適航指令資料庫查詢
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。
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發布日期
- 2020/12/29
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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.
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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.
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民航局AD編號
- CAA-2020-12-013
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原發布國
- FAA
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原AD編號
- 2020-25-10
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生效日期
- 2021/01/21
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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.
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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.
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存檔序號
- 109-12-014
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專業分項
- Powerplant
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產品類別
- Engine
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備註
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檔案下載
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1.本局早期(2012年前)所發布AD目前未提供檔案下載服務。如欲查詢,請自行連結原發布國民航主管機關網頁,再依”原AD編號”查詢。
2.我國目前所引進航空產品原發布國民航主管機關網頁聯結如下:
Canada、EASA、FAA、Israel、JapanCAB、UK、Brazil、CAA-CZ