交通部民用航空局

發布日期

2014/05/12

適用性說明

Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), except those on which Airbus modification (Mod) 55306 or 55792 has been embodied in production. Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN, except those on which Airbus Mod 55306 or 55792 has been embodied in production and except those on which Airbus Repair Drawing R57115053 or R57115051 or R57115047 has been embodied in service on both right-hand (RH) and left-hand (LH) sides.

型別

A330 and A340-200/-300 aeroplanes

民航局AD編號

CAA-2014-01-003A

原發布國

EASA

原AD編號

2014-0010R1

生效日期

2014/05/12

主旨摘要

Wings – Centre Wing Box Keel Beam Fastener Holes at Frame 40 – Inspection

參考資訊（版本/ATA/SB）

ATA 57. This AD revises EASA AD 2014-0010(CAA-2014-01-003) dated 08 January 2014, which superseded EASA AD 2010-0024(CAA-2010-02-004) dated 12 February 2010. Ref. Airbus SB A330-57-3081 original issue dated 30 October 2003, or Revision 01 dated 18 May 2004, or Revision 02 dated 24 January 2006, or Revision 03 dated 31 July 2009, or Revision 04 dated 31 May 2011, or Revision 05 dated 13 November 2012.

存檔序號

103-05-001

專業分項

Structure

產品類別

Airplane

備註

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