SAFETY & STYLE
SAFETY & STYLE
The quest for perfection
The GOGETAIR AIRCRAFT
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 G750. Designed to be the ultimate safe, affordable, attractive, and top-performing sport-family aircraft with an option for 2+2 seating configuration and MTOW 750 kg in the Experimental category.
INTELIGENCE & automation
YOU ARE Safe in every situation
Featuring Dynon Skyview or Garmin G3X touch 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 914 turbo engine enables take-off in less than 200 meters and a climb rate of up to 1500 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.
|Maximum Gross Weight||1653 lbs||750 kg||Manufacturer||Rotax||Rotax||Rotax|
|Standard Base Weight (Rotax 912iS)||882 lbs||400 kg||Model||912iS||914UL||915iS|
|Standard Base Weight (Rotax 914UL)||915 lbs||415 kg||Horsepower||100HP||115 HP||141HP|
|Standard Base Weight (Rotax 915iS)||965 lbs||438 kg|
|Usable Fuel Capacity||36,5gal||138 l||Takeoff||240 m||150 m||120 m|
|Takeoff Over 50 ft Object||385 m||225 m||175 m|
|Dimensions:||Climb Rate||650 ft/min||1050 ft/min||1450 ft/min|
|Length||23.4 ft||7,13 m||Max Operating Altitude||14.760 ft||14.760 ft||14.760 ft|
|Height||6.9 ft||2,1 m||Stall Speed in Lan with Flaps||38 KIAS||38 KIAS||38 KIAS|
|Wingspan||31.8 ft||9,69 m||Vne||152 KIAS||152 KIAS||152 KIAS|
|Cabin Length||88.6 in||225 cm||Optimal Cruise speed (65%)||114 KIAS||121 KIAS||138 KIAS|
|Cabin Width (inside)||47.6 in||121 cm||Max Cruise Speed||138 KIAS||138 KIAS||138 KIAS|
|Cabin Height||46 in||117 cm||Landing Ground Roll||130 m||140 m||160 m|
|Aerodynamic mean chord (MAC)||48 in||121 cm||Cruise Range with Reserve (65% PWR)||1050nm||900nm||950nm|
|Wing area||130 sq feet||12m2||Endurance||9h||6,5h||7,2h|