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FAA AC 120-73 : 0

Current

Current

The latest, up-to-date edition.

DAMAGE TOLERANCE ASSESSMENT OF REPAIRS TO PRESSURIZED FUSELAGES

Available format(s)

Hardcopy , PDF

Language(s)

English

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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