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| |
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| Engine make/model: | Lycoming IO-360-A3B6D
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| Horsepower@rpm@altitude: | 200@2700@SL |
| Horsepower for takeoff: | 200 |
TBO hrs.:
| 2000 |
| Fuel type: | 100LL
|
Propeller type/diameter:
| McCauley CS
|
Landing gear type:
| Tri/Retr.
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| Max ramp weight (lbs.): | 2740
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| Gross weight (lbs.): | 2740 |
| Max landing weight (lbs.): | 2740
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| Empty weight, std. (lbs.): | 1695
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| Useful load, std. (lbs.): | 1045
|
Payload, full std. fuel (lbs.):
| 661
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| Usable fuel, std. (gals.): | 64 |
| Oil capacity (qts.): | 8
|
| Wingspan: | 36 ft. 1in. |
| Overall length: | 24 ft. 9 in. |
| Height: | 8 ft. 4 in. |
| Wing area (sq. ft.): | 174.8 |
Wing loading (lbs./sq. ft.):
| 15.7
|
Power loading (lbs./hp.):
| 13.7
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Wheel size (in.):
| 6.00 x 6
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| Seating capacity: | 4
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Cabin doors:
| 1
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| Cabin width (in.): | 43.5 |
| Cabin height (in.): | 45 |
| Baggage capacity (lbs./cu. ft.): | 120/13.5
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| |
PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power: | 171 |
| 65% power: | 162* |
55% power:
| 145 |
| | |
| Max range (w/ reserve) (nm): | |
75% power:
| 740** |
65% power:
| 800** |
55% power:
| 940**
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| | |
Fuel consumption (gph):
| |
| 75% power: | 10.8 |
| 65% power: | 9.3** |
55% power:
| 7.9**
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| | |
| Estimated endurance (65%) (hrs): | 5.5 |
Vs (kts.):
| 61
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Vso (kts.):
| 54
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| Best rate of climb (SL fpm): | 1050
|
Best rate of climb, 8,000 ft. (fpm):
| 700
|
| Service ceiling (ft.): | 18,600 |
| Takeoff ground roll (ft.): | 900 |
| Takeoff over 50-ft. obstacle (ft.): | 1700
|
| Landing ground roll (ft.): | 677 |
Landing over 50-ft. obstacle (ft.):
| 1600
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* estimated
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** calculated
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Sources: ABPD, Jane’s All The World’s Aircraft
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