-24-30 DC Generation-24-40 External Power-24-50 AC Electrical Load Distribution-24-60 DC Electrical Load Distribution-25-00 Equipment/Furnishings - General-25-10 Flight Compartment-25-20 Passenger Compartment-25-30 Galley-25-40 Lavatories-25-60 Emergency-25-80 Insulation-26-00 Fire Protection - General-26-10 Detection-26-20 Extinguishing-26-30 Explosion Suppression-27-00 Flight Controls - General-27-10 Aileron & Tab-27-20 Rudder & Tab-27-30 Elevator & Tab-27-40 Horizontal Stabilizer-27-50 Flaps-27-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -27-70 Gust Lock & Dampener-27-80 Lift Augmenting-28-00 Fuel - General-28-10 Storage-28-20 Distribution-28-30 Dump-28-40 Indicating-29-00 Hydraulic Power - General-29-10 Main-29-20 Auxiliary-29-30 Indicating-30-00 Ice and Rain Protection - General-30-10 Airfoil-30-20 Air Intakes-30-30 Pitot and Static-30-40 Windows, Windshields and Doors-30-50 Antennas And Radomes-30-60 Propellers/Rotors-30-70 Water Lines-30-80 Detection-31-00 Indicating/Recording Systems - General -31-10 Instrument and Control Panels-31-20 Independent Instruments-31-30 Recorders-31-40 Central Computers-31-50 Central Warning Systems-31-60 Central Display Systems-31-70 Automatic Data Reporting Systems-32-00 Landing Gear- General-32-10 Main Gear and Doors-32-20 Nose Gear and Doors-32-30 Extension and Retraction-32-40 Wheels and Brakes-32-50 Steering-32-60 Position And Warning-32-70 Supplementary Gear-33-00 Lights - General-33-10 Flight Compartment-33-20 Passenger Compartment-33-30 Cargo and Service Compartments-33-40 Exterior-33-50 Emergency Lighting-34-00 Navigation - General-34-10 Flight Environment Data-34-20 Attitude & Direction-34-30 Landing and Taxiing Aids-34-40 Independent Position Determining-34-50 Dependent Position Determining-34-60 Flight Management Computing-35-00 Oxygen - General-35-10 Crew-35-20 Passenger-35-30 Portable-36-00 Pneumatic - General-36-10 Distribution-36-20 Indicating-37-00 Vacuum - General-37-10 Distribution-37-20 Indicating-38-00 Water/Waste - General-38-10 Potable-38-20 Wash-38-30 Waste Disposal-38-40 Air Supply-44-00 Cabin Systems - General-44-10 Cabin Core System-44-20 In-flight Entertainment System-44-30 External Communication System-44-40 Cabin Mass Memory System-44-50 Cabin Monitoring System-44-60 Miscellaneous Cabin System-45-00 Central Maintenance System (CMS) General -45-05 CMS/Aircraft General-45-20 CMS/Airframe Systems-45-45 Central Maintenance System-45-50 CMS/Structures-45-60 CMS/Propellers-45-70 CMS/Power Plant-46-00 Information Systems - General-46-10 Airplane General Information Systems-46-20 Flight Deck Information Systems-46-30 Maintenance Information Systems-46-40 Passenger Cabin Information Systems-46-50 Miscellaneous Information Systems-49-00 Airborne Auxiliary Power - General-49-10 Power Plant-49-20 Engine-49-30 Engine Fuel And Control-49-40 Ignition And Starting-49-50 Air-49-60 Engine Controls-49-70 Indicating-49-80 Exhaust-49-90 Oil-50-00 Cargo And Accessory Compartments General -50-10 Cargo Compartments-50-20 Cargo Loading Systems-50-30 Cargo Related Systems-50-40 Available-50-50 Accessory Compartments-50-60 Insulation-52-00 Doors - General-52-10 Passenger/Crew-52-20 Emergency Exit-52-30 Cargo-52-40 Service-52-50 Fixed Interior-52-60 Entrance Stairs-52-70 Door Warning-52-80 Landing Gear-53-00 Fuselage - General-54-00 Nacelles/Pylons - General-54-10 Nacelle Section-54-50 Pylon-55-00 Stabilizers - General-55-10 Horizontal Stabilizer or Canard-55-20 Elevator-55-30 Vertical Stabilizer-55-40 Rudder-56-00 Windows - General-56-10 Flight Compartment-56-20 Passenger Compartment-56-30 Door-56-40 Inspection and Observation-57-00 Wings - General-57-10 Center Wing-57-20 Outer Wing-57-30 Wing Tip-57-40 Leading Edge and Leading Edge Devices-57-50 Trailing Edge and Trailing Edge Devices -57-60 Ailerons-57-70 Spoilers-57-90 Wing Folding System-61-00 Propellers/Propulsors - General-61-10 Propeller Assembly-61-20 Controlling-61-30 Braking-61-40 Indicating-61-50 Propulsor Duct-62-00 Rotors-63-00 Rotor Drives-64-00 Tail Rotor-65-00 Tail Rotor Drive-66-00 Folding Blades/Pylon-67-00 Rotors Flight Control-71-00 Power Plant - General-71-10 Cowling-71-20 Mounts-71-30 Fire seals-71-40 Attach Fittings-71-50 Electrical Harness-71-60 Air Intakes-71-70 Engine Drains-72-00 Engine Turbine/Turbo Prop Ducted Fan/Unducted Fan-72-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted GearDriven Propulsor)-72-20 Air Inlet Section-72-30 Compressor Section-72-40 Combustion Section-72-50 Turbine Section-72-60 Accessory Drives-72-70 By-pass Section-72-80 Propulsor Section (Rear Mounted)-73-00 Engine Fuel And Control - General-73-10 Distribution-73-20 Controlling-73-30 Indicating-74-00 Ignition - General-74-10 Electrical Power Supply-74-20 Distribution-74-30 Switching-75-00 Air - General-75-10 Engine Anti-Icing-75-20 Cooling-75-30 Compressor Control-75-40 Indicating-76-00 Engine Controls - General-76-10 Power Control-76-20 Emergency Shutdown-77-00 Engine Indicating - General-77-10 Power-77-20 Temperature-77-30 Analyzers-77-40 Integrated Engine Instrument Systems -78-00 Exhaust - General-78-10 Collector/Nozzle-78-20 Noise Suppressor-78-30 Thrust Reverser-78-40 Supplementary Air-79-00 Oil - General-79-10 Storage-79-30 Indicating-80-00 Starting - General-80-10 Cranking98 *Reserved for Airline Use99 *Unassigned100 *Do not use101 *Do not use102 *Do not use103 *Do not use104 *Do not use105 *Do not use106 *Do not use107 *Do not use108 *Do not use109 *Do not use110 *Do not use111 *Do not use112 *Do not use113 *Do not use114 *Do not use115 Flight Simulator Systems。
ATA章节翻译
05time limits/maintenace chack(时限/维护检查) 06dimensions and areas（区域）07liftng and shoring（顶起和支撑）08leveling and weighing（水平和称重）09towing and taxing（拖行和滑行）10parking moorin（停留、系留）11placards and markings（标志、标牌）12servicing（勤务）20 standard practices（标准施工）AIR FRAME21 air conditioning(空调系统)22 auto fight（自动飞行）23 communication（通讯系统）24 electrical power(电源系统)25 equipment/furnishings(设备、设施)26 fire protection (防火系统)27 flight controls(飞行控制)28 fuel(燃油)29 hydraulic power(液压动力系统)30 ice and rain protection(防冰、防雨系统)31 indicating(指示系统)RECORDING SYSTEMS32 landing gear(起落架系统)33 light(灯光系统)34 navigation(导航系统)35 oxygen(氧气系统)36 pneumatic(气源系统)38 water/waste(水、污水系统)49airborne auxiliary power(APU/辅助动力装置) 51 standard practices(标准施工) ANDSTRUCTURES-GENERAL(结构部分)52 doors(舱门)53 fuselage(机身)54 nacelles/pylons（短舱）55 stabilizers(安定面)56 windows(窗户)57 wings(机翼)70 standard practices(标准施工)ENGINES(发动机部分)71 power plant(动力装置)72 engine（发动机本体）73 engine fuel and control(发动机燃油控制系统)74 ignition(点火系统)75 air(空气系统)76 engine controls(发动机控制系统)77 engine indicating(发动机指示系统)78 exhaust(排气系统)79 oil(滑油系统)80 starting(起动系统)。
