This procedure is applicable only in digital mode.

The primary document containing the procedures for the continuing airworthiness of an airplane is the airplane’s maintenance manual (Instructions for Continuing Airworthiness). A document prepared in accord with this Specification supplements, and is designed for use with, that maintenance manual.

A CAP supplements the airplane’s maintenance manual (or Instructions for Continuing Airworthiness) which is the primary document containing the procedures for the continuing airworthiness of the airplane.

Some airplanes, particularly relatively simple airplanes, may not need CAPs because adequate information to maintain their continuing airworthiness throughout their useful lives is contained in the airplane’s maintenance manual. In such cases, a CAP need not be published.

CAPs may be prepared for all types of general aviation airplanes and components certificated under the applicable Federal Aviation Regulations.

The primary document containing the procedures for the continued airworthiness of an airplane is the airplane’s maintenance manual. A document prepared in accord with this Specification supplements, and is designed for use with, that manual.

Recommendations for ATC holding operation in icing conditions for up to 45 minutes shall provided.

Before disassembly, make sure that you release all the nitrogen pressure from the shock absorber.

Tighten the turnbuckle until you have the correct tension in the cable.

Remove all the rigging pins and equipment that prevent free movement of the control surfaces.

To make the curing process slower, decrease the heat that you apply to the compound.