Back to
Aeris Naviter Aero Eli Aerokopter AgustaWestland
A109 AW109 MH-68 AW119 EH101 AW101 CH-149 HH-101 A129 AW129 T129 AW139 HH-139 AW149 Lynx AH Lynx HAS Lynx Lynx AH Lynx HMA Lynx AH Lynx Lynx 300 AW159 AW169 AW189 AW609 NH90 NH500 NH90 S-61 WAH-64 ICH-47 IS-2 SW-4 W-3A W-3AS Project Zero
Airbus Helicopters Airscooter corp Alpi Aviation Auroa helicopters Avia-Proekt Aviaimpex-Vertical AviCopter Bell Helicopter
47 204 205 206 210 212 214 222 230 407 ARH-70 412 417 427 429 430 449 525 OH-58 AH-1 UH-1 TR-911 AW609
Berkut Boeing Brantly Breguet Canadian Home Rotors Changhe Aircraft Cicare Composite Helicopter CSIST Denel Aerospace Systems DFH Dioferr Dynali E-Volo Eagle R and D Enstrom Erickson air-crane Eurocopter
BO103 Bo108 Bo46 Do132 Do32 AS332 AS532 AS350 AS355 AS550 AS555 AS365 AS565 BK117 BO105 EC120 EC130 EC135 EC635 EC145 UH-72 AAS72 EC645 EC155 X3 EC665 EC175 EC225 EC725 NH90 SA313 SA315 SA316 SA318 SA319 SA3210 SA321 SA330 SA331 SA341 SA342 SA360 HH65 SA361 SA365 SE3110 SE3120 SE3130 SE3131 SE3140 SE3150 SE3160 SE3180 SE3200 SO1221
FAMA helicopters Gen Corp Guimbal HAL Harbin Aircraft Heli-Sport Helowerks Hillberg Hughes Helicopters Hungaro Copter IHSRC Infotron KAI Kaman Kamov Kari Kawasaki Kazan Kinney Konner Rotorfly Ltd LCA helicopters Marenco SwissHelicopter MD Helicopters Microcopter Mil
Mi-2 Mi-4 Mi-8 Mi-17 Mi-171 Mi-172 Mi-12 Mi-24 Mi-26 Mi-28 Mi-34 Mi-35 Mi-37 Mi-38 Mi-40 Mi-44 Mi-46 Mi-52 Mi-54 Mi-58 Mi-60 X1
Mitsubishi Mosquito Aviation NADC NHI Northrop Grumman Parrot Piasecki PZL Swidnik Qingdao Haili Revolution Helicopter Corp Rinke Aerospace Robinson Rotorway Saab Sagita Schiebel Schweizer Scotts Bell Sikorsky
S-434 HH-3 CH-53 HH-53 MH-53 RH-53 AH-60 UH-60 EH-60 MH-60 HH-60 SH-60 VH-60 S-61 RAH-66 S-64 S-70 S-76 H-76 CH-148 S-92 H-92 S-97 X2 X-49
SKT Helicopters Skyline Solution F Sunward Tech TAI Ultrasport VAT Yoshine


EC130 B4

tags: ecureuil Civil Utility Transport Law






Commercial designation:


Technical designation:


Version, Variant:




Currently produced:


Typical missions:

Civil Utility Transport Law

Flight conditions:

First flight:


Landing system:


Blades number:


Tail blades number:



MTOW with external loads:

2800 kg

6174 lbs

MTOW with only internal loading:

2427 kg

5351.535 lbs

Empty weight:

1379 kg

3040.695 lbs

External payload:

1160 kg

2557.8 lbs

Internal payload:

1048 kg

2310.84 lbs

Standard fuel tank:

426 kg

939.33 lbs

with optionnal external fuel tank:

0 kg

0 lbs


Cruise speed:

235 km/h

126.9 kt

Maximum cruise speed:

240 km/h

129.6 kt


287 km/h

154.98 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

640 km

345.6 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

9.1 m/s

1790.88 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

0 m

0 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:

2535 m

8314.8 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:

4770 m

15645.6 ft

Max operating altitude, empty weight:

7010 m

22992.8 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-40 °C

-72 °F


APU in HC:


Engine manufacturer:



Arriel 2B1

Engines quantity:


Powerplant category:


Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

543 kW

737.937 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

632 kW

858.888 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 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:

12.64 m

41.4592 ft

Rotor diameter:

10.69 m

35.0632 ft

Tail rotor diameter:

1 m

3.28 ft

Fuselage length:

10.68 m

35.0304 ft

Overall height:

3.61 m

11.8408 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:

92 dB EPNL

Noise at takeoff, level:

85 dB EPNL

Noise at takeoff, limit:

93 dB EPNL

Noise at landing, level:

90 dB EPNL

Noise at landing, limit:

94 dB EPNL

crew and pax



Max pax number:



Average price:

0 $

cockpit front panel

Eurocopter EC130 EC130 B4



Eurocopter EC130 EC130 B4

from above

Eurocopter EC130 EC130 B4