AEROPRAKT-32 Pilot Operating Handbook
A32-iS-129-POH
29
NOTE: Both fuel pumps have capacity 120 l/h. Due to different flow resistance of the return
lines from the T-connector 26 (Fig. 3. Fuel system schematic) to the return outlets
inside the right and left tanks with both fuel valves 7 and 8 open (Fig. 3), the fuel will
be pumped from one of the tanks to the other. Fuel will fill that tank completely and
will start escaping it via the vent tube. For that reason, it is not recommended to
operate the engine with both fuel valves open.
CAUTION! If air gets to the fuel lines then starting the engine may take quite a long
time (several dozens of seconds). For that reason it is strictly not allowed
to empty completely any of the fuel tanks in flight.
Fig. 3. Fuel system schematic
Fuel pressure: maximum permissible
— 7 bar (101.5 psi);
Fuel pumps:
nominal voltage
— 12 V;
capacity
— approx. 120 l/h (31.7 gal/h);
pressure
— min. 4.5 bar (65.3 psi) (absolute pressure).
Содержание A32-iS-129-POH
Страница 26: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 26 No Equipment description and Part No Weight kg CG arm m...
Страница 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 36 Fig 10 Brake control system...
Страница 41: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 41 Fig 13 Wiring diagram of A 32 electrical system main...
Страница 47: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 47 Fig 19 Recovery system...