適航指令資料庫查詢
CAA-2012-03-012
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。
-
發布日期
- 2012/03/27
-
適用性說明
- This Airworthiness Directive applies to Embraer S.A. model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 STD ERJ 190-200 LR and ERJ 190-200 IGW airplanes; as identified in the Embraer Service Bulletin No. 190-53-0054, Revision 1, dated March 16, 2012 or Embraer Service Bulletin No. 190LIN-53-0059, Revision 01, dated March 16, 2012 or further revisions approved by the ANAC.
-
型別
- ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 ECJ, ERJ 190-100 SR, ERJ 190-200 STD ERJ 190-200 LR and ERJ 190-200 IGW airplanes.
-
民航局AD編號
- CAA-2012-03-012
-
原發布國
- ANAC
-
原AD編號
- 2012-03-03(BRAZIL)
-
生效日期
- 2012/04/13
-
主旨摘要
- It has been found the occurrences of chafing between the Auxiliary Power Unit (APU) Electronic Starter Controller (ESC) power cables (harness W205) and the airplane tail cone firewall due to the grommet installed in the tail cone firewall moves out of its place. This condition, if not corrected, may result in reduced structural integrity of the fuselage and empennage in an event of fire penetration through the firewall.
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.
-
參考資訊(版本/ATA/SB)
- EMBRAER 190-53-0054R1 and 190LIN-53-0059R1.
-
存檔序號
- 101-03-017
-
專業分項
- Structure
-
產品類別
- Airplane
-
備註
-
檔案下載
-
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