Airworthiness Directives (ADs)
CAA-2006-02-010B
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
- 2008/08/05
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Applicability
- Eurocopter SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers.
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Model Number
- Eurocopter SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1 helicopters, all serial numbers.
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CAA AD Number
- CAA-2006-02-010B
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2008-0147-E
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Effective Date
- 2008/08/05
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Subject
- Tail Rotor Drive – Tail Gearbox (TGB) Oil Level and Tail Rotor Pitch
Control Rod Bearing – Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 05, 65
This AD supersedes EASA AD 2006-0258R1-E(CAA-2006-02-010A).
Ref. Eurocopter AS365 ASB N° 05.00.54 Revision 1, Eurocopter SA366 ASB N° 05.37 Revision 1 and Eurocopter EC155 ASB N° 05A015 Revision 1.
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Remarks
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