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CAA-2009-02-004 修訂

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
2009/02/26
適用性說明
Embraer models ERJ 190-100 ECJ, 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 equipped with the outboard slat skew sensor part number (P/N) 1702286A or 1702288A.
型別
ERJ 190
民航局AD編號
CAA-2009-02-004 修訂
原發布國
ANAC
原AD編號
2009-02-03(BRAZIL) Corrected
生效日期
2009/02/16
主旨摘要
It has been found the occurrence of outboard slat skew sensor failure in open or closed position. The combination of an outboard slat skew sensor failed closed, an outboard slat actuator structural failure (rupture) and its adjacent actuator torque limiter failing high (allows higher loads to the panel structure) occurring in the same slat surface, under normal flight loads, may lead slat surface to detach from wing with the possibility of hitting and damaging the horizontal stabilizer and elevator, which may affect the airplane controllability.
參考資訊(版本/ATA/SB)
Aircraft Maintenance Manual (AMM) Task 27-83-01-710-801-A “Outboard Slat Skew Sensor - Operational Test”.
存檔序號
98-02-013
專業分項
Systems
產品類別
Airplane
備註
檔案下載

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