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The bible for the AMTs and plane proprietors alike, this reference outlines criteria for appropriate equipment, concepts, and practices for the inspection, fix, and alteration of plane. this can be Advisory round 43.13-1B/2A.
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Extra info for Aircraft Inspection, Repair & Alterations: Acceptable Methods, Techniques, & Practices (FAA Handbooks)
Sample text
Compression failures. This defect is caused from the wood being overstressed in compression due to natural forces during the growth of the tree, felling trees on rough or irregular ground, or rough handling of logs or lumber. Compression failures are characterized by a buckling of the fibers that appear as streaks on the surface of the piece substantially at right angles to the grain, and vary from pronounced failures to very fine hairlines that require close inspection to detect. Reject wood containing obvious failures.
11-208. 11-83 Figure 11-23. 11-84 Figure 11-24. 11-84 11-209. 11-83 11-210. 13-1B CHG 1 9/27/01 CONTENTS (CONTINUED) Paragraph Page 11-211. 11-212. 11-213. 11-214. 11-215. 11-216. 11-217. 11-86 Table 11-17. 11-86 11-218. 11-86 Figure 11-25. 11-87 11-219. 11-87 Figure 11-26. 11-87 Figure 11-27. 11-87 11-220. 11-87 Figure 11-28. 11-88 Figure 11-29. 11-88 Table 11-18. 11-88 Table 11-19. 11-89 Table 11-20. 11-89 Table 11-21. 11-89 Table 11-22. 11-89 Figure 11-30. 11-90 Figure 11-31. 11-90 11-221. 11-90 Figure 11-32.
If the mechanic detects any relative movement between two adjacent wood members, a failure of the bond is evident. Any loose fittings should arouse the mechanic’s suspicion, and the fittings should be removed to check for elongated bolt holes. Disassembly is warranted for further inspection. e. Odor is an important indicator of possible deterioration. During the initial inspection, as the access panels are being removed from the structure, the mechanic should be aware of any areas that smell musty or moldy.