ARROW
SECTION ID
.
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
0
20
°
Flaps up (gear down)
71
73
Flaps down (gear down)
64
66
FAA APPROVED October 14, 1971
40
°
50
°
60
°
81
88
100
73
80
90
REPORT:
VB-343
PAGE
3-
MODEL: PA-28R-
00
(
62
K
T
)
(
64
K
T
)
(
71
K
T
)
(
77
K
T
)
(
87
K
T
)
(
56
KT)
(
58
K
T
)
(
64
K
T
)
(
70
K
T
)
(
79
K
T
)
N16422 POH