AEROPRAKT-32 Pilot Operating Handbook
A32-103-POH
34
pulleys (12) on aft of the frame No.3 low in the middle, two pulleys (13) on aft of the frame
No.3 low on the sides, and two pulleys (14) on the frame No.3 up near the rear wing
attachment points.
The cable tension and flaperon position adjustment is achieved using the turnbuckles (15)
located near the inner rockers (5).
Deflection angles of the flaperons (as ailerons): up
– 20±1°, down – 13±1°.
The aileron drooping (flap extension) mechanism (
) consists of a beam with lever (1)
hinged to the upper rim of the frame No.3. Flap position setting is achieved with the fixer
(2) having three holes for the pin (3) on the lever. Unfixing is achieved by bending the
spring-like lever to the right. After the pin comes out of the fixer hole the lever can be set to
the selected position. When the pin aligns with another hole of the fixer the lever springs
back fixing the flaperons in a different position.
Fig. 8. Flap extension mechanism
Aileron drooping (flap extension) angles: 1
st
position
– 10±1°, 2
nd
position
– 20±1°.
Содержание A32-103-POH
Страница 25: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 25 No Equipment description and Part No Weight kg CG arm m...
Страница 29: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 29 Fig 3 Fuel system schematic...
Страница 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 36 Fig 10 Engine pre start mixture control...
Страница 38: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 38 Fig 12 Brake control system...
Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 43 Fig 15 Wiring diagram of A 32 electrical system main...
Страница 48: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 48 Fig 21 Wiring diagram for installation of PTT buttons...
Страница 50: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 50 Fig 22 Recovery system...
