1529. 为了在预处理空气连接单向阀在打开位置不工作时放行飞机,执行以下步骤。

1834. This information shall be presented along with information to aid recognition of icing conditions which may exceed the certificated capabilities of the aircraft and its ice protection system

1833. Examine the surface for cracks

1832. Without the modification, it is possible that the service life of this unit will be shorter than usual

1831. 描述机身、机翼和尾翼的结构。

1830. 使用单词前,应先阅读字典中“经批准词义”栏中的定义。

1829. 所有飞机发动机必须满足某些效率、经济性和可靠性的一般要求,这就要求点火系统能够在各种天气和其他不利条件下,在适当的时间向火花塞传递点火脉冲。

1828. This will allow the user to identify an affected airplane by examining one list rather than having to check each individual Continuing Airworthiness Program for applicability

1827. Do not install shims over 001 mm thick

1826. The Hydraulic Power Transfer Unit system is a hydraulic motor-pump assembly that supplies alternative pressure to leading edge flaps and slats and auto slat system if system B is de-pressurized

1825. If desired, the manufacturer may include more than one airplane model in the Maintenance Manual