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A CLASS 3 FAILURE:

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AMONG THE FOLLOWING, THE STEP NOT APPLICABLE TO THE STORAGE PROCEDURE FOR LESS THAN 6 MONTHS, IS:

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AT THE MAIN LANDING GEAR STATION, THE LOCATION FOR THE RAM AIR TURBINE (RAT) SAFETY DEVICE INSTALLATION IS ON THE:

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DMC 1 NORMALLY PROCESSES:

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EFIS AND ECAM DISPLAY UNITS (CRT'S) ARE:

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ELECTROSTATIC DISCHARGE SENSITIVE EQUIPMENT ARE IDENTIFIED BY:

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ELECTROSTATIC ELECTRICITY IS BUILD UP BY:

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IF BATTERY VOLTAGE IS BELOW 25 VOLTS, THE NECESSARY CHARGING CYCLE IS:

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IF ENGINE REVERSER COWLS HAVE BEEN OPENED FOR MAINTENANCE ACTION THE:

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IF THE AIRCRAFT POINTS INTO THE WIND AND WIND SPEED IS BETWEEN 50 AND 70 KTS, MOOR THE AIRCRAFT AT THE:

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IN NORMAL OPERATION, IF SOME LIGHTS ARE ILLUMINATED, THESE LIGHTS COULD BE:

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IN THE CENTRALIZED FAULT DISPLAY SYSTEM, FAILURE DETECTION IS PERFORMED BY THE:

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JACKING OPERATION IS LIMITED IF THE WIND VELOCITY EXCEEDS VALUES DEPENDING ON THE AIRCRAFT:

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LEVELING THE AIRCRAFT WITH THE ATTITUDE MONITOR CONSISTS IN:

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THE A321 IS THE A320 MODIFIED WITH:

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THE AIRCRAFT GROUNDING ATTACHMENT IS INSTALLED ON THE:

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THE AIRCRAFT IS EQUIPPED WITH:

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THE AIRCRAFT MAINTENANCE MANUAL (AMM) COVERS:

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THE ATTENTION GETTERS (AURAL WARNING AND WARNING LIGHTS) ARE GENERATED BY:

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THE BASIC PRECAUTIONS TO BE TAKEN IN THE CASE OF ELECTROSTATIC DISCHARGE SENSITIVE EQUIPMENT HANDLING ARE:

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THE CARBON FIBER REINFORCED PLASTIC (CFRP) IS MAINLY USED FOR:

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THE CRITERIA THAT DEFINE THE ENGINE NOISE DANGER AREAS ARE:

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THE CUSTOMIZED MANUAL CONTAINS INFORMATION APPLICABLE TO:

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THE FLIGHT PHASES ARE COMPUTED BY:

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THE FULL BITE FUNCTIONS AND MEMORIZATION OPERATE:

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THE GENERAL BELLY FAIRING SECTION BASE NUMBER IS:

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THE LAST ACTIONS OF THE COMPUTER INSTALLATION ARE TO:

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THE MAINTENANCE PLANNING DOCUMENT (MPD) COVERS:

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THE NEW TECHNOLOGY USED FOR LASER BEAM WELDED PANELS IS:

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THE NUMBER OF POTABLE WATER DRAIN PANELS FOR THE AIRBUS A320 IS:

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THE POSITION OF THE CHOCKS WHEN THE AIRCRAFT IS PARKED SHOULD BE:

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THE REFERENCE (X=0) FOR ALL STRUCTURAL MEASUREMENTS IN THE X-AXIS IS INSTALLED:

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THE SIDE STICKS AND NOSE WHEELS STEERING HANDLES ARE MOUNTED:

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THE SUB-ZONES 330 & 340 IDENTIFY THE LEFT HAND AND RIGHT HAND OF THE:

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TOWING SPEED LIMITATION DEPENDS ON:

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TURNING RADII DEPENDS ON:

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WHEN AN EFIS DISPLAY UNIT (DU) FAILS:

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WHEN THE PARKING BRAKE IS SET TO OFF:

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IPC中”RU010” 表示:

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导线3231-0019的种类, 直径, 长度及相关插钉件号可以在那种手册中找到:

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机身的蒙皮由于鸟击而出现凹坑, 则其允许损伤及放行标准一般在:

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机身外形整流罩丢失时, 放行可能参考:

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如要查询出与一个设备相连的所有导线, 则可通过:

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如在AMM中要求使用消耗材料04-024, 则:

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下列关于FIN号说法错误的是：

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下面哪个表述是正确的:

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线路损伤评估使用什么手册？

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线路修理方法使用什么手册？

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已知导线的识别号, 如何查找导线的插钉件号:

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在IPC 的件号有效性中, 有时需要参考某一服务信涵SIL了解件号的互换性和混装性, 而SIL 如何查寻:

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在根据PFR上的ECAM和CFDS信息确定排故程序时:

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飞机顶升时应：

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发动机参数在哪里显示？

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方向舵配平位置：

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滑梯不能自动充气怎么办？

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氧气选择开关在100%位时，

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ILS接收机：

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飞机上ATC天线的数量：

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当自动推力工作时：

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VHF COM3天线位于：

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所有通讯系统都可在MCDU上进行测试，除了：

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发动机表征推力的参数是N1

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发动机齿轮附件盒由_____驱动.

