ARROW
I1
SPECIFICATIONS
PERFORMANCE
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 the 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 Run
(ft)
Takeoff Run (Short field effort, 25O flaps) (ft)
Takeoff Distance Over 50-ft Obstacle (ft)
Takeoff Distance Over 50-ft Obstacle (Short field effort,
25O flaps) (ft)
Best Rate of Climb (rnph)
Rate of Climb (gear retracted) (ft per
min)
Best Angle of Climb (rnph)
Service Ceiling (ft)
Absolute Ceiling (ft)
Max
Speed (mph)
Optimum Cruising Speed (75% power, optimum altitude, 6600 ft) (mph)
Cruise Speed at best power mixture (rnph)
65% power, 9,750
ft
55% power, 13,000
ft
Range at best power mixture (mi)**
75% power, 6600
ft
65% power, 9750 ft
55% power, 13,000
ft
Cruise Speed at best economy mixture (rnph)
75% power, 6600
ft
65% power, 9700
ft
55% power, 13,100 ft
Range at best economy mixture (mi)**
75% power, 6600
ft
65% power, 9700 ft
55% power, 13,100 ft
Stalling Speed (flaps and gear down) (CAS) (rnph)
Stalling Speed (flaps and gear up) (CAS) (rnph)
Landing Roll (flaps down) (ft)
Landing Roll Over 50-ft Obstacle (ft)
*Gear retracted
**NO reserve
GENERAL SPECIFICATIONS
ISSUED:
JULY
13,1973
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