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Grob Aerospace
Grob G 120 Training

General information
Type Trainer
National origin Germany
Manufacturer Grob Aircraft
Status Active in production
Primary users French Air and Space ForceIsraeli Air Force
Royal Canadian Air Force
German Air Force
History
Manufactured 1999-present
First flight 1999
Developed from Grob G 115
Variants Grob G 120TP
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History Grob Aircraft, formerly Grob Aerospace
Grob G 120 is a two-seat training and aerobatic
Manufactured 1999-present



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 tricycle landing gear and a low tailplane.

Design and development The airframe is made of carbon fibre reinforced plastic and is stressed to +6/-4g. Its minimum service life is just over 15,000 flight hours.[1] 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.[citation needed] A second thrust lever is available..

Variants

G 120A
Piston powered version with a Lycoming AEIO-540-D4D5 six cylinder, four-stroke, air-cooled piston aircraft engine producing 260 hp (194 kW).
G 120TP
Turboprop powered version with a Rolls-Royce 250-B17F aircraft engine producing 456 shp (340 kW) for take-off and 380 shp (283 kW) for maximum cruise.

Operators

One of six G 120A of the Kenya Air Force
Grob G120A used by RCAF
Canada
France
Germany
Israel
 

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Max Crew

element
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Grob Aircraft, formerly Grob Aerospace

Grob Aircraft, formerly Grob Aerospace
Grob G 120 is a two-seat training and aerobatic Manufactured 1999-present

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General Info

      • Crew: Two
      • Length: 8.605 m (28 ft 3 in)
      • Wingspan: 10.19 m (33 ft 5 in)
      • Height: 2.57 m (8 ft 5 in)
      • Wing area: 13.29 m2 (143.1 sq ft)
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Powerplant


      • Empty weight: 960 kg (2,116 lb)
      • Gross weight: 1,440 kg (3,175 lb)
      • Max takeoff weight: 1,490 kg (3,285 lb) (Utility)
      • Fuel capacity: 256 litres (56 imp gal; 68 US gal)
      • Powerplant: 1 × Lycoming AEIO-540-D4D5 air-cooled flat-six, 190 kW (260 hp)
      • Propellers: 3-bladed Hartzell HC-C3YR-1RF/F7663R, 1.98 m (6 ft 6 in) diameter 
plane
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Performance

  • Maximum speed: 319 km/h (198 mph, 172 kn)
  • Cruise speed: 307 km/h (191 mph, 166 kn) at 75% power (1,500 m (5,000 ft))
  • Stall speed: 102 km/h (63 mph, 55 kn) with full flaps
  • Never exceed speed: 435 km/h (270 mph, 235 kn)
  • Range: 1,540 km (960 mi, 830 nmi) at 8,000 ft (2,400 m) and 45% power)
  • Endurance: 6.35 hours at 10,000 ft and maximum endurance power setting
  • Service ceiling: 5,500 m )
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Special Links Grob Aircraft, formerly Grob Aerospace

Links to Youtube & Others

This low-wing, aerobatic aircraft is the aircraft of choice in the first phase of flying for pilot candidates of the RCAF. The agility and precision of this aircraft provide a steep learning curve to all pilots in the RCAF to ensure they have the potential to operate in demanding operational environments.

Grob G 120 is a
two-seat training

Development of the type continue and in 1935 the Bf 108B appeared with the fin and rudder having undergone modifications.

interior

Youtube Link

Conceived as a competitive aircraft the Bf 108 would take part in the 1936 Berlin Olympics.

interior
Aircrafttotal : Aircraft

Read more in Bayerische Flugzeugwerke
(BFW) Messerschmitt

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