民航飞行记录本英译常用词句
记录本英译常用词句飞机 A/C（是aircraft 的英文缩写形式）航前检查 preflight check航后检查 postflight check短停检查 transit check定检 scheduled maintenance发现 found或revealed（注：对已发生事情的描述常用过去式）故障 trouble 或 failure 或 fault失效 fail 或 malfunction不工作 inoperative 缩写 INOP工作不稳定 rough工作稳定 smoothly排故 troubleshooting为了排故 for troubleshooting不能 fail to…或 can’t根据 refer 或 per to 或 according to；维护手册 AMM更换 replaced件号 part number 缩写P/N时控件 time control part拆下 removed安装 installed上件 part on下件 part off放行标准 DDG（是dispatch deviation guide的英文缩写形式）最低设备清单 MEL（是minimum equipment list的缩写形式）南航传真 CSN fax同意放行 dispatch approved 或 released因为 due 或 because因停场时间不足 due time short没有备件 lack parts 或 no spare parts available 或 no parts in stock 待件 wait for parts申请保留 apply for reservation保留故障 defer defect保留项目 defer item保留期限 due time关闭保留项目 close deferred item撤消保留项目 rescind deferred item前部 forward 缩写fwd后部 after 缩写aft左 left 缩写L 或 LH右 right 缩写R 或 RH上面 upper下面 lower内侧 inboard 缩写 I/B外侧 outboard 缩写 O/B内侧发动机 inboard engine外侧发动机 overboard engine起落架 landing gear 缩写 LDG主轮 main wheel前轮 nose wheel测试 test通电测试 power-on test安装测试 test for installation操作测试 operational test系统测试 test for system正常 normal 或 OK异常 abnormal在空中 in flight在地面 on ground地面检查 GND check试车检查 running-up test（同机）对串件 interchanged…with…（不同机间）对串件 exchanged…with… 或 robbed…from… 更新数据库 updated database开关 switch电门 switch正常位 NORM备用位 ALTN人工 manual自动 auto选择 select（注：通常也用缩写形式SEL）按钮 button旋钮 knob按压 press把住 hold释放 release顺时针 clockwise逆时针 counterclockwise预置 preset重新设置 reset一致 agree不一致 disagree不对称 asymmetric卡阻 jammed杆 lever 或 stick 或 column操纵杆 control column控制面板 control panel手柄 handle方向盘 steering wheel放电刷 static discharge wick遮光板 glare shield风挡 windscreen 或 windshield雨刷 wiper调整 adjust 或 regulate重新调整 readjust销子 pin 例如 安全销safety pin插头 plug插座 socket插针 pin电阻 resistor线路 wire在…之间 between…and…引线 lead跳开关 circuit breaker继电器 relay螺帽 nut螺栓 bolt螺钉 screw松动 loose脱落 fall off拧紧 tighten丢失 lost 或 missing鸟击 bird strike凹坑 dent损坏 damaged烧蚀 burn through烧坏 burn out扎伤 punctured磨损 wearing 或 worn在范围内 within limits超标 out of limits见线 exposed threads油箱 tank燃油 fuel滑油 oil液压油 hydraulic fluid泄露 leak（注：也常用名词leakage）& 是and的简写符号，表示“和”，“又”等意思 No. 是number的缩写，表示号码，例如1号为No.1 机长 captain副驾驶 first officer 缩写F/O观察员 observer乘务员 attendant飞机概述机头 nose机腹 belly蒙皮 skin机身 airframe翼肋 rib翼梁 spar机翼 wing翼尖 wing tip前缘 leading edge后缘 trailing edge操纵面 control surface客舱 cabin 或 passenger compartment 座位 seat排 row（如：第5排译作row 5）过道 aisle地板 floor天花板 ceiling隔板 partition厨房 galley厕所 toilet驾驶舱 cockpit货舱 cargo轮舱 wheel well 缩写W/W设备舱 bayATA 21空调空调 air-conditioning 缩写a/c空调舱 air-conditioning pack自动驾驶 autopilot冲压空气作动器 ram air actuator出气活门 air outlet valve排气活门 exhaust valve温度控制活门 TEMP CONT valve引气 bleed air自动 automatic缩写AUTO人工 manual正常 normal 缩写NORM备用 alternate 缩写ALTN设备冷却 equipment cooling排气扇 exhaust fan供气扇 supply fan低流量 low flow头顶分配管 overhead distribution duct进气管 inlet duct主热交换器 primary heat exchanger次热交换器 secondary heat exchanger增压室 plenum增压 pressurization加热 heating压力控制 pressure control滤网 filter温度指示器 temperature indicator客舱高度 cabin altitude压差指示器 differential press indicator客舱爬升率 cabin rate of climb空气循环机 air cycle machine 缩写ACM主分配管 main distribution manifold客舱压力控制组件 cabin press control module水分离器 water separator压力选择面板 press selector panel控制继电器 control relay人工超控继电器 manual override relay传感器 sensor过热电门 overheat switch压气机出口过热电门 compressor outlet overheat switch 外溢活门 outflow valve单向活门 check valve关断活门 shutoff valve释压活门 relief valve配平调节活门 trim modulating valve风挡 windshieldATA22 自动驾驶自动驾驶 autopilot液压 hydraulic 缩写 HYD副翼 aileron襟翼 flap缝翼 slat安定面 stabilizer方向舵 rudder升降舵 elevator扰流板 spoiler减速板 airbrake传感器 transducer发射机 transmitter马赫配平作动器 mach trim actuator自动油门 auto-throttle偏航阻尼器 yaw damper失速管理 stall management机长 captain副驾驶 first officer 缩写 F/O观察员 observer伺服马达 servo motor速度配平 speed trim巡航 cruise起飞/复飞电门 takeoff/go around switch俯仰 pitch横滚 roll驱动组件 drive unit跳开关 circuit breakerATA23 通信通信 communication旅客广播 passenger address 缩写PA天线 antenna选呼 select call 缩写SELCAL娱乐系统 entertainment system磁带机 tape reproducer内话 interphone语音记录器 voice recorder天线偶合器 antenna coupler乘务员面板 attendant panel话筒 headset指示灯 indicator light氧气面罩 oxygen mask音频控制面板 audio control panel音频选择面板 audio select panel语音/数据继电器 voice/data relay呼叫电门 call switch收发机 transceiver应急定位发射机 emergency locator transmitter 无线电频率组件 radio frequency unit遥控电子组件 remote electronics unitATA24 电源电源 electrical power电瓶 battery电压计 voltmeter发电机 generator启动机 starter静变流机 static inverter外电源 external power地面服务电门 ground service switch变压器 transformer汇流条电源控制组件 bus power control unit备用电源控制组件 standby power control unit变频器 converter整流器 rectifier保险丝 fuseATA25设备和装饰设备 equipment装饰 furnishing医药箱 medical kit厨房 galley厕所 lavatory旅客座位 passenger seat过道 aisle逃离绳 escape lanyard隔板 sidewall panel电子舱 electronics bay旅客服务组件 passenger service unit站位 station逃离滑梯 escape slide内窗 inner window后货舱 AFT cargoATA26 防火防火 fire protection灭火瓶 fire extinguisher bottle头顶探测器 overhead detector龙骨梁 keel beam过热探测器 overheat detector发动机支架 engine strut大翼过热探测器 wing overheat detector主轮舱 main wheel well烟雾探测 smoke detector厕所烟雾指示灯 lavatory smoke indicator light火警灯 fire warning light过热探测控制组件 overheat detector control module测试电门 test switch故障/不工作和过热/火测试电门 FAULT/INOP and OVHT/FIRE test switch 灭火测试电门 extinguisher switchATA27 飞行控制飞行控制 flight control机翼 wing翼尖 wing tip副翼配平作动器 aileron trim actuator升降舵调整片 elevator tab地面扰流板 ground spoiler前缘缝翼 leading edge slat缩写LE slat后缘襟翼 trailing edge flap缩写TE flap方向舵配平作动器 rudder trim actuator副翼组件 aileron assembly抖杆 stick shaker放出 extend收起 retract保险 fuse襟翼位置指示器 flap position indicator襟翼收放测试 test for R/E（retract/ extend的缩写形式）flaps 预位 arm转换机构 transfer mechanism驱动电动马达 drive electric motor驱动液压马达 drive hydraulic motor失速警告测试面板 stall warning test panel放下 down收上 up安定面配平 stabilizer trim控制杆 control column速度刹车 speed-brake自动缝翼控制活门 auto-slat control valve内锁活门 interlock valve旁通活门 bypass valve控制轮 control wheelATA28 燃油燃油 fuel中央油箱 center tank加油指示 fueling indicator预选 preselect加油喷嘴 refuel nozzle燃油系统面板 fuel system panel大翼加油面板 wing fueling panel增压泵 boost pump加油浮子电门 refuel float switchATA 29液压液压 hydraulic液压管路 hydraulic line液压作动筒 hydraulic actuator液压泵 hydraulic pump压力控制活门 pressure control valve压力传感器 pressure sensor释压活门 relief valve流量控制活门 flow control valve密封圈 seals刹车压力指示 brake press indicator故障探测 fault detector热交换器 heat exchanger排放油滤 drain filter储油箱 reservoir回油滤 return filter低压电门 low pressure switch液压过热警告电门 hydraulic overheat warning