CT, CT light sport aircraft, Flight Designs CT light sport aircraft updated for 2006.

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Flight Designs CT light sport aircraft updated for 2006.

The CT from Flight Design U.S.A. was one of the first aircraft to go through the light sport aircraft program and has become one of the fastest craft in it's class.

With the assistance of customer feed back from the CT has undergone some modifications for 2006 to make it "more suitable for the American market."

The 2006 CTSW now comes standard with a 1350 BRS parachute system, making it the second company in the world to offer the parachute recovery system as standard equipment on their plane.

The CTSW also features new taller sport seats with additional padding. A map pocket and door holders have been added for storage and convenience. The instrument panel has been completely redesigned with three separate compartment areas, for flight instruments, radio stack and engine instruments.

For 2006 a three axis trim system is standard which allows the pilot to trim the pitch, roll and yaw, enabling trim of the craft on long cross country flights for changing fuel load, cross wind conditions, and throttle settings.

The landing gear has been strengthened, and more vertical stabilizer area has been added to give better directional stability. The anti servo tab is now full span to give a little more stick feed back.

The CTSW comes standard with the Rotax 912 S 100 HP 4 cylinder aircraft engine. This gives craft a 1,000 mile range with the fuel on board when throttled back to 90 knots.

Controls are standard three axis controls with dual sticks and rudder pedals. The main difference that a conventional pilot will notice are that the design is very clean, is lighter with less mass, and low drag. Normally 5 to 7 hours of training on the plane will be required for most conventional pilots to feel comfortable.

Flight Design U.S.A. test flies each aircraft prior to delivery for a minimum of 2 hours. As of this writing the factory is nearing the completion of a new expanded facility to provide sales and service for customers.

The parent company of Flight Design has been serving the ultralight and light sport aircraft market for over 15 years, and has developed one of the highest ratings for honesty and integrity from customers and competition in the industry.

CTSW SPECIFICATIONS

PERFORMANCE
WING SPAN:
LENGTH:
HEIGHT:
WING AREA:
ASPECT RATIO:
EMPTY WEIGHT:
GROSS WEIGHT:
28 FT.
20 FT.4 IN.
7' 11"
107 SQ. FT.
7.29:1
649 LBS.
1320 LBS.
CRUISE SPEED (@ 75%)
STALL SPEED (VSO )
VNE
CLIMB RATE (FT/Min)

MAX. RANGE (W/34 GAL.)

NO RESERVE

TAKEOFF ROLL (@ Wg)
GLIDE RATIO (ENGINE OFF)
112 KTS
39 KTS
145 KTS
960 Ft

1080 MILES.

295 FT
14:1
FUEL CAPACITY: 34 GAL.

POWERPLANT:  ROTAX 912S (100HP)

FUEL ECONOMY: 4.5 GALS/HR

PROPELLERS: Ground Adjustable Composite

AIRFOIL TYPE:  

C 180 13.8% Thick

For more information contact:

FLIGHT DESIGN USA

91 ROUTE 169

P0 BOX 325 S.
WOODSTOCK, CT. 06267 
860-963-7272

Flight Designs CT light sport aircraft updated for 2006.
Flight Designs CT light sport aircraft updated for 2006.

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