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Airworthiness Directives (ADs)

CAA-2018-08-013(已被CAA-2020-10-008取代)

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
2018/08/31
Applicability
General Electric Company (GE) CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3, CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A5F, CF6-80C2A8, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6-80C2B7F, CF6-80C2D1F, CF6-80C2L1F, and CF6-80C2K1F turbofan engines with high-pressure turbine (HPT) disks with serial numbers listed in Table 1 and 2 of Appendix A in GE CF6-80C2 Service Bulletin (SB) 72-1562 R03, dated January 10, 2018; and Table 1 of Appendix A in GE CF6-80A SB 72-0869 R01, dated October 19, 2017.
Model Number
General Electric Company, CF6-80 serial Turbofan Engines
CAA AD Number
CAA-2018-08-013(已被CAA-2020-10-008取代)
Aeronautics Authority of Original AD
FAA
Original AD Number
2018-15-04
Effective Date
2018/10/02
Subject
Engine - High-Pressure Turbine of HPT stage 1 disk (CF6-80C2) and HPT stage 2 disk (CF6-80C2 and CF6-80A)- Inspection / Replacement / Modification
Reference Publications (Revision/ATA/SB)
ATA 72. Ref. GE CF6-80A Service Bulletin (SB) 72-0869 R01, dated October 19, 2017. and GE CF6-80C2 SB 72-1562 R03, dated January 10, 2018.
Remarks
Download
CAA-2018-08-013.pdf
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