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]
CJ-6A · Length
Single sourceConfiguration
| Specification | Grob G 115 | Nanchang CJ-6 |
|---|---|---|
| Type | Basic trainer[source] | Basic Trainer[source] |
| Manufacturer | Grob Aircraft[source] | Nanchang Aircraft Factory (Hongdu)[source] |
| Status | active[source] | In service[source] |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | People's Liberation Army Air Force Korean People's Army Air Force Bangladesh Air Force Sudanese Air Force |
8.46 m (27 ft 9 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]
CJ-6A · 1 × Zhouzhou (SMPMC) HS-6A radial engine
Single source1 × Zhouzhou (SMPMC) HS-6A radial engine , 213 kW (286 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] | 1958-present[source] |
|---|
| Introduction date | 1999[source] | 1960[source] |
|---|
| First flight | November 1985[source] | August 27, 1958[source] |
|---|
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | — |
|---|
| Aspect ratio | 8.2:1[source] | — |
|---|
| Airfoil | Eppler 696[source] | root: Clark YH (14.5%); tip: Clark YH (9.3%)[source] |
|---|
| Propellers | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] | 2-bladed variable-pitch propeller[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] | 370 km/h (230 mph, 200 kn)[source] |
|---|
| g limits | + 6.0/ - 3.0[source] | — |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
|---|
| Number built | — | 2,000+[source] |
|---|
| Guns | — | 2 x 7.62 mm machine guns[source] |
|---|
| Hardpoints | — | Weapons stations and hardpoints under the wings , with provisions to carry combinations of: Rockets: Rocket launchers Bombs: Bombs[source] |
|---|
| Rockets | — | Rocket launchers[source] |
|---|
| Bombs | — | Bombs[source] |
|---|
| National origin | — | China[source] |
|---|