Airworthiness Directives (ADs)
82-A300-138A
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
- 1996/06/21
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Applicability
- A300
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Model Number
- A300
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CAA AD Number
- 82-A300-138A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 96-12-02
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Effective Date
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Subject
- Requires measurements of the thickness of the inner skin of the longitudinal lap joint from the inside of the fuselage at certain stringers. Compliance: (a) Within 60 days after the effective date of this AD, accomplish paragraphs(a)(1) and (a)(2) I.A.W.
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Reference Publications (Revision/ATA/SB)
- AOT 53-05R1
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Remarks
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Download
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