適航指令資料庫查詢
CAA-2014-04-006(已有後續修訂版)
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
- 2014/04/30
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適用性說明
- HR Smith (Technical Developments) Crash Position Indicator (CPI) System 15-503-134 and 15-503-134-1 series, when equipped with Control Panel part number (P/N) 503-22-() and Beacon release unit P/N 503-21 and System Interface Unit P/N 503-24-() (including 503-24) or P/N 503-42-() (including 503-
42), except System Interface Units having P/N 503-24-A, P/N 503-24-()-A, P/N 503-24-G, P/N 503-24-()-G, P/N 503-42-A, P/N 503-42-()-A, P/N 503-42-G or P/N 503-42-()-G.
This CPI System is known to be installed on, but not limited to the following aircraft:
- Eurocopter Models EC 155B, EC 155 B1, SA 365 N, AS 365 N3, AS 332 L1, AS 332 L2 and EC 225 LP,
- Eurocopter Deutschland EC 135 series, BK117-C2, - Agusta Westland A109 series, AB139 and AW139, - Sikorsky S-61N, S-76 series and S-92A, and - MD Helicopters Inc. MD900.
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型別
- HR Smith Crash Position Indicator System
15-503-134 and 15-503-134-1 series
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民航局AD編號
- CAA-2014-04-006(已有後續修訂版)
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原發布國
- EASA
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原AD編號
- 2014-0095
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生效日期
- 2014/05/07
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主旨摘要
- Equipment / Furnishings – Crash Position Indicator – Modification
Aircraft Flight Manual – Amendment
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參考資訊（版本/ATA/SB）
- ATA 25. This AD supersedes EASA AD 2014-0019(CAA-2014-01-009) dated 17 January 2014.
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存檔序號
- 103-04-007
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專業分項
- Systems
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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