ARROW II
SPECIFICATIONS
PERFORMANCE
Performance figures are for airplanes equipped for cross-country transportation and flown
at gross weight under standard conditions at sea level or stated altitude. Any changes in
equipment may result in changes in performance.
Take-off Run (maximum effort, 25
°
flap) (ft)
770
Take-off Over 50-ft Barrier (maximum effort, 25
°
flap) (ft)
1600
Best Rate of Climb Speed (gear retracted) (mph)
100
Rate of Climb (ft per min)
900
Service Ceiling (ft)
15,000
Absolute Ceiling (ft)
17,000
Top Speed (mph)
175
Optimum Cruising Speed (75% power, optimum altitude) (mph)
165
Cruising Range (75% power, optimum altitude) (mi)
780
Optimum Cruising Range (55% power, optimum altitude) (mi)
900
Stalling Speed (flaps down, gear down) (mph)
64
Stalling Speed (flaps and gear up) (mph)
71
Landing Roll (flaps down) (ft)
780 *
Landing Roll Over 50-ft Barrier (ft)
1380 *
*This value applies only for the conditions indicated on the landing distance versus density
altitude chart.
WEIGHTS
Gross Weight (lbs)
Empty Weight (Standard) (lbs)
USEFUL LOAD (Standard) (lbs)
.
*These weights are approximate.
POWER PLANT
Engine (Lycoming)
Propeller (Hartzell)
Rated Horsepower
Rates Speed (rpm)
Bore (in.)
Stroke (in.)
Displacement (cu in.)
Compression Ratio
Dry Weight (lbs)
GENERAL SPECIFICATIONS
\SS\JED: November \S, \97\
REVISED: lune 15, 1972
2650
1499*
1151 *
10-360-C l C
HC-C2YK-1( )/7666A-2
or HC-C2YK-1 ( )F /F7666A-2
200
2700
5.125
4.375
361.0
8.7:1
326
1'-1
[
152kt
]
[
143kt
]
[
56kt
]
[62kt]
[677NM]
[782NM]
N16422 POH
