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Copies · 2
Copies of this document that the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.
Revision 1
© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0441, the docket of AD 2019-19-17. Not covered by OpenAirDocs’ CC0 dedication.
Revision 1
© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0441, the docket of AD 2019-19-17. Not covered by OpenAirDocs’ CC0 dedication.
- Manufacturer
- Airbus
- Type
- Service Bulletin
- Number
- A300-57-6062
- Latest revision known
- A300-57-6062, Revision 02, dated January 29, 1997
- Copies
- 2 files of 1 revision
A newer revision may exist than any OpenAirDocs knows of: check with the manufacturer.
ADs that cite it · 2
Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.
AD 2000-03-20 R1Forward Fittings in the Radius of Frame 40 Adjacent to the Tension Bolts in the Center Section of the Wings · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 3 moreAD 2000-03-20Wings · Airbus Industrie A300 Model B4-600 Series, A300 Model B4-600R Series, A300 Model F4-600R Series and 7 more
Also cited in 2 proposed ADs.