Vertipedia - Airbus Helicopters H135/EC 135 T3/EC135 P3

Previously designated EC135 T3/P3 before the change to Airbus Helicopters designations

2-Powerplants details for this aircraft- Pratt & Whitney PW206B3, or Turbomeca Arrius 2B2+ and available performance data is for Turbomeca Arrius 2B2+

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H135/EC135

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:	3.51 m	11.5 ft
Overall Length:	12.26 m	40.2 ft
Overall Width:	10.40 m	34.1 ft

Airframe Dimensions
Airframe Length:	10.20 m	33.5 ft
Airframe Width:	1.56 m	5.1 ft
Airframe Height:	3.35 m	11.0 ft

Landing Gear Dimensions
Landing Gear Base:
Landing Gear Track:

Cabin Dimensions
Cabin Internal Height:	1.26 m	4.1 ft
Cabin Internal Length:	4.04 m	13.3 ft
Cabin Internal Width:	1.56 m	5.1 ft

Weights
Max Gross Weight (ground):	2,980 kg	6,570 lb
Max Gross Weight (airborne):	2,980 kg	6,570 lb
Max Take-off Weight:	2,980 kg	6,570 lb
Empty Weight:	1,583 kg	3,490 lb

Climb Performance
Max Rate of Climb:	8 m/s	1,555 fpm

Hover Performance
Hover Ceiling IGE:	4,025 m	13,205 ft
Hover Ceiling OGE:	2,135 m	7,005 ft

Limitations
Max Level Flight Speed:	252 km/h	136 kts
Never Exceed Speed:	259 km/h	140 kts
Service Ceiling:	4,985 m	16,355 ft

Range and Endurance
Max Range:	614 km	332 nm
Max Endurance:	3 hrs

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

Powerplant
Number of engines:	2
Designation:	Turbomeca Arrius 2B2Plus turbine
Manufacturer:	Turbomeca

Normal Ratings
Max continuous:
Take-off / rated:
Intermediate:
Maximum:

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

Main Rotor Characteristics
Diameter:	10.40 m	34.12 ft
RPM:
Direction of Rotation:	Clockwise
Hub Type:	Bearingless

Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:
Blade Tip Geometry:
Blade Twist:
Number of Blades:	4

Main Rotor Derived Characteristics
Disc Area:	84.95 m²	914.4 ft²
Disc Loading:	35.08 kg/m²	7.185 lb/ft²
Solidity:

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

Tail Rotor Characteristics
Diameter:	1.00 m	3.28 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:	0.79 m²	8.5 ft²
Solidity:

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

References

References and sources used

airbus H135 Helionix Technical Data 2016

Airbus Helicopters
Airbus Helicopters, 09/21/2018
Report or Technical Manual

H135

Airbus Helicopters
http://www.airbushelicopters.com/website/docs_wsw/RUB_30/tile_2644/H135-BR-0515E.pdf, 20 Sept 2015 (page 20)
Report or Technical Manual