Airworthiness Directives (ADs)

Aviation Industry

CAA-2011-08-002

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: 2011/08/05

Applicability: SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers.

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

CAA AD Number: CAA-2011-08-002

Aeronautics Authority of Original AD: EASA

Original AD Number: 2011-0145

Effective Date: 2011/08/16

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

Reference Publications (Revision/ATA/SB): ATA 05,65. This AD supersedes EASA AD 2011-0117(CAA-2011-06-010) dated 24 June 2011. Ref. Eurocopter ASB AS365 No. 05.00.54 Revision 4 dated 16 May 2011, Eurocopter ASB SA366 No. 05.37 Revision 4 dated 16 May 2011, Eurocopter ASB EC155 No. 05A015 Revision 5 dated 25 July 2011, Eurocopter ASB AS365 No. 05.00.61 Revision 1 dated 13 July 2011, Eurocopter ASB SA366 No. 05.41 Revision 1 dated 13 July 2011, Eurocopter ASB EC155 No. 05A022 Revision 1 dated 13 July 2011, Eurocopter SB AS365 No. 65.00.17 Revision 1 dated 21 March 2011, Eurocopter SB SA366 No. 65.04 Revision 1 dated 21 March 2011, and Eurocopter SB EC155 No. 65-006 Revision 1 dated 21 March 2011.

Remarks

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