Airworthiness Directives (ADs)
83-JT8-025A
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
- 1999/11/18
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Applicability
- JT8D-209, 217, 217A, 217C and 219
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Model Number
- JT8D
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CAA AD Number
- 83-JT8-025A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 99-22-14
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Effective Date
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Subject
- To prevent damage to the airplane resulting from uncontained engine debris following a high pressure turbine (HPT) shaft fracture of a low pressure turbine (LPT) blade failure.
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Reference Publications (Revision/ATA/SB)
- ASB No.A6346R1, No.6149R1, FAA AD 93-23-10
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Remarks
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Download
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