switch压力传感器 pressure transmitterATA30 防冰/防雨防冰和雨 anti-ice & rain风挡 windshield雨刮 rain wiper皮托管 pitot废物 waste窗户加热电源 window heat power加热面板 heat panel总温传感器 total temperature sensor防冰自动油门电门 anti-ice auto-throttle switch风挡传感器电门 windshield sensor switch热电门 thermal switch左/右侧窗户温度热控制组件 L / R side window heat control unit 进气整流罩 inlet cowl热防冰活门 thermal anti-ice valveATA31 指示/记录系统指示 indicating仪表 indicator 或 gauge记录 recording显示 display控制面板 control panel飞行记录仪 flight recorder位置传感器 position sensor起落架音响警告 landing gear aural warning时钟显示 clock display主警告 master caution打印机 printer测试接头 test connector耦合器 coupler马赫空速 mach airspeed固态飞行数据记录仪 solid state flight data recorder控制杆位置传感器 control column position sensor控制轮 control wheel地面扰流板内锁活门 GND spoiler interlock valve升降舵位置传感器 elevator position sensor方向舵踏板位置传感器 rudder pedal position sensor副翼位置传感器 aileron position地面扰流板升起压力电门 GND spoiler up press switch显示组件 display unitATA32 起落架起落架 landing gear 缩写LDG机轮 wheel主轮 main wheel前轮 nose wheel左外 left outboard 或 left outside（注：left通常可用大写L表示）左内 left inboard 或left inside右外 right outboard 或 right outside（注：right通常可用大写R表示） 右内 right inboard 或 right inside刹车 brake刹车蓄压器 brake accumulator主起落架 main landing gear上锁作动器 uplock actuator下锁作动器 downlock actuator前起落架 nose landing gear转弯 steering防滞 anti-skid起落架锁定 gear locked起落架舱门 wheel door轮舱 wheel well放轮 gear extension收轮 gear retraction收放测试 test for R/E（retract/ extend的缩写形式）起落架被卡阻 gear jammed轮胎 tyre爆胎 burst瘪胎 deflated tyre轮胎被扎破 puncture轮胎 tyre见线 exposed threads磨损 wear 或 worn out裂纹 cracks超限 out of limits在范围内 within limits空/地继电器 air/ground relay自动刹车 autobrake刹车保险 brake fuse人工释放 manual extension液压刹车压力指示器 hydraulic brake pressure indicator 停留刹车 parking brake故障灯 fault light解除预位灯 disarm light不工作灯 INOP light限流器 flow limiter扭力杆 torsion link人工放出机构 manual extension mechanism放下并锁上传感器 down and locked sensor收上并锁上传感器 up and locked sensor下锁弹簧 downlock spring减振支柱 shock strut侧支柱 side strut阻力支柱 drag strut人工放出限制电门 manual extension limit switch刹车踏板电门 brake pedal switch前轮转弯电门 nose wheel steering switch防滞传感器 antiskid transducer刹车调节活门 brake metering valve加注活门 charging valve选择活门 selector valve转换活门 transfer valve隔离活门 isolation valve防滞活门 antiskid valve往复活门 shuttle valveATA33 灯灯 light闪光灯 strobe light航行灯 navigation light 缩写NAV light防撞灯 anti-collision light着陆灯 landing light信号灯 signal light下滑灯 approach light机翼照明灯 wing illumination light标志灯 logo light滑行灯 taxi light应急照明灯 emergency light机身灯 fuselage light转弯灯 turnoff light尾灯 tail light窗灯 window light荧光灯 fluorescent lamp地板灯 floor light阅读灯 reading lamp灯座 lamp socket 或 lamp base灯架 lampholder地图灯 cap light灯组件 light module明 bright暗 dim灯泡 bulb烧坏 burn out灯罩 lamp cover灯亮 on 或 illuminate灯灭 off 或 turn offATA34 导航导航 navigation 缩写NAV天线 antenna数据库 database顶端 top底端 bottom下滑道 glide slope指点信标 marker beacon无线电高度接收机 radio altitude receiver无线电高度发射天线 radio altitude transmitter antenna 气象雷达 weather radar近地警告 ground proximity warning 缩写 GND PROX WARN 无线电导航 radio navigation姿态指示仪 attitude indicator测距仪询问机 DME interrogator应答机 transponder收发机 transceiver惯导 inertial reference主注意 master cautionATA35 氧气氧气 oxygen氧气面罩 oxygen mask流量控制 flow control热补偿 thermal compensator机组氧气瓶 crew oxygen cylinder氧气发生器 oxygen generator氧气压力指示 oxygen pressure indicator旅客氧气面罩 passenger oxygen mask机组氧气面罩 crew oxygen mask氧气系统组件 oxygen system module氧气系统面板 oxygen system panel安全销 safety pin压力调节器 pressure regulator氧气指示继电器 oxygen indicator relay高度压力电门 altitude press switch机组氧气传感器 crew oxygen transducer乘务员服务组件 attendant service unit厕所服务组件 lavatory unit旅客服务组件 passenger service unit超压释放活门 overpressure relief valveATA36 气源系统气源 pneumatics引气活门 bleed air valve双压力指示 dual pressure indicator引气调节器 bleed air regulator预冷控制活门传感器 precooler control valve sensor 超温电门 over temperature switch恒温器 thermostat总管压力传感器 manifold press transmitterAPU引气活门 APU bleed air valve单向活门 check valve引气隔离活门 bleed air isolation valve预冷控制活门 precooler control valve地面气源 ground pneumaticATA38 水和废物水和废物 water & waste真空通风机 vacuum blower排放管 drain line排放接头 drain fitting厕所水加热器 lavatory water heater水压缩机 water compressor水量指示 water quantity indicator空气过滤 air filter水服务面板 water service panel废物量指示 waste quantity indicator不工作/测试电门 INOP/TEST switch逻辑控制组件 logic control module压缩机控制继电器 compressor control relay内锁电门 interlock switch水压限制电门 water pressure limit switch废物箱 waste tank水箱 water tank真空马桶 vacuum toilet加注/溢流活门 fill/overflow valve球形活门 ball valveATA49 辅助动力装置辅助动力装置 auxiliary power unit 缩写APU进气门作动器 air inlet actuator导向叶片 guide vane燃油增压泵 fuel boost pump排气温度 exhaust gas temperature 缩写EGT数据记忆组件 data memory module滑油位传感器 oil level sensor滑油温度传感器 oil temperature sensor速度传感器 speed sensor进气门位置电门 air inlet door position switch 热电耦 thermocouple燃油控制组件 fuel control unit点火组件 ignition unit喘振活门 surge valveATA52 门门 door登机门 entry door警告电门 warning switch平衡组件 counterbalance assembly紧急出口 emergency exit货舱门闩 cargo door latch接近面板 access panel门上锁面板 door unlock panel安定面配平 stabilizer trimATA56 窗窗 window门窗 door mounted window旅客窗 passenger compartment windowATA71 动力装置动力装置 power plant发动机 engine发动机短舱 nacelle发动机吊舱 pod风扇 fan风扇叶片 fan blade进气罩 inlet cowl涡流控制装置 vortex control device 缩写VCD 释压门 pressure relief door接近门 access door滑油箱 oil tank风扇罩 fan cowl铰链 hinge风扇罩面板闩 fan cowl panel latch发动机架 engine mount发动机燃烧室 engine combustor高压涡轮组件 high pressure turbine assembly 附件齿轮箱 accessory gearbox传动齿轮箱 transfer gearbox转子，叶轮 spinner气缸 cylinder转速 revolution per minute 缩写RPM尾喷管 nozzle磁堵 magnetic plug发动机慢车位 idle发动机喘振 surge发动机停车 engine shutdown发动机熄火 engine flame outATA73 发动机燃油和控制发动机燃油和控制 engine fuel & control燃油系统 fuel system燃油箱 fuel tank通气孔 vent加油栓 fuel hydrant燃油管路 fuel line放油活门 dump valve燃油泵 fuel pump燃油滤 fuel filter接头 joint燃油流量表 fuel flow indicator导线束 wiring harness燃油总管 fuel manifold燃油喷嘴 fuel nozzle发动机控制面板 engine control panel插头 plug备用电源继电器 alternate power relay风扇进气温度传感器 fan inlet temperature sensor压差电门 differential pressure switch电子发动机控制 electronic engine control 缩写EEC燃油流量传感器 fuel flow transmitterATA74 点火点火 ignition点火激励器 ignition exciter发动机起动电门 engine start switch发动机点火电门 engine ignition switchATA75 发动机空气发动机空气 engine air可变引气活门 variable bleed valve 缩写VBV高压涡轮间隙活门 HP turbine clearance valve 缩写HPTCV 低压涡轮间隙活门 LP turbine clearance valve 缩写LPTCV 位置传感器 position transducer过渡引气活门 transient bleed valveATA76 发动机控制发动机控制 engine control起动杆 start lever点火电门 ignition switchATA77 发动机指示发动机指示 engine indicatingATA78 排气排气 exhaust反推 thrust reverser套筒 sleeve同步锁 SYNC lock顺序电门 sequence relay控制电门 control switch发动机附件组件 engine accessory unitATA79 发动机滑油发动机滑油 engine oil润滑剂 lubricant润滑 lubrication滑油管路 oil line探测器 detector回油 scavenge回油过滤 scavenge filter主滑油/燃油热交换器 main oil/fuel heat exchanger滑油压力传感器 oil pressure sensor滑油压力表 oil pressure indicator滑油温度表 oil temperature indicator滑油散热器 oil cooler滑油温度传感器 oil temperature sensor滑油滤旁通警告电门 oil filter bypass warning switch滑油箱 oil tank滑油量传感器 oil quantity transmitter润滑组件 lubrication unitATA80 起动起动 stating发动机起动活门 engine start valve常用语句……检查发现……1. 航后检查发现左后航行灯不亮。
