Airworthiness Directives (ADs)
CAA-2012-06-008A
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
- 2019/09/20
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Applicability
- SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers, if a frame No. 9 is installed:
- on which doublers or repairs at the level of the latch support and/or stretcher support have been installed in service in accordance with Eurocopter SA 365 / AS 365 ASB 53.00.42, or ASB 53.00.43; or
- on which doublers or repairs have been installed in production in accordance with drawing 365A094158, or drawing 365A094159; or
- on which doublers or repairs have been installed in service in accordance with Mechanical Repair Manual Work Card 53.10.22.772 or Work Card 53.10.22.773;
except helicopters that have embodied Eurocopter modification (MOD) 53C17 or MOD 53D02, or AH MOD 07 53D21 or MOD 07 53D22.
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Model Number
- SA 365 and AS 365 helicopters
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CAA AD Number
- CAA-2012-06-008A
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2012-0108R1
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Effective Date
- 2019/10/03
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Subject
- Fuselage – Frame No. 9 – Inspection / Repair
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Reference Publications (Revision/ATA/SB)
- ATA 53. This AD revises EASA Emergency AD 2012-0108-E(CAA-2012-06-008) dated 15 June 2012. Ref. Publications: Eurocopter AS365 Emergency ASB 05.00.63 original issue dated 12 June 2012, or Revision 1 dated 18 June 2012, or AH AS365 Emergency ASB 05.00.63 Revision 2 dated 20 December 2018.
AH SB AS365-53.00.57 original issue dated 20 December 2018.
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Remarks
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