The basic training aircraft success story.
The G 120 is a success story on its own. With an extensive proven performance record with world class air forces around the globe, the G 120 outperforms any aircraft in its class with a track record of the highest dispatch reliability.
Built to perform and work, the G 120 has the lowest maintenance effort to flight hour’s relation in the industry. Cost efficiency and reliability, combined with excellent handling; make this the aircraft of choice in the piston trainer segment.
The existing operating success story of the GROB G 120 is our proof of concept.
Perfect match for full aerobatic and military training capability.
The G 120A is certified by both the EASA and the FAA to +6/-4 g. It
providesthe ideal training platform for the full range of conventional
high-performance aerobatic maneuvers, including spins, inverted spins,
loops, rolls, stall turns, outside turns and recovery from unusual
attitudes.
This versatile aircraft also offers excellent handling at
both high and low airspeeds, making it ideal to tackle the full spectrum
of primary training requirements, including pilot screening, instrument
flying, navigation and missionoriented tasks.
The ample power of its well-proven and reliable 260 HP Lycoming engine fitted with a 3-bladed constant-speed propeller, combined with a super lightweight composite airframe, provides the ideal power-to-weight ratio for primary pilot training and translates into superb flight characteristics in any situation.
The aircraft is equipped with robust, retractable landing gear, specifically designed for the high number of cycles and hard landings typical of a training environment.
SPECIFICATION
| Airframe and wing structure | Carbon fiber |
| Passenger seats | 2 (side-by-side) |
| Type of operation |
VFR day / night and IFR in non-icing conditions |
| Engine |
Lycoming AEIO-540-D4D5 by Textron Lycoming |
| Power |
260 HP 194 kW |
| Propeller |
3-blade / constant speed |
| External dimensions |
Height: 8 ft 8 in 2,66 m Wing span: 33 ft 5 in 10,18 m Length: 26 ft 7 in 8,11 m Wing area: 143,2 ft 13,3 m |
| Minimum structural service life |
15,000 flight hours (Aerobatic) |