
Loading the evidence…
Preparing your view.
Preparing your view.


At a glance
Measured figures
T-5 · Length
Single source8.4 m (27 ft 7 in)[source]
G 115E · Length
Single sourceConfiguration
| Specification | Fuji T-5 | Grob G 115 |
|---|---|---|
| Type | Basic trainer[source] | Basic trainer[source] |
| Manufacturer | Fuji Heavy Industries[source] | Grob Aircraft[source] |
| Primary user | Japan Maritime Self-Defense Force[source] | — |
| Introduction date | 1988[source] | 1999[source] |
| First flight |
7.79 m (25 ft 7 in)[source]
Cruise; T-5 · Cruise speed
Single sourceMaximum; T-5 · at 2,440 m (8,005 ft)
Single source357 km/h (222 mph, 193 kn) at 2,440 m (8,005 ft)[source]
287 km/h (178 mph, 155 kn)[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · Maximum speed
Single sourceT-5 · 1 × Allison Model 250-B17D turboprop
Single source1 × Allison Model 250-B17D turboprop , 261 kW (350 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.
28 June 1984[source] |
November 1985[source] |
| Developed from | Fuji KM-2[source] | — |
|---|
| Airfoil | root: NACA 23016.5 ; tip: NACA 23012[source] | Eppler 696[source] |
|---|
| Propellers | 3-bladed constant-speed propeller[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)[source] | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] |
|---|
| Never exceed speed | 413 km/h (257 mph, 223 kn)[source] | 341 km/h (212 mph, 184 kn)[source] |
|---|
| National origin | Japan[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] |
|---|
| Fuel capacity | — | 143 L (31 imp gal; 38 US gal) usable[source] |
|---|
| Aspect ratio | — | 8.2:1[source] |
|---|
| g limits | — | + 6.0/ - 3.0[source] |
|---|
| Country of origin | — | Deutschland[source]Country of design · Entwurfsland |
|---|