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Price:
| $138,500 (incl. basic avionics) |
| Engine make/model: | Cont IO-360-ES4
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| Horsepower@rpm@altitude: | 185@2550@SL |
| Horsepower for takeoff: | 185 |
TBO hrs.:
| 1800 |
| Fuel type: | 100/100LL
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Propeller make/type:
| Three-blade CS*
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Landing gear type:
| Fixed/Tri
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| Max ramp weight (lbs.): | 2286
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| Gross weight (lbs.): | 2286 |
| Max landing weight (lbs.): | 2286
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| Empty weight, std. (lbs.): | 1350
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| Useful load, std. (lbs.): | 39
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Payload, full std. fuel (lbs.):
| 696
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| Usable fuel (gals.): | 39 |
| Oil capacity (qts.): | 8
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| Wingspan: | 38 ft. 6 in. |
| Overall length: | 24 ft. |
| Height: | 8 ft. 10 in. |
| Wing area (sq. ft.): | 167 |
Wing loading (lbs./sq. ft.):
| 13.7
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Power loading (lbs./hp.):
| 12.3
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| Wheel track: | 7 ft. 4 in.
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Wheel size (in.):
| 6.00 x 6
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| Seating capacity: | 4
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Cabin doors:
| 2
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| Cabin width (in.): | 45.5 |
| Cabin height (in.): | 51.3
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| Baggage capacity (lbs.): | 100 |
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PERFORMANCE |
| Cruise speed (kts.): | |
| 75% power: | 126 |
| 65% power: | 121 |
55% power:
| 110 |
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| Max range (w/ reserve) (nm): | |
75% power:
| 375 |
65% power:
| 420
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55% power:
| 440
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Fuel consumption (gph):
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| 75% power: | 11.5 |
| 65% power: | 9.8 |
55% power:
| 8.2 |
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| Estimated endurance (65% power w/1 hr reserve) (hrs): | 3.5 |
| Stall speed (flaps up) (knots): | 47
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| Stall speed (flaps down) (knots): | 43
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| Best rate of climb (fpm): | 1050 |
Best rate of climb - 8000 ft (fpm):
| 800
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| Service ceiling (ft.): | 18,000 |
| Takeoff ground roll (ft.): | 670
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| Takeoff over 50-ft. obstacle (ft.): | 1140 |
| Landing ground roll (ft.): | 500
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Landing over 50-ft. obstacle (ft.):
| 800
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*Fixed-pitch, two-blade prop will be fitted to production aircraft.
All specifications and performance listed above are based on preliminary tests in proof-of-concept aircraft and are subject to revision in final production models of the Luscombe Spartan IIE.
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