FAA AC 120-73 : 0
Current
The latest, up-to-date edition.
DAMAGE TOLERANCE ASSESSMENT OF REPAIRS TO PRESSURIZED FUSELAGES
Hardcopy , PDF
English
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1 PURPOSE
2 RELATED DOCUMENTS
3 DISCUSSION
4 BACKGROUND
5 REPAIR ASSESSMENT PROCESS
6 IMPLEMENTATION
7 REPAIRS TO STRUCTURAL MODIFICATIONS CERTIFIED BY A
SUPPLEMENTAL TYPE CERTIFICATE (STC)
8 ALTERNATIVE METHODS
Gives guidance on incorporating FAA-approved "repair assessment guidelines" in air carrier maintenance or inspection programs subject to Title 14, Code of Federal Regulations (14 CFR) part 121.
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 129-4 : 2009 | MAINTENANCE PROGRAMS FOR U.S.-REGISTERED AIRCRAFT OPERATED UNDER 14 CFR PART 129 |
| FAA AC 120-16 : 2016 | AIR CARRIER MAINTENANCE PROGRAMS |
| FAA AC 120-104 : 2011 | ESTABLISHING AND IMPLEMENTING LIMIT OF VALIDITY TO PREVENT WIDESPREAD FATIGUE DAMAGE |
| FAA AC 91-56 : 2008 | CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES |
| FAA AC 25.1529-1 : 2007 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS OF STRUCTURAL REPAIRS ON TRANSPORT AIRPLANES |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
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