THRUSH S2R-H80 Flight Manual page 40

Climb
a. Maintain maximum continuous power as necessary
b. After obstacles are cleared a power reduction and a propeller speed
reduction for noise may be desirable.
Maximum engine efficiency is achieved at 1900 propeller RPM.
Glide and Approach
a. Prop Control
b. Flaps
Go-Around
a. Power
b. Flaps
c. Airspeed
Approach, Landing & Clearing the Runway
a. Airspeed on Approach
b. Wing Flaps
c. Touchdown
d. Landing Roll
e. Reverse Propeller
f. Brakes
The tail wheel is unlocked by full forward movement of
the control stick. This should be delayed until slow taxi
speed to prevent nose over of the aircraft.
AFM H8001 SINGLE & DUAL COCKPIT Revision B
FAA APPROVED: 3/19/2015
S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
NOTE:
SET full high RPM/Forward
SET as desired.
INCREASE to the takeoff setting.
RETRACT slowly while retaining
altitude.
Maintain best-rate-of-climb speed of
106 MCAS with flaps up
1.3
configuration.
See charts in Section 4.3.
As Required
Main Wheels
Lower tail smoothly – Close the
throttle.
Reverse may be used after the tail is
on the ground.
Use as necessary.
CAUTION
V for flap &
S
weight
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