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Airworthiness Directives (ADs)

86-JT8-043

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.

Issue Date
1997/10/09
Applicability
JT8D
Model Number
JT8D
CAA AD Number
86-JT8-043
Aeronautics Authority of Original AD
FAA
Original AD Number
97-19-12
Effective Date
Subject
To prevent 4th stage LPT blade failure due to hub cracking, which can result in an uncontained engine failure and damage to the aircraft.
Reference Publications (Revision/ATA/SB)
ASB A6247
Remarks
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