Airworthiness Directives (ADs)
85-A320-089
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
- 1996/12/04
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Applicability
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Model Number
- A320
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CAA AD Number
- 85-A320-089
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Aeronautics Authority of Original AD
- DGAC
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Original AD Number
- 96-237-090(B)
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Effective Date
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Subject
- In order to detect fatigue cracks on the connecting angle between frame 56 and frame support at stringer 38, which could affect the structural integrity of the airplane.
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Reference Publications (Revision/ATA/SB)
- A320-53-1084R1, A320-53-1011
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Remarks
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