Aircraft Inspection, Repair & Alterations: Acceptable by Federal Aviation Administration

By Federal Aviation Administration

The bible for the AMTs and airplane proprietors alike, this reference outlines criteria for appropriate tools, innovations, and practices for the inspection, fix, and alteration of plane. this can be Advisory round 43.13-1B/2A.

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Additional resources for Aircraft Inspection, Repair & Alterations: Acceptable Methods, Techniques, & Practices (FAA Handbooks)

Example text

1-3. MODIFIED WOOD PRODUCTS. The most common forms of modified woods found in aircraft construction are plywood. Although not a wood product, Phenolic parts are sometimes incorporated into structures. These products are used whenever the manu- Par 1-2 facturer requires specialized strength or durability characteristics. 1-4. ADHESIVES. Because of the critical role played by adhesives in aircraft structure, the mechanic must employ only those types of adhesives that meet all of the performance requirements necessary for use in certificated civil aircraft.

B. Common types of adhesives that are or have been used in aircraft structure fall into two general groups: casein and syntheticresins. Adhesive technology continues to evolve, and new types (meeting the requirements of paragraph 1-4a) may become available in the future. (1) Casein adhesive performance is generally considered inferior to other products available today, modern adhesives should be considered first. CAUTION: Casein adhesive deteriorates over the years after exposure to moisture in the air and temperature variations.

Cross grain. Spiral grain, diagonal grain, or a combination of the two is acceptable providing the grain does not diverge from the longitudinal axis of the material more than specified in column 3. A check of all four faces of the board is necessary to determine the amount of divergence. The direction of free-flowing ink will frequently assist in determining grain direction. b. Wavy, curly, and interlocked grain. Acceptable, if local irregularities do not exceed limitations specified for spiral and diagonal grain.

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