FORCETALLY
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At a glance
Measured figures
MD 600N · Length
Single source35 ft 5 in (10.80 m)[source]
CH-148 Cyclone · Length
Single sourceConfiguration
| Specification | MD Helicopters MD 600 | Sikorsky CH-148 Cyclone |
|---|---|---|
| Type | Light utility helicopter[source] | Maritime helicopter[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | McDonnell Douglas Helicopter Systems MD Helicopters[source] | Sikorsky Aircraft[source] |
| Status | In service[source] |
Length
Single sourcefuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
MD 600N · 1 × Allison Model 250-C47 turboshaft engine, 600 shp (
Single source1 × Allison Model 250-C47 turboshaft engine, 600 shp (450 kW)[source]
2 × General Electric CT7-8A7 turboshaft engines, 3,000 shp ( ) each
Single source2 × General Electric CT7-8A7 turboshaft engines, 3,000 shp (2,200 kW) each[source]
MD 600N · 2,070 ft/min (
Single source2,070 ft/min (10.5 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| Primary user | United States Border Patrol[source] | Royal Canadian Air Force[source] |
|---|
| Manufactured | 1995–present[source] | — |
|---|
| First flight | 22 November 1994[source] | 15 November 2008[source] |
|---|
| Developed from | MD Helicopters MD 500[source] | Sikorsky S-92[source] |
|---|
| Capacity | 8 total[source] | 6 in mission configuration, up to 22 in utility configuration.[source] 22 passengers[source] |
|---|
| Main rotor area | 594.03 sq ft (55.187 m 2 )[source] | 2,650 sq ft (246 m 2 ) S-92[source] |
|---|
| Blade section | - NACA 0012[source] | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09 - S-92[source] |
|---|
| Role | light utility civilian helicopter[source] | — |
|---|
| Source measurement | Length: 35 ft 5 in (10.80 m)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Height: 8 ft 9 in (2.67 m)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Empty weight: 2,100 lb (953 kg)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Max takeoff weight: 4,100 lb (1,860 kg)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Powerplant: 1 × Allison Model 250-C47 turboshaft engine, 600 shp (450 kW)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Main rotor diameter: 27 ft 6 in (8.38 m)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Main rotor area: 594.03 sq ft (55.187 m 2 )[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Maximum speed: 152 kn (175 mph, 282 km/h)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Cruise speed: 135 kn (155 mph, 250 km/h)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Range: 357 nmi (411 mi, 661 km)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Service ceiling: 18,700 ft (5,700 m)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage Rate of climb: 2,070 ft/min (10.5 m/s)[source]MD Helicopters MD 600 · Specifications (MD 600N); only the objects and conditions stated in this passage | — |
|---|
| Number built | — | 28[source] |
|---|
| Introduction date | — | July 2018[source] |
|---|
| Folded Length | — | 14.78 m (48.5 ft)[source] |
|---|
Maximum take-off; Max takeoff weight
Single source15,600 lb (7,076 kg) S-92[source]
29,300 lb (13,290 kg)[source]
13,000 kg[source]CH-148 Cyclone · Maximum gross weight
Maximum; Maximum speed
Single source