Credit
Jim Duell · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Bell 429 · Length
Single source41 ft 8 in (12.70 m)[source]
Chinook HC6A · Length
Single sourceConfiguration
| Specification | Bell 429 GlobalRanger | Boeing Chinook (UK variants) |
|---|---|---|
| Type | Multipurpose utility helicopter[source] | Transport helicopter[source] |
| National origin | United States/Canada/South Korea[source] | — |
| Manufacturer | Bell Helicopter[source] | Boeing Defense, Space & Security[source] |
| Status | In service[source] | In service[source] |
Chinook / RAF specification (variant not stated) · Length · Length
Single sourceBell 429 · Main rotor diameter
Single source36 ft (11 m)[source]
Bell 429 · pilot
Single source1 pilot[source]
Chinook 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; Bell 429 · Cruise speed
Single source150 kn (170 mph, 280 km/h)[source]
Bell 429 · 2 × Pratt & Whitney Canada PW207D1 (or PW207D2 with fuel heater installed) turboshaft , 625 shp ( ) each maximum continuous
Single source2 × Pratt & Whitney Canada PW207D1 (or PW207D2 with fuel heater installed) turboshaft , 625 shp (466 kW) each maximum continuous[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 | Canadian Coast Guard Royal Australian Navy (historical) Swedish Police Delaware State Police[source] | — |
|---|
| Number built | 500 (July 2024)[source] | 72 (all RAF models)[source] |
|---|
| Manufactured | 2007–present[source] | — |
|---|
| Introduction date | 2009[source] | 22 November 1980 (with RAF)[source] |
|---|
| First flight | February 27, 2007[source] | 23 March 1980 (HC1)[source] |
|---|
| Developed from | Bell 427[source] | Boeing CH-47 Chinook[source] |
|---|
| Capacity | 7 passengers (six in passenger compartment; one beside pilot) / 2,755 lb (1,250 kg) payload[source] | 55 soldiers and up to 10 tonnes of freight or equipment[source] |
|---|
| Cabin volume | 204 ft 3 (5.78 m 3 )[source] | — |
|---|
| Fuel capacity | 215 US gal (179 imp gal; 814 L) usable with 40 US gal (33 imp gal; 151 L) auxiliary fuel[source] | — |
|---|
| Main rotor area | 1,018 sq ft (94.6 m 2 )[source] | 5,655.2 sq ft (525.39 m 2 )[source] |
|---|
| Blade section | - Narramore[source] | - root: Boeing VR-7; tip: Boeing VR-8[source] |
|---|
| Never exceed speed | 155 kn (178 mph, 287 km/h)[source] | — |
|---|
| Hover ceiling IGE | 14,130 ft (4,307 m)[source] | — |
|---|
| Hover ceiling OGE | 11,280 ft (3,438 m)[source] | — |
|---|
| Designer | — | Boeing-Vertol[source] |
|---|
| Primary user | — | Royal Air Force[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 |
|---|
| 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 |
|---|
Maximum take-off; Chinook HC6A · Max takeoff weight
Single source