適航指令資料庫查詢
CAA-2024-04-011
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
- 2024/05/03
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適用性說明
- This AD applies to CFM International, S.A. (CFM) Model LEAP-1A23, LEAP-1A24, LEAP-1A24E1, LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1, LEAP-1A29, LEAP-1A29CJ, LEAP-1A30, LEAP-1A32, LEAP-1A33, LEAP-1A33B2, and LEAP-1A35A engines with an installed No. 3 bearing spring finger housing having part number (P/N) 2629M62G01 and aserial number identified in Table 1 or Table 2 of CFM Service Bulletin (SB) LEAP-1A-72-00-0504-01A-930A-D, Issue002, dated October 17, 2023 (CFM SB LEAP-1A-72-00-0504-01A-930A-D, Issue 002).
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型別
- CFM LEAP-1A23, LEAP-1A24, LEAP-1A24E1,
LEAP-1A26, LEAP-1A26CJ, LEAP-1A26E1,
LEAP-1A29, LEAP-1A29CJ, LEAP-1A30,
LEAP-1A32, LEAP-1A33, LEAP-1A33B2,
and LEAP-1A35A engines.
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民航局AD編號
- CAA-2024-04-011
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原發布國
- FAA
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原AD編號
- 2024-07-06
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生效日期
- 2024/06/03
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主旨摘要
- This AD requires initial and repetitive calculations of the levels of NSV, inspection of the stage 2 high-pressure turbine nozzle assembly honeycomb and HPT stator stationary seal honeycomb and, depending on the results of the calculations and inspections, replacement of certain parts. and also requires replacement of certain No. 3 bearing spring finger housings at a certain time.
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參考資訊(版本/ATA/SB)
- ATA 72 .Ref. CFM International, S.A. Service Bulletin LEAP-1A-72-00-0504-01A-930A-D, Issue 002, dated October 17, 2023.
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存檔序號
- 113-04-020
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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