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FAA AC 43-214 : 2016

Current

Current

The latest, up-to-date edition.

REPAIRS AND ALTERATIONS TO COMPOSITE AND BONDED AIRCRAFT STRUCTURE

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2016

€35.89
Excluding VAT

1. PURPOSE
2. DEFINITIONS
3. RELATED READING MATERIAL (current editions)
4. BACKGROUND
5. ENGINEERING DATA AND PROCEDURES
6. RAW MATERIAL INSPECTION PROCEDURES
7. MATERIAL HANDLING AND STORAGE PROCEDURES
8. HANGARS, FACILITIES, AND EQUIPMENT
9. FABRICATION AND PROCESSES PROCEDURES
10. NDI PROCEDURES
11. PERSONNEL QUALIFICATION
12. INSPECTION RECORDS PROCEDURES

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, 129 (U.S.-registered airplanes), 133, 135, 137, and 145 regarding procedures and facilities for repairs and alterations of structures 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).

DocumentType
Standard
Pages
25
PublisherName
Federal Aviation Administration
Status
Current

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