1983 Cessna Turbo 210N Centurion II
1983 Cessna Turbo 210N Centurion II Used Price: $207,000 Engine make/model: Continental TSIO-520-R Horsepower@rpm, 35-in. manifold pressure (hp@rpm): 285@2600 Horsepower for takeoff@rpm, 36.5-in. manifold pressure(hp@rpm):: 310@2700 TBO hrs.: 1600 Fuel…
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1983 Cessna Turbo 210N Centurion II
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| Used Price: | $207,000 | |
| Engine make/model: | Continental TSIO-520-R | |
| Horsepower@rpm, 35-in. manifold pressure (hp@rpm): | 285@2600 | |
| Horsepower for takeoff@rpm, 36.5-in. manifold pressure (hp@rpm):: |
310@2700 | |
| TBO hrs.: | 1600 | |
| Fuel Type: | 100/100LL | |
| Propeller type/diameter (in.): | McCauley CS/80 | |
| Landing Gear type: | Tri./Retr. | |
| Max ramp weight (lbs.): | 4016 | |
| Gross weight (lbs.): | 4000 | |
| Landing weight (lbs.): | 3800 | |
| Empty weight, std. (lbs.): | 2303 | |
| Empty weight, as tested (lbs.): | 2400* | |
| Useful load, std. (lbs.): | 1697 | |
| Payload (lbs.): | 896** | |
| Usable fuel, std. (gals.): | 90 | |
| Oil capacity (qts.): | 11 | |
| Wingspan: | 39 ft. 9 in.*** | |
| Overall length: | 28 ft. 2 in. | |
| Height: | 9 ft. 8 in. | |
| Wing area (sq. ft.): | 181 | |
| Wing loading (lbs./sq. ft.): | 22.9 | |
| Power loading (lbs./hp.): | 12.9 | |
| Wheel base (in.): | 72 | |
| Seating capacity: | 6 | |
| Cabin doors: | 2 | |
| Cabin width (in.): | 41.8 | |
| Cabin height (in.): | 48 | |
| Baggage capacity (lbs.): | 370 | |
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PERFORMANCE
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| Cruise speed (kts.): | ||
| 75% power @ 2000/24,000 ft.: | 157/192 | |
| 65% power @ 2000/24,000 ft.: | 150/175 | |
| 45% power @ 2000/24,000 ft.: | 135/154 | |
| Range (w/45-min. reserve) (nm): | ||
| 75% power @ 2000/24,000 ft.: | 1000/1075 | |
| 65% power @ 2000/24,000 ft.: | 1200/1125 | |
| 45% power @ 2000/24,000 ft.: | 1350/1200 | |
| Fuel consumption (est. @ .44 lbs./hp/hr. sfc gph): | ||
| 75% power: | 17 | |
| 65% power: | 15 | |
| 45% power: | 12 | |
| Estimated endurance (65%) (hrs): | 8.0 | |
| Vso (kts.): | 58 | |
| Best rate of climb (fpm): | 930 | |
| Best rate of climb, 8,000 ft. (fpm): | 850 | |
| Service ceiling (ft.): | 27,000 | |
| Takeoff ground roll (ft.): | 1300 | |
| Takeoff over 50-ft. obstacle (ft.): | 2160 | |
| Landing ground roll (ft.): | 765 | |
| Landing over 50-ft. obstacle (ft.): | 1500 | |
| *Estimated | ||
| ** With 120-gallon auxillary tanks | ||
| *** With Flint Tip Tanks | ||
| Sources: Aircraft Bluebook Price Digest and Jane's All The World's Aircraft Company | ||
StaffWriter
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