航空飞机维修涨级考试空客波音各种机型题库
8. 备用方式控制座舱压 力时，哪条是错误的
9. 所谓非计划下降指的 是
1. 当外电源接头面板上 的“未使用”和“连接 ”灯亮时表示外电源：
B. 变化
率自动控
A. 感受 制在小于
大气数据 或等于
计算机信 500英尺
号
／分
B. 指飞
机没有上
升到飞行
A. 进入 员认可的
不正确的 高度就下
下降程序 降
A．插头 B．插头
门( 工超 B. 加油活
控）
门电门
7. 燃油交输的哪种说法 是错误的？
A. 在空中 B. 只有在 可以进行 地面才能 燃油交输 进行交输
8. 燃油关断活门是由： 9. 交输活门是由：
A. 只有起 B. 只有灭
动手柄控 火手柄控
制
制
A. 只有 P5
板上的旋
转开关控 B. 人工控
制
制
A. 可以直
接从油尺
火手柄时 ,____ 系统 EDP
的关断活门关闭 , 同时 A．A, 低 B．B, 低
EDP的______不工作． 压电门 压电门
A．A系统 B．B系统
4. 下列哪一个压力值未 输出压力 输出压力
在驾驶舱面板上显示
值
值
B737 机械
ATA 29 液压系统
B737 机械
ATA 29 液压系统
B737 机械
ATA21 空 调系统
B737 机械
ATA21 空 调系统
5. 设备冷却系统中的低 流量探测器探测到 _____，会发出警告。
6. 下面关于前外流活门 哪条是错误的：
A. 设备 B. 设备 冷却空气 冷却空气 温度过高 温度过低 A. 再循 B. 再循 环风扇工 环风扇工 作，前放 作，前放 气活门一 气活门不 定关闭 一定打开
B737机电部分试题(有答案)
B737机电部分试题（有答案）ATA21空调系统1．飞机在地面，发动机不工作，用APU向空调系统供气，左右组件电门均放正常位置时A．左、右组件均提供80磅流量B．仅左组件提供55磅流量C．仅右组件提供55磅流量D．仅左组件提供80磅流量答案：AATA21空调系统2．当管道过热灯（DUCTOVERHEAT）亮时A．关断组件活门关闭B．空调温度控制电路失效所引起C．混合活门将固定在冷位D．P5面板温度选择电门处于关断位答案：CATA21空调系统3．水分离器不会结冰是由于有A．空气循环机（ACM）B．过热控制电门C．水分离器D．35F控制装置答案：DATA21空调系统4．空气循环机（ACM）的压缩机出口过热电门设定在A．400FB．390FC．190FD．250F答案：BATA21空调系统5．设备冷却系统中的低流量探测器探测到_____，会发出警告。
A．设备冷却空气温度过高B．设备冷却空气温度过低C．设备冷却空气的流量过低D．A或C答案：DATA21空调系统6．下面关于前外流活门哪条是错误的：A．再循环风扇工作，前放气活门一定关闭B．再循环风扇工作，前放气活门不一定打开C．后外流门全开，前外流门一定打开D．后外流门全关，前外流门一定关闭答案：B ATA21空调系统8．备用方式控制座舱压力时，哪条是错误的A．感受大气数据计算机信号B．变化率自动控制在小于或等于500英尺／分C．落地后座舱高度低于跑道200英尺是人工调整的D．后外流活门是直流电机控制的答案：BATA21空调系统9．所谓非计划下降指的是A．进入不正确的下降程序B．指飞机没有上升到飞行员认可的高度就下降C．指飞机没有进入等压程序就下降D．飞行员选择的程序与正常的程序不同步答案：CATA24Electricalpower(10)1．当外电源接头面板上的“未使用”和“连接”灯亮时表示外电源:A．插头接触不良,外电源不能使用B．插头接触正常,外电源不能使用C．插头接触正常,外电源不能使用D．以上答案都不对答案：C ATA24Electricalpower(10)2．主电瓶装在:A．前设备舱B．主设备舱E3-1架C．主设备舱E3-2架D．主设备舱E2架左前方答案：DATA24Electricalpower(10)3．在完成测试工作后,M400S2电门应该转回到:A．B位置B．C位置C．A或C位置D．A,B,C任何位置答案：AATA24Electricalpower(10)4．与一号发电机断路器不能互换的是:A．二号发电机断路器(GB)B．二号发电机APU发电机断路器C．一号APU发电机断路器D．汇流条转换继电器答案：DATA24Electricalpower(10)5．APU发电机地面工作时A．既可供电又可供气B．可自动向左右两边网络供电C．可同时接通左右两边电门向网络供电D．可先后接通左右两边电门向网络供电答案：DATA24Electricalpower(10)6．哪两个接触器可同时在接通位A．一号发电机GB和一号APUGBB．二号发电机GB和二号APUGBC．一号外电源接触器和一号APUGBD．一号APUGB和二号APUGB答案：DATA24Electricalpower(10)7．共有几个变压整流组件(TRU)A．5B．4C．3D．2答案：CATA24Electricalpower(10)8．“汇流条转换”(BUSTRANS)电门置于断开时:A．TR3停止给DCBATBUS供电B．TR3停止给DCBUS2供电C．转换汇流条将断电D．将失去电瓶充电机备份电源答案：CATA24Electricalpower(10)9．APU发电机地面工作时的额定值是:A．125amp(45KVA)B．150amp(55KVA)C．165amp(60KVA)D．200amp(90K VA)答案：CATA25/52DOOR/WINDOWS/EQUIPMENT/AIRSTAIR1．不能从内外两边都能开的舱门是:A．登机门/厨房勤务门B．货舱门C．翼上紧急出口D．前设备舱门答案：DATA25/52DOOR/WINDOWS/EQUIPMENT/AIRSTAIR2．驾驶舱门的电磁锁锁上后,下列说法正确的是:A．除非使很大的力使锁销剪断,外人进不去B．乘务员用钥匙可开门进去C．机组拧门把手可开门出来D．以上都正确答案：DATA25/52DOOR/WINDOWS/EQUIPMENT/AIRSTAIR3．旅客窗户分几层承受增压负载的是哪一层A．一层．B．两层．外层C．三层．外层,中层．D．三层．内层答案：CATA25/52DOOR/WINDOWS/EQUIPMENT/AIRSTAIR4．驾驶舱窗户维护注意事项有A．螺钉安装要按一定的交叉顺序B．螺钉拧紧力矩有限制C．断开电源D．以上都是答案：DATA25/52DOOR/WINDOWS/EQUIPMENT/AIRSTAIR5．自动厨房卸载电路的作用是A．一条发电机汇流条断电时断开厨房供电,保证重要系统供电．B．APU供电超载时断开厨房供电,保证重要系统供电．C．厨房电负载过高时断开厨房供电,保证重要系统供电．D．A和B答案：D ATA25/52DOOR/WINDOWS/EQUIPMENT/AIRSTAIR6．紧急情况下撤离飞机的途径有:A．登机门/厨房勤务门的应急滑梯B．驾驶舱逃生带C．翼上应急出口逃生带D．以上都是答案：DATA26防火系统1．机身防火左侧有13个过热探测元件串联，右侧有6个串联，其中：A．任何一个探测元件探测到过热都会使警铃响B．两边均探测到过热警铃才响C．任何一个探测到过热过热灯都会亮D．任何一个探测到过热相应一边的过热灯亮答案：DATA26防火系统2．火警温度探测元件是温度上升，A．电流变小B．电压变小C．电阻变小D．电容变小答案：CATA26防火系统3．对电阻感温式KIDDLE火警探测器来说,在没有按压发动机和APU火警探测附件组件(M279)上的”测试”(TEST)钮时,组件上的某只琥珀色灯亮表明:A．某台发动机灭火手柄的电路开路B．某台发动机灭火瓶释放电路短路．C．某台发动机火警感应元件内失压D．某台发动机火警探测环路短路答案：DATA26防火系统4．检查APU灭火瓶压力合适与否的方法是：A．瓶上的表头。
最新ATA100各章节内容汇总
A T A100各章节内容ATA100各章节内容【附图】ATA100是美国航空运输协会联合各航空公司、航空器制造商出版的一种航空器制造使用规范，将航空器的制造、日常维护工作进行了合理的划分，成为不同的章节。
现在几乎每架飞机都必须遵循这一标准，作为航空器维护人员，了解ATA100是非常重要的。
ATA100 5-12章为航空器日常勤务维护工作，包括时间限制和目视检查、清洁、勤务等等，这里不详细叙述了……21章开始为各个系统章节，分别为：21 AIRCONDITIONNING 空调系统介绍座舱空调系统的加温、冷却、增压、清洁等内容，上图是ECAM的空调系统显示部分。
22 AUTOPILOT 自动飞行现代飞机除去起飞着陆外都采用自动飞行，上边这个就是自动飞行控制面板，通过它可以操作飞机的自动飞行系统，节约人力，安全有效。
23 COMMUNICATIONS 通讯系统飞机在飞行过程中必须受到“空中警察”的管制，与管制员的交流就需要通讯系统，VHF、HF等等。
另外客舱内部飞行员和乘务员也需要交流，这也是通讯系统的一部分。
上图为737NG内话。
24 ELECTRICAL POWER 电源系统飞机运行离不开电，上图为地面电源车，在空中则靠发动机驱动的发电机工作，这章还讲述配电和用电器的相关情况。
25 EQUIP/FURNISHINGS 设备与装饰这章涉及的就是飞机内部的客舱座椅、厨房等各种设备和装饰，与乘客关系和密切。
26 FIRE PROTECTION 防火这是飞机上的灭火器，这章讲述的便是飞行上的防火系统。
27 FLIGHTCONTROLS 飞行操纵这章讲述的是飞行员如何操控飞机的，副翼、升降舵、方向舵等等。
上图就是飞机的驾驶舱。
28 FUEL 燃油飞机使用燃油的储存，释放等等。
上图为加油车。
29 HYDRAULIC POWER 液压系统飞机的各个操纵面、起落架的收放等都需要液压系统的参与，这章讲述的便是液压系统的工作情况、显示等等。
ATA章节中英对照
Chapter 1 – Brief History of AviationChapter 2 – DeregulationChapter 3 – Structure of the IndustryChapter 4 – Airline EconomicsChapter 5 – How Aircraft FlyChapter 6 – SafetyChapter 7 – SecurityChapter 8 – AirportsChapter 9 – Air Traffic ControlChapter 10 – Airlines and the Environment5章时间限制、维修检查(Time Limits,Maint. Checks)6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage) 11章标牌和铭记(Placards and Markings)12章勤务(Servicing)20章标准施工---机体(Standard Practices---Airframe) 21章空调（Air Conditioning）22章自动飞行（Auto Flight）23章通讯（Communications）24章电源（Electrical Power）25章设备/装饰（Equipment/Furnishings）26章.防火(Fire Protection)27章飞行操纵（Flight Controls）28章燃油（Fuel）29章液压源（Hydraulic Power）30章防冰和排雨（Ice and Rain Protection）31章指示/记录系统（Indicating/Recording system）32章起落架(Landing Gear)33章灯光（Lights）34章导航（Navigation）35章氧气(Oxygen)36章气源(Pneumatic)37章真空（Vacuum）38章水/污水（Water/waste）45章中央维护系统（Central maintenance System）49章机载辅助动力装置(Airborne Auxiliary Power)51章结构与标准施工(Structures & Standard Practices) 52章舱门(Doors)53章机身(Fuselage)54章发动机吊舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)安定面56章窗户(Windows)57章机翼(Wings)70章标准施工—发动机(Standard Practices—Engines)71章动力装置(Power Plant( Package))72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))01 INTRODUCTION05 PERIODIC INSPECTIONS06 DIMENSIONS AND AREAS07 LIFTING AND SHORING08 LEVELING AND WEIGHING09 TOWING AND TAXIING10 PARKING, MOORING, STORAGE AND RETURN TO SERVICE11 PLACARDS AND MARKINGS12 SERVICING - ROUTINE MAINTENANCE18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)20 STANDARD PRACTICES - AIRFRAME21 AIR CONDITIONING22 AUTO FLIGHT23 COMMUNICATIONS24 ELECTRICAL POWER25 EQUIPMENT / FURNISHINGS26 FIRE PROTECTION27 FLIGHT CONTROLS28 FUEL29 HYDRAULIC POWER30 ICE AND RAIN PROTECTION31 INDICATING / RECORDING SYSTEMS32 LANDING GEAR33 LIGHTS34 NAVIGATION35 OXYGEN36 PNEUMATIC37 VACUUM38 WATER / WASTE39 ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS41 WATER BALLAST45 CENTRAL MAINTENANCE SYSTEM (CMS)46 INFORMATION SYSTEMS49 