Airworthiness Directives (ADs)
CAA-2010-05-010(已有後續修訂版)
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
- 2010/05/27
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Applicability
- SA 365 N1, AS 365 N2, N3 helicopters delivered before 01 May 2010, flying in IMC (Instrumental Meteorological Conditions), IFR (Instrument Flight Rules) or Night VFR (Visual Flight Rules) conditions, if equipped with the vertical gyro units GV76-1 installed on the rear left hand (LH) or rear right hand (RH) rack, on which modification 365P081895 (reinforcement of rack for vertical gyro unit GV76-1 in
the rear compartment) has not been incorporated.
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Model Number
- EUROCOPTER SA 365 and AS 365 helicopters
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CAA AD Number
- CAA-2010-05-010(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0100-E(BRAZIL)
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Effective Date
- 2010/05/28
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Subject
- Navigation - Vertical Gyro Unit Data Output - Operational Limitation / Operational procedure / Reinforcement
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Reference Publications (Revision/ATA/SB)
- ATA 34. Ref. This AD supersedes EASA AD 2009-0241-E(CAA-2009-11-002 修訂) dated 05 November 2009, Eurocopter EASB AS 365 N1, N2, N3 No. 01.00.61 revision 2 dated 25 May 2010 and Eurocopter EASB AS 365 No. 34.00.31 revision 0 dated 25 May 2010.
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Remarks
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Download
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