Airworthiness directives › 2013-23-13
AD 2013-23-13 Airworthiness Directives; Airbus Airplanes
Models named: A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, B4-203, A300 B4-601, B4-603, B4-620. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes, on which any repair has been done as specified in Airbus Service Bulletin A300-53-0337, dated February 4, 1999; or Airbus Service Bulletin A300-53-0337, Revision 01, dated March 17, 2003. (2) Airbus Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes; Model A300 B4-605R and B4-622R airplanes; Model A300 F4-605R and F4-622R airplanes; and A300 C4-605R Variant F airplanes; on which any repair has been done as specified in any of the service information identified in paragraphs (c)(2)(i), (c)(2)(ii), (c)(2)(iii), (c)(2)(iv), (c)(2)(v), and (c)(2)(vi) of this AD. (i) Airbus Service Bulletin A300-53-6111, dated February 4, 1999. (ii) Airbus Service Bulletin A300-53-6111, Revision 01, dated March 17, 2003. (iii) Airbus Service Bulletin A300-53-6111, Revision 02, dated September 13, 2004. (iv) Airbus Service Bulletin A300-53-6111, Revision 03, dated September 30, 2009. (v) Airbus Mandatory Service Bulletin A300-53-6111, Revision 04, dated August 25, 2011. (vi) Airbus Mandatory Service Bulletin A300-53-6111, Revision 05, dated January 28, 2013.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Required actions
Within 1,000 flight hours after the effective date of this AD: Check the airplane maintenance records to determine if repairs were done in area 1 of the frame base fittings as defined in Appendix 1 of Airbus Alert Operators Transmission A53W001-12, dated July 4, 2012.
Unsafe condition
This AD was prompted by a report that cracking was found in area 2 of the frame base fittings between frame 41 and frame 46. We are issuing this AD to detect and correct cracking in area 2 of the frame base fittings between frame 41 and frame 46, which could adversely affect the structural integrity of the airplane.
Affected ADs
None.
Read the original on the Federal Register →
You just looked this one up by hand
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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