Airworthiness Directives (ADs)
CAA-2002-09-001B
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
- 2004/09/10
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Applicability
- CFM56-5C series turbofan engines
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Model Number
- CFM565
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CAA AD Number
- CAA-2002-09-001B
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 97-09-02R3
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Effective Date
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Subject
- To prevent low cycle fatigue (LCF) failure of the high pressure turbine rotor (HPTR) front shaft, HPTR front air seal, and booster spool, which could result in an uncontained failure and damage to the airplane.
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Reference Publications (Revision/ATA/SB)
- Revises AD 97-09-02R2(CCAA AD 2002-09-001A).
Ref. Current airworthiness limitations section of Chapter 05 of the CFM56-5C Engine Shop Manual, CFMI-TP.SM.8.
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Remarks
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