Airworthiness Directives (ADs)
CAA-2021-07-017
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
- 2021/07/27
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Applicability
- CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3, CF6-80C2A1, CF6-80C2A2, CF6-80C2A3, CF6-80C2A5, CF6-80C2A5F, CF6-80C2A8, CF6-80C2B1, CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2, CF6-80C2B2, CF6-80C2B2F, CF6-80C2B3F, CF6-80C2B4, CF6-80C2B4F, CF6-80C2B5F, CF6-80C2B6, CF6-80C2B6F, CF6-80C2B6FA, CF6-80C2B7F, CF6-80C2B8F, CF6-80C2D1F, CF6-80C2K1F, and CF6-80C2L1F model turbofan engines with an installed thermal shield having one of the following part numbers: 2787M85P01, 9315M41P09, 9315M41P13, 9315M41P14, 9315M41P15, 9315M41P16, 9315M41P20, 9348M13P01, 9367M63P01, 9367M63P02, 9367M63P03, 9367M63P04, 9367M63P05, 9367M63P06, 9367M63P07, or 9315M41P20.
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Model Number
- General Electric - CF6-80A and CF6-80C2 turbofan engines.
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CAA AD Number
- CAA-2021-07-017
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2021-14-11
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Effective Date
- 2021/08/27
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Subject
- This AD requires visual inspection and fluorescent penetrant inspection of the HPT thermal shield and, if cracking is detected, removal from service of the HPT thermal shield, HPT
rotor stage 1 disk and HPT rotor stage 2 disk.
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Reference Publications (Revision/ATA/SB)
- None
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Remarks
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Download
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