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| Engine make/model: | Lycoming IO-360-A1D6 |
| Horsepower@altitude: | 350 (x2) |
TBO (hrs):
| 200@SL |
Propeller type:
| MTV-15-B/205-58 |
Airfoil:
| Modified Clark Y |
Landing gear type:
| Fixed tailwheel
|
| Gross weight (lbs.): | 2000
|
| Max landing weight (lbs.): | 2000
|
| Empty weight, std. (lbs.): | 1320
|
| Useful load, std. (lbs.): | 680
|
| Fuel capacity, std. (gals.): | 52
|
Oil capacity (qts.):
| 8
|
Baggage capacity (cu.ft./lbs.):
| 50 |
| Payload, full std. fuel (lbs.): | 380 |
| Wingspan: | 35 ft. 6 in. |
| Overall length: | 22 ft. 7 in.
|
| Height: | 7 ft. 5 in. |
| Wing area (sq. ft.): | 183 |
Wing loading (lbs./sq. ft.):
| 10.9 |
Power loading (lbs./hp.):
| 10
|
| Seating capacity: | 2 |
| Cabin width (in.): | 48 |
| Cabin height (in.): | 27
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PERFORMANCE |
| Cruise speed (kts.): | |
55% power (mph/gps):
| 138 |
| | |
| Max range (nm): | 828
|
Fuel consumption (gph):
| 7.6
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| | |
| Dirty stall speed (kts.): | 53 |
| Best rate of climb, SL (fpm): | 1700 |
| Service ceiling (ft.): | 20,000 |
| Takeoff ground roll (ft.): | 265
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| Takeoff over 50 ft. obstacle (ft.): | 780
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| Landing ground roll (ft.): | 398
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| Landing over 50 ft. obstacle (ft.): | 1025
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Source: Aviat Aircraft
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