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| |
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| Engine make/model: | Lycoming O-540-B4B5
|
| Horsepower@altitude: | 235@SL |
| Horsepower for takeoff: | 235
|
TBO hrs.:
| 2000 |
| Fuel type: | 100/100LL
|
Propeller type/diameter:
| Hartzell CS
|
Landing gear type:
| Tri/Fixed
|
| Max ramp weight (lbs.): | 2900
|
| Gross weight (lbs.): | 2900 |
| Landing weight (lbs.): | 2900
|
| Empty weight, std. (lbs.): | 1467
|
| Useful load, std. (lbs.): | 1433
|
Payload, full std. fuel (lbs.):
| 929
|
| Usable fuel, std. (gals.): | 84 |
| Oil capacity (qts.): | 12
|
| Wingspan: | 32 ft. |
| Overall length: | 23 ft. 9 in. |
| Height: | 7 ft. 1 in. |
| Wing area (sq. ft.): | 171.6 |
Wing loading (lbs./sq. ft.):
| 17
|
Power loading (lbs./hp.):
| 12.4
|
Wheel size (in.):
| 6.00 x 6
|
| Seating capacity: | 4
|
Cabin doors:
| 1 |
| Cabin width (in.): | 44 |
| Cabin height (in.): | 47 |
| Baggage capacity (lbs.): | 200
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| |
PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power @ 8,000 ft.: | 136 |
| 65% power @ 8,000 ft.: | 130 |
55% power @ 8,000 ft.:
| 122 |
| | |
| Max range (w/ reserve) (nm): | |
75% power:
| 813* |
65% power:
| 879* |
55% power:
| 949* |
| | |
Fuel consumption (gph):
| |
| 75% power: | 12.3* |
| 65% power: | 10.7* |
55% power:
| 9.0* |
| | |
| Estimated endurance (65%) (hrs): | 6.5*
|
| Stall speed (flaps up) (knots): | 57
|
| Stall speed (flaps down) (knots): | 52 |
| Best rate of climb (SL fpm): | 825 |
Best rate of climb, 8000 ft. (fpm):
| 500*
|
| Service ceiling (ft.): | 14,500 |
| Takeoff ground roll (ft.): | 800
|
| Takeoff over 50-ft. obstacle (ft.): | 1360
|
| Landing ground roll (ft.): | 680 |
Landing over 50-ft. obstacle (ft.):
| 1300 |
| |
| * calculated |
|
