Credit
Raimond Spekking · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AW119Kx · Length
Single source12.92 m (42 ft 5 in)[source]
Length
Configuration
| Specification | AgustaWestland AW119 Koala | UH-1Y Venom |
|---|---|---|
| Type | Utility helicopter[source] | Utility helicopter[source] |
| Manufacturer | Leonardo , previously Finmeccanica, AgustaWestland , Agusta[source] | Bell Textron[source] |
| Status | In production[source] | In service[source] |
| Primary users | State of Mexico Government Finnish Border Guard Portuguese Air Force United States Navy[source] |
58 ft 4 in (17.78 m)[source]
AW119Kx · Range
Single source954 km (593 mi, 515 nmi)[source]
with 2,182 lb (990 kg) payload
Single source130 nmi (150 mi, 240 km) with 2,182 lb (990 kg) payload[source]
AW119Kx · 1 × Pratt & Whitney Canada PT6 B-37A turboshaft engine 917shp
Single source1 × Pratt & Whitney Canada PT6 B-37A turboshaft engine, 747 kW (1,002 hp) 917shp[source]
2 × General Electric T700-GE-401C turboshaft , 1,828 shp ( ) each for 2 minutes 30 seconds
Single source2 × General Electric T700-GE-401C turboshaft , 1,828 shp (1,363 kW) each for 2 minutes 30 seconds[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Marine Corps Czech Air Force[source]
| Number built | ~300 (2018)[source] | 160[source] |
|---|
| Manufactured | 2000–present[source] | 2001–present[source] |
|---|
| Introduction date | 2000[source] | 8 August 2008[source] |
|---|
| First flight | February 1995[source] | 20 December 2001[source] |
|---|
| Developed from | AgustaWestland AW109[source] | Bell UH-1N Twin Huey[source] |
|---|
| Capacity | 6-7 passengers or 1,400 kg (3,086 lb) sling load[source] Crew 1-2 Passengers Up to 6[source] | 6,660 lb (3,021 kg) / up to ten crashworthy passenger seats / six litters / equivalent cargo[source] |
|---|
| Fuel capacity | 3-cell fuel system 605 L (160 US gal) 4-cell fuel system 711 L (188 US gal) 5-cell fuel system 870 L (230 US gal)[source] | — |
|---|
| Main rotor area | 92.1 m 2 (991 sq ft)[source] | 1,808 sq ft (168.0 m 2 )[source] |
|---|
| Never exceed speed | 282 km/h (175 mph, 152 kn)[source] | 198 kn (228 mph, 367 km/h)[source] |
|---|
| Powerplant | 1 x Pratt & Whitney Canada PT6B-37A[source] | — |
|---|
| Country of origin | Italien[source]Country of design · Entwurfsland | — |
|---|
| National origin | — | United States[source] |
|---|
| Blade section | — | Narramore[source] |
|---|