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21Dec
Glasair GlaStar
The Glastar is a versatile, two-seat, high-wing aircraft designed by Glasair Aviation for recreational flying, light-duty utility, and amateur-built markets. Known for its blend of solid performance, reliability, and adaptability, the Glastar has earned a strong reputation among pilots seeking an affordable yet high-performing aircraft. The Glastar is available as a kit-built aircraft, appealing to aviation enthusiasts who enjoy the challenge of assembling their aircraft while tailoring it to their preferences.
Description
The Glastar features a high-wing design with a semi-monocoque fuselage, combining a tubular steel frame with lightweight composite and aluminum components. This hybrid construction ensures structural strength and corrosion resistance while keeping the aircraft light and efficient. Its tricycle landing gear is rugged and optionally interchangeable with conventional taildragger gear, making the Glastar adaptable to a range of terrain, including grass strips and unimproved fields.
The cockpit is spacious for a two-seat aircraft, accommodating taller pilots comfortably while providing ample visibility. The panel layout supports modern avionics upgrades, with space for glass cockpit systems and traditional instrumentation. A generous baggage area, accessible from the cabin or through an external door, enhances its utility, making the Glastar suitable for weekend getaways or cross-country trips.
Specifications
| General Specifications | Details |
|---|---|
| Manufacturer | Glasair Aviation |
| Role | Recreational, Utility |
| Seating Capacity | 2 (Pilot and Passenger) |
| Length | 22 ft 0 in (6.71 m) |
| Wingspan | 35 ft 0 in (10.67 m) |
| Height | 8 ft 8 in (2.64 m) |
| Wing Area | 128 sq ft (11.89 m²) |
| Empty Weight | 1,250 lbs (567 kg) |
| Max Takeoff Weight (MTOW) | 1,960 lbs (889 kg) |
| Engine Options | Lycoming O-320 or O-360, 150–180 hp (112–134 kW) |
| Propeller | Fixed-pitch or constant-speed |
| Fuel Capacity | 40 gallons (151 liters) |
| Range | 800 nautical miles (920 mi / 1,480 km) |
| Cruise Speed | 120–140 knots (138–161 mph / 222–259 km/h) |
| Service Ceiling | 15,000 ft (4,570 m) |
| Takeoff Distance (50 ft obstacle) | 750 ft (229 m) |
| Landing Distance (50 ft obstacle) | 700 ft (213 m) |
Performance
The Glastar delivers dependable performance suitable for various aviation missions, from casual flying to backcountry adventures. Depending on the engine configuration, the Glastar can cruise between 120 and 140 knots, offering respectable speed for cross-country flights. With a fuel capacity of 40 gallons, it has an impressive range of up to 800 nautical miles, making it a capable platform for extended trips.
Takeoff and landing performance is one of the Glastar’s highlights. The aircraft’s short takeoff and landing (STOL) capabilities allow it to operate out of small or remote airstrips with ease. Its robust airframe and undercarriage can handle rough field operations, while the option for tundra tires or floats extends its versatility.
The Glastar’s handling is stable and predictable, offering confidence to less experienced pilots while providing enough responsiveness to satisfy seasoned aviators. Its lightweight structure and efficient design contribute to a low stall speed, enhancing safety during critical phases of flight.
Conclusion
The Glastar’s combination of versatility, performance, and kit-building accessibility makes it a standout choice in the light aircraft market. Whether used for recreational flying, backcountry exploration, or cross-country journeys, the Glastar remains a beloved option for pilots who value adaptability and reliability in their aircraft.
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