Airworthiness directives › 2017-05-01
AD 2017-05-01 Airworthiness Directives; Airbus Airplanes
Models named: A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, B4-203. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes, certificated in any category, all manufacturer serial numbers.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 4 months after the effective date of this AD, verify whether the Airbus modifications specified in table 1 to paragraphs (g), (h), and (i) of this AD, as applicable to airplane model, have been embodied on the airplane, in accordance with the Accomplishment Instructions of the applicable Airbus service bulletin specified in table 1 to paragraphs (g), (h), and (i) of this AD. A review of the airplane maintenance records is acceptable to accomplish the verification required by this paragraph, provided those records can be used to conclusively determine whether the modifications have been embodied. Table 1 to Paragraphs ( g ), ( h ), and ( i ) of This AD—Airbus Modification and Applicable Service Bulletin Set Airbus modification Applicable Airbus service bulletin Set 1A 751 A300-53-247, Revision 2, dated July 20, 1990. 7301 A300-53-0239, Revision 02, dated March 6, 2000. 10326 A300-57-0203, Revision 04, dated February 18, 2015. 12735 A300-53-0366, dated April 7, 2005. 12736 A300-53-0368, dated April 7, 2005. 12737 A300-53-0369, Revision 03, dated September 1, 2010. 12798 A300-53-0375, Revision 01, dated June 24, 2013. 07757 and 12977 A300-53-0271, Revision 05, dated June 21, 2013. 13611 A300-57-0258, dated September 30, 2014. 13692 A300-53-0393, dated September 27, 2013. 13716 A300-57-0259, dated September 30, 2014. Set 1B 12794 A300-53-0374, Revision 04, dated July 5, 2013. 12796 A300-53-0373, Revision 03, dated September 1, 2010.
Unsafe condition
This AD was prompted by an evaluation by the design approval holder that indicates that a section of the wing and aft fuselage is subject to widespread fatigue damage. We are issuing this AD to prevent reduced structural integrity of these airplanes due to the failure of certain structural components.
Affected ADs
This AD affects AD 2004-23-20, Amendment 39-13875 (69 FR 68779, November 26, 2004) (“AD 2004-23-20”).
Read the original on the Federal Register →
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1