Airworthiness Directives (ADs)
CAA-2006-10-011A
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.
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Issue Date
- 2006/11/28
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Applicability
- AIRBUS A330 aircraft, models -201, -202, - 203, - 223, -243, -301, -321, -
322, -323, -341, -342 and -343, all serial numbers, except those on which
AIRBUS modification 49202 has been embodied in production or AIRBUS
Service Bulletin (SB) A330-57-3090 has been embodied in service.
AIRBUS aircraft A340-200 and A340-300 series, all certified models, all
serial numbers, except those on which AIRBUS modification 49202 has
been embodied in production or AIRBUS Service Bulletin (SB) A340-57-
4098 has been embodied in service.
This Airworthiness Directive (AD) is not applicable to A340 200/-300
aircraft repaired in accordance with Repair Drawing R57115053 or
R57115051 or R57115047 (installation of Titanium Doubler) which are
covered by EASA AD 2006-0314.
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Model Number
- A330 and A340-200/-300 aircraft
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CAA AD Number
- CAA-2006-10-011A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2006-0315R1
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Effective Date
- 2006/10/27
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Subject
- Wings – Centre Wing Box – Keel beam fastener holes at frame 40 - Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 57
Revision/Supersedure : This AD revises and supersedes EASA AD 2006-0315(CAA-2006-10-011)
AIRBUS Service Bulletin A330-57-3081 Revision 02;
AIRBUS Service Bulletin A340-57-4089 Revision 02.
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Remarks
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