Chapter 1Aircraft general.docx

1、Chapter 1 Aircraft generalChapter 1 Aircraft general01 Aircraft generalBTHE AIRCRAFT MAINTENANCE MANUAL (AMM) COVERS: Time Limits for aircraft components. System Descriptions, Test Procedures and Instructions for Removal/Installation and Deactivation/Reactivation. Maintenance Planning Data and Lette

2、r Check Intervals.01 飞机概述B飞机维修手册(AMM)涉及：飞机部件的时效限制系统描述，安装/拆卸及保留/复原测试程序和指令维修计划数据和信函核对间隔01 Aircraft generalCTHE MAINTENANCE PLANNING DOCUMENT (MPD) COVERS: Time frames for tire removal. Planning data for unscheduled maintenance work. Time intervals for maintenance, inspections/checks and additional dat

3、a.01 飞机概述C维修计划文件(MPD)涉及：轮胎拆卸的时间限定非定期维修工作的计划数据维修，检验/检查，和附加数据的时间间隔01 Aircraft generalATHE CARBON FIBER REINFORCED PLASTIC (CFRP) IS MAINLY USED FOR: Primary structures. Secondary structures.Primary and secondary structures.01 飞机概述A碳纤维强化塑料(CFRP)主要用在主要的结构上次主要的结构上主要的和次主要的结构上01 Aircraft generalBTHE NUMBER

4、 OF POTABLE WATER DRAIN PANELS FOR THE AIRBUS A320 IS: 1. 2. 3.01 飞机概述B空客A320飞机上饮用水排放面板有几个？ 1. 2.3.01 Aircraft generalCTURNING RADII DEPENDS ON: Effective turn angle. Steering angle. Effective turn angle and steering angle.01 飞机概述C旋转半径取决于有效的旋转角度转弯角度有效的旋转角度和转弯角度01 Aircraft generalATHE SINGLE AISLE FA

5、MILY AIRCRAFT WITH THE HIGHER RANGE IS: The A319. The A318 or the A320. The A321.01 飞机概述A有着较高范围的单过道飞行器系列是 A319. A318 或 A320. A321.01 Aircraft generalBTHE SIDE STICKS AND NOSE WHEELS STEERING HANDLES ARE MOUNTED: On the center pedestal. On the side consoles. Below the main instrument panel.01 飞机概述B操纵

6、杆和前轮转弯把手安装在操纵台的中心操纵台的旁边主设备面板的下面01 Aircraft generalAIN NORMAL OPERATION, IF SOME LIGHTS ARE ILLUMINATED, THESE LIGHTS COULD BE: Blue or Green. Green and white. Blue and white.01 飞机概述A在正常操作中，如果一些灯亮了，这些灯可能是蓝色或绿色绿色和白色蓝色和白色01 Aircraft generalBTHE A321 IS THE A320 MODIFIED WITH: Two extra fuselage section

7、s and room for 26 more passengers. Two extra fuselage sections and room for 36 more passengers. Three extra fuselage sections and room for 36 more passengers.01 飞机概述BA321对A320作了哪些改装？加了两个机身段和空间，能多容纳26名乘客加了两个机身段和空间，能多容纳36名乘客加了三个机身段和空间，能多容纳36名乘客01 Aircraft generalATHE AIRCRAFT OF THE SINGLE AISLE FAMIL

8、Y WITH THE LOWEST FUEL CONSUMPTION IS: The A319. The A320. The A321.01 飞机概述A耗油量最低的单过道飞机是 A319. A320. A32101 Aircraft generalCTHE AIRCRAFT OF THE SINGLE AISLE FAMILY WITH THE LOWEST COST PER PASSENGER MILE IS: The A319. The A320. The A321.01 飞机概述A耗油量最低的单过道飞机是 A319. A320. A32101 Aircraft generalBTHE C

9、USTOMIZED MANUAL CONTAINS INFORMATION APPLICABLE TO: All airlines for one aircraft type family. A particular airline or a group of operators. Only to specific aircraft, type or series.01 飞机概述B客户化的手册的信息适用于同一种飞机类型的所有航空公司一个特定的航空公司或一批经营者特定的飞机，型号和系列01 Aircraft generalBIF BATTERY VOLTAGE IS BELOW 25 VOLTS

10、, THE NECESSARY CHARGING CYCLE IS: 15 minutes. 20 minutes. 25 minutes.01 飞机概述B如果电瓶电压低于25伏，必要的充电周期是 15 分钟 20 分钟. 25分钟01 Aircraft generalCTHE POSITION OF THE CHOCKS WHEN THE AIRCRAFT IS PARKED SHOULD BE IN FRONT OF: The Nose Landing Gear (NLG) wheels, and behind the Main Landing Gear (MLG) wheels. And

