CTHIn ForceLegislation
AD/A330/99 - Centre Wing - Frame 40 Rear Fitting Web
//
© 2026 Zoe. All rights reserved.
Zoe is a legal information platform. Always consult the Federal Register of Legislation for authoritative text.
AD/A330/99 - Centre Wing - Frame 40 Rear Fitting Web
Start here
Turn the raw legal text into a practical explanation grounded in AD/A330/99 - Centre Wing - Frame 40 Rear Fitting Web.
| AD/A330/99 | Centre Wing - Frame 40 Rear Fitting Web | 3/2009 |
|---|
| Applicability: | Model A330-301, -321, -322, -341, and -342 aircraft, all serial numbers; except aircraft with modification 44360 incorporated in production. |
|---|---|
| Requirement: | Action in accordance with the requirements of EASA AD 2009-0001.Note: AIRBUS Service Bulletin A330-57-3107 original issue, or later EASA approved revision, refers. |
| Compliance: | As specified in the Requirement document, with a revised effective date of12 March 2009. |
| This Airworthiness Directive becomes effective on 12 March 2009. | |
| Background: | During accomplishment of A330-300 Airworthiness Limitation Item task57.11.04-01-02 of a fastener hole between stringer 38 and 39 at FR40 rear fitting web, a crack was found on an adjacent hole at vertical post Y1959 lower attachment on both sides. Other crack findings on this adjacent hole have been reported onA330-300 and A340-200/300 aircraft as a result of sampling inspections. Unless detected and corrected, crack propagation could result in the loss of fuselage structural integrity. |
Image unavailable in extracted text
David Punshon
Delegate of the Civil Aviation Safety Authority
14 January 2009