Credit
Alan Wilson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
Length
Single sourceConfiguration
| Specification | Grob G 115 | Tecnam P2006T |
|---|---|---|
| Type | Basic trainer[source] | — |
| Manufacturer | Grob Aircraft[source] | Tecnam[source]P2006T |
| Status | active[source] | — |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | — |
| Manufactured | 1985–present[source] | 2007–present |
8.7 m (28 ft 7 in)[source]
G 115E · 1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)[source]
2 × Rotax 912isc 3 Sport horizontally opposed four-cylinder geared piston engines each
Single source2 × Rotax 912isc 3 Sport horizontally opposed four-cylinder geared piston engines , 75 kW (100 hp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Introduction date | 1999[source] | June 2009[source]P2006T |
|---|
| First flight | November 1985[source] | 13 September 2007[source]P2006T |
|---|
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | 200 litres (44 imp gal; 53 US gal)[source] |
|---|
| Aspect ratio | 8.2:1[source] | 8.80[source] |
|---|
| Airfoil | Eppler 696[source] | — |
|---|
| Propellers | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] | 2-bladed MT Propeller MTV-21, 1.78 m (5 ft 10 in) diameter constant-speed, fully feathering[source] |
|---|
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] | 104 km/h (64 mph, 56 kn)[source] |
|---|
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | — |
|---|
| g limits | + 6.0/ - 3.0[source] | — |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
|---|
| Role | — | Light twin-engine utility aircraft / multi-engine trainer[source]P2006T |
|---|
| National origin | — | Italy[source]P2006T |
|---|
| Designer | — | Luigi Pascale[source]P2006T |
|---|
| Number built | — | Over 400 (as of 2025)[source]P2006T |
|---|
| Developed into | — | NASA X-57 Maxwell[source]P2006T |
|---|
| Capacity | — | 3 passengers[source] |
|---|