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Airworthiness directives › 2013-13-13

AD 2013-13-13 Airworthiness Directives; Airbus Airplanes

Superseded. This directive was replaced by AD 2017-21-08. Work to the current one.
2014-09-23
2014-08-19
39-17501
FAA-2012-1158
Airframe
2017-21-08

Models named: A310-203, -204, -221, -222, 304, -322, -324, -325, A300 B4-601, B4-603. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to all Airbus model airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Model A310-203, -204, -221, -222, 304, -322, -324, and -325 airplanes. (2) Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

(1) For Model A300-600 series airplanes: Within 3 months after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the structural inspections and inspection intervals defined in Airbus A300-600 Airworthiness Limitation Items Document AI/SE-M2/95A.1310/07, Issue 13, dated October 2010. The initial compliance time for accomplishing the inspections is at the later of the times specified in paragraphs (g)(1)(i) and (g)(1)(ii) of this AD. (i) At the applicable times specified in Airbus A300-600 Airworthiness Limitation Items Document AI/SE-M2/95A.1310/07, Issue 13, dated October 2010, except as specified in paragraphs (g)(1)(i)(A) and (g)(1)(i)(B) of this AD. (A) For actions identified in Airbus A300-600 Airworthiness Limitation Items Document AI/SE-M2/95A.1310/07, Issue 13, dated October 2010; and Airbus TR 13.1, dated February 2011, to the Airbus A300-600 Airworthiness Limitation Items Document AI/SE-M2/95A.1310/07, Issue 13, dated October 2010: Use the applicable compliance time specified in Airbus Temporary Revision (TR) 13.1, dated February 2011, to the Airbus A300-600 Airworthiness Limitation Items Document AI/SE-M2/95A.1310/07, Issue 13, dated October 2010. (B) Where compliance times in paragraph 3., “Special Compliance Times,” in the “Record of Revisions” section of Airbus A300-600 Airworthiness Limitation Items Document AI/SE-M2/95A.1310/07, specify “from approval date of A300-600 ALI Document Issue 13,” “from date approval of A300-600 ALI Document Issue 13,” or “from A300-600 ALI Document Issue date of publication,” for this AD use “after the effective date of this AD” for those compliance times. (ii) Within 3 months after the effective date of this AD. (2) For Model A310 series airplanes: Within 3 months after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the structural inspections and inspection intervals defined in Airbus A310 Airworthiness Limitation Items Document AI/SE-M2/95A.1309/07, Issue 8, dated October 2010. The initial compliance time for accomplishing the inspections is at the later of the times specified in paragraph (g)(2)(i) and (g)(2)(ii) of this AD. (i) At the applicable times specified in Airbus A310 Airworthiness Limitation Items Document AI/SE-M2/95A.1309/07, Issue 8, dated October 2010; except where compliance times in paragraph 3., “Special Compliance Times,” in the “Record of Revisions” section of Airbus A310 Airworthiness Limitation Items Document AI/SE-M2/95A.1309/07, Issue 8, dated October 2010, specify “from date of approval of ALI Document Issue 8,” or “from date approval of the ALI document Issue 8,” for this AD use “after the effective date of this AD” for those compliance times. (ii) Within 3 months after the effective date of this AD.

Unsafe condition

This AD was prompted by revisions of certain Airbus Airworthiness Limitation Items (ALI) documents, which require more restrictive maintenance requirements and airworthiness limitations. We are issuing this AD to prevent fatigue cracking, damage, or corrosion in principal structural elements, which could result in reduced structural integrity of the airplane.

Affected ADs

This AD affects AD 2011-10-17, Amendment 39-16698 (76 FR 27875, May 13, 2011).

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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