Airworthiness Directives (ADs)
CAA-2010-05-010A(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
- 2010/08/09
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Applicability
- SA 365 N1, AS 365 N2 and AS 365 N3 helicopters, all serial numbers except 6698, 6701, 6723, 6737 and 6741, 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 ertical 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-2010-05-010A(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0100R1
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Effective Date
- 2010/08/18
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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. This AD revises EASA Emergency AD 2010-0100-E(CAA-2010-05-010) dated 26 May 2010, which superseded EASA AD 2009-0241-E(CAA-2009-11-002 修訂) dated 05 November 2009 and its correction dated 10 December 2009. Ref. Eurocopter AS365 ASB No.01.00.61 Revision 3 dated 28 July 2010.
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Remarks
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