Airworthiness Directives (ADs)
CAA-2017-07-011(已被CAA-2021-07-006取代)
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
- 2017/07/26
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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
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Model Number
- Airbus AS 365 helicopters
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CAA AD Number
- CAA-2017-07-011(已被CAA-2021-07-006取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2017-0125
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Effective Date
- 2017/07/28
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Subject
- Tail Rotor – Pitch Control Rod Bearing – Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA This AD supersedes EASA AD 2017-0007(CAA-2017-01-004) dated 13 January 2017. Ref. Publications:
Eurocopter AS365 SB 65.00.17 Revision 1 dated 23 February 2011. and Airbus Helicopters ASB AS365-01.00.67 original issue dated 04 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016, or Revision 3 dated 20 July 2017.
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Remarks
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