適航指令資料庫查詢
CAA-2012-07-016
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
- 2012/08/01
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適用性說明
- Model HH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH-1F, UH-1H, UH-1L, and UH-1P helicopters, and Southwest Florida Aviation Model UH-1B series (SW204 series and SW204HP) and UH-1H series (SW205 series) helicopters, with a tail rotor blade (blade), part number (P/N) 212-010-750-009 through -129, all serial numbers except serial numbers with a prefix of ''A'' or ''AFS,'' and the number 11926, 13351, 13367, 13393, 13400, 13402, 13515, 13540, 13568, 13595 through 13602, 13619, and subsequent larger numbers, installed, certificated in any category.
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型別
- Model HH-1K, TH-1F, TH-1L, UH-1A, UH-1B, UH-1E, UH-1F, UH-1H, UH-1L, and UH-1P helicopters.
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民航局AD編號
- CAA-2012-07-016
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原發布國
- FAA
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原AD編號
- 2012-14-12
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生效日期
- 2012/09/04
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主旨摘要
- Tail Rotor Blades - Forward Tip Weight Retention Block (tip block) and the Aft Tip Closure - Inspection/ Modification
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參考資訊（版本/ATA/SB）
- Bell Helicopter Textron Alert Service Bulletin No. 212-00-111, Revision D, dated March 18, 2005.
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存檔序號
- 101-07-020
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專業分項
- Structure
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產品類別
- Helicopter
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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