Credit
Airwolfhound from Hertfordshire, UK · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
AW149 · Length
Single source17.57 m (57 ft 8 in)[source]
Chinook HC6A · Length
Single sourceConfiguration
| Specification | AgustaWestland AW149 | Boeing Chinook (UK variants) |
|---|---|---|
| Type | Medium-lift military helicopter[source] | Transport helicopter[source] |
| National origin | Italy[source] | — |
| Manufacturer | AgustaWestland Finmeccanica Leonardo S.p.A.[source] | Boeing Defense, Space & Security[source] |
| Status | In service[source] | In service[source] |
Chinook / RAF specification (variant not stated) · Length · Length
Single sourceAW149 · Width
Single source3.06 m (0 in)[source]
AW149 · Main rotor diameter
Single source14.6 m (47 ft 11 in)[source]
AW149 · Diameter
Single source14.60 m (47 ft 11 in)[source]
Maximum take-off; AW149 · Max takeoff weight
Single source8,600 kg (18,960 lb)[source]
AW149 · Crew
Single sourceChinook HC6A · pilot, copilot, two weapon system operators/loadmasters
Single source4 (pilot, copilot, two weapon system operators/loadmasters)[source]
2 Pilots, 2 Weapon System Operators[source]Chinook / RAF specification (variant not stated) · AircrewSource text · numeric interpretation needs review
Cruise; AW149 · Cruise speed
Single sourceMaximum; AW149 · Maximum speed
Single source310 km/h (190 mph, 170 kn)[source]
278 km/h (173 mph, 150 kn)[source]
Maximum; Chinook HC6A · Maximum speed
Single sourceMaximum; Chinook / RAF specification (variant not stated) · Maximum speed · Maximum speed
Single sourceAW149 · 2 × Safran Aneto -1K each Maximum continuous power
Single source2 × Safran Aneto -1K , 1,715 kW (2,300 hp) each Maximum continuous power[source]
Chinook HC6A · 2 × Honeywell T55-GA-714A turboshaft free-turbine engines, 3,750 shp ( ) each
Single source2 × Honeywell T55-GA-714A turboshaft free-turbine engines, 3,750 shp (2,800 kW) each[source]
Chinook HC6A · 1,980 ft/min ( )Thrust 2x 4,168shp each engine
Single source1,980 ft/min (10.1 m/s)Thrust 2x 4,168shp each engine[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Egyptian Navy Royal Thai Army Polish Army[source] | — |
|---|
| Manufactured | 2009–present[source] | — |
|---|
| First flight | 13 November 2009[source] | 23 March 1980 (HC1)[source] |
|---|
| Developed from | AgustaWestland AW139[source] | Boeing CH-47 Chinook[source] |
|---|
| Variant | AgustaWestland AW189[source] | — |
|---|
| Developed into | Leonardo Helicopters AW249[source] | — |
|---|
| Capacity | 19 troops with light equipment, 16 combat laden troops[source] | 55 soldiers and up to 10 tonnes of freight or equipment[source] |
|---|
| Endurance | five hours and five minutes[source] | — |
|---|
| Hardpoints | four, with the following combinations:[source] | — |
|---|
| Volume | 11.2 m 3 (400 cu ft) for the cab, 2.4 m 3 (85 ft 3 ) for stowage[source] | — |
|---|
| Useful lift | 3,880 kg (8,550 lb) useful load, 2,800 kg (6,200 lb) for the cargo hook[source] | — |
|---|
| Rockets | FZ231 pod with 12 × 70 mm rocket[source] | — |
|---|
| Missiles | a multi-launcher pod capable of 4 × AGM-114 Hellfire II[source] | — |
|---|
| Designer | — | Boeing-Vertol[source] |
|---|
| Primary user | — | Royal Air Force[source] |
|---|
| Number built | — | 72 (all RAF models)[source] |
|---|
| Introduction date | — | 22 November 1980 (with RAF)[source] |
|---|
| Variants | — | HC1, HC1B, HC2, HC3, HC4, HC5, HC6, HC6A, HC7[source] |
|---|
| Guns | — | 2× M134 Miniguns and 1× M60 machine gun[source] 2 x M134 Miniguns, 1 x M60 Machine Gun[source]Chinook / RAF specification (variant not stated) · Guns |
|---|
| Main rotor area | — | 5,655.2 sq ft (525.39 m 2 )[source] |
|---|
| Blade section | — | - root: Boeing VR-7; tip: Boeing VR-8[source] |
|---|
| Cockpit Avionics | — | Glass cockpit with a BAE Systems Digital Advanced Flight Control System (DAFCS), includes automatic modes such as auto-hover and auto-descend to ease pilot workload.[source] |
|---|
| Sensors | — | Electro-Optical Sensor Turret (EOST) with two infrared cameras and a low-light TV function .[source] EOST turret including two infrared cameras and a low-light TV function[source]Chinook / RAF specification (variant not stated) · Electro optics |
|---|
| Defensive Aids | — | Missile Warning Receiver, Infrared Warning Receiver, Radar Warning Receiver, Counter-measure dispensing system (flares).[source] |
|---|
| Country of origin | — | United States[source]Boeing Chinook (UK variants) · origin explicitly stated in the linked current national-inventory row; no inference from operator or shipyard |
|---|
| Powerplant | — | Two Honeywell 55-L-714A Free-Turbine engines[source]Chinook / RAF specification (variant not stated) · Powerplant |
|---|
| Reported engine rating | — | 4,168shp each[source]Chinook / RAF specification (variant not stated) · ThrustSource text · numeric interpretation needs review |
|---|
| Flight altitude | — | 15,000ft[source]Chinook / RAF specification (variant not stated) · Maximum altitude |
|---|