A、 To give indications and test to the wing/body overheat system, 115v ac power must be connected. When installing an element, do not bend the element unless the bend radius is less than one inch. If the bend radius is less than one inch, damage to the element can occur.
B、 For the indications and test of the wing/body overheat system, 115v ac power must be ON. When you install an element,do not bend the element until the bend radius is less than one inch. If the bend radius is less than one inch, damage to the element can occur.
C、 115v dc power must be supplied for the indications and test of the wing/body overheat system. When you install an element, do not bend the element radius less than one inch. If you bend the radius less than one inch, damage to the element can occur.
答案：B
A、 To give indications and test to the wing/body overheat system, 115v ac power must be connected. When installing an element, do not bend the element unless the bend radius is less than one inch. If the bend radius is less than one inch, damage to the element can occur.
B、 For the indications and test of the wing/body overheat system, 115v ac power must be ON. When you install an element,do not bend the element until the bend radius is less than one inch. If the bend radius is less than one inch, damage to the element can occur.
C、 115v dc power must be supplied for the indications and test of the wing/body overheat system. When you install an element, do not bend the element radius less than one inch. If you bend the radius less than one inch, damage to the element can occur.
答案：B
A. The standby altimeter is supplied with static pressure by the standby probes to indicate the altitude of the aircraft in abnormal condition.
B. The standby alitimeter indicates the barometric altitude of the aircraft, it depends on static pressure supplied by the standby probes.
C. The standby altimeter is supplied with pitot pressure by the standby probes to indicate the barometric altitude of the aircraft.
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. Fueling can be accomplished only by use of a pressure fueling station and in this way all tanks will be partially or completely filled.
B. Fueling can be completed through a single pressure fueling station, and with this station, all tanks can be filled in different level.
C. Fueling can be completed by use of a separate pressure fueling station by which all tanks can be filled continuously or completely.
A. 缓慢地转动旋钮。
B. 缓慢地转动电门。
C. 缓慢地转动手柄。
A. 拆下将发射器壳体紧固在发动机上的螺栓
B. 拆下螺栓紧固的发动机壳体
C. 拆下用螺栓紧固在发动机上的发射器壳体
A. 油屑监测器用于监控除油系统中黑色金属和有色金属屑的大小和质量。
B. 磁屑探测器用于探测排油系统中含铁和不含铁金属的尺寸和数量。
C. 油屑探测器用于检测回油系统中黑色金属和有色金属的尺寸和数量。
A. 适用时,本章可代替飞机的-00至-70部分,以飞机附带的制造商资料为准。本章中可能包含制造商认为适用的大修资料。
B. 适用时,本章可代替飞机的-00至-70部分,以飞机附带的供应商资料为准。本章中可能包含制造商认为适用的大修资料。
C. 适用时,本章可代替飞机的-00至-70部分,以飞机附带的制造商资料为准。本章中可能包含制造商认为适用的手册资料。
A. That portion of the system which is used to dissipate static electricity.
B. That portion of the system which is used to discharge static electricity.
C. That portion of the system which is used to remove static electricity.
A. 发行人栏目,出版物名称,飞机型号和发行或修订日期都应该出现在活页文件页面中。
B. 制造商的刊头,出版物标,飞机型号和发行或修订日期必须出现在活页文件的所有页面。
C. 生产商发行人栏目,出版物名称,飞机类型和发布或修订日期都应该出现在活页文件所有页面中。
A. 连接可以连接的导线
B. 把断开的导线重新断开
C. 连接断开的导线
