FORCETALLY
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At a glance
Measured figures
T-7 · Length
Single source8.59 m (28 ft 2 in)[source]
G 115E · Length
Single sourceConfiguration
| Specification | Fuji T-7 | Grob G 115 |
|---|---|---|
| Type | Primary/Basic Trainer[source] | Basic trainer[source] |
| National origin | Japan[source] | — |
| Manufacturer | Fuji Heavy Industries[source] | Grob Aircraft[source] |
| Status | Active[source] | active[source] |
| Primary user | Japan Air Self-Defense Force |
7.79 m (25 ft 7 in)[source]
Cruise; T-7 · at 915 m (3,002 ft)
Single source298 km/h (185 mph, 161 kn) at 915 m (3,002 ft)[source]
G 115E · 45% power at FL 80, 45 min reserves
Single source1,150 km (710 mi, 620 nmi) (45% power at FL 80, 45 min reserves)[source]
T-7 · 1 × Rolls-Royce 250-B17F turboprop engine
Single source1 × Rolls-Royce 250-B17F turboprop engine, 336 kW (451 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]
G 115E · Service ceiling
Single source6,095 m (20,000 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.
| — |
| Number built | 49[source] | — |
|---|
| Manufactured | 2002-present[source] | 1985–present[source] |
|---|
| Developed from | Fuji T-3[source] | — |
|---|
| Airfoil | root: NACA 23016.5 ; tip: NACA 23012[source] | Eppler 696[source] |
|---|
| Propellers | 3-bladed constant-speed propeller, 2.12 m (6 ft 11 in) diameter[source] | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] |
|---|
| Stall speed | 104 km/h (65 mph, 56 kn) flaps and gear down[source] | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] |
|---|
| Wing loading | 96.1 kg/m 2 (19.7 lb/sq ft)[source] | — |
|---|
| Power/mass | 0.2114 kW/kg (0.1286 hp/lb)[source] | — |
|---|
| Take-off distance to 15 m (49 ft) | 608 m (1,995 ft)[source] | — |
|---|
| Landing distance from 15 m (49 ft) | 566 m (1,857 ft)[source] | — |
|---|
| Primary users | — | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] |
|---|
| Introduction date | — | 1999[source] |
|---|
| First flight | — | November 1985[source] |
|---|
| Fuel capacity | — | 143 L (31 imp gal; 38 US gal) usable[source] |
|---|
| Aspect ratio | — | 8.2:1[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 |
|---|