交通部民用航空局

發布日期

2020/06/15

適用性說明

Model 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, as identified in Embraer Service Bulletin 190-54-0015, revision 03, dated February 04, 2019. and Model 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, as identified in Embraer Service Bulletin 190-54-0016, Revision 2, dated September 12, 2016. and Model ERJ190-100 ECJ airplanes, as identified in Embraer Service Bulletin 190LIN- 54-006, revision 03, dated July 17, 2019.and Model ERJ 190-100 ECJ airplanes, as identified in Embraer Service Bulletin 190LIN- 54-0008, dated October 2, 2015.

型別

Embraer Model ERJ 190-100 STD, 190-100 LR, 190-100 IGW, 190-100 SR, 190-200 STD, 190-200 LR, and 190-200 IGW

民航局AD編號

CAA-2020-06-008(已有後續修訂版)

原發布國

ANAC

原AD編號

2020-06-02

生效日期

2020/06/16

主旨摘要

This AD is issued to reduce the applied torque to the castellated nuts of the external shear pins, to include the inspection/replacement, if applicable, of the external shear pin and to change the compliance time for the pylon lower link fitting modification.

參考資訊（版本/ATA/SB）

This AD cancels and supersedes the AD No. 2014-07-01(CAA-2014-07-004) – Embraer S.A./39-1384, dated July 10, 2014, and AD No. 2017-04-01(CAA-2017-04-008) – Embraer/39-1413, dated April 25, 2017

存檔序號

109-06-010

專業分項

Structure

產品類別

Airplane

備註

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