Grob G 120A-F (2007 utility-category production)
Explore the Grob G 120A-F (2007 utility-category production) in side view and top view to compare its silhouette and proportions.
From Wikipedia
The Grob G 120 is a two-seat training and aerobatic low-wing aircraft with a carbon composite airframe, built by Grob Aircraft. It is based on the Grob G 115TA training aircraft and is specially designed for military and civil pilots training. It has a retractable tricycle landing gear and a low tailplane.
Summary of “Grob G 120” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Grob G 120A-F (2007 utility-category production) by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/G120/), CC BY 4.0Specifications
- Length
- 8.07 m26.5 ft
- Wingspan
- 10.19 m33.4 ft
- Max take-off weight
- 1.49 t3,300 lb
- Cruise speed
- 252 km/h157 mph
- Range
- 1,296 km805 mi
- Ceiling
- 5,486 m18,000 ft
- Engines
- 1 × Lycoming AEIO-540-D4D5
- Power
- 260 hp
- First flight
- 1999
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
