交通部民用航空局

發布日期

2020/08/04

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 ERJ 190-100 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-2020-06-008A(已有後續修訂版)

原發布國

ANAC

原AD編號

2020-06-02R01

生效日期

2020/08/03

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, to change the compliance time for the pylon lower link fitting modification and revised to include further SB revisions approved by the ANAC and to clarify the termiatnion requirements.

參考資訊（版本/ATA/SB）

This AD cancels and supersedes the AD No. 2020-06-02(CAA-2020-06-008) – 39-1464, dated June 16, 2020

存檔序號

109-08-002

專業分項

Structure

產品類別

Airplane

備註

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