交通部民用航空局

發布日期

2014/06/30

適用性說明

Models RB211 Trent 553-61, 553A2-61, 556-61, 556A2-61, 556B-61, 556B2-61, 560-61 and 560A2-61 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A340-500 and A340-600 series aeroplanes. and Models RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A330 series aeroplanes. Models RB211 Trent 875-17, 877-17, 884-17, 884B-17, 892-17, 892B-17 and 895-17 engines, all serial numbers. These engines are known to be installed on, but not limited to, Boeing 777 series aeroplanes. and Models RB211 Trent 970-84, 970B-84, 972-84, 972B-84, 977-84, 977B-84 and 980-84 engines, all serial numbers. These engines are known to be installed on, but not limited to, Airbus A380 series aeroplanes.

型別

RB211 Trent 500, 700, 800 and 900 engines

民航局AD編號

CAA-2014-06-012修訂

原發布國

EASA

原AD編號

2014-0152Correction

生效日期

2014/07/04

主旨摘要

Engine – Intermediate Pressure Compressor Rotor Shaft and Balance Weights – Inspection / Modification

參考資訊（版本/ATA/SB）

ATA 72. This AD supersedes EASA AD 2013-0002(CAA-2013-01-001) dated 04 January 2013. Ref. Rolls-Royce NMSB RB.211-72-AG085 Revision 2 dated 7 July 2011. and Rolls-Royce NMSB RB.211-72-AG264 Revision 5 dated 21 March 2011. and Rolls-Royce NMSB RB.211-72-AG270 Revision 4 dated 21 March 2011. and Rolls-Royce NMSB RB.211-72-G448 Revision 3 dated 7 July 2011. and Rolls-Royce SB RB.211-72-AG401 Revision 2 dated 5 July 2011, or Revision 3 dated 28 January 2014. and Rolls-Royce SB RB.211-72-AG402 Revision 2 dated 7 July 2011. and Rolls-Royce NMSB RB.211-72-AH058 dated 13 December 2012. and Rolls-Royce NMSB RB.211-72-AH059 dated 11 December 2012. and Rolls-Royce SB RB.211-72-AH555 original dated 18 October 2013, or Revision 1 dated 13 December 2013. and Rolls-Royce SB RB.211-72-AH561 dated 21 October 2013.

存檔序號

103-06-017

專業分項

Powerplant

產品類別

Engine

備註

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