Download Aircraft Inspection, Repair & Alterations: Acceptable by Federal Aviation Administration PDF
By Federal Aviation Administration
The bible for the AMTs and airplane proprietors alike, this reference outlines criteria for appropriate equipment, innovations, 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)
Roughening smooth, well-planed surfaces of normal wood before bonding is not recommended. Such treatment of well-planed wood surfaces may result in local irregularities and objectionable rounding of edges. 13-1B surfaces. Sanding should never be continued to the extent that it alters the flatness of the surface. Very light sanding may also improve the wetting of the adhesive to very hard or resinous materials. b. Wetting tests are useful as a means of detecting the presence of wax, old adhesive, and finish.
11-80 11-193. 11-80 11-194. 11-81 11-195. 11-81 11-196. 11-81 11-197. 11-204. ].................................................................................................................. 11-81 SECTION 16. WIRE MARKING 11-205. 11-206. 11-207. 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.
Whenever repairs are made that require replacing a portion that includes drain holes, skin stiffeners, or any other items, the repaired portion must be provided with similar drain holes, skin stiffeners, or items of the same dimensions in the same location. Additional drain holes may be required if reinforcement under a skin repair interferes with waterflow to existing drain holes. Make any additional drain holes the same diameter as originals, usually 1/4 inch. 1-38. CONTROL SURFACE FLUTTER PRECAUTIONS.