Single engine utility helicopter

The H125 is a single-engine helicopter, mostly used for utility, passenger transport, surveys, and training.

The H125, a standout in the Ecureuil family, surpasses all other single-engine helicopters in performance, versatility, safety, and cost-efficiency. Known for its resilience in extreme heat and high altitudes, it set records by landing on Mount Everest in 2005. The H125 model boasts the Safran Arriel 2D engine with dual digital engine control (FADEC) and an independent system for seamless start-up and engine management, enhancing operational reliability and ease of use.

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Technical Specifications

Capacity
ConfigurationPilotPassenger
High density version16
Standard version15
Comfort version14/5
Air medical transportation
ConfigurationPilotDoctorStretcher
Casualty evacuation121
Load transportation
ConfigurationPilotLoad in Cabin
Cargo carrying1105.9 ft3 (3 m3)
Weights
Maximum takeoff weight
With the optional “kit to increase Internal Gross Weight”
4,960 lb / 2,250 kg
5,225 lb / 2,370 kg
Maximum takeoff weight with external load6,172 lb / 2,800 kg
Maximum cargo-swing load3,086 lb / 1,400 kg
Engine1 SAFRAN ARRIEL 2D turbine engine
Takeoff power847 shp / 632 kW

 

Performance at Max. GROSS WEIGHT, ISA, SL
Maximum speed (Vne)155 kts / 287 km/hr
Fast cruise speed140 kts / 345 nm
Range with standard tank127 kts / 638 km
Max Endurance4 hrs 23 min
Rate of climb1,959 ft/min / 10 m per sec
Service ceiling16,550 ft / 5,044 m
Hover ceiling IGE13,200 ft / 4,023 m
Hover ceiling OGE11,100 ft / 3,383 m

 

Operation Limitations
Maximum altitude (PA)23,000 ft / 7,010 m
Minimum temperature– 40°C / – 40°C
Maximum temperatureISA + 35°C / + 95°F, limited to + 50°C / + 122°F

 

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