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Airworthiness directives › 2013-16-26

AD 2013-16-26 Airworthiness Directives; Airbus Airplanes

Superseded. This directive was replaced by AD 2018-02-17. Work to the current one.
2013-10-04
2013-08-30
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Airframe
2018-02-17

Models named: A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes; and Model A340-211, -212, -213, -311, -312, and -313 airplanes; certificated in any category; all manufacturer serial numbers (MSNs).

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

For Model A330-200, -200 Freighter, and -300 airplanes up to MSN 0162 inclusive, except those on which Airbus Service Bulletin A330-52-3044 has been embodied in service; and for Model A340-200 and -300 airplanes up to MSN 0164 inclusive, except those on which Airbus Service Bulletin A340-52-4054 has been embodied in service: Before the accumulation of 15,800 total flight cycles since the airplane's first flight or within 100 flight cycles after the effective date of this AD, whichever occurs later, do a detailed inspection of the outer skin rivets at the frame fork end of frame (FR)60 and FR60A of the aft cargo door for sheared, loose, or missing rivets; and do a detailed inspection of the whole FR60 and FR60A forks for cracking and for sheared, loose, or missing rivets at the frame web and flanges; in accordance with Airbus Alert Operator Transmission (AOT) A330-A52L001-12, dated December 3, 2012; or Airbus AOT A340-A52L002-12, dated December 3, 2012; as applicable. Repeat the inspections thereafter at intervals not to exceed 400 flight cycles.

Unsafe condition

This AD was prompted by reports of cracked adjacent frame forks of a forward cargo door. We are issuing this AD to detect and correct cracked or ruptured cargo door frames, which could result in reduced structural integrity of the forward or aft cargo door.

Affected ADs

None.

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