Airworthiness Directives (ADs)

Aviation Industry

CAA-2015-06-003A

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: 2015/06/17

Applicability: Airbus A330-201, A330-202, A330-203, A330-223, A330-243, [deleted], A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, and Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all manufacturer serial numbers (MSN) up to MSN 1 600 inclusive.

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

CAA AD Number: CAA-2015-06-003A

Aeronautics Authority of Original AD: EASA

Original AD Number: 2015-0101R1

Effective Date: 2015/06/17

Subject: Fuselage – Skin and Structure / Allowable Damage Limits – Records Check / Repair

Reference Publications (Revision/ATA/SB): ATA 53. This AD revises EASA AD 2015-0101(CAA-2015-06-003), dated 03 June 2015. Ref. Publications: Airbus SB A330-53-3232 original issue dated 04 November 2014. and Airbus SB A340-53-4222 original issue dated 25 November 2014. and Airbus SB A330-53-3233 original issue dated 26 September 2014. and Airbus SB A340-53-4223 original issue dated 26 September 2014. and Airbus SB A330-53-3234 original issue dated 08 December 2014. and Airbus SB A340-53-4224 original issue dated 15 December 2014 and Airbus SB A330-53-3235 Revision 01 dated 14 January 2015. and Airbus SB A340-53-4225 Revision 01 dated 14 January 2015. Airbus SRM dated April 2013. and Airbus SRM TR 53-001 dated 28 November 2014. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Remarks

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