Airworthiness Directives (ADs)
CAA-2011-08-012(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.
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Issue Date
- 2011/08/29
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Applicability
- EC 155 B, EC 155 B1, SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3 and SA 366 G1 helicopters, all serial numbers except helicopters on which MOD 0767B65 has been embodied in-production or having embodied MOD 0767B65 in-service through accomplishment of Eurocopter AS365 Service Bulletin (SB) No. 67.00.12. or SA 366 SB No. 67.07 or EC 155 SB No. 67-009 Revision 1, as applicable to helicopter version.
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Model Number
- EUROCOPTER AS 365, EC 155, SA 365 and SA 366
helicopters
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CAA AD Number
- CAA-2011-08-012(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2011-0154
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Effective Date
- 2011/09/05
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Subject
- Rotor Flight Controls – Collective Pitch Lever Restraining Tab –
Inspection / Adjustment
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Reference Publications (Revision/ATA/SB)
- ATA 67. This AD supersedes DGAC France AD F-2005-127 R1 dated 01 February 2006 and EASA approval number 2006-0019. Ref. Eurocopter AS 365 Alert Service Bulletin No. 67.00.10 Revision 1 dated 25 February 2009. and Eurocopter SA 366 Alert Service Bulletin No. 67.05 Revision 1 dated 25 February 2009. and Eurocopter EC 155 Alert Service Bulletin No. 67A007 Revision 1 dated 25 February 2009. and Eurocopter AS 365 Service Bulletin No. 67.00.12 dated 25 February 2009. and Eurocopter SA 366 Service Bulletin SB No. 67.07 dated 25 February 2009. and Eurocopter EC 155 Service Bulletin SB No. 67-009 Revision 1 dated 19 July 2010.
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Remarks
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Download
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