Spin recovery procedures for multi-engine airplanes may be included at the option of the manufacturer.

The second method does not require pressurization of the pneumatic crossover manifold, but utilizes an external air source connected to the air charging valve manifold to pressurize the reservoirs for ground maintenance.

In some cases, the Specification is used to prepare a Continuing Airworthiness Program for acceptance by an airworthiness authority other than FAA.

These tests should require no special equipment or facilities other than that installed on the aircraft and should be comparable to the tests performed by the flight crews.

The emergency procedures check list should be in concise, abbreviated form designed to remind pilots of items to check without providing details concerning the operation of any system.

The function and operation of each unit in the system should be described as well as the location of the units.

The removal/installation portion shall state clearly the sequence of steps required to remove and reinstall a component or unit, along with precautions to be observed.

"Maintenance Practices" which are a combination of servicing, removal/installation, adjustment/test, inspection/check, cleaning/painting, and approved repairs should follow the Troubleshooting Section.

动力装置是指包括发动机、进气道、安装架、整流罩、勺形进气口、整流罩盖板、冷却隔板等在内的整体动力组合。

涡桨发动机控制装置包括到调节器或等效装置的连杆装置和控制装置，以及从调节器或等效装置到螺旋浆调速器、燃油控制组件的连杆装置和控制装置，或其他受控组件。

涡轮发动机包括控制流经发动机空气流量的压气机引气系统、空气冷却系统、用于发动机防冰的热空气系统和发动机启动系统。