本手册中的定义应与联邦航空法规中的定义一致。

That portion of the systems which controls the position and movement of the ailerons and aileron tabs. Includes items such as the control wheels, cables, boosters, linkages, control surfaces, indicators, etc., as applicable.

The section containing "Emergency Procedures" shall have a red plasticized tab divider.

Each Handbook shall have a log of Revisions or effective pages, listing all revisions or effective pages, immediately following the Title Page.

If a paragraph contains subparagraphs, the order of presentation of the subparagraphs in this Specification is for guidance only and need not be followed.

A gear up emergency landing, if necessary, can be deferred until after all other methods of lowering the gear have been unsuccessfully tried and a suitable landing area has been selected.

If the maneuver cannot be performed safely, a warning against attempting it shall be provided.

Procedures shall be provided for making emergency descent.

A statement of the minimum crew and the function of each flight crew member, if more than one is required shall be provided.

Total capacity and usable fuel shall be stated and, if the unusable fuel exceeds the limits of FAR 23, information shall be given identifying the quantities unusable in flight.

For turbopropeller powered airplanes only, the established temperatures and corresponding altitude limits of powerplant components and engine fluids shall be stated.