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Quote for Grob G 120A Parts

Have you been in search of parts and components for the Grob G 120A and similar aircraft? The Grob G 120A is a piston powered trainer aircraft, designed and manufactured by Grob Aircraft. First introduced in 1999 and beginning manufacturing in the same year, the Grob G 120A still remains in active service under operators such as the Mexican Air Force, Kenya Air Force, Israeli Air Force, Royal Canadian Air Force, and French Air Force. The Grob G 120A features a low-wing configuration, and its airframe is composed of carbon composites. As a trainer, the 120A is mostly utilized for both military and civil pilot training.

Aircraft Model Grob G 120A Details

Model No : Grob G 120A
Aircraft Type : Aerobatic
Manufacturer : Grob Aircraft
Country : Germany
Manufactured : 2005 to: Present
ICAO : NA
Avionics : NA
Engine : 1 × Lycoming AEIO-540-D4D5 6-cylinder
Power : 260 horse[Power]
Max Cruise Speed : 106 knots - 196 Km/h
Approach Speed : NA
Travel Range : NA
Fuel Economy : 14.3 nautical mile / gallon - 6.996 kilometres / litre
Service Ceiling : NA
Rate of Climb : NA
Take Off Distance : 199 metre - 652.88 feet
Landing Distance : 171 metre - 561.02 feet
Max Tak eOff Weight : 3,175 Kg - 7,000 lbs
Max Payload : 163 Kg - 359 lbs
Fuel Tank Capacity : NA
Baggage Volume : NA
Seats Economy/General Class : 2 seats
Seats Business Class : 0
Seats First Class : 0
Cabin Height : NA
Cabin Width : NA
Cabin Length : NA
Exterior Length : NA
Tail Height : NA
Fuselage Diameter : NA
Wing Span Rotor Diameter : NA
Wing Tips : NA
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With a single Lycoming AEIO-540-D4D5 air-cooled flat-six engine producing 260 horsepower, the Grob G 120A can travel at a maximum speed of 172 knots. The aircraft also features a fuel tank capacity of 68 gallons, permitting a travel range of 830 nautical miles. As a two-seat aircraft, two individuals are required for the piloting of the aircraft. With the crew members, fuel, and cargo altogether, the Grob G 120A may perform with a maximum takeoff weight of 3,285 pounds.

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