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Beechcraft Beech 95 2017 - Landing Gear and Brake Systems

Beechcraft Beech 95 2017
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Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 64
The above diagram shows the location of all the fuel systems drains. It also shows vent
line routing and the location of all check valves.
Gear
The gear is electrically operated tricycle landing gear. The gear is operated through push-
pull tubes by a reversible electric motor and actuator gearbox under the front seat. A two-
position landing gear switch located on the right hand side of the center console controls
the motor. Limit switches and a dynamic braking system automatically stop the retract
mechanism when the gear reaches its full up or full down position.

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