Airworthiness Directives (ADs)
86-A300-224
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
- 1997/07/02
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Applicability
- A300, A310, A300-600
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Model Number
- A300
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CAA AD Number
- 86-A300-224
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Aeronautics Authority of Original AD
- DGAC
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Original AD Number
- 1997-124-223(B)
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Effective Date
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Subject
- In order to detect and prevent crack initiation and propagation, associated with fatigue phenomena on the forward passenger door stop fittings, which could lead to the rupture of one of the fittings and thus to reduction of the fatigue strength of the other fittings.
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Reference Publications (Revision/ATA/SB)
- SB A300-53-0309, A310-53-2087, A300-53-6060
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Remarks
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Download
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