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 | Thai Aviation Industries RTAF-6 |
|---|---|---|
| Type | Basic trainer[source] | Trainer aircraft[source] |
| Manufacturer | Grob Aircraft[source] | Thai Aviation Industry[source] |
| Status | active[source] | In service, in production[source] |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | — |
8.35 m (27.39 ft)[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]
1 × Allison 250 -B17-D turboprop
Single source1 × Allison 250 -B17-D turboprop , 313 kW (420 hp)[source]
G 115E · Wing area
Single source12.21 m 2 (131.4 sq ft)[source]
G 115E · 1,050 ft/min
Single source5.3 m/s (1,050 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1985–present[source] | 2014–present[source] |
|---|
| Introduction date | 1999[source] | 2014[source] |
|---|
| First flight | November 1985[source] | 14 June 2012[source] |
|---|
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | — |
|---|
| Aspect ratio | 8.2:1[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] | — |
|---|
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[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 | — |
|---|
| National origin | — | Thailand[source] |
|---|
| Primary user | — | Royal Thai Air Force[source] |
|---|
| Number built | — | 3 (2017), 25 reported built[source] |
|---|
| Developed from | — | SIAI-Marchetti SF.260[source] |
|---|
| Hardpoints | — | 4 with a capacity of up to 68 kg (150 lb) on inner, 100 lb (45 kg) on outer[source] |
|---|