THRUSH S2R-H80 Flight Manual page 16

STARTER:
FUEL PUMPS:
AIR STARTS:
AMBIENT
TEMPERATURE:
PROPELLER:
0
PROPELLER
LIMITATIONS:
REVERSE POWER: Do not use in flight.
NOISE
ABATEMENT:
AFM H8001 SINGLE & DUAL COCKPIT Revision B
FAA APPROVAL DATE: 3/19/2015
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
Maximum starter engagement duration is 30 seconds
followed by a 60 second cool-down period; a total of 3 cycles
to be followed by a 30 minute starter cool-down period.
Continuous simultaneous operation of both fuel pumps is
prohibited due to high fuel pressure.
Normal air starts are approved from sea level to 12,000 feet
and from 80 MPH to 126 MPH air speed. (Refer to Section
III.)
Satisfactory engine cooling has been demonstrated at a
temperature of 38° C.
Hartzell Four Blade Propeller:
Model #HC-B4TW-3/T10282N(S)
Minimum Diameter: 102" / Maximum Diameter: 103"
Stabilized ground operation is prohibited between 400
and 1100 RPM. The propeller may be operated when
feathered at or below 400 RPM.
This airplane has not been shown to comply with the
noise limits in 14 CFR Part 36 and must be operated
in accordance with the noise operating limitation
prescribed under 14 CFR Part 91.815.
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