Standard: EASA - AD 2009-0094

FUSELAGE / WINGS - FRAME 40 FORWARD FITTING BETWEEN STRINGERS 32 AND 33 - INSPECTION / REPAIR (APPLICABLE TO AIRBUS A300 AND A300-600 AEROPLANES) [CORRECTED: 29 MAY 2009]

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Organization: European Aviation Safety Agency
Document Number: ad 2009-0094
Publish Date: 2009-04-21
Page Count: 3
Change Type: NEW ADDITION
Available Languages: EN
DOD Adopted: NO
ANSI Approved: NO
Most Recent Revision: YES
Current Version: YES
Status: Inactive

This Standard References

Showing 6 of 6.

AD 2011-0163
CRD-PAD-09-012
EASA.EC.216.2008
EASA.IR.21
EASA.IR.M
PAD-09-012

Standards That Reference This Standard

Showing 7 of 7.

AD 2011-NM-183
AD 2011-0163
FAA AD 2012-25-06
FAA AD 2009-NM-089
EASA AD 2014-0199
FAA AD 2014-NM-181
EASA AD 2015-0232

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