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CAA-2020-12-013

依據民用航空法規,航空器所有人或使用人除應遵守本國民航局所發布適航指令,亦應遵守航空器設計國之民航主管機關所通告之適航指令。

發布日期
2020/12/29
適用性說明
GE model GEnx-1B67/P2, GEnx-1B70/75/P2, GEnx-1B70/P2, GEnx-1B70C/P2, GEnx-1B74/75/P2, GEnx-1B76/P2, and GEnx-1B76A/P2 model turbofan engines that have a high-pressure turbine (HPT) rotor stage 2 disk, part number (P/N) 2383M86P02, and a serial number (S/N) listed in paragraph 4, Appendix–A, Table 1, Table 2, or Table 3, of GE GEnx-1B Service Bulletin (SB) 72-0463 R01, dated January 6, 2020, installed. and GEnx-2B67/P model turbofan engines that have a HPT rotor stage 2 disk, P/N 2383M86P02, and a S/N listed in paragraph 4, Appendix–A, Table 1, Table 2, or Table 3, of GE GEnx-2B SB 72-0402 R01, dated January 8, 2020, installed.
型別
General Electric GEnx-1B64/P2, GEnx-1B67/P2, GEnx-1B70/75/P2, GEnx-1B70/P2, GEnx-1B70C/P2, GEnx-1B74/75/P2, GEnx-1B76/P2, GEnx-1B76A/P2, and GEnx-2B67/P model turbofan engines.
民航局AD編號
CAA-2020-12-013
原發布國
FAA
原AD編號
2020-25-10
生效日期
2021/01/21
主旨摘要
This AD requires an immersion ultrasonic inspection of the HPT rotor stage 2 disk and, depending on the results of the inspection, replacement of the HPT rotor stage 2 disk with a part eligible for installation.
參考資訊(版本/ATA/SB)
ATA 72. Ref. GEnx-1B Service Bulletin (SB) 72-0463 R01, dated January 6, 2020, and GEnx-2B SB 72-0402 R01, dated January 8, 2020.
存檔序號
109-12-014
專業分項
Powerplant
產品類別
Engine
備註
檔案下載
CAA-2020-12-013.pdf

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