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Airworthiness Directives (ADs)

CAA-2005-08-016

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
2005/08/25
Applicability
GE CF6-80C2 and CF6-80E1
Model Number
GECF6
CAA AD Number
CAA-2005-08-016
Aeronautics Authority of Original AD
FAA
Original AD Number
2005-17-05
Effective Date
Subject
To prevent failure of the HPCR stage 11-14 spool shaft due to low-cycle fatigue that could result in an uncontained engine failure.
Reference Publications (Revision/ATA/SB)
SB CF6–80C2 S/B 72–1052R2 and CF6–80E1 S/B 72–0232R1
Remarks
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