S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B Page 18
FAA APPROVAL DATE: 3/19/2015
Position 5:
a. Engine CHECK for oil leaks, loose fittings cracked
exhaust stacks, and excessive dirt or
corrosion.
b. Engine CHECK oil level and secure oil cap.
c. Propeller CHECK for spinner damage or oil leaks.
d. Propeller CHECK the propeller blades for nicks,
cracks, or excessive erosion of the leading
edge.
d. Dispersal Equipment (if installed) CHECK the pump, the pump fan, the hose or
the spreader for mounting and security.
e. Oil Quantity CHECK Dipstick and secure cap.
Position 6:
d. Wheel Chocks REMOVE
e. Main Wheel Tire and Brake CHECK for inflation, damage and wear.
f. Baggage Compartment CHECK security of baggage and secure
door.
Position 7:
a. Wing Leading Edge CHECK for damage.
NOTE:
Operate between 1 and 2 liters below the maximum oil level mark
on the oil dipstick.
NOTE:
When Rear Seat of Dual Cockpit S2R-H80 is to be occupied in
flight, check that hopper rinse tank is full.
The owner and pilot are responsible for keeping the
airplane’s CG within allowable limits.
Instructions for using removable ballast have been
included in the limitations section and weight and
balance section of this manual.
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