
Loading the evidence…
Preparing your view.
Preparing your view.


At a glance
Measured figures
AS550 C3 · fuselage length
Single sourceAS550 C3 · overall length, rotors turning
Single sourceConfiguration
| Specification | Eurocopter Fennec | Sikorsky S-92 |
|---|---|---|
| Type | Light utility military helicopter[source] | Medium-lift transport/utility helicopter[source] |
| National origin | France[source] | United States[source] |
| Manufacturer | Aérospatiale Eurocopter Airbus Helicopters[source] | Sikorsky Aircraft[source] |
| Status | In service[source] |
10.93 m (35 ft 10 in) (fuselage length), 12.94 m (42 ft 6 in) (overall length, rotors turning)[source]
S-92 · Length
Single source68 ft 6 in (20.88 m)[source]
S-92 · fuselage
Single source17 ft 3 in (5.26 m) fuselage[source]
AS550 C3 · 1 × Turbomeca Arriel 2B turboshaft 847 shp) (limited to
Single sourceAS550 C3 · 671 shp for take-off
Single source1 × Turbomeca Arriel 2B turboshaft , 632 kW (847 shp) (limited to 500 kW (671 shp for take-off))[source]
S-92 · 2 × General Electric CT7-8A turboshaft engines, 2,520 shp ( ) each
Single source2 × General Electric CT7-8A turboshaft engines, 2,520 shp (1,880 kW) each[source]
AS550 C3 · 2,028 ft/min
Single source10.30 m/s (2,028 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source] |
| Primary users | French Army Light Aviation French Air and Space Force Argentine Naval Aviation Royal Danish Air Force Indonesian Army Aviation Center Royal Malaysian Navy Aviation Pakistan Army Aviation Corps[source] | CHC Helicopter Petroleum Helicopters International Bristow Helicopters Cougar Helicopters[source] |
|---|
| Manufactured | 1990–present[source] | 1998–present[source] |
|---|
| Introduction date | 1990[source] | 2004[source] |
|---|
| Developed from | Eurocopter AS350 Écureuil Eurocopter AS355 Écureuil 2[source] | Sikorsky S-70[source] |
|---|
| Capacity | 4 passengers[source] | 19 passengers[source] |
|---|
| Fuel capacity | 540 L (143 US Gal)[source] | — |
|---|
| Main rotor area | 89.75 m 2 (966.1 sq ft) Royal Thai Army AS550 armed with .50" HMP POD[source] | 2,492.3 sq ft (231.54 m 2 )[source] |
|---|
| Never exceed speed | 287 km/h (178 mph, 155 kn)[source] | — |
|---|
| Source measurement | Twelve AS550 C2helicopters were purchased by the Royal Danish Air Force in 1987, with the first helicopters delivered on August 1990. Due to a change in the geopolitical environment following the collapse of the Soviet Union and the end of the Cold War , the Fennec helicopters were gradually repurposed for other tasks, primarily observation and light transport duties. In 2003, they were primarily employed by the Eskadrille 724 . In 2002, 3 Danish Fennec helicopters were deployed to Macedonia during Operation Amber Fox . In December 2005, Fennec helicopters were deployed to support the Danish forces in Iraq and from August 2007, 4 more were deployed to the troubled country as a replacement for the withdrawn ground troops. In 2008, 4 Fennec helicopters were deployed to the Danish forces in Afghanistan . As a result of various defense agreements, the number of active Fennecs in the Air Force has been reduced to 8 in 2006.[source]Eurocopter Fennec · Operational history; only the objects and conditions stated in this passage AS555 AN Fennec 2 – Armed military version, can be fitted with a 20 mm cannon.[source]Eurocopter Fennec · Variants; only the objects and conditions stated in this passage Capacity: 4 passengers[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Length: 10.93 m (35 ft 10 in) (fuselage length), 12.94 m (42 ft 6 in) (overall length, rotors turning)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Height: 3.34 m (10 ft 11 in)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Empty weight: 1,220 kg (2,690 lb)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Max takeoff weight: 2,250 kg (4,960 lb)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Powerplant: 1 × Turbomeca Arriel 2B turboshaft , 632 kW (847 shp) (limited to 500 kW (671 shp for take-off))[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Main rotor diameter: 10.69 m (35 ft 1 in)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Main rotor area: 89.75 m 2 (966.1 sq ft) Royal Thai Army AS550 armed with .50" HMP POD[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Maximum speed: 246 km/h (153 mph, 133 kn) (max cruise)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Never exceed speed : 287 km/h (178 mph, 155 kn)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Range: 648 km (403 mi, 350 nmi)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Service ceiling: 5,280 m (17,320 ft)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Rate of climb: 10.30 m/s (2,028 ft/min)[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage 20 mm Giat M621 cannon[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage Fabrique Nationale de Herstal twin 7.62 mm or 12.7 mm machine gun pods[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage 7 x 70mm (2.75") Forges de Zeebrugge rocket launcher FZ220 or 12 x 68 mm Thales Brandt rockets[source]Eurocopter Fennec · Specifications (AS550 C3); only the objects and conditions stated in this passage | — |
|---|
| Number built | — | at least 300[source] |
|---|
| First flight | — | December 23, 1998[source] |
|---|
| Variants | — | Sikorsky CH-148 Cyclone Sikorsky VH-92[source] |
|---|
| Cabin dimensions | — | 20 ft (6 m) long by 6.6 ft (2 m) tall[source] |
|---|
| Blade section | — | - root: Sikorsky SC2110; tip: Sikorsky SSC-A09[source] |
|---|
| Disk loading | — | 9.8 lb/sq ft (48 kg/m 2 )[source] |
|---|
| Power/mass | — | 0.23 hp/lb (0.38 kW/kg)[source] |
|---|
Maximum take-off; S-92 · Max takeoff weight
Single source