INTELLIGENCE
Designed for military pilot training, this side-by-side trainer aircraft offers optimal conditions for instruction and communication. The seating layout enhances situational awareness and facilitates real-time feedback between instructor and trainee. Certified for +6 / -4 g, it is ideal for advanced flight maneuvers and tactical training scenarios.
SIMPLICITY
Simplicity in pilot operation and system functions make the G 120TP the only sophisticated mission training platform that can accommodate typical elementary, basic and advanced pilot training segments.
EFFICIENCY
Built with advanced composite materials, the G 120TP combines low maintenance costs with high training efficiency and outstanding flight characteristics. Designed for military use, it delivers robust performance, high maneuverability, and a modern cockpit environment ideal for basic to advanced pilot training.
POWER
Powered by the reliable Rolls-Royce M250-B17F turbine engine delivering 456 SHP, combined with operating simplicity makes the ideal platform for learning the first steps of flying all the way to pushing the envelope at 6g during the aerobatic training phase.
GROB AIRCRAFT TRAINING CONCEPT
Designed around the proven G 120TP, our integrated training platform combines versatility, efficiency, and performance in a single aircraft. It enables seamless execution of all core training phases - from ab initio to advanced - while eliminating costly type transitions.
The result: reduced training time, lower overall costs, and consistently high training quality.
But it delivers more than just an aircraft - it offers a complete, future-ready training ecosystem tailored to the needs of modern air forces.
TECHNICAL SPECIFICATIONS
Operating speed range
| Max. operating speed Vmo MSL up to 13,000 ft | 235 KIAS |
|---|---|
| Max. mach number Mmo above 13,000 ft | 0.45 |
| Stall speed Vs (MSL landing config., utility) | 57 KIAS |
Take off and landing distances (MSL, ISA)
| Take off distance over 50 ft (MTOW, no wind, no slope, utility) | 395 m |
|---|---|
| Landing distance over 50 ft (MLW, no wind, no slope) | 480 m |
Cruise speeds, rate of climbs (ISA, MTOW)
| Max. cruise speed (MSL, MCP, ISA) | 205 KTAS |
|---|---|
| Max. cruise speed (10,000 ft, ISA, MCP, utility) | 226 KTAS |
| Rate of climb (MSL, MP, aerobatic) | 2,800 ft/min |
| Sustained g (MSL, MCP, 1400 kg aircraft weight) | 3.0 g |
Range / Endurance (ISA, 30 min reserve fuel, utility)
| Air Range (5,000 ft, LRC speed) | 880 NM |
|---|---|
| Air Range (10,000 ft, LRC speed) | 790 NM |
| Endurance (10,000 ft, max endurance power) | 5.8 hrs |
| Max. take-off weight (MTOW, utility) | 1,625 kg | 3,852 lb |
|---|---|
| Max. take-off weight (MTOW, aerobatic) | 1,515 kg | 3,340 lb |
| Max. landing weight (MLW) | 1,545 kg | 3,406 lb |
| Power loading (at MTOW, utility) | 3.56 kg / HP |
| Power loading (at MTOW, aerobatic) | 3.56 kg / HP |
| Max. usable fuel capacity | 275 kg | 606 lb |
| Max. baggage weight | 50 kg | 110 lb |
| Type | Rolls Royce M250-B17F |
|---|---|
| Fuel | Jet A, Jet A1, JP-8, JP-5 |
| Max. continuous power (MCP) | 380 SHP |
| Max. power (MP, 5 min limit) | 456 SHP |
| Overall length | 8.42 m |
|---|---|
| Overall span | 10.31 m |
| Overall height | 2.62 m |
| Aircraft Type | Two-seat turboprop trainer |
|---|---|
| Cockpit Configuration | Side-by-Side, dual controls |
| Aerobatic Capability | Full Aerobatic |
| Max. load factors aerobatic (G Limits) | +6 / -4 G |
| Max. operating altitude | 25,000 ft |
| Landing gear | - Retractable - For paved and unpaved runways |
| Avionics | Genesys IDU-680 Full glass cockpit - EFIS (rendundant) - VFR day / night and IFR |
| Certification | EASA CS-23 Flight into known icing conditions |