Grob G-120

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Grob G 120A
Grob G 120A
Role Trainer
National origin Germany
Manufacturer Grob Aircraft
First flight 1999
G120TP variant in 2011

The Grob G 120A is a two seated 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 tricycle landing gear and a low tailplane.

The first buyer was Lufthansa Flight Training.[citation needed]

Contents

[edit] Design

The airframe made of carbon fibre reinforced plastic and is stressed to +6/-4g. Its minimum service life is just over 15,000 flight hours.[citation needed]

The cockpit provides room for students wearing military equipment and helmets. The plane is equipped with movable seats and rudder pedals and an air conditioning system. A second thrust lever is available.[citation needed]

[edit] Specifications

Data from[citation needed]

General characteristics

  • Crew: Two
  • Length: 8.11 m (26 ft 7 in)
  • Wingspan: 10.18 m (33 ft 5 in)
  • Height: 2.66 m (8 ft 9 in)
  • Wing area: 13.3 m² (143.1 ft²)
  • Empty weight: 1100kg (2425lb)
  • Useful load: 360 kg (792 lb)
  • Max. takeoff weight: 1440 kg (3,175 lb)
  • Powerplant: 1 × Lycoming AEIO-540-D4D5 6-cylinder, horizontally opposed engine, 194 kW (260 hp)
  • Propeller: 3-blade constant speed
  • Max. landing weight: 1440kg (3,168 lb)
  • Usable fuel: 252 ltr / 66.6 US Gal
  • Aspect ratio: 7.82

Performance

  • Maximum speed: 320 km/h (172 knots, 197 mph)
  • Cruise speed: 307 km/h (166 knots, 189 mph)
  • Stall speed: 102 km/h (55 knots, 63 mph)
  • Range: 1535 km (830 nm, 947 mi)
  • Rate of climb: 6.51 m/s (1,280 ft/min)
  • Wing loading: kg/m² (lb/ft²)
  • Power/mass: W/kg (hp/lb)
  • Take-off distance to 15m/50ft: 654 m (2,150 ft)
  • Landing distance to 15m/50ft: 562 m (1,845 ft)
  • Max. load factors: +6g / -4g
  • Min structural service life (aerobatic): 15,000 flight hours

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[edit] References

[edit] External links

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