Previously designated EC145 T2 and MBB-BK 117 D-2. Includes Helionix digital avionics suite, a 4-axis autopilot, Fenestron tail rotor and Ariel 2E engines.

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H145/EC145

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height: 3.95 m 13.0 ft
Overall Length: 13.64 m 44.8 ft
Overall Width: 11.00 m 36.1 ft
Airframe Dimensions
Airframe Length: 6.17 m 20.2 ft
Airframe Width: 1.73 m 5.7 ft
Airframe Height: 3.46 m 11.4 ft
Landing Gear Dimensions
Landing Gear Base:  
Landing Gear Track:  
Cabin Dimensions
Cabin Internal Height: 1.22 m 4.0 ft
Cabin Internal Length: 4.65 m 15.3 ft
Cabin Internal Width: 1.40 m 4.6 ft

Weights and Performance

Data on aircraft weight and flight characteristics

http://www.airbushelicopters.com/site/en/ref/Characteristics_1127.html

Weights
Max Gross Weight (ground):  
Max Gross Weight (airborne): 3,700 kg 8,157 lb
Max Take-off Weight: 3,700 kg 8,157 lb
Empty Weight: 1,919 kg 4,231 lb
Useful Load: 1,781 kg 3,926 lb
Empty Weight Fraction: 0.519
Climb Performance
Max Rate of Climb:  
Hover Performance
Hover Ceiling IGE: 3,825 m 12,549 ft
Hover Ceiling OGE: 2,667 m 8,750 ft
Limitations
Max Level Flight Speed: 240 km/h 130 kts
Never Exceed Speed: 265 km/h 143 kts
Service Ceiling: 5,029 m 16,499 ft
Range and Endurance
Max Range: 651 km 352 nm
Max Endurance: 4 hrs 4 hrs

Engine Details

Aircraft powerplant (lift and/or propulsion)

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

Powerplant
Number of engines: 2
Designation: Turbomeca Arriel 2E turbine
Manufacturer: Turbomeca
Normal Ratings
Max continuous: 575 kW 771 hp
Take-off / rated: 667 kW 894 hp
Intermediate:  
Maximum:  
OEI Ratings
OEI contingency: 775 kW 1039 hp
OEI continuous: 710 kW 952 hp
OEI 30-second: 800 kW 1072 hp
OEI intermediate:  

Primary Lift Device

Data on primary lift devices such as main rotors

Main Rotor Characteristics
Diameter: 11.00 m 36.09 ft
RPM:  
Direction of Rotation: Unknown
Hub Type: Hingeless
Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:  
Blade Tip Geometry:
Blade Twist:  
Number of Blades: 4
Main Rotor Derived Characteristics
Disc Area: 95.03 m² 1023.0 ft²
Disc Loading:  
Solidity:  
Main Rotor Blade Derived Characteristics
Blade area per blade:  
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Diameter: 1.15 m 3.77 ft
Configuration: Unknown
Direction of Rotation: Unknown
RPM:  
Tail Rotor Blade Characteristics
Number of Blades: 1
Blade Construction:  
Blade Chord:  
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area: 1.04 m² 11.2 ft²
Solidity:  
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade):  

Related VFS Resources

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Related Public Resources

Resources related to the H145/EC145 T2/MBB-BK 117 D-2 , provided by public sources across the internet.

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