CHEROKEE
ARCHER
GE'NERAL SPECIFICATIONS
PERFORMANCE
Published are for standard airplanes flown at gross weight under standard
conditions at sea unless otherwise stated. Performance for a specific airplane may vary
from published depending
upon
the equipment installed, the condition
of
engine,
airplane 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, 25 ° flaps, sea level
(ft)
Distance Over 50-ft Obstacle, 25° flaps, sea level
(ft)
Best
Rate
of
Climb Speed
(mph)
Rate
of
Climb
(ft
per min)
Best Angle
of
Climb Speed, sea level
(mph)
Max sea level
(mph)
Optimum Altitude
9300
ft,
75'Yo
power (TAS) (mph)
(
(ft)
at best power mixture
(mph)
power.
2,800
ft
power.
14,000
ft
Range at best power mixture (mi)**
power,
9300
ft
power, l 2,800 ft
at best economy mixture (mph)
power,
9300
ft
power, 12,600 ft
Range
at
best economy mixture (mi)**
pOWl.)L
9300
ft
12.600 rt
down (CAS) (mph)
up
(CAS)
(mph)
Landing sea level, flaps down (ft)
Distance Over 50-ft Obstacle, sea level
(ft)
are with optional wheel fairings installed. Subtract 3
mph
if wheel
WEIGHTS
Gross
Standard
I Wl'iglil (lbs)
Maximum Useful Load (lbs)
GENERAL
SPECIFICATIONS
REVISED: NOVEMBER 21, 1975
720
1625
85
725
76
148*
141*
14,150
16,500
132*
125*
705
131*
123*
715
774
61
68
11
2450
1404
1046
1-1
