Piper cherokee WARRIOR Pilots Operating Manual page 5

CHEROKEE WARRIOR
GENERAL SPECIFICATIONS
PERFOR.MANCE
Published figures are for standard airplanes flown at gross weight under standard
conditions at sea level, unless otherwise stated. Performance for a specific airplane may vary
from published figures depending upon the equipment installed, the condition of engine,
airplane and equipment, atmospheric conditions and piloting technique. Each performance
figure below is subject to the same conditions as on the corresponding performance chart from
which it is taken in the Performance Charts Section.
Takeoff Ground Run (minimum) (ft)
Takeoff Distance Over 5Gft Obstacle (25
o
flaps) (ft)
Best Rate of Climb Speed (mph)
Rate of Climb (ft per min)
Service Ceiling (ft)
Absolute Ceiling (ft)
Top Speed (mph)
Optimum Cruising Speed (75% power, optimum altitude, leaned to
best power) (mph)
Cruising Range (75% power, optimum altitude, leaned to best economy.
no reserves) (mi)
Optimum Cruising Range (55% power. optimum altitude, leaned to
best economy, no reserves) (mi)
Stalling Speed (flaps down) (mph)
Stalling Speed (flaps up) (mph)
Landing Roll (flaps down) (ft)
Landing Roll Over 50-ft Banier (flaps down) (ft)
l 0 6 5
1 7 6 0
8 7
649
12,700
14,960
I 3 5 *
I 3 3 *
720*
7 8 5 *
5 8
6 4 . 5
s 9 5
l l l 5
WEIGHTS
Gross Woight (lbs)
Standard Empty Wciglrt (lbs)
Maximum Useful Load (lbs)
*With Optional Wheel Fairings installed.
GENERAL SPECIFICATIONS
REVISED: JULY 14.1975
2325
1 3 3 I
994
-JL-*-
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