Airworthiness Directives (ADs)
2002-12-013
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
- 2002/12/25
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Applicability
- GE CF6-45, -50, -80A, -80C2, and -80E1 turbofan engines with high pressure compressor rotor (HPCR) stage 3-9 spools
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Model Number
- GECF6
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CAA AD Number
- 2002-12-013
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2002-25-08
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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 possible uncontained engine failure.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 95-18-14(CCAA AD 84-GECF6-011); AD 99-24-15(CCAA AD 84-GECF6-012A); and AD 2000-16-12(CCAA AD 89-GECF6-026).
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Remarks
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