Airworthiness Directives (ADs)
CAA-2021-02-004(已被CAA-2023-03-011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
- 2021/02/20
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Applicability
- AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3, AS 350 D, EC 130 B4 and
EC 130 T2 helicopters, all serial numbers (s/n); AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all s/n; and
SA 365 C1, SA 365 C2, SA 365 C3, SA 365 N, SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all s/n.
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Model Number
- Airbus Helicopters AS 350, EC 130, AS 355,
AS 365 and SA 365
helicopters
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CAA AD Number
- CAA-2021-02-004(已被CAA-2023-03-011取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2021-0048
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Effective Date
- 2021/03/02
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Subject
- Main Rotor – Pitch Rod Upper Links – Marking / Inspection
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Reference Publications (Revision/ATA/SB)
- ATA 62. Ref. Publications: AH ASB AS350-05.01.01 original issue dated 09 February 2021. and AH ASB EC130-05A037 original issue dated 09 February 2021. and AH ASB AS355-05.00.85 original issue dated 09 February 2021. and AH ASB SA365-05.34 original issue dated 09 February 2021. and AH ASB AS365-05.00.82 original issue dated 09 February 2021.
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Remarks
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