Airworthiness Directives (ADs)

Aviation Industry

CAA-2012-09-003A(已有後續修訂版)

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date: 2013/10/28

Applicability: SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers, except those modified in accordance with Eurocopter modification (mod) 07 65B63.

Model Number: EUROCOPTER SA 365, AS 365, SA 366 and EC 155 helicopters

CAA AD Number: CAA-2012-09-003A(已有後續修訂版)

Aeronautics Authority of Original AD: EASA

Original AD Number: 2012-0170R1

Effective Date: 2013/10/18

Subject: Time Limits and Maintenance Checks – Tail Rotor Gearbox (TGB) Oil Level and Magnetic Chip Detector – Inspection, and Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement

Reference Publications (Revision/ATA/SB): ATA 05&65. This AD revises EASA AD 2012-0170(CAA-2012-09-003), dated 31 August 2012, which superseded EASA AD 2011-0145(CAA-2011-08-002) dated 02 August 2011. Ref. Eurocopter AS365 ASB No. 05.00.54 evision 4 dated 16 May 2011. and Eurocopter AS365 ASB No. 05.00.61 Revision 2 dated 05 July 2012, or Revision 3 dated 25 June 2013. and Eurocopter AS365 SB No. 65.00.17 Revision 1 dated 21 March 2011, and Eurocopter SA366 ASB No. 05.37 Revision 4 dated 16 May 2011, and Eurocopter SA366 ASB No. 05.41 Revision 2 dated 05 July 2012, and Eurocopter SA366 SB No. 65.04 Revision 1 dated 21 March 2011, and Eurocopter EC155 ASB No. 05A015 Revision 5 dated 25 July 2011, and Eurocopter EC155 ASB No. 05A022 Revision 2 dated 04 July 2012, or Revision 3 dated 25 June 2013, and Eurocopter EC155 SB No. 65-006 Revision 1 dated 21 March 2011.

Remarks

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