2006 FLIGHT DESIGN CTSW


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    Aircraft Summary


    General

    Year
    2006
    Manufacturer
    FLIGHT DESIGN
    Model
    CTSW
    Condition
    Used
    Total Time
    458.1
    Description
    2006 Flight Design CTSW Full Frame Parachute, Like Cirrus Dynon PFD & MFD EMS D120 , Autopilot Full Glass Cockpit Engine make/model: Rotax912S Horsepower for takeoff: 100 TBO hrs.: 1500 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.): 525 Next Chute repack due 6/2026

    Airframe

    Airframe Notes
    2006 Flight Design CTSW N38BC S-LSA (factory built in Ukraine) BRS ballistic Parachute 1350 US distributor Airtime aviation Tulsa Oklahoma

    Engine

    Engine 1 Time
    358.1
    Engine 1 Overhaul Type
    SOH

    Avionics

    Avionics/Radios
    Dynon EFIS D100/ Dynon EMS D120(glass cockpit) Plus mechanical, Airspeed, Altimeter, Compass Garmin 496 GPS with moving map and XM Weather plus Garmin GA35 GPS WAAS Antenna TruTrak Digiflight II VS Autopilot


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