適航指令資料庫查詢
CAA-2010-06-006A
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
- 2010/08/09
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適用性說明
- This Airworthiness Directive is applicable to Embraer Models ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR and ERJ 190-200 IGW airplanes with serial numbers 19000002, 19000004, 19000006 thru 19000108, 19000110 thru 19000139, 19000141 thru 19000157, 19000160, 19000165, 19000167 thru 19000176, 19000178 thru 19000199, 19000273 thru 19000276, 19000279 thru 19000286, 19000288 thru 19000295,19000297 thru 19000304, and 19000309.
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型別
- EMBRAER ERJ-190
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民航局AD編號
- CAA-2010-06-006A
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原發布國
- ANAC
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原AD編號
- 2010-06-02R1(BRAZIL)
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生效日期
- 2010/08/25
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主旨摘要
- It has been found the occurrence of drill marks at the lower ring region of the rear pressure bulkhead between circumferential splice joint and rear skin located between stringers 12 and 13.
These marks may result in formation of fatigue cracks accelerated by corrosion reducing the structural strength of the rear pressure bulkhead, which may cause a sudden decompression of the passenger cabin.
Since this condition may occur in other airplanes of the same type and affects flight safety, a corrective action is required. Thus, sufficient reason exists to request compliance with this AD in
the indicated time limit.
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參考資訊（版本/ATA/SB）
- This AD cancels and supersedes the AD No.2010-06-02(CAA-2010-06-006).
Ref. Embraer Service Bulletin No.190-53-0042.
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存檔序號
- 99-08-009
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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