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Superiority
MODERN: The AS550 C3 offers the most modern design complying with more and more demanding battlefields and missions.
PROVEN: The AS550 C3 is already operational from the highest altitudes (6000 m/19,685 ft) to the hottest and sandy environments (+ 50°C/122°F).
MULTI-MISSION: The AS550 C3 is fitted with a large amount of already integrated equipment to perform the widest range of missions.
COST EFFECTIVE: The simple design, reliability of equipment, low fuel consumption and light maintenance make the AS550 C3 the most cost effective weapon and mission system.
The AS550 C3’s powerful engine and its modern design make it the most efficient and reliable scout helicopter.
CAPACITY |
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| Passenger transport | 1 pilot + 5 passengers (standard version)
1 pilot + 4 or 5 passengers (comfort version) 1 pilot + 6 passengers (high density version) |
| Casualty evacuation | 1 pilot + 1 or 2 patient stretchers + 2 doctors |
WEIGHTS |
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| Maximum take-off weigh | 2,250 kg | 4,960 lb |
| MTOW with jettisonable armament | 2,450 kg | 5,401 lb |
| Maximum take-off weight with external load | 2,800 kg | 6,172 lb |
| Empty weight, standard configuration | 1,202 kg | 2,650 lb |
| Useful load, standard configuration | 1,048 kg | 2,310 lb |
| Maximum cargo-swing load | 1,400 kg | 3,086 lb |
| Standard fuel capacity | 426 kg | 939 lb |
POWERPLANT |
1 TURBOMECA ARRIEL 2B turbine engine |
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| Take-off power | 632 kW | 847 shp |
PERFORMANCE |
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| Maximum speed (VNE) | 287 km/hr | 155 kts |
| Fast cruise speed (at MCP) | 258 km/hr | 140 kts |
| Recommended cruise speed | 225 km/hr | 121 kts |
| Rate of climb at MTOW, sea level | 9,8 m/sec | 1,935 ft/min |
| Service ceiling | >7,000 m | 22,965 ft |
| Hover ceiling OGE at take-off power (MTOW) | 3,220 m | 10,560 ft |
| Maximum range without reserve at RCS (MTOW) | 645 km | 348 nm |
| Endurance without reserve at 100 km/hr-54 kts (MTOW) | 4h07 |
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OPERATING LIMITATIONS |
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| Maximum operating altitude | 7,000 m | 22,965 ft |
| Minimum temperature | - 40°C |
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| Maximum temperature | ISA + 35°C
limited to + 50°C |
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The data set forth in this document is for information purposes only, and may vary with conditions. For performance data and operating limitations,
reference see approved flight manual and all appropriate documents. May 2004
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