Airworthiness Directives (ADs)
89-767-154(已有後續修訂版)
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
- 2000/06/29
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Applicability
- 767 series airplanes.
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Model Number
- 767
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CAA AD Number
- 89-767-154(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2000-12-17
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Effective Date
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Subject
- To detect fatigue cracks in the pitch load fittings of the wing front spar, which could result in reduced structural integrity of the strut.
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Reference Publications (Revision/ATA/SB)
- SB767-57-0053R2
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Remarks
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Download
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