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
0 0
64.5
5 8
60'
9 l
8 2
400
74
66
20"
67
60
5 0 0
80
72
REPORT: VB-573 PAGE 3-7
MODEL: PA-28-151