適航指令資料庫查詢
CAA-2006-10-002
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
- 2006/10/04
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適用性說明
- This AD applies to those Lycoming Engines (L)O-360, (L)IO- 360, AEIO-360, O-540, IO-540, AEIO-540, (L)TIO-540, IO-580, and IO- 720 series reciprocating engines listed by engine model number and serial number in Table 1, Table 2, Table 3, or Table 4 of Lycoming Mandatory Service Bulletin (MSB) 569A, dated April 11, 2006, and those engines with crankshafts listed by crankshaft serial number in Table 5 of Lycoming MSB 569A, dated April 11, 2006. These applicable engines are manufactured new or rebuilt, overhauled, or had a crankshaft installed after March 1, 1997.
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型別
- Lycoming Engines (L)O-360, (L)IO-360, AEIO-360, O-540, IO-540, AEIO-540, (L)TIO-540, IO-580, and IO-720 Series Reciprocating Engines
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民航局AD編號
- CAA-2006-10-002
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原發布國
- FAA
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原AD編號
- 2006-20-09
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生效日期
- 2006/11/03
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主旨摘要
- To prevent failure of the crankshaft, which will result in total engine power loss, in-flight engine failure, and possible loss of the aircraft.
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參考資訊（版本/ATA/SB）
- Lycoming Engines Service Instruction No. 1009AS and Lycoming Engines Mandatory Service Bulletin No. 569A.
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存檔序號
- 95-10-004
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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