AIRBORNE AUXILIARY POWER51 STANDARD PRACTICES AND STRUCTURES - GENERAL52 DOORS53 FUSELAGE54 NACELLES / PYLONS55 STABILIZERS56 WINDOWS57 WINGS60 STANDARD PRACTICES - PROPELLER / ROTOR61 PROPELLERS / PROPULSORS62 MAIN ROTOR(S)63 MAIN ROTOR DRIVE(S)64 TAIL ROTOR65 TAIL ROTOR DRIVE66 ROTOR BLADE AND TAIL PYLON FOLDING67 ROTORS FLIGHT CONTROL70 STANDARD PRACTICES - ENGINE71 POWER PLANT - GENERAL72 ENGINE72(T) ENGINE - TURBINE / TURBOPROP, DUCTED FAN / UNDUCTED FAN 72(R) ENGINE - RECIPROCATING73 ENGINE - FUEL AND CONTROL74 IGNITION75 BLEED AIR76 ENGINE CONTROLS77 ENGINE INDICATING78 EXHAUST79 OIL80 STARTING81 TURBINES (RECIPROCATING ENGINES)82 WATER INJECTION83 ACCESSORY GEAR BOXES (ENGINE DRIVEN)84 PROPULSION AUGMENTATION91 CHARTS5章时间限制、维修检查(Time Limits,Maint. Checks)6章尺寸和区域(Dimensions and Access Panels)7章顶起和支撑(Lifting and Shoring)8章对准和称重(Leveling and Weighing)9章飞机拖曳(Towing and Taxiing)10章飞机停场，系留，封存(Parking,Mooring,Storage)11章标牌和铭记(Placards and Markings)12章勤务(Servicing)BMS3-33润滑脂的介绍20章标准施工---机体(Standard Practices---Airframe)21章空调(Air Conditioning)空调出口温度高原创]关于737-300/500的空调空中超温，会有那些原因引起呢（专业贴）22章自动飞行(Auto Flight)737NG的Y/D故障分析供大家参考23章通讯(Communications)24章电源(Electrical Power)IDG和GEN B2972电源及APU自动关车排故思路之分析25章设备/装饰(Equipment/Furnishings)26章防火(Fire Protection)有关737灭火瓶...... 火警探测27章飞行操纵(Flight Controls)28章燃油(Fuel)737飞机燃油浮子电门29章液压源(Hydraulic Power)液压问题关于液压保险在液压管路的作用和位置请教液压系统故障30章防冰和排雨(Ice and Rain Protection)31章指示/记录系统(Indicating/Recording system)32章起落架(Landing Gear)如何延长飞机轮胎的使用寿命前轮磨损谁能说说金属刹车片和碳刹车片的优缺点请问哪位对防滞刹车结构熟悉的，简单介绍一下，谢谢那里有资料，网上有吗请教:飞机换轮子的时候为什么要转动轮子一起B737-300飞机使用自动速度刹车时，AUTO SPEED BRAKE 跳开关跳开33章灯光(Lights)34章导航(Navigation)35章氧气(Oxygen)36章气源(Pneumatic)一起引气故障导致的增压故障（B737NG）37章真空(Vacuum)38章水/污水(Water/waste)45章中央维护系统(Central maintenance System)49章机载辅助动力装置(Airborne Auxiliary Power)APU启动不起来了! 维护灯亮51章结构与标准施工(Structures & Standard Practices)52章舱门(Doors)53章机身(Fuselage)54章发动机短舱/吊架(Nacelles/Pylons)55章稳定装置(Stabilizers)56章窗户(windows)[讨论]玻璃上裂纹深度的测量57章机翼(wings)70章标准施工---发动机(Standard Practices---Engines)71章动力装置(Power Plant (Package))IAEV2500系列发动机试车总结72章发动机（内部）(Engine (Internals))73章发动机燃油和控制(Engine Fuel and Control)74章点火装置(Ignition)75章发动机空气(Air)76章发动机操纵(Engine Controls)77章发动机指示(Engine Indicating)78章排气系统(Exhaust)737反推故障79章发动机滑油系统(Oil)80章发动机起动(Starting)82章注水(Water Injecting)91章图表（不同性质的）(Charts (Miscellaneous))ATA Specification 22001 *Reserved for Airline Use2 *Reserved for Airline Use3 *Reserved for Airline Use4 *Reserved for Airline Use5 TIME LIMITS/ MAINTENANCE CHECKS-00 General-10 Time Limits-20 Scheduled Maintenance Checks-30 & -40 Reserved-50 Unscheduled Maintenance checks6 DIMENSIONS AND AREAS7 LIFTING & SHORING-00 General-10 Jacking-20 Shoring8 LEVELING & WEIGHING-00 General-10 Weighing and Balancing-20 Leveling9 TOWING & TAXIING-00 General-10 Towing-20 Taxiing10 PARKING, MOORING, STORAGE & RETURN TO SERVICE -00 General-10 Parking/Storage-20 Mooring-30 Return to Service11 PLACARDS AND MARKINGS-00 General-10 Exterior Color Schemes and Markings-20 Exterior Placards and Markings-30 Interior Placards12 SERVICING-00 General-10 Replenishing-20 Scheduled Servicing-30 Unscheduled Servicing13 *Unassigned14 *Unassigned15 *Unassigned16 *Unassigned17 *Unassigned18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY) -00 GENERAL --10 VIBRATION ANALYSIS-20 NOISE ANALYSIS19 *Unassigned20 STANDARD PRACTICES-AIRFRAME-90 *Reserved for Airline Use21 AIR CONDITIONING-00 General-10 Compression-20 Distribution-30 Pressurization Control-40 Heating-50 Cooling-60 Temperature Control-70 Moisture/Air Contaminant22 AUTO FLIGHT-00 General-10 Autopilot-20 Speed-Attitude Correction-30 Auto Throttle-40 System Monitor-50 Aerodynamic Load Alleviating23 COMMUNICATIONS-00 General-10 Speech Communications-15 SATCOM-20 Data Transmission and Automatic Calling-30 Comfort-40 Interphone-50 Audio Integrating-60 Static Discharging-70 Audio & Video Monitoring-80 Integrated Automatic24 ELECTRICAL POWER-00 General-10 Generator Drive-20 AC Generation-30 DC Generation-40 External Power-50 AC Electrical Load Distribution-60 DC Electrical Load Distribution25 EQUIPMENT/FURNISHINGS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Galley-40 Lavatories-50 Additional Compartments-60 Emergency-70 Available-80 Insulation26 FIRE PROTECTION-00 General-10 Detection-20 Extinguishing-30 Explosion Suppression27 FLIGHT CONTROLS-00 General-10 Aileron & Tab-20 Rudder & Tab-30 Elevator & Tab-40 Horizontal Stabilizer-50 Flaps-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -70 Gust Lock & Dampener-80 Lift Augmenting28 FUEL-00 General-10 Storage-20 Distribution-30 Dump-40 Indicating29 HYDRAULIC POWER-00 General-10 Main-20 Auxiliary-30 Indicating30 ICE AND RAIN PROTECTION-00 General-10 Airfoil-20 Air Intakes-30 Pitot and Static-40 Windows, Windshields and Doors -50 Antennas and Radomes-60 Propellers/Rotors-70 Water Lines-80 Detection31 INDICATING/RECORDING SYSTEMS-00 General-10 Instrument & Control Panels-20 Independent Instruments-30 Recorders-40 Central Computers-50 Central Warning Systems-60 Central Display Systems-70 Automatic Data Reporting Systems 32 LANDING GEAR-00 General-10 Main Gear and Doors-20 Nose Gear and Doors-30 Extension and Retraction-40 Wheels and Brakes-50 Steering-60 Position and Warning-70 Supplementary Gear33 LIGHTS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Cargo and Service Compartments -40 Exterior-50 Emergency Lighting34 NAVIGATION-00 General-10 Flight Environment-20 Attitude & Direction-30 Landing and Taxiing Aids-40 Independent Position Determining -50 Dependent Position Determining -60 Flight Management Computing35 OXYGEN-00 General-10 Crew-20 Passenger-20 Passenger-30 Portable36 PNEUMATIC-00 General-10 Distribution-20 Indicating37 VACUUM-00 General-10 Distribution-20 Indicating38 WATER/WASTE-00 General-10 Potable-20 Wash-30 Waste Disposal-40 Air Supply39 *Unassigned40 *Unassigned41 WATER BALLAST-00 General-10 Storage-20 Dump-30 Indication42 *Unassigned43 *Unassigned44 CABIN SYSTEMS-00 General-10 Cabin Core System-20 Inflight Entertainment System-30 External Communication System-40 Cabin Mass Memory System-50 Cabin Monitoring System-60 Miscellaneous Cabin System45 CENTRAL MAINTENANCE SYSTEM-00 General-5 thru -19 CMS/Aircraft General-20 thru -49 CMS/Airframe Systems-45 Central Maintenance System-50 thru -59 CMS/Structures-60 thru -69 CMS/Propellers-70 thru -89 CMS/Power Plant45INFORMATION SYSTEMS-00 General-10 Airplane General Information Systems -20 Flight Deck Information Systems-30 Maintenance Information Systems-40 Passenger Cabin Information Systems -50 Miscellaneous Information Systems47 *Unassigned48 *Unassigned49 AIRBORNE AUXILIARY POWER-00 General-10 Power Plant-20 Engine-30 Engine Fuel and Control-40 Ignition/Starting-50 Air-60 Engine Controls .