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d.
Throttle - FORWARD approximately one inch
e.
Mixture - AS REQUIRED for flight altitude
f.
Propeller - FORWARD of detent
g.
Starter Button or Ignition Switch - PRESS or START
h.
Primer Switch or Auxiliary Fuel Pump - ACTIVATE or PRIME
i.
Primer Switch and Starter or Ignition Switch - RELEASE when
engine fires
j.
Auxiliary Fuel Pump - AS REQUIRED to prevent fuel flow
fluctuations
k.
Mixture - AS REQUIRED
l.
Power - INCREASE after cylinder head temperature reaches 2000F
with gradual mixture enrichment as power increases
m.
Cowl Flap - AS REQUIRED (310R Only)
n.
Alternator or Generator - ON
2.
Aircraft With Optional Propeller Unfeathering System:
NOTE
(310F, G
&
H Aircraft Only)
If auxiliary fuel pump is in ON or PRIME position, purge
engine by turning auxiliary fuel pump OFF, throttle full open
and mixture IDLE CUT-OFF for approximately 5 minutes prior to
restart.
a.
Auxiliary Fuel Pump - CHECK OFF.
If ON, LOW or PRIME, purge
engine by turning OFF auxiliary fuel pump, mixture to IDLE
CUT-OFF, throttle full open, magneto switches OFF and
rotating engine 15 revolutions with starter
b.
Magneto or Ignition Switch(es) - ON or BOTH
c.
Fuel Selector - MAIN TANK (Feel For Detent)
d.
Throttle - FORWARD approximately one inch
e.
Mixture - AS REQUIRED for flight altitude
f.
Propeller - FULL FORWARD
g.
Propeller - RETARD to detent when propeller reaches 1000 RPM
h.
Auxiliary Fuel Pump - AS REQUIRED to prevent fuel flow
fluctuations
i.
Mixture - AS REQUIRED
j.
Power - INCREASE after cylinder head temperature reaches 2000F
with gradual mixture enrichment as power increases
k.
Cowl Flap - AS REQUIRED (310R Only)
l.
Alternator or Generator - ON
ENGINE DRIVEN FUEL PUMP FAILURE
1.
Fuel Selector - MAIN TANK (Feel For Detent)
2.
Auxiliary Fuel Pump - ON
3.
Cowl Flap - OPEN (310R Only)
4.
Mixture - ADJUST for smooth engine operation
5.
As Soon as Practical - LAND
6,
Fuel in auxiliary tank is unusable
7.
Fuel in opposite main tank is unusable (except 310C, D
&
F)
NOTE
e(Applicable to 310C, D
&
F aircraft)
In the event that both an·
engine-driven fuel pump and an auxiliary fuel pump fail, fuel may
be supplied to the failing engine by feeding it from the tank with
the operative auxiliary fuel pump.
The engine with the operative
engine-driven fuel pump should be fed from the tank containing the
inoperative auxiliary fuel pump.
This will permit all fuel to be
used from the main tanks.
However, it is impossible to use fuel
from the auxiliary fuel tank on the same side as the inoperative
engine-driven fuel pump.
e(Applicable to all 310's except 310C, D
&
F aircraft)
If both an
engine-driven fuel pump and an auxiliary fuel pump fail on the
same side of the aircraft, the failing engine cannot be supplied
with fuel from the.opposite MAIN TANK since that auxiliary fuel
pump will operate on the low pressure setting as long as the
corresponding engine fuel pump .is operative.
2
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