交通部民用航空局

發布日期

2007/05/29

適用性說明

Boeing Model 737-200, 737-300, 737-400, 737-500, 737-600, 737-700, 737-800, 737-900, 757-200, and 757-300 Series Airplanes; and McDonnell Douglas Model DC-10-10, DC-10-10F, DC- 10-30, DC-10-30F, DC-10-40, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes;Equipped With Reinforced Flight Deck Doors Installed in Accordance With Supplemental Type Certificate (STC) ST01335LA, STC ST01334LA, and STC ST01391LA, Respectively.

型別

737,757,MD11

民航局AD編號

CAA-2003-07-014B

原發布國

FAA

原AD編號

2007-10-12

生效日期

2007/06/27

主旨摘要

To prevent inadvertent release of the decompression latch and consequent opening of the decompression panel in the flight deck door, or penetration of the flight deck door by smoke, any of which could result in injury to the airplane flightcrew. Also,to detect and correct wire chafing, which could result in arcing, fire, and/or reduced controllability of the airplane.

參考資訊（版本/ATA/SB）

Supersedes AD 2005-12-05(CAA AD 2003-07-014A). Ref. C&D Aerospace ASB B221001–52A02 and B221001–52A05R3; C&D Aerospace SB B211200–52–01R3, B211200–52–02R1&R2, B221001–52–03R3, B221200-52-01R1, B231001-52-02R4 and B251200–52–01; Report CDRB22–69RE.

存檔序號

96-05-015

專業分項

Systems

產品類別

Airplane

備註

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