ARROW
SECTION
111
PERFORMANCE
A. STALLS
The following performance figures were obtained during FAA type tests and may be
realized under conditions indicated with the airplane and engine in good condition and
with average piloting technique. All performance is given for
2650
pounds.
Loss of altitude during stalls varied from
100
to
300
feet, depending on configuration
and power.
Stalling speeds, in mph, power off, versus angle of bank (Calibrated airspeed):
Angle of bank
0" 20" 40" 50" 60"
Flaps up (gear down)
7
1
73
8
1
88 100
Flaps down (gear down)
64 66
73
80 90
FAA
APPROVED MAY
14,1973
REPORT:
VB-560
PAGE
3-13
MODEL: PA-28R-200
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