Piper cherokee WARRIOR - PERFORMANCE DATA; FAA Type Test Data and Stall Speeds

CHEROKEE WARRIOR
SECTION M
PERFORMANCE
The following
performance
figures were obtained during
FAA
type tests and may be
reahzed under conditions
indicated
with
the airplane
and engine in
good
condition
and with
average
piloting
technique.
All
performance
is
given
for 2325
pounds.
Loss of altitude during stalls
varied from 100
to275
feet, depending on configuration
and
power.
Stalling speeds, in mph.
power
off,
versus
angle
of bank
(Calibrated
Airspeed):
Angle of Bank
Flaps
Up
Flaps
Down
FAA APPROVED JULY
25,1973
REVISED:
AUGUST
30. 1973
00
64.5
58
60'
9l
82
400
74
66
20"
67
60
500
80
72
REPORT:
VB-573 PAGE
3-7
MODEL: PA-28-151