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Airworthiness Directives (ADs)

CAA-2015-12-003(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.

Issue Date
2015/12/17
Applicability
ATR 42-500 and ATR 72-212A aeroplanes, all manufacturer serial numbers modified in production by incorporating ATR modification 5948 (New Avionics Suite installation), except aeroplanes modified in production in accordance with ATR modification 6977 (New Avionics Suite Standard 2) or modified in service by incorporation of ATR Service Bulletin (SB) ATR42-31-0091 (applicable to ATR 42-500 aeroplanes) or ATR SB ATR72-31-1092 (applicable to ATR 72-212A aeroplanes).
Model Number
ATR 42 and 72 aeroplanes
CAA AD Number
CAA-2015-12-003(已有後續修訂版)
Aeronautics Authority of Original AD
EASA
Original AD Number
2015-0237
Effective Date
2015/12/29
Subject
Auto Flight – Auto Pilot and Yaw Damper – Operational Limitations Master Minimum Equipment List – Amendment
Reference Publications (Revision/ATA/SB)
ATA 22. This AD supersedes EASA AD 2015-0230(CAA-2015-12-001) dated 01 December 2015. Ref. Publications: ATR SB ATR42-31-0091, dated 17 December 2014. and ATR SB ATR72-31-1092, dated 07 October 2014.
Remarks
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CAA-2015-12-003.pdf
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