N912TL - 2003 TL ULTRALIGHT TL2000 STING

2003

TL-ULTRALIGHT

TL2000 STING

N912TL

TLUSA102912S

Used

565.0

Trades Welcome! • Always Hangared • No Corrosion "Composite Structure: The Sting has a fully tapered wing, fixed horizontal and vertical stabilizers, split flaps and powerful elevator, rudder and aileron surfaces. Conformal cowling follows the engine contours, directing cooling air precisely to the areas where it is needed. This permits the use of smaller air inlets, presents less frontal and wetted area and reduces drag. The aerodynamic shape of the Sting makes it agile in flight and gives it an impressive 12:1 glide ratio. The Sting is built with composite-reinforced epoxy structures. For weight-savings and superior strength, carbon fiber products comprise approximately 85% of the reinforcing materials. The wing surfaces and fuselage are made from carbon/epoxy sandwich construction cored with closed-cell foam and assembled with epoxy adhesives. Wing and fuselage skins are vacuum bagged and oven cured. Wing spar caps and other heavily loaded components are autoclaved. High-quality molds and care in layup yield a sleek, paintable exterior surface without the need for gel coat, saving 50 pounds of non-structural dead weight. Wings, fuselage and empennage are finished in white, two-part epoxy paint. Colorful graphics are available in vinyl, applied over the painted finish. Passenger and pilot are enclosed in the carbon-fiber-reinforced cockpit cage with integral rollover protection." Dimensions, Weights & Capacities: Cockpit width: 44" Wingspan: 29.9 ft Length: 20.3 ft Height: 6.3 ft Max takeoff weight: 1,320 lbs

565 Hours Total Time Since New

Rotax 912S Engine - 100 hp

Speeds & Distances Never exceed (Vne): 164 knots Max, continuous power (Vh): 120 knots  Cruise (Vc): 116 knots Takeoff (Vlof): 42 knots Stall, no flaps (Vs): 39 knots Stall, full flaps (Vso): 34 knots Demonstrated crosswind: 17 knots Takeoff roll: 295 feet Take off over 50" obstacle: 745 feet Landing roll: 345 feet Landing over 50' obstacle: 1,020 feet Rate of climb: 1,000+ fpm  Glide ratio: 12:1 Range @ Vc, no wind, 30 minute reserve, standard tank: 495 nm Range @ Vc, no wind, 30 minute reserve, with wing tanks: 790 nm  Endurance @ Vbe, standard tank: 5+ hours  Endurance @ Vbe, with wing tanks: 7.5+ hours

Garmin 496 GPS GRT Sport EFIS and Moving Map Garmin SL40 Radio DRE-244E Intercom GTX 327 Transponder AP1 Autopilot (GPS Coupler and S2 Servo)

GRS Galaxy Rescue System (Parachute) 30 Gallon Fuel Capacity - Mogas 6 gal/hr Fuel Burn

White with Fire Engine Red & Blue Stripes

Dark Grey Cloth with Multicolored Speckles

We fly the aircraft to your ramp for inspection by you and your mechanic at no cost or obligation to you. All Specifications Subject To Verification Upon Inspection