Overview
The AgustaWestland AW101 Merlin was developed as a next-generation medium-lift helicopter capable of operating in demanding naval and military environments. Designed through a joint British-Italian program, it combined range, payload, and advanced mission systems to replace earlier maritime helicopters. Its three-engine configuration and modern avionics made it one of the most capable rotorcraft in its class.
Live Fleet Activity (EH10)
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Specifications
Units
- Engine
- 3 × Rolls-Royce Turbomeca RTM322-01
- Engine type
- Turboshaft
- Power
- 3 × 2,100 shp · 1,566 kW
- Avionics
- NVG compatible glass cockpit, Smiths Industries OMI 20 SEP
- Wing tips
- No winglets
- Seats
- 45
- Crew
- —
- Cabin width
- 7 ft 10 in · 2.39 m
- Cabin height
- 6 ft 3 in · 1.90 m
- Cabin length
- 21 ft 4 in · 6.50 m
- Exterior length
- 74 ft 10 in · 22.80 m
- Tail height
- 21 ft 10 in · 6.65 m
- Fuselage diameter
- 9 ft 2 in · 2.80 m
- Wing span
- 61 ft 0 in · 18.60 m
- Baggage volume
- 1,095 ft³ · 31.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 34,400 lb · 15,600 kg
- Max landing weight
- —
- Max payload
- 12,000 lb · 5,450 kg
- Fuel capacity
- 1,100 gal · 4,200 L · 3,300 kg (Jet A)
- Max cruise speed
- 150 kt · 173 mph · 278 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 540 nm · 620 mi · 1,000 km
- Fuel burn
- 0.45 nm/gal · 0.22 km/L
- Ceiling
- 15,000 ft · 4,600 m
- Rate of climb
- 2,000 ft/min · 10 m/s
- Takeoff distance
- —
- Landing distance
- —
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Live fleet activity details
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