Schweizer RU-38B Twin Condor
| Specifications | |
|---|---|
| Never Exceed Speed (KIAS) | 168 |
| Stall Speed (KIAS) | 62 |
| Service Ceiling | 30,000 ft |
| Mission Speed (KIAS) | 83 |
| Best Climb Speed (KIAS) | 83.5 |
| Take Off Distance | 965 ft |
| Take Off Distance (50' Obst.) | 1020 ft |
| Landing Ground Roll Distance | 1970 ft |
| Landing Distance (50' Obst.) | 3100 ft |
| Wing Span | 84.13 ft/ 25.65 m |
| Wing Area | 334.2 ft2/ 31.06 m2 |
| Length | 35.1 ft/ 10.7 m |
| Gross Weight | 7200 lbs/ 3265 kg |
| Empty Weight | 4265 lbs/ 1934 kg |
| Payload | 800 lbs/ 363 kg |
| Fuel | 1475 lbs/ 669 kg (220 gal) |
| Pilot and Crew | 660 lbs/ 299 kg |
| Power Plant | 2 Rolls Royce Allison 250-B17F or 2 Teledyne Continental GIO-550A flat-six engines, each w/ 350 hp |
| Propeller | Constant Speed, Full Feather |
| Useable Fuel | 280 Gallons/ 1059 Litres |
| Seating Capacity | 3 Person Crew: Pilot, Dual Controls |
| Operating Range | 6-10 hours endurance |
| Avionics | AN/APN-215(V) Color Weather/Search radar AN/AAQ-15 Forward-Looking Infrared system |
| Crew | 2 (Pilot, Co-Pilot) |
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