11、 behind the MLG wheels. And behind NLG and MLG wheels.01 飞机概述C当飞机停留时，轮挡应放在前起落架(NLG) 车轮的前面，主起落架 (MLG)车轮的后面主起落架 (MLG)车轮的后面前起落架(NLG)和主起落架 (MLG)车轮的后面01 Aircraft generalBLEVELING THE AIRCRAFT WITH THE ATTITUDE MONITOR CONSISTS IN OPERATING THE AIRCRAFT JACKS TO MOVE THE BUBBLE TO POSITION: C4. D4. E4.01

12、飞机概述B用姿态监视仪瞄准飞机在于操作飞机千斤顶使水泡达到什么位置？ C4. D4. E4.01 Aircraft generalCJACKING OPERATION IS LIMITED IF THE WIND VELOCITY EXCEEDS VALUES DEPENDING ON THE AIRCRAFT: Operating Empty Weight (OEW) and center of gravity position. Gross weight and the wind direction. Gross weight and center of gravity position.

13、01 飞机概述C如果风速超过了依据什么得出的数值，顶飞机的操作将受到限制？操作空重(OEW) 和重心位置总重和风向总重和重心位置01 Aircraft generalATHE AIRCRAFT IS EQUIPPED WITH: Three jacking points with its jacking pads and a safety jack at the rear. Three jacking points with its jacking pads and two safety jacks at the rear. Four jacking points with its jacki

14、ng pads.01 飞机概述A飞机配有：三个千斤顶支点及其顶托衬套和一个尾部的安全千斤顶三个千斤顶支点及其顶托衬套和两个尾部的安全千斤顶 四个千斤顶支点及其顶托衬套01 Aircraft generalATOWING SPEED LIMITATION DEPENDS ON THE: Position of the passenger/crew and cargo doors. Tractor. Position of the engine cowl doors.01 飞机概述A牵引速度的限制取决于乘客/机组和货舱门的位置拖拉机发动机整流罩舱门位置01 Aircraft generalCWHE

15、N THE PARKING BRAKE IS SET TO OFF: The accumulator pressure pointer goes down to zero. The brake pressure pointers keep their position. The brake pressure pointers go down to zero.01 飞机概述C当停留刹车设置为OFF（关）作动器压力显示器下降到0刹车压力显示器保持在原来位置刹车压力显示器下降到001 Aircraft generalBTHE CRITERIA THAT DEFINE THE ENGINE NOISE

16、 DANGER AREAS ARE: The distance from engine only. The distance from the engine, the power setting and the time exposure. The distance from the engine and the power setting only.01 飞机概述B定义发动机噪音危险区域的标准仅是距离发动机的距离是距离发动机的距离，动力设置以及曝光时间仅是距离发动机的距离以及动力设置01 Aircraft generalBCOMPARED TO THE A320, THE A318 VERT

17、ICAL STABILIZER FIN TIP IS: 100 mm longer. 750 mm longer. 75 mm shorter.01 飞机概述B和A320相比，A318垂直安定面垂尾端点要长100mm要长750mm要短75mm01 Aircraft generalACOMPARED TO THE A319, THE A318 CARGO DOORS ARE: Smaller. Larger. Identical.01 飞机概述A和A320相比，A318货舱门更小更大一样01 Aircraft generalCTHE NEW TECHNOLOGY USED FOR LASER B

18、EAM WELDED PANELS IS: Frame/clip riveted, clip/skin riveted and stringer/skin riveted. Frame/clip welded, clip/skin welded and stringer/skin riveted. Frame/clip riveted, clip/skin riveted and stringer/skin welded.01 飞机概述C用于激光束焊接面板的新技术是结构/夹子用铆钉铆定，夹子/蒙皮用铆钉铆定，珩条/蒙皮用铆钉铆定结构/夹子焊接的，夹子/蒙皮焊接的，珩条/蒙皮用铆钉铆定结构/夹子

19、用铆钉铆定，夹子/蒙皮焊接的，珩条/蒙皮焊接的01 Aircraft generalBTHE A318 IS DERIVED FROM THE A319 BY REDUCING THE FORWARD SECTION BY: 3 frames bays and the rear section by 1.5 frames. 1.5 frames bays and the rear section by 3 frames. 1.5 frames bays and the rear section by 1.5 frames.01 飞机概述BA318 源于A319，只是减少了前面部分3个隔框，后面

20、1.5个隔框1.5个隔框，后面3个隔框1.5个隔框，后面1.5个隔框01 Aircraft generalCWHEN AN EFIS DISPLAY UNIT (DU) FAILS: The ND Display is presented on the remaining DU. Both PFD and ND displays are presented on the remaining DU. The PFD display is presented on the remaining DU.01 飞机概述C电子飞行仪表系统（EFIS）显示组件(DU)失效导航显示出现在剩下的显示组件(DU)

