AEROPRAKT-32 Pilot Operating Handbook
A32-214-POH
30
7.7 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 stick. The rudder and nose
wheel control is foot-actuated using pedals.
7.7.1 AMHT control system
The all-moving horizontal tail (AMHT) control system (see
) is combined, it consists of
two
4.0 mm (5/32") cables, passing through a block of pulleys and a fairlead, rocker and
pushrod.
“Push” and “pull” forces are applied by the pilot to the control stick (1) is passed via the
control column, pushrod (2) and bellcrank (3) to the cables (4). Then via the bellcrank (5)
located near the frame No.9, the control forces is passed to the pushrod (6) connected to
the AFHT arm (7). The cables routing is ensured with a block of pulleys (8), located in front
of the seat beam and fairlead (9) on the luggage container wall. The cable tension and AFHT
incidence angle adjustment is ensured using the turnbuckles (10) located forward of the
bellcrank (5).
AMHT deflection angles: 15±1° up and 5±1° down.
Fig. 4 AMHT control system
Содержание A32-214-POH
Страница 25: ...AEROPRAKT 32 Pilot Operating Handbook A32 214 POH 25 No Equipment description and Part No Weight kg CG arm m...
Страница 29: ...AEROPRAKT 32 Pilot Operating Handbook A32 214 POH 29 Fig 3 Fuel system schematic...
Страница 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 214 POH 36 Fig 10 Engine pre start mixture control...
Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 214 POH 43 Fig 15 Wiring diagram of A32 electrical system main...
Страница 49: ...AEROPRAKT 32 Pilot Operating Handbook A32 214 POH 49 Fig 23 Wiring diagram for installation of PTT buttons...
Страница 51: ...AEROPRAKT 32 Pilot Operating Handbook A32 214 POH 51 Fig 24 Recovery system...
