Credit
John Davies · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
CH-146 Griffon · Length
Single sourceCH-146 · Length
Single sourceConfiguration
| Specification | Bell CH-146 Griffon | TAI T625 Gökbey |
|---|---|---|
| Type | Utility helicopter[source] | Utility helicopter[source] |
| National origin | United States / Canada[source] | Turkey[source] |
| Manufacturer | Bell Helicopter[source] | Turkish Aerospace Industries[source] |
| Status | In service[source] | In service |
56 ft 1 in (17.09 m)[source]
17.1 m[source]CH-146 Griffon
17.1 m[source]CH-146 Griffon
17.1 m[source]CH-146 Griffon
Length
Single source15.87 m (52 ft 1 in)[source]
Gross; CH-146 Griffon · Gross weight · Maximum gross weight
Single sourceMaximum take-off; CH-146 · Max takeoff weight
Single source11,900 lb (5,398 kg)[source]
5,400 kg[source]CH-146 Griffon · Maximum gross weight
Maximum take-off; Max takeoff weight
Single source6,050 kg (13,338 lb)[source]
Cruise; CH-146 · Cruise speed
Single sourceMaximum; CH-146 Griffon · Maximum speed
Single sourceMaximum; CH-146 · Maximum speed
Single source140 kn (160 mph, 260 km/h)[source]
118 kn (136 mph, 219 km/h)[source]
260 km/h[source]CH-146 Griffon
260 km/h[source]CH-146 Griffon
260 km/h[source]CH-146 Griffon
Cruise; Cruise speed
Single sourceMaximum; Maximum speed
Single sourceCH-146 · 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac coupled turboshaft engine, 1,250 shp (
Single source1 × Pratt & Whitney Canada PT6T-3D Twin-Pac coupled turboshaft engine, 1,250 shp (930 kW)[source]
2 × LHTEC CTS800-4A , ( TEI TS1400 - undergoing testing / scheduled for 2027) turboshaft engine each
Single source2 × LHTEC CTS800-4A , ( TEI TS1400 - undergoing testing / scheduled for 2027) turboshaft engine, 1,024 kW (1,373 hp) each[source]
Service ceiling
Single source6,096 m (20,000 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | Royal Canadian Air Force[source] | — |
|---|
| Number built | 100 (85 in service)[source] | 4 prototypes built for tests + 7 Delivered to Turkish Armed Forces[source] |
|---|
| Manufactured | 1992–1997[source] | — |
|---|
| Introduction date | 1995[source] | 29 October 2024[source] |
|---|
| First flight | 1992[source] | 6 September 2018[source] |
|---|
| Developed from | Bell 412[source] | — |
|---|
| Capacity | 10 troops or 6 stretchers (some sources state maximum 8 passengers)[source] | 12 passengers(Included Crew)[source] |
|---|
| Main rotor area | 1,662 sq ft (154.4 m 2 )[source] | — |
|---|
| Blade sections | - root Boeing VR-7; tip Wortmann FX 71-H-080[source] | — |
|---|
| Designer | — | Aselsan Turkish Aerospace Industries[source] |
|---|
| Primary users | — | Turkish Armed Forces Gendarmerie General Command[source] |
|---|