Overview
The Eurocopter EC 725 Caracal is a military transport helicopter derived from the Super Puma family. Entering service in the 2000s, it supports combat search and rescue and troop transport missions. The aircraft emphasizes range and survivability.
Specifications
Units
- Engine
- 2 × Turbomeca Makila 1A4 turboshafts
- Engine type
- Turboshaft
- Power
- 2 × 2,382 shp · 1,776 kW
- Avionics
- Wind River Glass Cockpit
- Wing tips
- No winglets
- Seats
- 28
- Crew
- —
- Cabin width
- 5 ft 11 in · 1.80 m
- Cabin height
- 4 ft 9 in · 1.45 m
- Cabin length
- 25 ft 10 in · 7.87 m
- Exterior length
- 64 ft 0 in · 19.50 m
- Tail height
- 16 ft 4 in · 4.97 m
- Fuselage diameter
- 6 ft 7 in · 2.00 m
- Wing span
- 53 ft 2 in · 16.20 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 24,700 lb · 11,200 kg
- Max landing weight
- —
- Max payload
- 12,500 lb · 5,650 kg
- Fuel capacity
- 810 gal · 3,100 L · 2,400 kg (Jet A)
- Max cruise speed
- 140 kt · 161 mph · 259 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 500 nm · 580 mi · 930 km
- Fuel burn
- 0.80 nm/gal · 0.39 km/L
- Ceiling
- 19,997 ft · 6,100 m
- Rate of climb
- 1,064 ft/min · 5 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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Operational Context
Sources and references used for research and fact-checking.
- https://en.wikipedia.org/wiki/Eurocopter_EC725
- https://www.airbus.com/helicopters/military-helicopters/heavy/h225m.html
- https://www.airbushelicopters.com/website/docs_wsw/pdf/EC725/EC725-MP-06%2014E.pdf
- https://military.wikia.org/wiki/Eurocopter_EC725
- https://www.militaryfactory.com/aircraft/detail.php?aircraft_id=1020