Sikorsky

Manufacturer:

Sikorsky

Country:

USA

Commercial designation:

S-76

Technical designation:

S-76

Version, Variant:

D

Type:

Conventional

Currently produced:

Y

Typical missions:

ALL

Flight conditions:

IFR

First flight:

0

Landing system:

wheels

Blades number:

4

Tail blades number:

4

MTOW with external loads:

0 kg

0 lbs

MTOW with only internal loading:

5306 kg

11699.73 lbs

Empty weight:

3269 kg

7208.145 lbs

External payload:

0 kg

0 lbs

Internal payload:

2037 kg

4491.585 lbs

Standard fuel tank:

893 kg

1969.065 lbs

with optionnal external fuel tank:

309 kg

681.345 lbs

Cruise speed:

267 km/h

144.18 kt

Maximum cruise speed:

285 km/h

153.9 kt

Vne:

287 km/h

154.98 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

818 km

441.72 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:25:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

2957 m

9698.96 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

1524 m

4998.72 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

4572 m

14996.16 ft

Max operating altitude, empty weight:

4575 m

15006 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Pratt & Whitney

Model:

PW210S

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

410 kg/kW/h

672.4 lbs/hp/h

Minimum consumption speed @ SL:

135 km/h

72.9 kt

Fuel consumption @ eco cruise speed @SL:

410 kg/h

904.05 lbs/h

Fuel consumption @ min consumption speed @ SL:

295 kg/h

650.475 lbs/h

Engines nominal power:

1574 kW

2139.066 hp

Transmission shaft max continuous power:

1440 kW

1956.96 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

1606 kW

2182.554 hp

OEI 30s power:

924 kW

1255.716 hp

OEI 2min power:

883 kW

1199.997 hp

OEI max continuous power :

803 kW

1091.277 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

16 m

52.48 ft

Rotor diameter:

13.41 m

43.9848 ft

Tail rotor diameter:

2.438 m

7.99664 ft

Fuselage length:

13.21 m

43.3288 ft

Overall height:

4.39 m

14.3992 ft

Main rotor blades chord:

0.39 m

1.2792 ft

Tail rotor blades chord:

0.16 m

0.5248 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

2

Max pax number:

13

Average price:

0 $