Airworthiness Directives (ADs)

Aviation Industry

CAA-2013-10-003

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date: 2013/10/04

Applicability: Airbus A330-301, A330-321, A330-322, A330-341 and A330-342 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification 42605 has been embodied in production, and Airbus A340-211, A340-212, A340-213, A340-311, A340-312, and A340-313 aeroplanes, all manufacturer serial numbers, except those on which Airbus modification 42605 has been embodied in production.

Model Number: AIRBUS A330-300 and A340-200/-300 aeroplanes

CAA AD Number: CAA-2013-10-003

Aeronautics Authority of Original AD: EASA

Original AD Number: 2013-0241

Effective Date: 2013/10/15

Subject: Fuselage – Center Landing Gear Door / Structure – Joint Area Between Frames 49 and 53.2 – Inspection

Reference Publications (Revision/ATA/SB): ATA 53. This AD supersedes the DGAC France AD 96-056-029(B) dated 23 March 1996 and DGAC France AD 96-057-042(B) dated 23 March 1996. Ref. Airbus SB A330-53-3019 Original issue dated 30 November 1995, Revision 01 dated 23 July 1998, and Airbus SB A330-53-3020 Original issue dated 30 November 1995, Revision 01 dated 24 April 1996, Revision 02 dated 16 December 2011, and Airbus SB A340-53-4028 Original issue dated 30 November 1995, Revision 01 dated 27 May 1998, and Airbus SB A340-53-4029 Original issue dated 30 November 1995, Revision 01 dated 24 April 1996, Revision 02 dated 16 December 2011.

Remarks

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