Performance - Piper CHEROKEE CRUISER PA-28-140 Information Manual

CHEROKEE CRUISER
SECTION III
PERFORMANCE
All performance is gi ven for a weight of 2150 pounds.
Loss of altitude during stalls can be as great as 200 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
Air Conditioner Models only:
0°
64
55
When the full throttle position is not used or in the event of a malfunction which
causes the compressor to operate and the condenser door to remain extended, a decrease in
rate of climb of as much as 100 fpm can be expected at all altitudes.
FAA APPROVED MAY 14, 1973 REPORT: VB-5S7 PAGE 3-9
MODEL: PA-28 140