交通部民用航空局

發布日期

2014/02/14

適用性說明

ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial numbers: These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale) AS 350 B, BA, BB, B1and B2, AS 365 and SA 365, Airbus Helicopters Deutschland (formerly Eurocopter Deutschland, Messerschmidt-Bölkow-Blohm) MBB-BK117-C1 and -C2, AgustaWestland (formerly Agusta) A 109 K2, and Sikorsky S-76A helicopters. ARRIEL 2B, 2B1, 2B1A, 2B1B, 2C, 2C1, 2C2, 2S1 and 2S2 engines, all serial numbers: These engines are known to be installed on, but not limited to, Eurocopter AS 350 B3, EC 130 B4, AS 365 N3 and EC 155 B1, Changhe Z11 and Sikorsky S-76C helicopters.

型別

ARRIEL 1 and ARRIEL 2 engines

民航局AD編號

CAA-2014-02-003

原發布國

EASA

原AD編號

2014-0036

生效日期

2014/02/25

主旨摘要

Engine – Accessory Gear Box (M01) – 41/23 Tooth Bevel Gear Assembly – Check / Replacement

參考資訊（版本/ATA/SB）

ATA 72. Ref, Turbomeca MSB 292 72 0839 version B dated 25 November 2013. and Turbomeca MSB 292 72 2849 version B dated 25 November 2013. and Turbomeca Technical Instruction (TI) X 292 72 0839 update 1. and Turbomeca TI X 292 72 2849 update 1. and Turbomeca TI X 292 72 0840 original issue. and Turbomeca TI X 292 72 2850 original issue. and Turbomeca Internal Directive (ID) 383952 version C. and Turbomeca Repair Technical Directive (RTD) X 292 65 327 2. and Turbomeca Engine Test Bed Acceptance Test Specifications (CCT) as listed in Appendix 2 of this AD. and Turbomeca Maintenance Manuals (MM) as listed in Appendix 3 of this AD.

存檔序號

103-02-003

專業分項

Powerplant

產品類別

Engine

備註

檔案下載