Detection system is used to detect and indicate the formation of ice.

A review of test results applicable to the design was made. The loading conditions together with the resulting margins of safety were evaluated. The resulting data were used to determine if the component should be considered for incorporation into the CAP.

The effects of corrosion have not been considered in the rationale in selecting inspection times or in the effects on the fatigue stresses. It is very difficult to determine the effects of corrosion but, as the reports from the CAP inspections are received, the inspection times will be adjusted for any severe problems.

High-time airplanes, disassembled for major overhaul, were inspected to assist in selecting inspection items. Other high-time airplanes’ special Continuing Airworthiness Program Inspection results supplement these inspections.

In addition to understanding FAA Advisory Circulars AC 91-60 and AC 91-56, familiarity with GAMA Specification No.2, Manufacturers Maintenance Data and Air Transport Association of America Specification No.100, Specification for Manufacturers Technical Data, will aid in the preparation of a CAP for a specific airplane.

The Continuing Airworthiness Program Inspection Document (CAP) is inspection data that, when combined with the operator’s existing maintenance program, will help maintain the structural integrity and continued airworthiness of the ABC XXX Series airplanes.

REPAIR/MODIFICATION sets forth repair or modification instructions and may refer to a standard repair in another document or a special repair or modification defined elsewhere, such as in a service kit, service bulletin, etc.

SIGNIFICANT INSPECTION CONDITION (detectable crack size, wear limits, corrosion condition, ctc.) specifies, for a crack inspection, the minimum size crack expected to be discovered. Specifies, for other inspection conditions, the wear limits, corrosion pit depth. etc.

INSPECTION COMPLIANCE sets forth instructions regarding “when” an inspection is required and whether it is repetitive. Also state if additional repetitive inspections are required based on initial inspection results.

In two digits of Section Number in the Continuing Airworthiness Program lnspection number, the first digit is determined by GAMA Specification No. 2 Numbering System, and the second digit is determined sequentially by the manufacturer.

The manufacturer may establish procedures to provide feedback (from operators and maintenance facilities who comply with a CAP) on unairworthy conditions (whether covered or not covered by the CAP) that were discovered when complying.