Airworthiness Directives (ADs)
86-JT8-042
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
- 1997/02/20
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Applicability
- JT8D-200 series turbofan engines
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Model Number
- JT8D
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CAA AD Number
- 86-JT8-042
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 97-02-11
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Effective Date
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Subject
- To prevent front compressor front hub (fan hub) failure due to tierod, counterweight, or bushed hole cracking, which could result in an uncontained engine failure and damage to the aircraft
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Reference Publications (Revision/ATA/SB)
- A6272, NDIP-892,
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Remarks
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Download
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