適航指令資料庫查詢
CAA-2010-01-002
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
- 2010/01/05
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適用性說明
- This AD applies to the Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, "Parallel Valve," reciprocating engines listed in Table 1 of this AD, with ECi cylinder assembly, part number (P/N) AEL65102 series "Titan," and with cylinder head, P/N AEL85099, installed.
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型別
- Engine Components, Inc. (ECi) Reciprocating Engine Cylinder Assemblies
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民航局AD編號
- CAA-2010-01-002
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原發布國
- FAA
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原AD編號
- 2009-26-12
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生效日期
- 2010/02/04
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主旨摘要
- To prevent loss of engine power due to cracks at the head-to-barrel interface and possible engine failure caused by separation of a cylinder head, which could result in loss of control of the aircraft.
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參考資訊（版本/ATA/SB）
- This AD supersedes AD 2008-19-05(CAA-2008-09-003).
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存檔序號
- 99-01-002
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專業分項
- Powerplant
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產品類別
- Application
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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