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General Data | BK117 C1 |
| Empty Weight of Standard Aircraft | 3,891 lbs. |
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| Maximum Takeoff Weight | 7,385 lbs |
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| Useful Load | 3,494 lbs. |
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| Maximum Takeoff Weight . . .with External Load | 7,716 lbs. |
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| Usable Fuel Capacity . . . Standard Tank | 184 gal. |
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| Baggage Compartment Volume | Continuous Cabin |
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| Power Plant | 2 Turbomeca Arriel 1E2 |
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| Cabin Volume | 176.5 cu.ft. |
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| Standard Seating Capacity | 1 + 7 |
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| * Performance data is provided at Sea Level, ISA conditions, maximum gross weight, with standard fuel. It is not intended for flight planning purposes. | ||
| Performance Data | ||
| Never Exceed Speed | 140 kts. |
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| Fast Cruise Speed | 133 kts. |
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| Maximum Range with no reserves | 292 nm. |
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| Maximum Endurance with no reserves | 2.9 hrs. |
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| Hover In Ground Effect Ceiling (5 ft. skid height) | 8,300 ft. |
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| Hover Out of Ground Effect Ceiling | 4,850 ft. |
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| Takeoff Power Per Engine | 738 shp. |
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| Rate of Climb (all engines operative, MCP) | 1,765 fpm. |
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| Exterior Dimensions | ||
| Overall length with blade in front (tail rotor horizontal) | 39.9 ft. |
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| Minimum width with all blades | 23.7 ft. |
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