交通部民用航空局

發布日期

2014/10/30

適用性說明

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Beech Aircraft Corporation) airplanes identified in paragraphs (c)(1)(i), (c)(1)(ii), and (c)(1)(iii) of this AD. (i) Model 400 Beechjet airplanes having serial numbers RJ-1 through RJ-65, inclusive. (ii) Model 400A Beechjet airplanes having serial numbers RK-1 through RK-604, inclusive. (iii) Model 400T Beechjet airplanes having serial numbers TT-1 through TT-180, inclusive; and TX-1 through TX-13, inclusive. (2) Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company; Mitsubishi Heavy Industries, Inc. Ltd.) Model MU-300 airplanes, having serial numbers A003SA through A093SA, inclusive.

型別

Beech Aircraft Model 400, 400A, 400T, and MU-300 airplanes

民航局AD編號

CAA-2014-10-007

原發布國

FAA

原AD編號

2014-21-06

生效日期

2014/11/28

主旨摘要

We are issuing this AD to prevent failure of the Acme nut threads in the PTA, which could lead to loss of control of pitch trim and reduced controllability of the airplane.

參考資訊（版本/ATA/SB）

ATA 27. Ref. Hawker Beechcraft Service Bulletin SB 27-4100, dated March 2012.

存檔序號

103-10-011

專業分項

Systems

產品類別

Airplane

備註

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