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Airworthiness Directives (ADs)

CAA-2019-06-007

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
2019/06/17
適用機型摘要
This AD applies to The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-53A1368, dated February and Installation of Supplemental Type Certificate (STC) ST00830SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST00830SE is installed, a “change in product” alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.
型別
The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes
民航局AD編號
CAA-2019-06-007
原發布國
FAA
原AD編號
2019-11-06
生效日期
2019/07/17
主旨摘要
This AD requires repetitive inspections of the skin under the drag link assembly for any cracks, and applicable on-condition actions.
參考資訊(版本/ATA/SB)
ATA 53. Ref. Boeing Alert Service Bulletin 737-53A1368, dated February 27, 2018.
存檔序號
108-06-008
專業分項
Structure
產品類別
Airplane
備註
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