Overview
The Eurocopter AS355 is a twin-engine development of the AS350 family. Introduced in the late 1970s, it offers increased redundancy and payload compared with its single-engine counterpart. The helicopter serves in civil and governmental roles.
Live Fleet Activity (AS55)
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Specifications
- Engine
- 2 × Allison 250-C20F turboshaft engine
- Engine type
- Turboshaft
- Power
- 2 × 420 shp · 313 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 6
- Crew
- —
- Cabin width
- 5 ft 5 in · 1.65 m
- Cabin height
- 4 ft 3 in · 1.30 m
- Cabin length
- 7 ft 11 in · 2.42 m
- Exterior length
- 42 ft 5 in · 12.94 m
- Tail height
- 10 ft 7 in · 3.22 m
- Fuselage diameter
- 6 ft 2 in · 1.87 m
- Wing span
- 35 ft 1 in · 10.69 m
- Baggage volume
- 35 ft³ · 1.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 5,750 lb · 2,600 kg
- Max landing weight
- —
- Max payload
- 1,950 lb · 900 kg
- Fuel capacity
- 190 gal · 700 L · 600 kg (Jet A)
- Max cruise speed
- 129 kt · 148 mph · 239 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 380 nm · 440 mi · 700 km
- Fuel burn
- 2.31 nm/gal · 1.13 km/L
- Ceiling
- 11,200 ft · 3,400 m
- Rate of climb
- 1,280 ft/min · 7 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
Live fleet activity details
Operational Context
Eurocopter AS355 — light twin-engine helicopter
The AS355 first flew in 1979 and entered service in the early 1980s. It features a compact fuselage and three-blade main rotor. The twin-engine configuration improves safety margins.
Two turboshaft engines producing approximately 420 shaft horsepower each power the helicopter. Cruise speed approaches 135 knots (250 km/h). Maximum takeoff weight exceeds 5,700 pounds (2,585 kg).
The AS355 has been used in law enforcement, utility, and passenger transport roles. Its adaptability supported broad export success. Production eventually transitioned to newer Airbus Helicopters models.
Sources and references used for research and fact-checking.