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At a glance
Measured figures
Length
Single source8.05 m (26 ft 5 in)[source]
G 115E · Length
Single sourceConfiguration
| Specification | Aeromot AMT-200 Super Ximango | Grob G 115 |
|---|---|---|
| Type | Motor glider[source] | Basic trainer[source] |
| National origin | Brazil[source] | — |
| Manufacturer | Aeromot[source] | Grob Aircraft[source] |
| Designer | René Fournier[source] | — |
| Number built | 126 (2009) |
7.79 m (25 ft 7 in)[source]
1 × Rotax 914 -S4 piston engine
Single source1 × Rotax 914 -S4 piston engine, 60 kW (80 hp)[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Introduction date | 1993[source] | 1999[source] |
|---|
| Developed from | AMT-100 Ximango[source] | — |
|---|
| Aspect ratio | 16[source] | 8.2:1[source] |
|---|
| Airfoil | NACA 64 3 -618[source] | Eppler 696[source] |
|---|
| Fuel capacity | 90 L (24 US gal; 20 imp gal)[source] | 143 L (31 imp gal; 38 US gal) usable[source] |
|---|
| Propellers | 2-bladed Hoffmann HO-V62R/170FA , 1.70 m (5 ft 7 in) diameter[source] | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] |
|---|
| Stall speed | 76 km/h (47 mph, 41 kn)[source] | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] |
|---|
| Never exceed speed | 245 km/h (152 mph, 132 kn)[source] | 341 km/h (212 mph, 184 kn)[source] |
|---|
| Maximum glide ratio | 31[source] | — |
|---|
| Rate of sink | .93 m/s (183 ft/min)[source] | — |
|---|
| Wing loading | 45.3 kg/m 2 (9.3 lb/sq ft)[source] | — |
|---|
| 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] |
|---|
| First flight | — | November 1985[source] |
|---|
| g limits | — | + 6.0/ - 3.0[source] |
|---|
| Country of origin | — | Deutschland[source]Country of design · Entwurfsland |
|---|