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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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Page last modified: 28-07-2011 00:50:59 ZULU