適航指令資料庫查詢
CAA-2009-04-011
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
- 2009/04/28
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適用性說明
- This Airworthiness Directive (AD) applies to Embraer Model ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-200 IGW, ERJ 190-200 LR and ERJ 190-200 STD airplanes.
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型別
- Embraer Model ERJ 190-100 IGW, ERJ 190-100 LR, ERJ 190-100 STD, ERJ 190-200 IGW, ERJ 190-200 LR and ERJ 190-200 STD airplanes.
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民航局AD編號
- CAA-2009-04-011
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原發布國
- ANAC
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原AD編號
- 2009-04-02(BRAZIL)
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生效日期
- 2009/04/29
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主旨摘要
- During ERJ 190 airplane full scale fatigue test, cracks were found in some structural components of the airplane. Analysis of these cracks resulted in modifications on the airplane Airworthiness Limitation Items (ALI), to include new inspections tasks or modification of existing ones and its respective thresholds and intervals. Failure to inspect these components according to the new tasks, thresholds and intervals could prevent a timely detection of fatigue cracks. Undetected fatigue cracks in these areas could
adversely affect the structural integrity of these airplanes.
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參考資訊（版本/ATA/SB）
- Temporary Revisions (TR) 2-5, dated 06 Dec. 2007; and TR 2-6, dated 12 Feb. 2008 of the Embraer 190 MRB Report (MRB-1928).
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存檔序號
- 98-04-014
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專業分項
- Structure
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產品類別
- Airplane
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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