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1948 Aeronca Sedan N1000H
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| Base price: | $22,000 | |
| Engine make/model: | Continental C-145, 6-cylinder | |
| Horsepower@rpm@altitude: | 145@2700@SL | |
| Horsepower for takeoff: | 145 | |
| Fuel type: | 100LL | |
| Propeller type/diameter: | McCauley Fixed Pitch | |
| Landing gear type: | Conventional | |
| Max ramp weight (lbs.): | 2050 | |
| Gross weight (lbs.): | 2050 | |
| Landing weight (lbs.): | 2050 | |
| Empty weight, std. (lbs.): | 1050 | |
| Useful load, std. (lbs.): | 900 | |
| Payload, full std. fuel (lbs.): | 684 | |
| Usable fuel, std. (gals.): | 36 | |
| Oil capacity (qts.): | 8 | |
| Wingspan: | 37 ft. 6 in. | |
| Overall length: | 25 ft. 3 in. | |
| Height: | 7 ft. | |
| Wing area (sq. ft.): | 216.4 | |
| Wing loading (lbs./sq. ft.): | 9.47 | |
| Power loading (lbs./hp.): | 14.1 | |
| Wheel base (in.): | 84 | |
| Wheel size (in.): | 6.00 x 6 | |
| Seating capacity: | 4 | |
| Cabin doors: | 1 | |
| Baggage capacity (lbs.): | 120 | |
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PERFORMANCE
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| Cruise speed (kts.): | ||
| 75% power @ 2,000 ft.: | 120 | |
| 65% power @ 2,000 ft.: | 105 | |
| Max range (w/ reserve) (nm): | ||
| 75% power @ 2,000 ft.: | 430 | |
| Fuel consumption (gph): | ||
| 75% power @ 2,000 ft.: | 8.8 | |
| Estimated endurance (65%) (hrs): | 4 | |
| Vs (kts.): | 53 | |
| Vso (kts): | 45 | |
| Best rate of climb (SL fpm): | 570 | |
| Service ceiling (ft.): | 12,400 | |
| Takeoff ground roll (ft.): | 500 | |
| Landing ground roll (ft.): | 1300 | |
| Sources: Manufacturer’s specs and type certificates | ||
1948 Aeronca Sedan N1000H
Key Takeaways:
- The article presents detailed specifications for the 1948 Aeronca Sedan N1000H, a four-seater aircraft powered by a 145-horsepower Continental C-145 6-cylinder engine, with a listed base price of $22,000.
- It has a maximum gross weight of 2050 lbs, an empty weight of 1050 lbs, and offers a useful load of 900 lbs, with a usable fuel capacity of 36 gallons.
- Key performance figures include a cruise speed of 120 knots (at 75% power), a maximum range of 430 nautical miles, a service ceiling of 12,400 feet, and a takeoff ground roll of 500 feet.
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