Document ID: chunk:federal_register_of_legislation:F2006B03703:body:0
Version: federal_register_of_legislation:F2006B03703
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105
CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES

Beechcraft 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/49 Landing Gear Motor Control Circuit Breaker 11/90

Applicability: All models as listed in the Requirement Document.

Requirement: Install a circuit breaker on the landing gear motor control panel in accordance with
Beechcraft Mandatory Service Bulletin 2035 Revision II or later revision.

Compliance: Prior to exceeding 100 hours time in service after 1 November 1990.

Background: Compliance with this AD is required to install a circuit breaker in the landing gear
motor circuit which will trip and open circuit the landing gear motor circuit before the
motor is damaged. Failure to comply with this AD may result in damage to the
landing gear motor in a manner which could restrict operation of the manual landing
gear extension system, resulting in an inability to manually lower the landing gear.

Federal Register of Legislative Instruments F2006B03703