88.The exhaust gas temperature indicator, on piston engine powered
airplanes, is the instrument used to identify the lean fuel flow mixtures
for various power settings.

687.机动速度是全行程操纵产生的气动载荷不会使飞机过度受力的最大速度。

686.THE SHOCK MOUNT( ) THE VIBRATION.

685.The loading conditions together with the resulting margins of safety
were evaluated.

684.Normally,when pages are added to the end of a section,or to the back
of a publication--not affecting pages already in the manual--a revision
shall always be prepared.

683.If you do not do this at the same time, the alignment pins will get
caught.

682.The Specification was developed with the objective of minimizing the
cost to, and efforts of general aviation airplane owners and operators
and maintenance personnel by standardizing the format and general content
of Continuing Airworthiness Programs.

681.IF YOU ( )THAT THE HYDRAULIC PUMP DOES NOT OPERATE CORRECTLY, EXAMINE
THE PUMP.

680.Optional information including ( ) the rationale
utilized to select CAPs - how the CAP requirements were determined.

679.NOTE、 This system does not supersede the normal channels of
communication for items not covered by the CAP.

678.THE SAFETY INSTRUCTIONS.