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正常飞行期间，当蒙皮温度低于+35℃时，电子舱通风系统控制冷却空气的温度，方法是：

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A PACK FLOW CONTROL VALVE IS ELECTRICALLY CONTROLLED TO CLOSE:

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AN OUTLOW VALVE REGULATES THE ESCAPE OF AIR FROM THE PRESSURIZED AREAS:

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CABIN PRESSURE CONTROLLER TRANSFER OCCURS:

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CABIN PRESSURIZATION IS CONTROLLED BY:

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CONCERNING THE PRESSURIZATION SAFETY VALVES, THE CORRECT STATEMENT IS:

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DURING MANUAL PRESSURIZATION CONTROL, PRESSURIZATION DATA FOR ECAM DISPLAY IS AVAILABLE FROM:

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EACH CABIN PRESSURE CONTROLLER (CPC) CONTROLS:

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FOR GROUND OPERATIONS IN HEAVY RAIN, THE AVIONICS VENTILATION SYSTEM SHOULD BE RECONFIGURED BY:

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IF BOTH CHANNELS OF A PACK CONTROLLER FAIL, THE PACK OUTLET TEMPERATURE IS PNEUMATICALLY CONTROLLED TO 15 DEG C. BY:

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IF THE MOD SEL P/B ON THE PRESS PANEL IS SET TO MAN, THEN THE DITCHING P/B IS SET TO ON:

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IF THERE IS A PRIMARY CHANNEL FAILURE IN THE ZONE CONTROLLER:

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IF THERE IS AN OVERHEAT IN A ZONE DISTRIBUTION DUCT:

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IN ANTI-ICE MODE, THE PACK ANTI-ICE VALVE IS CONTROLLED BY:

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IN CASE A FWD CARGO DUCT OVERHEAT CONDITION OCCURS, THE:

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IN MANUAL MODE, THE SIGNALS FOR WARNINGS AND INDICATIONS COME FROM:

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IN NORMAL CONDITIONS, THE AIR SENT TO THE COCKPIT IS:

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IN NORMAL CONDITIONS:

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IN THE AFT CARGO COMPARTMENT VENTILATION/HEATING SYSTEM,THE HOT AIR P/BSW CONTROLS THE:

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IN THE AVIONICS VENTILATION SYSTEM, THE FAULT LIGHT ON THE BLOWER P/B SWITCH ILLUMINATES IN CASE OF:

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IN THE AVIONICS VENTILATION SYSTEM, THE FAULT LIGHT ON THE EXTRACT P/B SWITCH ILLUMINATES IN CASE OF:

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IN THE FORWARD CARGO COMPARTMENT VENTILATION/HEATING SYSTEM,THE HOT AIR P/BSW CONTROLS THE:

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LANDING GEAR CONTROL AND INTERFACE UNITS (LGCIU) 1 AND 2 SEND A SIGNAL TO THE:

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LAVATORY AND GALLEY EXTRACTED AIR IS ALSO USED TO VENTILATE THE:

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ON MANUAL MODE, AS LONG AS THE MANUAL VERTICAL/SPEED CONTROL SWITCH IS HELD IN THE DOWN POSITION, THE MANUAL MOTOR CONTROLS THE OUTFLOW VALVE TO:

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ON THE CLASSIC SYSTEM, AFTER A PACK CONTROLLER FAILURE, TO MAINTAIN A PACK TEMPERATURE OF 15Hv (59Kv), THE ANTI-ICE (A.ICE) VALVE IS CONTROLLED BY:

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ON THE CLASSIC SYSTEM, THE PACK OUTLET TEMPERATURE IS CONTROLLED BY:

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THE CONTROL OF THE COCKPIT AND CABIN AIR CONDITIONING SYSTEM IS NOW ENSURED BY:

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THE FLOW RATE OF THE PACK FLOW CONTROL VALVE (FCV) IS CONTROLLED:

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ONE OF THE FOLLOWING AVIONICS VENTILATION SYSTEM COMPONENTS IS NOT AN LRU:

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OPERATION OF THE AIR CONDITIONING PACK ANTI ICE VALVE BY THE ACSC IS BASED UPON:

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THE A/C SKIN TEMPERATURE IS MONITORED BY THE AEVC BECAUSE IT IS USED TO:

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THE AIR CONDITIONING PACK RAM AIR INLET ACTUATOR INTEGRATES:

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THE AVIONICS VENTILATION SYSTEM IS IN OPEN CONFIGURATION:

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THE AVIONICS VENTILATION SYSTEM PROVIDES COOLING FOR:

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THE AVIONICS VENTILATION SYSTEM USES AIR FROM THE AIR CONDITIONING SUPPLY DUCT WHEN:

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THE BASIC TEMPERATURE IS REGULATED BY THE ZONE CONTROLLER (ZC) BY USING THE: