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General

In making aircraft structural repair, the primary objective is to restore the damaged parts to their original condition. Frequently, the only effective way is to replace the damaged part or parts. However, each damage must be studied carefully to determine if repairing or replacing is the course to follow. If a damaged part can be repaired, its purpose or function must be fully understood. The reason for this is that while strength may be the principal requirement in some structures, others might need totally different characteristics. For example, fuel tanks, floats, and hulls must be leak proof; however, cowlings, fairings, and similar parts must be smooth and streamlined.

This section discusses damage assessment, cracks, damage classification, corrosion control, corrosion inspection, structural member stresses, and repair practices.

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