THRUSH S2R-H80 Flight Manual page 31

Position 4, 6 and 1 SHALL be sequenced as shown below to
prevent introduction of air in the fuel system during fuel system
check.
Position 4:
a. Wing Tie Down
b. Left Wing Main Sump
c. Left Wing Fuel Vent Sump
d. Left Wing Fuel Vent
Position 6:
a. Wing Tie Down
b. Right Wing Main Sump
c. Right Wing Fuel Vent Sump
Position 4: Cont'd
e. Header Tank Sump
Position 1:
l. Battery Switch -
m. Emergency Fuel Pump Switch -
Position 4: Cont'd
f. Firewall Fuel Filter
Position 1:
n. Battery Switch -
o. Emergency Fuel Pump Switch -
Position 4: Cont'd
g. Main Wheel Tire and Brake
h. Accessory Section
i. Oil Cooler
j. Air Filter
k. Baggage Compartment Door
AFM H8001 SINGLE & DUAL COCKPIT Revision B
FAA APPROVAL DATE: 3/19/2015
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
NOTE:
REMOVE
DRAIN
DRAIN
CHECK for obstruction
REMOVE
DRAIN
DRAIN
DRAIN
ON
ON
DRAIN
OFF
OFF
CHECK for inflation, damage and wear
CHECK for debris, oil leaks or any
other irregularities.
CHECK for leaks and stoppage
CHECK for cleanliness and condition.
CHECK security of baggage and secure
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