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- U.S. economic impact
• Estimated at $740 million in direct activity and business brought to the network of some 1,000 vendors
- Industrial footprint
• Nearly 1 million square feet
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- American Eurocopter’s heritage
• Our products have been flying in the USA since 1957
- American Eurocopter’s heritage
• Our first U.S. sales partnership was established in 1963
- American Eurocopter’s heritage
• Our first U.S. manufacturing partnership was established in 1969
- American Eurocopter’s heritage
• Our SA.313 Alouette II was the first ever light turbine helicopter to enter civil operation in the U.S. (with PHI)
- American Eurocopter’s heritage
• We have been a fully-owned U.S. helicopter manufacturer since 1974
- #1 in the marketplace
• We have been the #1 producer of civil turbine helicopters in the U.S. for 9 of the past 10 years
- #1 in the marketplace
• We are #1 in four market segments
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• From the 2 ton EC120 to the 11 ton EC225
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• Our AS350 AStar is one of the most popular helicopters used in the movies!
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• To U.S. operators since 1957
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• Our U.S. aircraft fly the equivalent of 3,500 flights around the world each year
Products > AS355 NP Specifications
AS355 NP Specifications
At a glance
Max weight: 5,723 lbs.
Capacity: 1 pilot + 5/6
passengers
Powerplant: 2 Turbomeca
Arrius 1A1
Fast cruise speed: 120 kts.
External dimensions
Minimum width with all blades: 35.1 ft.
Overall width with two blades folded: 10.0 ft.
Documentation
General data
Empty weight of standard aircraft: 3,285 lbs.
Maximum takeoff weight: 5,732 lbs.
Useful load: 2,447 lbs.
Maximum takeoff weight (with external load): 6,172 lbs.
Usable fuel capacity (standard tank): 193 gal.
Powerplant: 2 Turbomeca Arriel 2A1
Cabin volume: 105.94 cu. ft.
Baggage compartment volume: 35.3 cu. ft.
Standard seating capacity: 1+5
*Performance data
Never exceed speed: 150 kts.
Fast cruise speed: 120 kts.
Maximum range (with no reserves): 395 nm.
Maximum endurance
(with no reserves):
4.6 hrs.
Hover In ground effect ceiling (5 ft. skid height): 8,450 ft.
Hover out of ground effect ceiling: 7,080 ft.
Takeoff power per engine: 460 shp.
Rate of climb (all engines operative, MCP): 1,296 fpm.
