Overview
The Grob G-120A is a two-seat composite training aircraft developed for military and civilian flight schools. Designed to provide modern handling and low operating costs, it supports early-phase pilot training. The aircraft reflects Grob’s emphasis on composite airframe technology.
Live Fleet Activity (G120)
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Specifications
Units
- Engine
- 1 × Lycoming AEIO-540-D4D5 6-cylinder
- Engine type
- Piston
- Power
- 260 hp · 194 kW
- Avionics
- IFR instrumentation with EFIS and King / Bendix components
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 26 ft 7 in · 8.11 m
- Tail height
- 8 ft 9 in · 2.66 m
- Fuselage diameter
- 4 ft 3 in · 1.30 m
- Wing span
- 33 ft 5 in · 10.18 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 3,300 lb · 1,500 kg
- Max landing weight
- 3,150 lb · 1,450 kg
- Max payload
- 500 lb · 200 kg
- Fuel capacity
- 70 gal · 300 L · 200 kg (AvGas)
- Max cruise speed
- 172 kt · 198 mph · 319 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 56 kt · 64 mph · 104 km/h
- Range
- 830 nm · 960 mi · 1,540 km
- Fuel burn
- 14.30 nm/gal · 7.00 km/L
- Ceiling
- 18,000 ft · 5,500 m
- Rate of climb
- 1,280 ft/min · 7 m/s
- Takeoff distance
- 2,300 ft · 710 m
- Landing distance
- 1,840 ft · 560 m
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Live fleet activity details
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