Airworthiness Directives (ADs)
89-GECF6-026
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
- 2000/09/05
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Applicability
- CF6-45, -50, -80A, -80C2, and –80E1 Turbofan Engines
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Model Number
- GECF6
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CAA AD Number
- 89-GECF6-026
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2000-16-12
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Effective Date
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Subject
- To detect cracks which can cause separation of the HPCR stage 3-9 spool and result in an uncontained engine failure.
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Reference Publications (Revision/ATA/SB)
- ASB’s No. CF6-50 72-A1108, Revision 3; CF6-80A 72-A0678, Revision 3; CF6-80C2 72-A0812, Revision 2; CF6-80E1 72-A0135, Revision 1;ASB’s CF6-80C2 72-A0848, Revision 5; and CF6-80E1 72-A0126, Revision 3
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Remarks
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Download
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