关于如何在恶劣天气下停放的说明，请参阅第6章。

Use aluminum fitting torque values for aluminum, steel, or titanium fittings installed in aluminum bosses.

Make sure that you do not bend the rod end on the LVDT or shaft when you install the LVDT. If you bend the rod end or shaft, an incorrect indication or damage to equipment can occur.

That portion of the systems protects the control surfaces from movement by wind while the aircraft is on the ground.

They are reserved for use in those cases where the number of breakouts provided by the fourth digit in the 05-20 breakout is not sufficient to cover all of the maintenance checks dictated by subsystem 05-10 above.

In general, it is desired that the following chapter arrangements and breakdown be followed uniformly and to the maximum extent practicable in all manuals.

For turbo-propeller powered airplanes only, the Minimum and Maximum Outside Air Temperature Limits shall be presented as a function of pressure altitude.

The exact content of the Abnormal Procedures Section shall be determined by each Handbook producer, considering the design features of each airplane.

Data shall be presented as Calibrated Airspeed versus Indicated Airspeed assuming zero instrument error.

The flow of the system shall be presented in patterned shading with a minimum of turns in the lines.

Cotter pins are used on engine controls, landing gear, and tailwheel assemblies, or any other point where an actuating movement takes place.