A、 面罩
B、 护目镜
C、 防护服
答案:B
A. 把上凸轮放到与拆下时所做标记一致的位置。
B. 上部卡箱安装的位置应该与拆卸标记保持一致。
C. 经同意后,对应拆卸时所作的标记将上部曲柄安装在位。
A. WORKS
B. OPERATES
C. MAKES
A. The APU isolation check valve is in the left side of the center tank.
B. The APU isolation check valve is in the inside wall of the centre tank.
C. The APU isolation check valve is in the left side of the dry bay.
A. A component of a system used to treat waste water. Including washbasin, water cabinet, toilet system, etc.
B. That portion of the system which is used for disposal oil water and waste. Includes items such as wash basins, water closets, flushing systems, etc.
C. The part of a system used to treat waste water. Including washbasin, water pipe, flushing system and so on.
A. The Continuing Airworthiness Program Inspection number is also provided above the page and is the CAP chapter number.
B. The Continuing Airworthiness Program Inspection number is also displayed at the bottom of the page and is the CAP section number.
C. The Continuing Airworthiness Program Inspection Code is also showed under the page and is the CAP item number.
A. 故障隔离手册提供的信息可以用来标识,定位和纠正可能在飞机上发生的任何故障。
B. 故障隔离手册提供信息用于标识、定位和修正已经在飞机上发生的任何故障的信息。
C. 飞机士出现的任何故障信息都可以参照故障隔离手册提供的标识来定位并排故。
A. Static discharger attached to the flight control surface is used to discharge static electricity which builds up as air flows across the surface.
B. Static discharger attached to the aircraft fuselage is used to discharge static electricity which builds up as air flows across the surface.
C. Static discharger attached to the flight control surface is used to discharge direct current electricity which builds up as air flows across the surface.
A. The removal of the piston is involved in the steps
B. The removal of the piston is not included in the procedure
C. The procedure eliminates the piston
A. Continuing Airworthiness Program Inspection Number; Airplane Model and Serial Number; Airplane Hours; Title of Continuing Airworthiness Program Inspection; Location and Description of the Damage and How Detected should be included in the CAP report;
B. The report of discrepancy should contain the following: Continuing Airworthiness Program Inspection Number; Airplane Model and Serial Number; Airplane Hours; Heading of Continuing Airworthiness Program Inspection; Location and Description of the Damage; Detecting ways;
C. The discrepancy report should cover the information other than the following: Continuing Airworthiness Program Inspection Number; Airplane Model and Serial Number; Airplane Hours; Title of Continuing Airworthiness Program Inspection; Location and Description of the Damage; How Detected;
A. Maximum landing weight is maximum weight approved for the landing touchdown.
B. Maximum landing weight is maximum weight supplied for the landing contact.
C. Maximum landing weight is minimum weight provided for the landing touchdown.