適航指令資料庫查詢

民航業務

CAA-2025-09-006

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。

適用性說明: This AD applies to all airplanes, certificated in any category, with a restraint system with a PacificScientific Company rotary buckle assembly (buckle) part number (P/N) 1111475 (all dash numbers) orP/N 1111548-01 installed having a date of manufacture (DOM) between January 2012 and April 2013inclusive, or an unknown DOM. These buckles may be installed on, but not limited to, The BoeingCompany model airplanes. Note 1 to paragraph (c): The buckle may be included as a component of a different part-numberedrestraint system assembly. Note 2 to paragraph (c): These buckles may also be installed on helicopters; however, the FAAdetermined that a shorter compliance time to accomplish the required actions is required for bucklesinstalled on helicopters. Accordingly, the FAA published a separate AD (AD 2024-20-04, Amendment39-22863 ( 89 FR 85040 , October 25, 2024)) to address all helicopters with an affected buckleinstalled.

主旨摘要: This AD requires inspecting the buckle screws, and depending on the results, reidentifying the buckle, replacing the screws and reidentifying the buckle, or replacing the buckle. This AD also allows optionally prohibiting use of the seat until the actions required by this AD are accomplished. This AD also prohibits installing certain buckles on any airplane.

參考資訊（版本/ATA/SB）: ATA 25. Ref. Parker Meggitt Service Bulletin SB 1111475-25-001-2023, Revision 002, dated April 1, 2024. and Parker Meggitt Service Bulletin SB 1111548-25-001-2023, Revision 002, dated April 1, 2024.

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