-70 Indicating-80 Exhaust-90 Oil50 Cargo and Accessory Compartments-00 General-10 Cargo Compartments-20 Cargo Loading Systems-30 Cargo Related Systems-40 Available-50 Accessory-60 Insulation51 Standard Practices, General-00 General-10 Investigation, Cleanup and Aerodynamic Smoothness-20 Processes-30 Materials-40 Fasteners-50 Support of Airplane for Repair and Alignment Check Procedures -60 Control-Surface Balancing-70 Repairs-80 Electrical Bonding52 DOORS-00 General-10 Passenger/Crew-20 Emergency Exit-30 Cargo-40 Service and Miscellaneous-50 Fixed Interior-60 Entrance Stairs-70 Monitoring and Operation-80 Landing Gear53 FUSELAGE-00 General-10 thru -90 (As Required) Fuselage Sections54 NACELLES/PYLONS-00 General-10 thru -40 (As Required) Nacelle Section-50 thru -80 (As Required) Pylon55 STABILIZERS-00 General-10 Horizontal Stabilizer or Canard-20 Elevator-30 Vertical Stabilizer-40 Rudder56 WINDOWS-00 General-10 Flight Compartment-20 Passenger Compartment-30 Door-40 Inspection and Observation57 WINGS-00 General-10 Center Wing-20 Outer Wing-30 Wing Tip-40 Leading Edge and Leading Edge Devices -50 Trailing Edge Trailing Edge Devices -60 Ailerons and Elevons-70 Spoilers-80 (as required)-90 Wing Folding System58 *Unassigned59 *Reserved for Airline Use60 STANDARD PRACTICES - PROPELLER/ROTOR61 PROPELLERS/PROPULSION-00 General-10 Propeller Assembly-20 Controlling-30 Braking-40 Indicating-50 Propulsor Duct62 ROTOR(S)-00 General-10 Rotor blades-20 Rotor head(s)-30 Rotor Shaft(s)/Swashplate Assy(ies) -4063 ROTOR DRIVE(S)-00 General-10 Engine/Gearbox couplings-20 Gearbox(es)-30 Mounts, attachments-40 Indicating64 TAIL ROTOR-00 General-10* Rotor blades-20* Rotor head-30 Available-40 Indicating65 TAIL ROTOR DRIVE-00 General-10 Shafts-20 Gearboxes-30 Available-40 Indicating66 FOLDING BLADES/PYLON-00 General-10 Rotor blades-20 Tail pylon-30 Controls and Indicating67 ROTORS FLIGHT CONTROL-00 General-10 Rotor-20 Anti-torque Rotor control (Yaw control)-30 Servo-control System68 *Unassigned69*Unassigned70 STANDARD PRACTICES - ENGINES71 POWER PLANT-00 General-10 Cowling-30 Fireseals-40 Attach Fittings-50 Electrical Harness-60 Air Intakes-70 Engine Drains72 ENGINE TURBINE/TURBO PROP DUCTED FAN/UNDUCTED FAN-00 General-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted Gear Driven Propulsor) -20 Air Inlet Section-30 Compressor Section-40 Combustion Section-50 Turbine Section-60 Accessory Drives-70 By-pass Section-80 Propulsor Section (Rear Mounted)73 ENGINE FUEL AND CONTROL-00 General-10 Distribution-30 Indicating74 IGNITION-00 General-10 Electrical Power-20 Distribution-30 Switching75 AIR-00 General-10 Engine Anti-Icing-20 Cooling-30 Compressor Control-40 Indicating76 ENGINE CONTROLS-00 General-10 Power Control-20 Emergency Shutdown77 ENGINE INDICATING-00 General-10 Power-20 Temperature-30 Analyzers That-40 Integrated Engine Instrument Systems 78 EXHAUST-00 General-10 Collector/Nozzle-20 Noise Suppressor-30 Thrust Reverser-40 Supplementary Air79 OIL-00 General-10 Storage-20 Distribution-30 Indicating80 STARTING-00 General-10 Cranking81 TURBINES-00 General-10 Power Recovery-20 Turbo-Supercharger82 WATER INJECTION-00 General-10 Storage-20 Distribution-30 Dumping and Purging83 ACCESSORY GEAR-BOXES-00 General-10 Drive Shaft Section-20 Gearbox Section84 Propulsion Augmentation-00 General-10 Jet Assist Takeoff85 *Unassigned86 *Unassigned87 *Unassigned88 *Unassigned89 *Unassigned90 *Unassigned91 CHARTS92 *Unassigned93 *Unassigned94 *Unassigned95 *Reserved for Airline Use96 *Reserved for Airline Use97 WIRING REPORTING-00-00 General-01-00 Zone 100 Fuselage Lower-02-00 Zone 200 Fuselage Top-03-00 Zone 300 Stabilizers-04-00 Zone 400 Nacelles-Pylons-05-00 Zone 500 Left Wing-06-00 Zone 600 Right Wing-07-00 Zone 700 Landing Gear Compartment -08-00 Zone 800 Doors-09-00 Zone 900 Lavatories & Galleys-20-00 Electrical Standard Items/Practices -21-00 Air Conditioning - General-21-10 Compression-21-20 Distribution-21-30 Pressurization Control-21-40 Heating-21-50 Cooling-21-60 Temperature Control-21-70 Moisture/Air Contaminant Control-22-00 Auto Flight - General-22-10 Autopilot-22-20 Speed - Attitude Correction-22-30 Auto Throttle-22-40 System Monitors-22-50 Aerodynamic Load Alleviating-23-00 Communications - General-23-10 Speech Communications-23-15 SATCOM-23-20 Data Transmission and Automatic Calling-23-30 Passenger Address, Entertainment and Comfort-23-40 Interphone-23-50 Audio Integrating-23-60 Static Discharging-23-70 Audio and Video Monitoring-23-80 Integrated Automatic Tuning-24-00 Electrical Power - General-24-10 Generator Drive-24-20 AC Generation-24-30 DC Generation-24-40 External Power-24-50 AC Electrical Load Distribution-24-60 DC Electrical Load Distribution-25-00 Equipment/Furnishings - General-25-10 Flight Compartment-25-20 Passenger Compartment-25-30 Galley-25-40 Lavatories-25-60 Emergency-25-80 Insulation-26-00 Fire Protection - General-26-10 Detection-26-20 Extinguishing-26-30 Explosion Suppression-27-00 Flight Controls - General-27-10 Aileron & Tab-27-20 Rudder & Tab-27-30 Elevator & Tab-27-40 Horizontal Stabilizer-27-50 Flaps-27-60 Spoiler, Drag Devices and Variable Aerodynamic Fairings -27-70 Gust Lock & Dampener-27-80 Lift Augmenting-28-00 Fuel - General-28-10 Storage-28-20 Distribution-28-30 Dump-28-40 Indicating-29-00 Hydraulic Power - General-29-10 Main-29-20 Auxiliary-29-30 Indicating-30-00 Ice and Rain Protection - General-30-10 Airfoil-30-20 Air Intakes-30-30 Pitot and Static-30-40 Windows, Windshields and Doors-30-50 Antennas And Radomes-30-60 Propellers/Rotors-30-70 Water Lines-30-80 Detection-31-00 Indicating/Recording Systems - General -31-10 Instrument and Control Panels-31-20 Independent Instruments-31-30 Recorders-31-40 Central Computers-31-50 Central Warning Systems-31-60 Central Display Systems-31-70 Automatic Data Reporting Systems-32-00 Landing Gear- General-32-10 Main Gear and Doors-32-20 Nose Gear and Doors-32-30 Extension and Retraction-32-40 Wheels and Brakes-32-50 Steering-32-60 Position And Warning-32-70 Supplementary Gear-33-00 Lights - General-33-10 Flight Compartment-33-20 Passenger Compartment-33-30 Cargo and Service Compartments-33-40 Exterior-33-50 Emergency Lighting-34-00 Navigation - General-34-10 