SAFETY & STYLE
SAFETY & STYLE
The quest for perfection in the light aircraft category
The G600 ULA/LSA
The aircraft design process balances many competing and demanding requirements to produce an aircraft that is strong, lightweight, economical, and can carry an adequate payload while being sufficiently reliable to safely fly for the design life of the aircraft. The technique is highly iterative, involving high-level configuration tradeoffs, a mixture of analysis and testing, and the detailed examination of the adequacy of every part of the structure.
The result of this quest for perfection is G600. Designed to be the ultimate safe, affordable, attractive, and top-performing ULN or LSA with MTOW of 600 kg
INTELIGENCE & automation
YOU ARE Safe in every situation
Featuring Dynon Skyview and Autopilot GOGETAIR will lever or return to home from every situation you might encounter in the air.
LEVEL button, to level the aircraft from any bank or pitch and
HOME button to fly to your home airport from any position.
Ergonomy and comfort
Your hand will find the throttle control where you expect it to be thus giving your freedom to effortlessly adjust power for the required flight phase.
ANDAIR fuel selector with dual return line and fuel tank change warning will give you peace of mind on longer flights.
Click on blinking square to show feature
AVEO wingtip lights
Rotax 914 Turbo
(AOA) Angle of attack pitot tube
Beringer or Goldfren
UV and bird strike
Aerodynamic and constructional
Lamborghini style doors
CARBON SAFETY CAGE
Kevlar cabin interior
Built to certified aircraft standards.
Intuitive and informative panel
LEVEL and HOME
Dynon AP control
BRS parachute handle
Prop flap controller
12V Charging station
Our passionate team who have designed GOGETAIR aircraft, wanted it to be fitted with the best possible components and technology available to the aircraft in its class. Bellow, find the most known and appreciated producers of parts and avionic, that is installed on GOGETAIR aircraft.
ROTAX 914 UL/F
The turbo charged aircraft engine Rotax 914 series offers more performance at high altitudes while delivering lower weight engines. This series offers a time between overhauls of 2,000 hrs and delvers reliable operation
DIMENSIONS AND PERFORMANCE
GOGETAIR aircraft can stay in the air for a total of up to 9 hours, the aircraft is equipped with adjustable rudder pedals as well as adjustable seats and 3 different foam density of seat cushioning for maximum comfort. All this gives to any pilot between 163 and 202cm in height the feeling of home comfort.
The plane also offers a lot of room for the front fellow passenger. The back seat can be used as baggage space or you can also take 2 children up to 25 kg each and not more than 150cm in height. In case the plane is to carry four people, some of the baggage can still be stored in the small baggage space behind the back seats.
GOGETAIR is not only a fast but also an economical plane. The Rotax 912 engine enables take-off in less than 250 meters and a climb rate of up to 1000 ft/min. At the optimum flight speed, i.e. 125 KTAS, it will use only about 16 liters of fuel an hour. In the best conditions, a full tank (of useful 135 liters) will keep you airborne for 9+ hours and make for a potential range of over 1,100 nautical miles or 2,000 km. Due to its huge flaps aircraft is easily operated on 450m runway.
You can find more detailed information about the dimensions and the capabilities of GOGETAIR aircraft in the table below. 2
|Maximum Gross Weight||1322 lbs||600 kg||Manufacturer||Rotax|
|Standard Base Weight||870 lbs||395 kg||Model||912 ULS|
|Useful Load||451 lbs||205 kg||Horsepower||100 HP|
|Usable Fuel Capacity||36,5gal||138 l|
|Length||23.4 ft||7,13 m||Takeoff||787 ft||240 m|
|Height||6.9 ft||2,1 m||Takeoff Over 50 ft Object||1148 ft||350 m|
|Wingspan||31.8 ft||9,69 m||Climb Rate||1000 ft/min||5 m/sec|
|Cabin Length||88.6 in||225 cm||Max Operating Altitude||13.500 ft||4100 m|
|Cabin Width (inside)||47,6 in||121 cm||Stall Speed with Flaps||38 KCAS||70 km/h|
|Cabin Height||46 in||117 cm||Vne||152 KTAS||282 km/h|
|Max Cruise Speed||138 KTAS||256 km/h|
|Landing Ground Roll||460 ft||140 m|
|Cruise Range with Reserve (65% PWR)||1038nm||1922 km|