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
065
17 60
87
649
12,700
14,960
I
35*
I 33*
720*
785
*
58
64.5
s95
lll5
WEIGHTS
Gross
Woight
(lbs)
Standard
Empty
Wciglrt
(lbs)
Maximum
Useful
Load
(lbs)
*With
Optional
Wheel Fairings
installed.
GENERAL SPECIFICATIONS
REVISED: JULY 14.1975
2325
133
I
994
-JL-*-
l-l
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