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Airbus Helicopters

EC135 T2+

tags: t2i Civil Utility Transport Law

aircraft

Manufacturer:

Airbus Helicopters

Country:

Europe

Commercial designation:

EC135

Technical designation:

EC135

Version, Variant:

T2+

Type:

Fenestron

Currently produced:

Y

Typical missions:

Civil Utility Transport Law

Flight conditions:

IFR

First flight:

2006

Landing system:

skids

Blades number:

4

Tail blades number:

10

weight

Weight class:

2

MTOW with external loads:

2900 kg

6395 lbs

MTOW with only internal loading:

2910 kg

6417 lbs

Empty weight:

1455 kg

3208 lbs

External payload:

1300 kg

2867 lbs

Internal payload:

1455 kg

3208 lbs

Standard fuel tank:

560 kg

1235 lbs

with optionnal external fuel tank:

730 kg

1610 lbs

performance

Cruise speed:

240 km/h

130 kt

Maximum cruise speed:

254 km/h

137 kt

Vne:

259 km/h

140 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

620 km

335 nm

Max range with auxiliary external tanks:

815 km

440 nm

Max endurance @ min consumption speed:

03:23:00 h:min

Rate of climb @ SL:

7.6 m/s

1496 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3045 m

9988 ft

IGE max hovering altitude, empty:

0 m

0 ft

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

2395 m

7856 ft

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

0 m

0 ft

OGE max hovering altitude, MTOW:

2010 m

6593 ft

OGE max hovering altitude, empty:

0 m

0 ft

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

1450 m

4756 ft

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

0 m

0 ft

Service ceiling ISA, MTOW:

3045 m

9988 ft

Max operating altitude, empty weight:

6095 m

19992 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-35 °C

-63 °F

power

APU in HC:

Engine manufacturer:

Turbomeca

Model:

Arrius 2B2

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0.26527 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

120 km/h

65 kt

Fuel consumption @ eco cruise speed @SL:

221 kg/h

487 lbs/h

Fuel consumption @ min consumption speed @ SL:

173 kg/h

381 lbs/h

Engines nominal power:

884 kW

1201 hp

Transmission shaft max continuous power:

566 kW

769 hp

Transmission shaft max power:

640 kW

870 hp

Takeoff power 5 min:

946 kW

1286 hp

OEI 30s power:

609 kW

828 hp

OEI 2min power:

580 kW

788 hp

OEI max continuous power :

528 kW

718 hp

OEI max continuous transmission power:

368 kW

500 hp

OEI 30 sec transmission power:

526 kW

715 hp

OEI 2 min transmission power:

513 kW

697 hp

dimensions

Overall length:

12.16 m

40 ft

Rotor diameter:

10.2 m

33 ft

Tail rotor diameter:

1 m

3 ft

Fuselage length:

10.2 m

33 ft

Overall height:

3.51 m

12 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

noise

Noise at flyover, level:

85.7 dB EPNL

Noise at flyover, limit:

93.7 dB EPNL

Noise at takeoff, level:

88.3 dB EPNL

Noise at takeoff, limit:

94.7 dB EPNL

Noise at landing, level:

94.9 dB EPNL

Noise at landing, limit:

95.7 dB EPNL

seating

Crew:

1

Max pax number:

7

use

Average price:

3.5e+06 $

tags:

t2i

remarks:

general

Airbus Helicopters EC135 EC135 T2+