Flight Environment Data-34-20 Attitude & Direction-34-30 Landing and Taxiing Aids-34-40 Independent Position Determining-34-50 Dependent Position Determining-34-60 Flight Management Computing-35-00 Oxygen - General-35-10 Crew-35-20 Passenger-35-30 Portable-36-00 Pneumatic - General-36-10 Distribution-36-20 Indicating-37-00 Vacuum - General-37-10 Distribution-37-20 Indicating-38-00 Water/Waste - General-38-10 Potable-38-20 Wash-38-30 Waste Disposal-38-40 Air Supply-44-00 Cabin Systems - General-44-10 Cabin Core System-44-20 In-flight Entertainment System-44-30 External Communication System-44-40 Cabin Mass Memory System-44-50 Cabin Monitoring System-44-60 Miscellaneous Cabin System-45-00 Central Maintenance System (CMS) General -45-05 CMS/Aircraft General-45-20 CMS/Airframe Systems-45-45 Central Maintenance System-45-50 CMS/Structures-45-60 CMS/Propellers-45-70 CMS/Power Plant-46-00 Information Systems - General-46-10 Airplane General Information Systems-46-20 Flight Deck Information Systems-46-30 Maintenance Information Systems-46-40 Passenger Cabin Information Systems-46-50 Miscellaneous Information Systems-49-00 Airborne Auxiliary Power - General-49-10 Power Plant-49-20 Engine-49-30 Engine Fuel And Control-49-40 Ignition And Starting-49-50 Air-49-60 Engine Controls-49-70 Indicating-49-80 Exhaust-49-90 Oil-50-00 Cargo And Accessory Compartments General -50-10 Cargo Compartments-50-20 Cargo Loading Systems-50-30 Cargo Related Systems-50-40 Available-50-50 Accessory Compartments-50-60 Insulation-52-00 Doors - General-52-10 Passenger/Crew-52-20 Emergency Exit-52-30 Cargo-52-40 Service-52-50 Fixed Interior-52-60 Entrance Stairs-52-70 Door Warning-52-80 Landing Gear-53-00 Fuselage - General-54-00 Nacelles/Pylons - General-54-10 Nacelle Section-54-50 Pylon-55-00 Stabilizers - General-55-10 Horizontal Stabilizer or Canard-55-20 Elevator-55-30 Vertical Stabilizer-55-40 Rudder-56-00 Windows - General-56-10 Flight Compartment-56-20 Passenger Compartment-56-30 Door-56-40 Inspection and Observation-57-00 Wings - General-57-10 Center Wing-57-20 Outer Wing-57-30 Wing Tip-57-40 Leading Edge and Leading Edge Devices -57-50 Trailing Edge and Trailing Edge Devices -57-60 Ailerons-57-70 Spoilers-57-90 Wing Folding System-61-00 Propellers/Propulsors - General-61-10 Propeller Assembly-61-20 Controlling-61-30 Braking-61-40 Indicating-61-50 Propulsor Duct-62-00 Rotors-63-00 Rotor Drives-64-00 Tail Rotor-65-00 Tail Rotor Drive-66-00 Folding Blades/Pylon-67-00 Rotors Flight Control-71-00 Power Plant - General-71-10 Cowling-71-20 Mounts-71-30 Fire seals-71-40 Attach Fittings-71-50 Electrical Harness-71-60 Air Intakes-71-70 Engine Drains-72-00 Engine Turbine/Turbo Prop Ducted Fan/Unducted Fan-72-10 Reduction Gear, Shaft Section (Turbo-Prop and/or Front Mounted Gear Driven Propulsor)-72-20 Air Inlet Section-72-30 Compressor Section-72-40 Combustion Section-72-50 Turbine Section-72-60 Accessory Drives-72-70 By-pass Section-72-80 Propulsor Section (Rear Mounted)-73-00 Engine Fuel And Control - General-73-10 Distribution-73-20 Controlling-73-30 Indicating-74-00 Ignition - General-74-10 Electrical Power Supply-74-20 Distribution-74-30 Switching-75-00 Air - General-75-10 Engine Anti-Icing-75-20 Cooling-75-30 Compressor Control-75-40 Indicating-76-00 Engine Controls - General-76-10 Power Control-76-20 Emergency Shutdown-77-00 Engine Indicating - General-77-10 Power-77-20 Temperature-77-30 Analyzers-77-40 Integrated Engine Instrument Systems-78-00 Exhaust - General-78-10 Collector/Nozzle-78-20 Noise Suppressor-78-30 Thrust Reverser-78-40 Supplementary Air-79-00 Oil - General-79-10 Storage-79-30 Indicating-80-00 Starting - General-80-10 Cranking98 *Reserved for Airline Use99 *Unassigned100 *Do not use101 *Do not use102 *Do not use103 *Do not use104 *Do not use105 *Do not use106 *Do not use107 *Do not use108 *Do not use109 *Do not use110 *Do not use111 *Do not use112 *Do not use113 *Do not use114 *Do not use115 Flight Simulator Systems。
A320机型试题6-ATA_26防火
ATA 26防火200. APU仅在地面起火时起动什么附加的外部警告：A 一个外部喇叭警告B 一个火警铃声警告C APU火警灯和一个外部喇叭警告201. 通过测试按钮可测试哪些系统？A 火警探测系统B 灭火系统C 以上两者202. 发动机和APU灭火系统是由相关的火警探测组件(FDUS)控制的吗：A 不是B 是203. 灭火剂按钮何时起动：A 发动机防火按钮拉出并爆破（SQUIB）灯亮。
B 相应的“释放”(DISCH)灯亮C 发动机防火按钮开关处于“ON”位204. APU在地面起火时，正常情况下如何灭火A 从APU防火面板B 自动C 从外部电源面板205. 在无电源连接的情况下，如何探测APU灭火瓶的热敏释放：A 由飞行指引组件(FDU)B 由ECAMC 由红圆盘指示器206. APU火警探测系统有几个火警感应元件：A 三个B 两个C 一个207. APU防火按钮释放时，什么系统被隔离：A 燃油，电气B 空气，电气C 燃油，空气，电气208. 当发动机防火手柄拉出时，哪些个活门受影响：A ENG低压燃油关闭活门和回油活门+液压防火关断活门+引气活门+PACK流量控制活门+发电机B 液压防火关断活C 吸力供油活门209. 当APU防火手柄拉出时：A APU发电机断电B APU发电机断开C APU发电机通电210. 在地面进行APU自动灭火时，是否需要使用外部电源面板上的APU关断活门：A 是B 不是211. 发动机火警探测器位于何处？A 吊架，风扇及核心机部分B 核心机和齿轮箱C 风扇和涡轮212. 发动机防火手柄拉出时，哪些飞机系统被隔离：A 燃油，电气，空气B 燃油，液压，空气C 燃油，液压，电气，空气213. 当一个发动机防火手柄拉出时，爆炸帽指示灯是否燃亮A 是B 否214. 发动机和APU防火系统包括：A 每台发动机两个灭火瓶，APU一个灭火瓶B 每台发动机一个灭火瓶，APU一个灭火瓶C 每台发动机两个灭火瓶，APU两个灭火瓶215. 发动机灭火系统由FDU（火警探测组件）控制吗？A 是。
ATA章节号(english)
A T A章节号ATA05 Time Limits/Maintenance Check 时限ATA06 Dimensions and Areas 尺寸和区域ATA07 Lifting and Shoring 顶升与支撑ATA08 Leveling and Weighting 平衡与称重ATA09 Towing and Taxing 牵引与滑行ATA10 Parking and Mooring 停放与系留ATA11 Placards 标牌ATA12 Servicing 勤务ATA20 Standard Practices-Airframe 系统标准施工ATA21 Air Conditioning 空调ATA22 Auto Flight 自动驾驶ATA23 Communications 通信ATA24 Electrcal Power 电源ATA25 Equipment/Furnishings 设备和装饰ATA26 Fire Protection 防火ATA27 Flight Controls 飞行控制ATA28 Fuel 燃油ATA29 Hydraulics Power 液压ATA30 Ice and Rain Protection 防冰/防雨ATA31 Instruments 指示/记录系统ATA32 Landing Gear 起落架ATA33 Lights 灯光ATA34 Navigation 导航ATA35 Oxygen 氧气ATA36 Pneumatic 气源系统ATA38 Water and Waste 水和废物ATA44 Cabin 客舱系统ATA49 Airborne Auxiliary Power Unit 辅助动力装置ATA51 StructuresATA52 Doors 门ATA55 Stabilizers 安定面ATA56 WindowsATA57 Wings 机翼ATA61 PropellerATA70 Standard Practices-EngineATA71 Power Plant 动力装置ATA72 Engine 发动机ATA73 Engine Fuel and Controls 发动机燃油和控制ATA74 Ignition 点火ATA75 Air 发动机空气ATA76 Engine Controls 发动机控制ATA77 Engine Indicating 发动机指示ATA78 Exhaust 排气ATA79 Oil 发动机滑油ATA80 Starting 起动ATA91 Charts190 CMC阅读参数方式。
ATA26 维护程序(M)
防火
操作
结果
1. 在发动机吊架: 连接直流电压表 在: .
- 销钉1和地面接地点
电压表读数为 OVDC
- 销钉2和地面接地点
在ENG/APU FIRE面板1WD:
- 打开ENG 1(2) FIRE按压电门的保护罩
- 按下然后松开 ENG 1(2) FIRE按压电 门
4－Get Access (1) 放置工作梯在吊架下面 (2) 拆下接近面板: (a)对于6WE1 (BOTTLE 1-FIRE EXTING, ENG 1), 8WE1 (BOTTLE 2-FIRE EXTING, ENG 1) 415BR, 415BL (b) 对于6WE2 (BOTTLE 1-FIRE EXTING, ENG 2), 8WE2
防火
- 低压燃油关断活门 (APU)
- 燃油电磁阀活门(APU)
- 引气活门APU)
6－操作测试防火线路和测试线路
操作
结果
1.在电插头12WF-A: - 从销钉A和B上拆下暂时接地连接 2.在电插头12WF-A: - 连接万用表在销钉A和B之间
3.在APU防火面板20VU: -撤销接地然后按下，释放APU防火按压 电门 - 按压保持住APU AGENT 按压电门
