Airworthiness Directives (ADs)
CAA-2016-05-008A
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
- 2016/05/30
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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 Airbus Helicopters (AH) modification (mod) 07 65B63.
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Model Number
- SA 365, AS 365, SA 366 and EC 155 helicopters
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CAA AD Number
- CAA-2016-05-008A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2016-0097R1
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Effective Date
- 2016/05/25
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Subject
- Tail Rotor – Pitch Control Rod Bearing – Inspection/Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 65. This AD revises EASA AD 2016-0097-E(CAA-2016-05-008) dated 23 May 2016, which superseded EASA AD 2012-0170R2 dated 20 June 2014.
Ref. Publications: Airbus Helicopters ASB No. AS365-01.00.67 original issue dated 4 May 2016. and Airbus Helicopters ASB No. SA366-01.29 original issue dated 4 May 2016. and Airbus Helicopters ASB No. EC155-04A014 original issue dated 4 May 2016.
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Remarks
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