AEROPRAKT 484, Руководство по эксплуатации для пилотов

Страница: 10 / 53

A22L2 - POH-02
AEROPRAKT-22L2 Pilot Operating Handbook
10
NOTE: When both tanks are full, fuel may flow from one tank to the other (e . g . due to the
lateral forces during side slipping or when wings are not level on parking or during taxiing),
overfill it and spill out through the vent line
. To prevent fuel spilling out in th i s case it is
recommended to close one of the fuel valves and avoid side - slipping in flight.
CAUTION! At all times during the flight ensure fuel coming to the engine by opening
the valve(s) of the tank(s) WITH fuel. If one of the tanks is empty, close
its valve to prevent air getting into the fuel line and causing engine
malfunction or even failure.
Capacity of tanks:
Total capacity
:
Usable fuel:
Non-usable fuel :
Fuel:
2x45 I (2x11,9 US gal)
90 I (23,8 US gal)
89 I (23,5 US gal)
1 I (0,3 US gal)
un l eaded MOGAS min . RON 95 or AVGAS 100LL
2.6 Airplane control systems
Airplane control systems include control systems for drooping ailerons (flaperons), elevator
with trim tab, rudder and nose wheel, engine and brakes
.
The control system is combined consisting of foot- and hand - actuated subsystems .
Ailerons and elevator are hand-actuated and are controlled using yokes .
2.6.1 Elevator control system
The elevator control system linkage (see Fig . 3) is rigid, compns1ng 3 pushrods and 2
bellcranks . " Push" and "pull" forces are applied by the pilot to the stick 1 is passed via the
control column 2 to the pushrod 3, then via the bellcrank 4 to the pushrod 5 . The force is
transferred to the elevator via the pushrod 7, attached to the bellcrank 6. And the pushrod
7 is supported by the rollers 8 and connected to the e l evator arm 9.
Fig. 3