Credit
Alan Wilson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
Hürkuş-1 · Length
Single sourceConfiguration
| Specification | Grob G 115 | TAI Hürkuş |
|---|---|---|
| Type | Basic trainer[source] | Basic/advanced trainer aircraft Light attack aircraft[source] |
| Manufacturer | Grob Aircraft[source] | Turkish Aerospace Industries[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] | — |
11.17 m (36 ft 8 in)[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · Maximum speed
Single source250 km/h (160 mph, 130 kn)[source]
178 km/h (111 mph, 96 kn) (long range cruising speed)[source]
Cruise; Hürkuş-1 · Cruise speed
Single sourceMaximum; Hürkuş-1 · Maximum speed
Single sourceG 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]
Hürkuş-1 · 1 × Pratt & Whitney Canada PT6A-68T turboprop aircraft engine 1,600 shp
Single source1 × Pratt & Whitney Canada PT6A-68T turboprop aircraft engine , 1,200 kW (1,600 shp)[source]
G 115E · Wing area
Single source12.21 m 2 (131.4 sq ft)[source]
Hürkuş-1 · at 15000 ft (4572 m)
Single source4.25 hours at 15000 ft (4572 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured |
|---|
1985–present[source] |
| — |
| Introduction date | 1999[source] | — |
|---|
| First flight | November 1985[source] | Hürkuş-1: 29 August 2013 Hürkuş-2: 30 December 2024[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] | 5-bladed Hartzell Propeller HC-B5MA-3[source] |
|---|
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] | 143 km/h (89 mph, 77 kn)[source] |
|---|
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | — |
|---|
| g limits | + 6.0/ - 3.0[source] | +7/-3.5[source] |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
|---|
| National origin | — | Turkey[source] |
|---|
| Primary user | — | Turkish Air Force[source] |
|---|
| Capacity | — | one passenger[source] |
|---|
| Guns | — | 12.7 mm gun pods, 20 mm cannon pods[source] |
|---|
| Rockets | — | Roketsan Cirit , 2.75-inch rockets[source] |
|---|
| Missiles | — | Roketsan UMTAS[source] |
|---|
| Bombs | — | Mk-81 with LGK-81, Mk-82 , Tübitak SAGE HGK-3 (82) , Tübitak SAGE KGK-82, BDU33, MK106 training ordnance, TUBITAK-SAGE TOGAN, TUBITAK-SAGE BOZOK and MAM (Smart Micro Munition)[source] |
|---|