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Grob G115E Basic Trainer Aircraft

Role

Trainer Aircraft

Crew

Two

Maiden Flight

November 1985

Introduced

1999

Length

7.54m

Wingspan

10m

Height

2.4m

Wing Area

12.2m²

Empty Weight

685kg

Maximum Take-Off Weight

990kg

Maximum Landing Weight

990kg

Maximum Usable Fuel Capacity

103kg

Maximum Crew Weight

320kg

Maximum Baggage Weight

55kg

Type

Lycoming AEIO-360-B1F/B Piston Engine

Numbers of Engines

One

Power Capacity

180hp (139kW)

Propeller

Three bladed Hoffmann or MT-Propeller

Maximum Speed

343km/h

Cruise Speed

230km/h

Stall Speed

96km/h

Range

1,150km

Service Ceiling

3,050m

Rate of Climb

5.3m/s

Endurance

6.2 hours

Take-Off Distance

461m

Landing Distance

457m

Manufacturer

Grob Aircraft

Operators

Royal Air Force, Royal Navy and Egyptian Air Force

Engines

Textron Lycoming Engines

Propeller

MT Propellers

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