Airworthiness Directives (ADs)
83-A320-045C
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
- 1997/11/03
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Applicability
- A320
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Model Number
- A320
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CAA AD Number
- 83-A320-045C
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Aeronautics Authority of Original AD
- DGAC
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Original AD Number
- 1996-271-092(B)R1
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Effective Date
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Subject
- To detect wear of the inboard flap trunnion and on the protective shells installed on the trunnion caused by chafing of the sliding panel driving chain which could lead to rupture of the trunnion primary load path and subsequent adverse influence on the secondary load path fatigue life.
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Reference Publications (Revision/ATA/SB)
- AD 96-271-092(B), FAA AD 99-17-11
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Remarks
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Download
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