適航指令資料庫查詢
CAA-2012-08-008
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
- 2012/08/29
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適用性說明
- (1) PW4052, PW4152, and PW4056 turbofan engines, including models with any dash number suffix, with a high-pressure turbine (HPT) stage 1 front hub part number (P/N) listed in Table 1 to paragraph (c) of this AD installed. (2) PW4156A, PW4060, PW4060A, PW4060C, PW4062, PW4062A, PW4158, PW4460, and PW4462 turbofan engines, including models with any dash number suffix, with an HPT stage 1 front hub P/N listed in Table 1 to paragraph (c) of this AD installed. (3) PW4164, PW4164C, PW4164C/B, PW4168, and PW4168A turbofan engines with an HPT stage 1 front hub, P/N 51L901, installed with an S/N not listed in Table 3 of the Accomplishment
Instructions of Pratt & Whitney ASB No. PW4G-100-A72-246, dated June 28, 2012.
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型別
- Pratt & Whitney Division PW4000, PW4100, PW4400 turbofan engines.
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民航局AD編號
- CAA-2012-08-008
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原發布國
- FAA
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原AD編號
- 2012-16-01
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生效日期
- 2012/09/28
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主旨摘要
- Engine - high-pressure turbine (HPT) stage 1 front hubs - Removal/ Installation
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參考資訊（版本/ATA/SB）
- (i) Pratt & Whitney Alert Service Bulletin (ASB) No. PW4ENG A72-821, dated July 6, 2012. (ii) Pratt & Whitney ASB No. PW4G-100-A72-246, dated June 28, 2012.
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存檔序號
- 101-08-010
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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