The H215 (AS332) is a twin-engine medium-weight civil helicopter equipped with a new avionics glass cockpit. Its operational characteristics and its large cabin explain its success, particularly for passenger transport. The extensive power reserve, safety level and comfort make the SUPER PUMA H215 an aircraft perfectly suited for offshore or other civil operations.
|Empty weight, standard aircraft (including engine oil & unusable fuel)||4,510 kg / 9,943 lb|
|Useful load||4,090 kg / 9,017 lb|
|Maximum all-up weight||8,600 kg / 18,960 lb|
|Maximum cargo-sling load||4,500 kg / 9,920 lb|
|Maximum all-up weight in external load configuration||9,350 kg / 20,615 lb|
Note: Empty weight accuracy: within + 2%
|Maximum speed, VNE (Never Exceed Speed)||278 km/h / 150 kts|
|Fast Cruise speed at MCP (Max Continuous Power)||262 km/h / 141 kts|
|Rate of climb (85kt, 2 engines at MCP)||8.2 m/s / 1,618 ft/min|
|Service ceiling (Rate-of-climb : 0.508m/s 100 ft/mn)||2,895 m / 9,500 ft|
|Hover ceiling In Ground Effect (IGE)||3,250 m / 10,663 ft|
|Hover ceiling Out of Ground Effect (OGE)||2,300 m / 7,546 ft|
|Maximum range with standard tank||841 km / 454 nm|
At Max Gross Weight, at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition.
|Maximum emergency power (OEI 30”)||1,400 kW / 1,877 shp|
|Intermediate emergency power (OEI 2’)||1,330 kW / 1,783 shp|
|Take-off power||1,357 kW / 1,819 shp|
|Maximum continuous power||1,185 kW / 1,588 shp|
Power per engine, in standard atmosphere, at sea level.
The data set forth in this document is for informational purposes only and may vary with conditions. For performance data and operating limitations reference see approved flight manual and all related documentation.
Most modern technology inherited from the well-known H225/H225M includes:
- Advanced helicopter cockpit and avionics system (Airbus Helicopters CanadaS), including a full glass cockpit NVG compatible with the following:
- Four 6” x 8” navigation & mission displays
- Two 4” x 5’’ vehicle management system displays
- One integrated standby instrument display
- New digital dual duplex 4-axis autopilot (APM 2010)
- Latest generation navigation and flight
The H215 is a 9-ton class twin-engine helicopter in the famous COUGAR / SUPER PUMA family. They combine the rugged experience of the AS532 / AS332 dynamic and basic assemblies with the most advanced avionics of the H225M. They also include full glass cockpit avionics and the latest generation autopilot. These aircraft are reliable, fast helicopters and have outstanding all weather capabilities: a great power reserve and high maneuverability. The powerful MAKILA 1A1 engines give them the ability to fly almost any mission, no matter the temperature and altitude. They ensure maximum operational safety, even in the most difficult situations (discretion, low vulnerability, crash survivability and icing conditions).
These multipurpose helicopters can perform a wide range of missions including:
|AS332 L1e: from passenger transportation,
executive transportation to SAR
| H215: aerial work such as heavy sling,
logging and power line maintenance.
The large selection of available optional equipment allows for a wide spectrum of mission capabilities. In addition, the AS332 L1e and H215 are also cost effective aircraft due to their low maintenance and operating costs.