Vertipedia - Airbus Helicopters EC130 B4

Overview

Data on design, manufacture and status

Design authority: Eurocopter Group

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H130/EC130

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Fenestron/Shrouded tail rotor

Crew required: 1 in Side-by-side arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Layout and Dimensions

Weights and Performance

Engine Details

Primary Lift Device

Primary Control Device

Overall Dimensions
Overall Height:	3.61 m	11.8 ft
Overall Length:	12.64 m	41.5 ft
Overall Width:	10.69 m	35.1 ft

Airframe Dimensions
Airframe Length:	10.68 m	35.0 ft
Airframe Width:	2.03 m	6.7 ft
Airframe Height:	3.34 m	11.0 ft

Landing Gear Dimensions
Landing Gear Base:
Landing Gear Track:

Cabin Dimensions
Cabin Internal Height:	1.28 m	4.2 ft
Cabin Internal Length:	2.19 m	7.2 ft
Cabin Internal Width:	1.87 m	6.1 ft

Weights
Max Gross Weight (ground):	2,427 kg	5,351 lb
Max Gross Weight (airborne):
Max Take-off Weight:	2,427 kg	5,351 lb
Empty Weight:

Climb Performance
Max Rate of Climb:

Hover Performance
Hover Ceiling IGE:
Hover Ceiling OGE:

Limitations
Max Level Flight Speed:
Never Exceed Speed:	287 km/h	155 kts
Service Ceiling:	7,010 m	22,999 ft

Range and Endurance
Max Range:
Max Endurance:

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines:	1
Designation:	Turbomeca Arriel 2B1 turbine
Manufacturer:	Turbomeca

Normal Ratings
Max continuous:	543 kW	728 hp
Take-off / rated:	557 kW	747 hp
Intermediate:
Maximum:

OEI Ratings
OEI contingency:
OEI continuous:
OEI 30-second:
OEI intermediate:

Main Rotor Characteristics
Diameter:	10.69 m	35.07 ft
RPM:
Direction of Rotation:	Clockwise
Hub Type:

Main Rotor Blade Characteristics
Blade Construction:	Composite
Blade Chord:
Blade Tip Geometry:
Blade Twist:
Number of Blades:	3

Main Rotor Derived Characteristics
Disc Area:	89.75 m²	966.1 ft²
Disc Loading:	27.04 kg/m²	5.538 lb/ft²
Solidity:

Main Rotor Blade Derived Characteristics
Blade area per blade:
Tip Speed:

Tail Rotor Characteristics
Diameter:
Configuration:	Unknown
Direction of Rotation:	Unknown
RPM:

Tail Rotor Blade Characteristics
Number of Blades:
Blade Construction:	N/A
Blade Chord:
Blade Twist:

Tail Rotor Derived Characteristics
Disc Area:
Solidity:

Tail Rotor Blade Derived Characteristics
Tip Speed:
Blade Area (per blade):

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Overview

Attribution

Number of engines:	1 Turbine
Max Level Flight Speed:
Max Range:
Max Endurance:

Main Rotor Diameter:	10.69 m	35.07 ft
Max Gross Weight (ground):	2,427 kg	5,351 lb