Airworthiness Directives (ADs)
CAA-2008-03-002
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
- 2008/03/10
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Applicability
- AIRBUS aircraft A340-200 and A340-300 series, all certified models, all serial numbers.
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Model Number
- AIRBUS A340-200/-300 series aircraft
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CAA AD Number
- CAA-2008-03-002
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2008-0050
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Effective Date
- 2008/03/18
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Subject
- Fuselage – Internal structure – Frame Foot Junction with Lateral Frame (FR) from FR 40.3 to FR 45 - Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 53; AIRBUS A340 ALI Issue 10 referenced AI/SE-M4/95A.0051/97 approved under EASA.A.C.05841 on 13 April 2007. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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Remarks
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