S2R-H80 Single & Dual Cockpit
AIRPLANE FLIGHT MANUAL
AFM H8001 SINGLE & DUAL COCKPIT Revision B Page 26
FAA APPROVED: 3/19/2015
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.
Glide and Approach
a. Prop Control SET full high RPM/Forward
b. Flaps SET as desired.
Go-Around
a. Power INCREASE to the takeoff setting.
b. Flaps RETRACT slowly while retaining
altitude.
c. Airspeed Maintain best-rate-of-climb speed of
106 MCAS with flaps up
Approach, Landing & Clearing the Runway
a. Airspeed on Approach 1.3 V
S
for flap & weight
configuration.
See charts in Section 4.3.
b. Wing Flaps As Required
c. Touchdown Main Wheels
d. Landing Roll Lower tail smoothly – Close the
throttle.
e. Reverse Propeller Reverse may be used after the tail is
on the ground.
f. Brakes Use as necessary.
NOTE:
Maximum engine efficiency is achieved at 1900 propeller RPM.
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.
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