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| General Data |
| Empty Weight of Standard Aircraft |
3,977 lbs. |
| Maximum Takeoff Weight |
7,904 lbs. |
| Useful Load |
3,750 lbs. |
| Maximum Takeoff Weight . . .with External Load |
7,904 lbs. |
| Usable Fuel Capacity . . . Standard Tank |
1,530 lbs. |
| Power Plant |
2 Turbomeca
Arriel 1E2 turbine engines |
| Passenger Transport |
1 or 2 pilots
9 or 8 passengers |
| Casualty evacuation |
2 pilots
2 litters
3 crew seats for doctor and attendant |
Performance Data |
| Maximum speed (vne) |
145 kts. |
| Recommended cruise speed at SL |
131 kts. |
| Rate of climb at SL |
1,600 ft/min |
| Service ceiling at MCP |
17,200 ft. |
| Hover ceiling OGE (at 2,700 kg gross weight - TOP) |
16,800 ft. |
| Maximum range with standard tanks (at 2,700 kg gross weight) |
380 nm. |
| Endurance with standard tanks (at 2,700 kg gross weight) |
3h55' |
| * Performance data is provided at Sea Level, ISA conditions, maximum gross weight, with standard fuel. It is not intended for flight planning purposes. For performance data and operating limitations, see approved flight manual and all appropriate documents. October 2002. |
Operation Limitations |
| Maximum operating altitude |
18,000 ft. |
| Maximum operating altitude for hover in ground effect, take off and landing |
18,000 ft. |
| Minimum temperature |
-45 C |
| Maximum temperature |
ISA + 35C
(max + 50C) |
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