2006 FLIGHT DESIGN CTSW
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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