Eurocopter

Manufacturer:

Eurocopter

Country:

Europe

Commercial designation:

EC135

Technical designation:

EC135

Version, Variant:

P2+

Type:

Fenestron

Currently produced:

N

Typical missions:

Civil Utility Transport Law

Flight conditions:

IFR

First flight:

2006

Landing system:

skids

Blades number:

4

Tail blades number:

10

MTOW with external loads:

2900 kg

6394.5 lbs

MTOW with only internal loading:

2910 kg

6416.55 lbs

Empty weight:

1455 kg

3208.275 lbs

External payload:

1300 kg

2866.5 lbs

Internal payload:

1455 kg

3208.275 lbs

Standard fuel tank:

560 kg

1234.8 lbs

with optionnal external fuel tank:

730 kg

1609.65 lbs

Cruise speed:

230 km/h

124.2 kt

Maximum cruise speed:

254 km/h

137.16 kt

Vne:

259 km/h

139.86 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

635 km

342.9 nm

Max range with auxiliary external tanks:

835 km

450.9 nm

Max endurance @ min consumption speed:

03:35:00 h:min

Rate of climb @ SL:

7.6 m/s

1495.68 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3045 m

9987.6 ft

IGE max hovering altitude, empty:

0 m

0 ft

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

2435 m

7986.8 ft

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

0 m

0 ft

OGE max hovering altitude, MTOW:

2010 m

6592.8 ft

OGE max hovering altitude, empty:

0 m

0 ft

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

1480 m

4854.4 ft

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

0 m

0 ft

Service ceiling ISA, MTOW:

3045 m

9987.6 ft

Max operating altitude, empty weight:

6095 m

19991.6 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-35 °C

-63 °F

APU in HC:

Engine manufacturer:

Pratt & Whitney

Model:

PW206B2

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0.26527 kg/kW/h

0.4350428 lbs/hp/h

Minimum consumption speed @ SL:

120 km/h

64.8 kt

Fuel consumption @ eco cruise speed @SL:

208.5 kg/h

459.7425 lbs/h

Fuel consumption @ min consumption speed @ SL:

164.5 kg/h

362.7225 lbs/h

Engines nominal power:

914 kW

1242.126 hp

Transmission shaft max continuous power:

566 kW

769.194 hp

Transmission shaft max power:

640 kW

869.76 hp

Takeoff power 5 min:

996 kW

1353.564 hp

OEI 30s power:

609 kW

827.631 hp

OEI 2min power:

580 kW

788.22 hp

OEI max continuous power :

528 kW

717.552 hp

OEI max continuous transmission power:

368 kW

500.112 hp

OEI 30 sec transmission power:

526 kW

714.834 hp

OEI 2 min transmission power:

513 kW

697.167 hp

Overall length:

12.16 m

39.8848 ft

Rotor diameter:

10.2 m

33.456 ft

Tail rotor diameter:

1 m

3.28 ft

Fuselage length:

10.2 m

33.456 ft

Overall height:

3.51 m

11.5128 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

84 dB EPNL

Noise at flyover, limit:

93 dB EPNL

Noise at takeoff, level:

88 dB EPNL

Noise at takeoff, limit:

94 dB EPNL

Noise at landing, level:

92 dB EPNL

Noise at landing, limit:

95 dB EPNL

Crew:

1

Max pax number:

7

Average price:

3500000 $