適航指令資料庫查詢
CAA-2021-07-017
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
- 2021/07/27
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適用性說明
- 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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型別
- General Electric - CF6-80A and CF6-80C2 turbofan engines.
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民航局AD編號
- CAA-2021-07-017
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原發布國
- FAA
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原AD編號
- 2021-14-11
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生效日期
- 2021/08/27
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主旨摘要
- 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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參考資訊（版本/ATA/SB）
- None
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存檔序號
- 110-07-022
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專業分項
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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