Airbus Helicopters H155
Overview
The Airbus Helicopters H155 is a helicopter aircraft manufactured by Airbus Helicopters, with the profile centered on its civil helicopter role. It first flew in 1997-06-17 and entered service in 1999-03. The current production-status field is listed as In Production. The listed configuration provides for a crew of 2 and passenger capacity of 13. The profile records 2 engines. Its ICAO type designator is EC55. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
First Flight
Jun 17, 1997
Crew
2
Passengers
13
Range
463 nm
Cruise Speed
145 kt
Max Speed
175 kt
Specifications
| ICAO Type Code | EC55 |
|---|---|
| First Flight | Jun 17, 1997 |
| Introduction Date | Mar 1999 |
| Crew | 2 |
| Passenger Capacity | 13 |
| Length | 46 ft 11 in |
| Wingspan / Rotor Diameter | 41 ft rotor diameter |
| Height | 13 ft 8 in |
| Empty Weight | 5798 lb |
| Max Takeoff Weight | 10846 lb |
| Cruise Speed | 145 kt |
| Max Speed | 175 kt |
| Range | 463 nm |
| Service Ceiling | 15000 ft |
| Engine Manufacturer | Safran Helicopter Engines |
| Engine Model | Arriel 2C2 |
| Engine Count | 2 |
Data verification status: Unverified
Source: Wikipedia - Eurocopter EC155