1AD/BEECH 23/17 - Electric Flap System Mechanism

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

Image unavailable in extracted text Beechcraft 19, 23 and 24 Series Aeroplanes

 

AD/BEECH 23/17 Electric Flap System Mechanism 3/71 Applicability:              Models B19, C23, A24 and A24R equipped with the optional electric flap installation. Requirement:               Action in accordance with Beechcraft SI No. 0415-161.

Compliance: Forthwith.