Airworthiness Directives (ADs)
CAA-2011-08-010
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
- 2011/08/26
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Applicability
- This AD applies to General Electric Company (GE) CF34-10E2A1; CF34-10E5; CF34-10E5A1; CF34-10E6; CF34-10E6A1; CF34-10E7; and CF34-10E7-B turbofan engines, with a fan rotor spinner part number (P/N) 2050M34G03; 2050M34G04; 2050M34G05; 2050M34G06; 2437M60G01; or 2437M60G02, installed.
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Model Number
- General Electric Company CF34-10E2A1; CF34-10E5; CF34-10E5A1; CF34-10E6; CF34-10E6A1; CF34-10E7; and CF34-10E7-B Turbofan Engines
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CAA AD Number
- CAA-2011-08-010
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2011-18-02
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Effective Date
- 2011/09/26
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Subject
- To prevent high-cycle fatigue cracking of the fan rotor spinner support attachment lugs, leading to separation of the fan rotor spinner assembly, uncontained failure of the engine, and damage to the airplane.
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Reference Publications (Revision/ATA/SB)
- Refer to GE Service Bulletin No. CF34-10E S/B 72-0186
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Remarks
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