Grob G 120

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G120TP variant in 2011

The Grob G 120 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 operator of the aircraft was Lufthansa Flight Training.[citation needed]

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.[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]

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).[1]
G 120TP
Turboprop powered version with a Rolls Royce 250-B17F aircraft engine producing 456 shp (340 kW) for take-off.[2] The Indonesian Air Force signed a contract for about 18 G 120TP trainers in the elementary and basic flying training roles in September 2011 at a cost of approx US$4 million each. The Argentinian AF also bought 10 examples of the G120TP one of which landed gear-up after just 20 hours of flying. The Indian AF recently bought the PC7M Mk2 in preference to the G120TP as it includes local manufacture.[3]

Operators

One of six G 120A of the Kenya Air Force
Grob G-120A badge worn by a Canadian Forces military student pilot from 3 CFFTS.
 Canada
Royal Canadian Air Force[4]
 Germany
German Air Force[5]
 France
French Air Force[4]
 Israel
Israeli Air Force[4]
 Kenya
Kenya Air Force:[6] 6 (+6 option)

Specifications (G 120A)

Data from Jane's All The World's Aircraft 2003–2004[7]

General characteristics

  • 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)
  • Airfoil: Eppler E884
  • 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)[8]
  • 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 [8]

Performance

  • Maximum speed: 319 km/h; 198 mph (172 kn)
  • Cruise speed: 307 km/h; 191 mph (166 kn) at 75% power (5,000 ft (1,500 m))
  • Stall speed: 102 km/h; 63 mph (55 kn) with full flaps
  • Never exceed speed: 435 km/h; 270 mph (235 kn)
  • Range: 1,537 km; 955 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[8]
  • Service ceiling: 5,486 m (18,000 ft)
  • g limits: +6/-4G
  • Rate of climb: 6.5 m/s (1,280 ft/min)

Avionics

See also

Aircraft of comparable role, configuration and era

References

  1. Grob Aircraft (undated). "The basic training aircraft success story". Retrieved 20 March 2012. 
  2. Grob Aircraft (undated). "G 120 TP – The intelligent training solution of the 21st century". Retrieved 20 March 2012. 
  3. "Indonesian win launches Grob's G120TP". FlightGlobal. 2011-09-19. Retrieved 2012-04-01. 
  4. 4.0 4.1 4.2 "Customers Worldwide". Grob Aircraft, Retrieved 1 September 2012.
  5. Grob G120A Basic Trainer Aircraft, Germany,
  6. Augsburger Allgemeine (German regional daily)
  7. Jackson 2003, pp. 166–167.
  8. 8.0 8.1 8.2 Grob Aircraft (undated). "Grob 120A Technical Specifications". Retrieved 20 March 2012. 
  • Grob G 115,120 and 140 Information brochure and Technical Datasheet (Grob Aerospace Sales Department, 2004)
  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. ISBN 0-7106-2537-5.

External links

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