Airworthiness Directives (ADs)
85-JT8-041
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
- 1996/12/31
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Applicability
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Model Number
- JT8D
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CAA AD Number
- 85-JT8-041
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 96-23-14
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Effective Date
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Subject
- To prevent CCOC flange cracks that could result in uncontained engine failure, inflight engine shutdown, engine cowl release, and airframe damage.
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Reference Publications (Revision/ATA/SB)
- supersedes AD 87-11-07R1, 95-08-15, 取代75-JT8-011B, 84-JT8-035
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Remarks
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Download
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