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Main description

State of the Art
and Experienced
Tailored for the most demanding operators, the EC225 is an 11-ton helicopter integrating all of the latest technological innovations.
The two Turbomeca MAKILA 2A1 engines, the main gear box and the 5-blade rotor give this machine the power for a high payload, a long range and a fast cruise speed, along with flight endurance that exceeds 5 hours and 30 minutes. Most of all, this aircraft meets the latest CS-29 amendments, including the 30-minute dry run demonstration for the main gear box.

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Technical Data

Characteristics

Even more power

The EC225 offers high operational availability and payload, long range and fast speeds.

 

PASSENGER TRANSPORTATION
Passenger transport 2 pilots + 19 passengers with comfort seats
SAR 2 pilots + 4 crew with comfort seats + up to 20 pax or 3 stretchers
Executive / VIP  2 pilots + 8 to 12 passengers
WEIGHTS
Maximum take-off weight 11,000 kg   24,251 lb
Maximum take-off weight with external load 11,200 kg   24,690 lb
Useful load, standard configuration 5,457 kg   12,030 lb
Sling load 4,750 kg   10,472 lb
Std & central energy absorbing fuel tanks ( 2,908 l ) 2,297 kg   5,064 lb
Pod fuel tanks (600 l) 474 kg   1,045 lb
2 TURBOMECA MAKILA 2A1 TURBOSHAFT ENGINES
Maximum emergency power (OEI 30 sec) 1,776 kW 2,382 shp
PERFORMANCE
Maximum speed (VNE) 324 km/h 175 kts
Fast cruise speed (at MCP) 262 km/h 142 kts
Maximum range with standard + central tanks + pod 1,135 km 613 NM
Maximum endurance (standard + central tanks + pod) 5 hr 38 min

 

OPERATION LIMITATIONS
Maximum altitude (in flight) 6,095 m
(Pressure Altitude)
  20,000 ft
(Pressure Altitude)
Minimum temperature (basic) -30°C / -22°F
Minimum temperature
with extreme cold weather kit
-40°C / -40°F
Maximum temperature ISA + 40°C / ISA + 104°F (limited to 50°C / 122°F)

The data set forth in this document is for information purposes only, and may vary with conditions.
For performance data and operating limitation references, refer to the approved flight manual and all appropriate documents.

Glossary

ADELT: Automatically Deployable Emergency Locator Transmitter
AEO: All Engines Operative
AFCS: Automatic Flight Control System
FADEC: Full Authority Digital Engine Control
FLIR: Forward Looking Infrared
GPS: Global Positioning System
IFR: Instrumental Flight Rules
MCP: Maximum Continuous Power
OEI: One Engine Inoperative
SAR: Search and Rescue
TCAS: Traffic Collision and Avoidance System
VNE: Never Exceed Speed
VMS: Vehicle Management System

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