H125®: higher, further, better than all other helicopters in its category
The H125 is the high-performance version of the single engine Ecureuil® family. It demonstrated its tremendous capabilities
while breaking the world record for the highest altitude landing and takeoff: Mount Everest (29,029 ft / 8,848 m).
The H125 outclasses all other single engine helicopters for performance, versatility, maintenance costs, safety and low
acquisition. It excels in hot & high and in extreme environments.
The H125 is equipped with a Turbomeca Arriel 2D engine including an upgraded triple engine control: the dual channel
FADEC (Full Authority Digital Engine Control) unit plus a third independent & automatic back up channel.
The glass cockpit includes Vehicle and Engine Multifunction Display (VEMD), thus reducing the pilot’s workload and
enhancing safety.
Thanks to its versatile flat floored cabin, the H125 can be quickly and easily reconfigured for all types of missions, such
as aerial work, firefighting, law enforcement, Search And Rescue or passenger transport. The H125 offers a new interior
design-known as STYLENCE® - for increased comfort in passenger transport missions.
Making the Best
Even Better!
• Improved safety with "Vision 1000"
cockpit imaging & flight data
monitoring device
• Hydraulic system and flight control
improvements
• Increased MTOW 5,225 lb /
2,370 kg with “Kit to increase
Internal Gross Weight"
• Redesigned interior and seating
• Lower Direct Maintenance Cost
DIMENSIONS
Length (rotor rotating) 42.45 ft 12.94 m
Height 10.96 ft 3.34 m
Fuselage width 8.30 ft 2.53 m
Main rotor diameter 35.07 ft 10.69 m
Tail rotor diameter 6.10 ft 1.86 m
WEIGHT
Maximum takeoff weight (MTOW) 4,960 lb 2,250 kg
Maximum takeoff weight with cargo-swing load 3,086 lb 1,400 kg
Maximum takeoff weight with external load 6,172 lb 2,800 kg
WEIGHT with “Kit to increase Internal Gross Weight"
Maximum takeoff weight (MTOW) 5,225 lb 2,370 kg Printed on PEFC certified paper originating from sustainable forests.
CAPABILITY
1 pilot + 4 to 6 passengers (comfort, standard or high density version)
ENGINE
1 Turbomeca ARRIEL 2D turboshaft with FADEC
Maximum Takeoff Power (TOP at Sea level-ISA) 847 shp 632 kW
PERFORMANCE AT MAX. GROSS WEIGHT (ISA, SL)
Maximum speed (VNE) 155 kts 287 km/h
Fast cruise speed (at MCP) 140 kts 258 km/h
Range with standard fuel tank 351 NM 651 km
Endurance without reserve at 100 km/h (54 kts) 4 h 28 min
Rate of climb 1,959 ft/min 10 m/s
Service ceiling 16,550 ft 5,044 m
Hover ceiling IGE 13,200 ft 4,023 m
Hover ceiling OGE 11,100 ft 3,383 m
©AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex - France - 2014 - All rights reserved. Airbus Helicopters’ logo and the names of its products and services
are registered trademarks. AIRBUS HELICOPTERS reserves the right to make configuration and data changes at any time without notice. The facts and figures contained in this document and expressed in
good faith do not constitute any offer or contract with AIRBUS HELICOPTERS.
Photos: ©Anthony Pecchi - ©Eric Raz - ©Airbus Helicopters Jérôme Deulin - Concept design by Airbus Helicopters - Print in France by SPI - H125-MP-0515E
