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Grob G120A Basic Trainer Aircraft

Crew

Two

Maiden Flight

1999

Entry into Service

2001

Length

8.11m

Wingspan

10.18m

Height

2.66m

Wing Area

13.3m²

Empty Weight

1,345kg

Maximum Take-Off Weight

1,490kg

Maximum Landing Weight

1,440kg

Maximum Crew or Boarding Weight

220kg

Maximum Baggage Weight

50kg

Maximum Usable Fuel Capacity

182kg

Type

Lycoming AEIO-540-D4D5 Piston Engine

Number of Engines

One

Power Capacity

194kW

Propeller

Hartzell 3-Bladed Constant Speed

Maximum Speed

435km/h

Cruise Speed

318km/h

Stall Speed

103km/h

Range

1,352km

Service Ceiling

5,486m

Rate of Climb

6.5m/s

Endurance

6.35 hours

Take-Off Distance

707m

Landing Distance

562m

Manufacturer

Grob Aircraft

Operators

German Armed Forces and Canadian Armed Forces

Engines

Textron Lycoming Engines

Propellers

Hartzell Propellers

Global Positioning System (GPS)

Garmin

Electronic Flight Instrumentation System (EFIS)

Elbit Systems

Cockpit Seats

Martin Baker
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