Table of Contents
1.PURPOSE
2.DEFINITIONS
3.RELATEDREADINGMATERIAL(currenteditions)
4.BACKGROUND
5.ENGINEERINGDATAANDPROCEDURES
6.RAWMATERIALINSPECTIONPROCEDURES
7.MATERIALHANDLINGANDSTORAGEPROCEDURES
8.HANGARS,FACILITIES,ANDEQUIPMENT
9.FABRICATIONANDPROCESSESPROCEDURES
10.NDIPROCEDURES
11.PERSONNELQUALIFICATION
12.INSPECTIONRECORDSPROCEDURES Abstract
Gives information and guidance concerning an acceptable means, but not the only means, of demonstrating compliance with the requirements of Title 14 of the Code of Federal Regulations (14 CFR) parts 21, 23, 25, 26, 27, 29, 31, 33, 35, 43, 91, 121, 125, (U.S.-registered airplanes), 135, 137, and 145 regarding procedures and facilities for repairs and alterations of structure consisting of adhesively bonded (including metal bond) and fiber-reinforced materials (e.g., carbon, aramid, and glass-reinforced polymeric materials mentioned in the current edition of AC 20-107, Composite Aircraft Structure).
