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Airworthiness Directives (ADs)

CAA-2012-03-004

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
2012/03/09
Applicability
To all GE CF6-80C2 model turbofan engines, including engines marked on the engine data plate as CF6-80C2B7F1.
Model Number
General Electric Company (GE) Turbofan Engines
CAA AD Number
CAA-2012-03-004
Aeronautics Authority of Original AD
FAA
Original AD Number
2012-03-12
Effective Date
2012/04/05
Subject
We are issuing this AD to prevent an uncontained failure of the high-pressure compressor (HPC) rotor or the low-pressure turbine (LPT) rotor, or both, which could cause damage to the airplane.
Reference Publications (Revision/ATA/SB)
(i) General Electric Company (GE) Service Bulletin (SB) CF6-80C2 S/B 72-1405, dated June 30, 2011; (ii) GE SB CF6-80C2 S/B 72-1405, Revision 01, dated December 16, 2011; and (iii) GE SB CF6-80C2 S/B 72-1427, dated December 16, 2011.
Remarks
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CAA-2012-03-004.pdf
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