交通部民用航空局

發布日期

2011/03/21

適用性說明

This AD applies to Airbus A300-600 and A310, ATR 42 and ATR 72, BAE Systems (formerly British Aerospace) BAe146, AVRO 146-RJ and ATP, Boeing 707, 727, 737, 747, 757, 767 and 777, Fokker F27 Mark 050 and Mark 0502, F28 Mark 0070 and Mark 0100, Lockheed 382 (Hercules) and L-1011 (Tristar), McDonnell Douglas DC-8, DC-9, MD-88, MD-90-30, DC-10 and MD- 11, and Sabreliner Corporation (formerly North American) NA-265 aeroplanes, all models, all serial numbers, if equipped with Gables Engineering type G7490, G7492 or G7493 series ATC/TCAS Control Panels. The affected control panels can also be installed on these aeroplanes, if modified in accordance with a certain Supplemental Type Certificate, known to include, but not limited to, Rockwell-Collins STC ST01256WI-D, as issued by the FAA and validated in Europe by STC EASA.IM.A.S.01061. Other STC’s

型別

Airbus A300-600 and A310 aeroplanes, ATR-GIE Avions de Transport Régional ATR 42 and ATR 72 aeroplanes, BAE Systems (Operations) Ltd BAe146, AVRO 146-RJ and ATP aeroplanes, Boeing DC-8, DC-9, DC-10, MD-11, MD-88, MD-90-30, 707, 727, 737, 747, 757, 767 and 777 aeroplanes, Fokker Services F27 Mark 050 and 0502, and F28 Mark 0070 and 0100 aeroplanes, Lockheed-Martin 382 and L-1011 aeroplanes, Sabreliner Corporation NA-265 aeroplanes

民航局AD編號

CAA-2011-03-007

原發布國

EASA

原AD編號

2011-0043

生效日期

2011/03/30

主旨摘要

Navigation Systems – Mode-S Transponder Control Panels – Modification

參考資訊（版本/ATA/SB）

ATA 34. Ref. Gables Engineering publications: Service Information Letter (SIL) 85 dated 19 May 2009 and SB G7490 ( )-34-01 dated 19 May 2009 and SB G7492 ( )-34-01 Revision 01 dated 22 May 2009, and SB G7493 ( )-34-01 dated 19 May 2009.

存檔序號

100-03-011

專業分項

Avionics

產品類別

Airplane

備註

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