| General Data |
| Empty Weight of Standard Aircraft |
9,920 lbs. |
| Maximum Takeoff Weight |
18,960 lbs. |
| Useful Load |
9,040 lbs. |
| Maximum Takeoff Weight . . .with External Load |
20,615 lbs. |
| Usable Fuel Capacity . . . Standard Tank |
535 gal. |
| Baggage Compartment Volume |
Continuous Cabin |
| Power Plant |
2 Turbomeca
Makila 1A1 |
| Cabin Volume |
473.90 cu.ft. |
| Standard Seating Capacity |
2 + 20 |
Performance Data |
| Never Exceed Speed |
150 kts. |
| Fast Cruise Speed |
141 kts. |
| Maximum Range (with no reserves) |
449 nm. |
| Maximum Endurance
(with no reserves) |
4.2 hrs. |
| Hover In Ground Effect Ceiling |
7,546 ft. |
| Hover Out of Ground Effect Ceiling |
7,546 ft. |
Rate of Climb
(all engines operative, MCP) |
1,618 fmp. |
| Takeoff Power Per Engine |
1,819 shp. |
| * Performance data is provided at Sea Level, ISA conditions, maximum gross weight, with standard fuel. It is not intended for flight planning purposes. |
Exterior Dimensions |
| Overall length with blade in front |
63.95 ft. |
| Minimum width with all blades |
36.20 ft. |
| Overall width with blades folded |
12.50 ft. |
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