Control System - Urban Air UFM – 13 LAMBADA Operating And Maintenance Manual

Ultralite aeroplane
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OPERATING AND MAINTENANCE MANUAL FOR ULTRALIGHT AEROPLANE

2.3.5. Control system

There is the twisting spring controlled by lever next to the
control stick to trim a force in the longitudinal control
system.
Lever has following positions
1) takeoff position (fixed)
2) landing position (fixed)
3) airbrake position (free movement)
The rudder control system is dual too. The rudder is
controlled by cables attached at the rudder pedals and to
the hinges on the rudder bottom rib. There are the two
turn buckles to adjust the length of the cables.
The rudder control is connected by the rods to the
nose wheel steering arms.
Document No:
Date of issue: 30.01.2008
UFM-13 Lambada
The airplane is equipped with a classic
dual control system. The elevator and
ailerons are controlled
sticks, connecting rods and arms. The
longitudinal control system
attached to the seats. The lateral control
system steps are located on the control
sticks.
The wing flaperons and airbrakes are controlled with
a control lever between a seats. The lever is in a
changing gate and welded to a torsion tube. There are
the levers and rods at both ends of torsion tube to
control the flaperons and airbrakes.
by a control
stops are
2-6

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