Section VII BEECHCRAFT Bonanza
Syatems Description V35, V35A & V35B thru D-9947
electrical signals to the individual indicators that indicate
fuel remaining in the tank. There are sensors in each wing
tank system connected to the individual wing tank
indicator.
AUXILIARY FUEL PUMP
The electric auxiliary fuel pump is controlled by an ON-OFF
toggle switch on the control console. It provides pressure
for starting and emergency operation. Immediately after
starting, the auxiliary fuel pump can be used to purge the
system of vapor caused by an extremely high ambient
temperature or a start with the engine hot. The auxiliary
fuel pump provides for near maximum engine performance
should the engine driven pump fail.
FUEL TANK SELECTION
The fuel selector valve handle is located forward and to the
left of the pilot's seat. Take-offs and landings should be
made using the tank that is more nearly full.
If the engine stops because of insufficient fuel, refer to the
EMERGENCY PROCEDURES Section for the Air Start
procedures.
FUEL REQUIRED FOR FLIGHT
It is the pilot's responsibility to ascertain that the fuel
quantity indicators are functioning and maintaining a
reasonable degree of accuracy, and be certain of ample
fuel for a flight. Takeoff is prohibited if the fuel quantity
indicators do not indicate above the yellow arc. An
inaccurate indicator could give an er_roneous indication of
fuel quantity. A minimum of 13 gallons of fuel is required
in each tank before takeoff.
7-30
January 1982
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