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.
CAUTION