Aircraft > Single-Engine Piston > Flight Design > N134CT: Flight Design CTSW
2006 Flight Design CT No damage history Engine make/model: Rotax912S Horsepower@altitude: 100@SL Horsepower for takeoff: 100 Fuel type: 100/100LL Propeller type/diameter: Neuform FP Landing gear type: Tri./Fixed Max ramp weight (lbs.): 1320 Gross weight (lbs.): 1320 Landing weight (lbs.): 1320 Empty weight, std. (lbs.): 646 Useful load, std. (lbs.): 674 Useful fuel, std. (gals.): 34 Payload, full std. fuel (lbs.): 470 Wingspan: 28 ft. Overall length: 20 ft. 4 in. Height: 7 ft. 11 in. Wing area (sq. ft.): 107 Wing loading (lbs./sq. ft.): 12.3 Power loading (lbs./hp.): 13.2 Wheel size (in.): 6.00 x 6 Seating capacity: 2 Cabin doors: 2 Cabin width (in.): 49 PERFORMANCE Cruise speed (kts.): 75% power: 112 Max range (w/ reserve) (nm): 75% power: 600 Fuel consumption (gph): 75% power: 4.5 Vso (kts.): 39 Best rate of climb (SL fpm): 960 Service ceiling (ft.): 14,000 Takeoff ground roll (ft.): 295 Takeoff over 50-ft. obstacle (ft.): 52
Dynon / Garmin / Trutrack autopilot / ADSB in & out
*Sold* 2006 Flight Design Engine make/model: Rotax912S Horsepower@altitude: 100@SL Horsepower for takeoff:100 Fuel type:100/100LL Fuel capacity: 34 Propeller type/diameter: Neuform FP Landing gear type: Tri./Fixed Max ramp weight (lbs.): 1320 Gross weight (lbs.): 1320 Landing weight (lbs.): 1320 Empty weight, std. (lbs.): 646 Useful load, std. (lbs.): 674 Useful fuel, std. (gals.): 34 Payload, full std. fuel (lbs.): 470 Wingspan: 28 ft. Overall length: 20 ft. 4 in. Height: 7 ft. 11 in. Wing area (sq. ft.): 107 Wing loading (lbs./sq. ft.): 12.3 Power loading (lbs./hp.): 13.2 Wheel size (in.): 6.00 x 6 Seating capacity: 2 Cabin doors: 2 Cabin width (in.): 49 PERFORMANCE Cruise speed (kts.): 75% power: 115 Max range (w/ reserve) (nm): 75% power: 600 Fuel consumption (gph): 75% power: 4.5 Vso (kts.): 39 Best rate of climb (SL fpm): 960 Service ceiling (ft.): 14,000 Takeoff ground roll (ft.): 295 Takeoff over 50-ft. obstacle (ft.): 52
554tt
Interior 9/10