21、上主飞行显示器（PFD）和导航显示出现在剩下的显示组件(DU)上主飞行显示器（PFD）出现在剩下的显示组件(DU)上01 Aircraft generalCEFIS AND ECAM DISPLAY UNITS (CRTS) ARE: Not interchangeable at all. Electrically but not mechanically interchangeable. Fully interchangeable.01 飞机概述C电子飞行仪表系统（EFIS ）和ECAM显示组件根本无法互换电子上可换，但机械上不能互换可完全互换01 Aircraft generalATHE

22、REFERENCE (X=0) FOR ALL STRUCTURAL MEASUREMENTS IN THE X-AXIS IS INSTALLED: At 254 cm (100 in) forward of the A/C. On the forward pressure bulkhead. On the A/C nose.01 飞机概述AX轴上所有的结构性测量基准安装在飞机前面254 厘米 (100英寸)在前压力舱壁在飞机前部01 Aircraft generalCTHE GENERAL BELLY FAIRING SECTION BASE NUMBER IS: 40. 10. 60.0

23、1 飞机概述C总的底端整流段有几个底面？ 40. 10. 60.01 Aircraft generalBTHE SUB-ZONES 330 & 340 IDENTIFY THE LEFT HAND AND RIGHT HAND OF THE: Main landing gear. Horizontal stabilizer. Wings.01 飞机概述B分区 330 & 340可识别什么的左边和右边？主起落架水平安定面机翼01 Aircraft generalATHE LAST ACTIONS OF THE COMPUTER INSTALLATION ARE TO: Do a test thr

24、ough the MCDU and to close the access. Engage the nuts on the studs and tighten them. Install the computer on its rack and push it to connect the electrical connectors.01 飞机概述A安装电脑的最后一部是通过MCDU进行测试，关闭入口对准螺母并拧紧在架子上安装计算机，并推它使其和电气连接器相连01 Aircraft generalBELECTROSTATIC ELECTRICITY IS BUILD UP BY: Touchin

25、g electrical circuits under tension. Rubbing materials with each other or separating plastic sheets or tapes. Moving metals over plastic surfaces.01 飞机概述B静电电流如何安装？在张力下接触电路相互撵拓材料或区分开塑料纸或磁带蜕去塑料表面的金属01 Aircraft generalCELECTROSTATIC DISCHARGE SENSITIVE EQUIPMENT ARE IDENTIFIED BY: A circular red label.

26、 An orange triangular label. A black and yellow label.01 飞机概述C静电放电敏感元件通过什么来识别？一个圆形的红色标签一个橘黄色三角标签一个黑黄相间的标签01 Aircraft generalBTHE BASIC PRECAUTIONS TO BE TAKEN IN THE CASE OF ELECTROSTATIC DISCHARGE SENSITIVE EQUIPMENT HANDLING ARE: To cover the unit with plastic material. Do not touch connector pins

27、, place protective caps on them. To test circuits with dielectric testers if necessary.01 飞机概述B在处理静电放电敏感设备时须注意：要用塑料材料罩住组件不要触摸连接器插销，在上面放上保护罩如必要用绝缘测试器检测电路01 Aircraft generalCTHE AIRCRAFT GROUNDING ATTACHMENT IS INSTALLED ON THE: Nose Landing Gear (NLG). Main Landing Gear (MLG). NLG and/or MLG.01 飞机概述C

28、飞机接地线安装在前起落架(NLG)主起落架(MLG)前起落架(NLG)或主起落架(MLG)01 Aircraft generalBAT THE MAIN LANDING GEAR STATION, THE LOCATION FOR THE RAM AIR TURBINE (RAT) SAFETY DEVICE INSTALLATION IS ON THE: Right hand side of the A/C. Left hand side of the A/C. Center of the A/C.01 飞机概述B在主起落架位置上，冲压空气涡轮(RAT)安全设备安装的位置是在飞机的右手边飞机

29、的左手边飞机的中央01 Aircraft generalAIF ENGINE REVERSER COWLS HAVE BEEN OPENED FOR MAINTENANCE ACTION THE: Slats must be retracted. Flaps must be retracted. Slats and flaps must be retracted.01 飞机概述A如果为了维修，反推整流罩已经被打开缝翼必须收上襟翼必须收上缝翼和襟翼必须收上01 Aircraft generalBIF THE AIRCRAFT POINTS INTO THE WIND AND WIND SPEED

30、 IS BETWEEN 50 AND 70 KTS, MOOR THE AIRCRAFT AT THE: Main Landing Gear (MLG). Nose Landing Gear (NLG). MLG and NLG.01 飞机概述B如果飞机迎风停放，风速介于50和70节之间，应把飞机系在主起落架(MLG)前起落架(NLG)主起落架(MLG)和前起落架(NLG)01 Aircraft generalADMC 1 NORMALLY PROCESSES: PFD 1, ND 1 and E/W displays. PFD 1, ND 1 and System/Status displays. PFD 2,