在万用表 - 0 VDC显示 在万用表 - 28 VDC显示
NOTE: 忽略APU AGENT SQUIB符号和其他 后来的效应
4.在APU防火面板20VU: - 释放APU AGENT 按压电门
在万用表 - 0 VDC显示
防火
5.在电插头12WF-A: - 连接万用表在销钉B和地之间
6.在APU防火面板20VU: - 按压保持住APU AGENT 按压电门
ATA26 防火
ATA26 防火26-00-00 概述一、维护性安全防范措施1.在刚刚关车的发动机工作时要注意，发动机的高温将持续一个小时。
2．只在有好的通风条件下，使用溶解/清洁剂、密封剂和其他特殊的材料，遵守制造厂的说明。
穿防护衣，不要让它们进入嘴里，不要在工作区域吸烟，不要吸入这种气体。
这些材料是有毒、易燃且会刺激皮肤的，如果皮肤或眼睛受到刺激，寻求医疗救助。
3．在反推和反推附近工作时，反推液压控制组件必须解除。
没能正确解除可能导致反推的作动，造成人员受伤或设备损坏。
26-12-00 发动机火警及过热探测一、概述1.当做发动机火警自检测试时，测试按钮电门必须按压并保持住。
2．维护信息清单通过FDU送到CFDIU，故障在地面上发生，地面优先于维护信息。
二、目视检查发动机火警探测系统1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．在做维护工作前，确保发动机停车不低于5分钟。
3．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
26-12-12 发动机和APU防火面板的拆装一、拆装发动机和APU防火面板1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
2．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
3．在顶板25VU上，放警告牌以告诉人们不要起动APU。
二、拆装火警按钮电门1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
2．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
3．在顶板25VU上，放警告牌以告诉人们不要起动APU。
26-12-15/16/17 发动机风扇/短舱/核心机防火探测环路拆装一、注意事项1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
B级-ATA26-01探测系统【B级考试资料】
发动机火警探测器
下表列出安装在不同探测区域的探测器温度特性：
探测区域 风扇机匣上部 风扇机匣下部 核心机左侧 核心机右侧
过热 345F (174C) 345F (174C) 650F (343C) 650F (343C)
火警 580F (304C) 580F (304C) 850F (454C) 850F (454C)
货舱烟雾探测-部件位置
货舱烟雾探测-部件位置
前、后货舱，各装有多个烟雾探测器和1个CEU 前货舱，4个烟雾探测器；后货舱，6个烟雾探测器 探测器，安装在货舱天花板；拆下保护盖，接近烟雾探测器 CEU，安装在货舱天花板；拆下保护盖，接近CEU
货舱烟雾探测器
货舱烟雾探测器
烟雾探测器，监控烟雾和过热
发动机和APU火警探测控制盒
发动机和APU火警探测控制盒
控制盒，监控发动机火警探测器的过热和火警情况，也监控APU探测器的火警情况 控制盒内部，装有发动机过热/火警探测和APU火警探测相关控制电路 控制盒前面板，带有以下部件： -ENGINE 1 LOOP A 故障灯（琥珀色） -ENGINE 1 LOOP B 故障灯（琥珀色）
发动机和APU火警探测控制盒
当多个环路故障时，系统根据下表的优先级依次显示：
最高优先级
最低优先级
Engine 1 Engine 1 Engine 2 Engine 2 APU
Loop A Loop B Loop A Loop B
如果同时存在多个故障，只有当较高优先级的故障排除后，较低优先级的故障才会 显示
注
-ENGINE 2 LOOP A 故障灯（琥珀色） -ENGINE 2 LOOP B 故障灯（琥珀色） -APU故障灯（琥珀色） -FAULT DISPLAY 灯（红色）（3个） -FAULT/INOP 测试电门
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ATA26 防火26-00-00 概述一、维护性安全防范措施1.在刚刚关车的发动机工作时要注意，发动机的高温将持续一个小时。
2．只在有好的通风条件下，使用溶解/清洁剂、密封剂和其他特殊的材料，遵守制造厂的说明。
穿防护衣，不要让它们进入嘴里，不要在工作区域吸烟，不要吸入这种气体。
这些材料是有毒、易燃且会刺激皮肤的，如果皮肤或眼睛受到刺激，寻求医疗救助。
3．在反推和反推附近工作时，反推液压控制组件必须解除。
没能正确解除可能导致反推的作动，造成人员受伤或设备损坏。
26-12-00 发动机火警及过热探测一、概述1.当做发动机火警自检测试时，测试按钮电门必须按压并保持住。
2．维护信息清单通过FDU送到CFDIU，故障在地面上发生，地面优先于维护信息。
二、目视检查发动机火警探测系统1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．在做维护工作前，确保发动机停车不低于5分钟。
3．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
26-12-12 发动机和APU防火面板的拆装一、拆装发动机和APU防火面板1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
2．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
3．在顶板25VU上，放警告牌以告诉人们不要起动APU。
二、拆装火警按钮电门1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
2．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
3．在顶板25VU上，放警告牌以告诉人们不要起动APU。
26-12-15/16/17 发动机风扇/短舱/核心机防火探测环路拆装一、注意事项1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．在做维护工作前，确保发动机停车不低于5分钟。
3．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
4．固定卡箍将火警探测器元件和支撑管作为一个组件固定在一起。
26-12-34 发动机火警探测组件拆装一、注意事项1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．断开下列断路器，打保险并挂标签：（1）对于2WD149VU ENGINE/1/FIRE DET/LOOP A 7WD1 A06121VU ENGINE/ENG1/FIRE DET/LOOP B 8WD1 Q38（2）对于2WD249VU ENGINE/2/FIRE DET/LOOP B 8WD2 A07121VU ENGINE/ENG2/FIRE DET/LOOP A 7WD2 Q3926-13-00 APU火警及过热探测一、APU火警和过热探测系统的操作测试1．在测试期间，必需防止不必要的自动灭火器排放（参见TFU REF 26.22.00.007）。
26-13-15 APU防火探测环路拆装一、安装1．必须在工作时遵守其提供的间隙和长度限制。
26-13-34 APU火警探测组件拆装一、注意事项1．在顶板25VU上，放警告牌以告诉人们不要起动APU。
26-15-00 电子舱烟雾探测一、概述1．当烟雾的浓度下降到低于警戒水平时，烟雾探测器将返回初始状态。
二、电子舱烟雾探测操作测试1．飞机在全面供电后，通风系统将进行一次全面的测试，这个程序将持续大约2分钟。
2．压入靠近测试指示的行选键时，启动通风系统的全面测试。
三、清洁烟雾探测器管道1．在用压缩空气清洁管道时要戴上护目镜，防止压缩空气和吹出的碎片伤害眼睛。
26-15-15 电子舱烟雾探测器拆装一、安装电子舱烟雾探测器1．在安装烟雾探测器时，要将探测器上的挡片正确的安装在通气管道的相应标记的下部。
26-16-00 货舱烟雾探测一、通过CFDS对货舱烟雾探测作操作测试以确认隔离活门锁定电路的完整性1．开始测试前，确保SDCU通电至少一分钟。
二、货舱烟雾探测器敏感性功能测试1．烟雾探测器灵敏度时要在烟雾探测器的电路上连接一个测量仪，测量仪的最小输入电阻是10兆欧。
2．烟雾探测器有两种，一种是“电离型”，一种是“光电型”，两种型号使用与其相对应的程序。
26-16-15 货舱烟雾探测器拆装一、注意事项1．不要尝试打开或者修理烟雾探测器，探测器含有大约0.4微居里的放射性的镅241，只有通过制造商授权的车间可以处理烟雾探测器。
26-17-00 厕所烟雾探测一、厕所烟雾探测器敏感性功能测试1．SDCU做烟雾探测器的自动测试时，电压为6-6.5付直流电压，敏感性检查必须在探测器处于备用状况下大约10秒后进行。
26-17-15 厕所烟雾探测器拆装一、注意事项1．不要尝试打开或者修理烟雾探测器，探测器含有大约0.4微居里的放射性的镅241，只有通过制造商授权的车间可以处理烟雾探测器。
26-21-00 发动机灭火一、概述1．只要火警探测组件探测到火警，则发动机火警按钮电门灯就亮。
2．在发动机/APU火警面板上做灭火测试时，将测试按钮电门压下并保持到整个测试结束，相应的测试程序时间不超过1秒。
3．每个灭火瓶上的爆炸帽都有两条线路供电，虽然一条线路就能点燃爆炸帽，但测试只有在两条线路都供电的情况下才可通过。
测试电流被测试组件限定在80mA，而引爆电流却是50A。
4．压力电门的测试时：（1）P>最小压力=插钉2和3之间是通路；（2）P<最小压力=插钉1和3之间是通路。
二、灭火瓶压力检查1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．在做维护工作前，确保发动机停车不低于5分钟。
3．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
4．需要两个人来完成此项检查，一个人看测量仪的数值，另一人来操作六角扳手。
5．操作六角扳手时注意，不能强迫其转动，否则将损坏压力电门。
6．如果灭火瓶的压力是正常的，松开六角扳手，它将回到原始位置。
7．如果显示不正常，进行灭火瓶的称重。
8．在进行发动机火警和过热探测（环路/爆炸帽）做操作测试时，忽略在发动机/APU火警面板1WD上发动机灭火剂按钮电门上亮的DISCH灯。
三、发动机火警线路测试1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
三、AGENT按钮电门爆炸帽测试1．开始测试之前确保发动机1（2）火警按钮电门压入。
2．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
3．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
4．在做维护工作前，确保发动机停车不低于5分钟。
5．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
6．断开下列断路器，打保险并挂标签：121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/B 2WE1 Q44121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL1/SQUIB/A 1WE1 Q43121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/B 2WE2 Q42121VU ENGINE/ENG1 AND 2 FIRE EXTIG/BTL2/SQUIB/A 1WE2 Q417．在按下发动机火警按钮电门后将会有下列反应，确保操作不会对其它系统造成不必要的影响。
（1）发电机停止工作；（2）低压燃油活门关闭；（3）液压防火关断活门关闭；（4）引气活门关闭；（5）防冰活门关闭；（6）空调PACK活门关闭。
8．如果故障的爆炸帽灯亮：（1）更换爆炸帽；（2）从飞机接地点断开插钉1和2；（3）从爆炸帽上拆下分路装置；（4）连接插头5WE1-A（5WE2-A）和7WE2-A（7WE2-A）到爆炸帽；（5）确保插头正确地连接；（6）做发动机火警和过热探测（环路/爆炸帽）操作测试。
9．如果有故障的爆炸帽灯不亮：（1）火警测试系统故障；（2）做手册中相关测试以确保击发系统工作正常。
10．如测试OK：（1）击发系统正常，火警测试系统有故障，飞机能够继续飞行；（2）断开电压计；（3）从爆炸帽上拆下分路插头；（4）连接插头5WE1-A（5WE2-A）和7WE1-A（7WE2-A）到其爆炸帽；（5）确保插头正确地连接（6）在发动机/APU火警面板1WD上，关闭发动机1（2）火警按钮电门的护盖；（7）做发动机火警和过热探测（环路/爆炸帽）操作测试；（8）做液压火关断活门操作测试。
11．如果测试结果不正确（没有电压）：进行火警系统排故。
四、灭火瓶低压指示电路的操作检查1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．在做维护工作前，确保发动机停车不低于5分钟。
3．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
五、检查火警线路导通性1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
2．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
3．在做维护工作前，确保发动机停车不低于5分钟。
4．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
六、检查分配管路的泄漏和阻塞1．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。
2．在做维护工作前，确保发动机停车不低于5分钟。
3．在维护面板50VU上确保发动机FADEC地面电源按钮电门的ON灯熄灭，并且放置一块警告牌以告诉人们不要对FADEC系统通电。
4．在对加满的灭火瓶工作时必须非常小心，较大的振动将会引起灭火瓶的激发。
七、发动机火警电门的功能测试1．重置发动机1（2）APU火警按钮电门时，要在完全压下按钮电门至锁上位之后再关闭保护盖，不能试图将保护盖和按钮电门一同压入。
2．在中央操纵台上的发动机面板115VU 上放置一个警告牌，告诉人员不要起动发动机。