AEROPRAKT-32 Pilot Operating Handbook
A32-060-POH
31
7.7.3 Rudder and nose wheel control system
The rudder and nose wheel control system (
) is combined, it consists of pedals, nose
landing gear strut control bellcrank, two pushrods, two Ø2.5 mm (3/32 in) cables, passing
through two front and two rear pulleys.
Fig. 6. Rudder and nose landing gear control system
The front (right) pedals (1) and rear (left) pedals (2) are fixed with nylon supports to
longitudinal beams of the cockpit floor. The bellcrank (3) attached to the nose landing gear
strut is connected to the pedals with the right (4) and left (5) pushrods. The right (6) and
left (7) cables connect the pedals to the rudder arms. The cable routing is ensured with
two pulleys (8) on the frame No.3 and two pulleys (9) near the frame No.9.
Adjustment of the nose landing gear position is achieved with pedals set to neutral position
using pushrods (4) and (5). The cable tension and adjustment of the rudder position is
achieved using the turnbuckles (11) located near the frame No.9.
In its neutral position the rudder is deflected to the right by the angle of +2.5° (to the right)
for compensation of the engine torque. The rudder deflection angle to each side is 25±1°.
Содержание A32
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Страница 42: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 42 Fig 15 Wiring diagram of A 32 electrical system main...
Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 43 Fig 16 Block diagram of Garmin G3X system installation...
Страница 52: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 52 Fig 25 Recovery system...
