| WEIGHT |
SPEED |
|||
| Maximum Gross Weight, Internal |
16,300 lbs. |
VNE (Maximum Air Speed) | 167 kts. | |
| Maximum Gross Weight, External |
16,500 lbs. |
ECON. Cruise (Efficiency) | 135 kts. | |
| Empty Weight |
9,400 lbs. |
|||
| Useful Load (with 1 hour fuel): |
RANGE |
|||
| Internal |
5,500 lbs. |
Maximum Fuel Range |
300 nm. |
|
| External |
5,800 lbs. |
Endurance (No Reserves) |
2 hrs. @ 1282 lbs/hour |
|
| PERFORMANCE |
FUEL |
|||
| Service Ceiling |
16,500 ft. |
Fuel Capacity |
414 gal. |
|
|
Installed Horsepower |
2 engines; 1260 hp each |
Main + Aux. Tank |
599 gal. |
|
|
Takeoff Power |
1,475 lbs. |
|||
| Max. Continuous Power |
1,287 lbs. |
ENGINE |
||
| Manufacturer |
Turbomeca | |||
| CAPACITIES |
Model |
Turmo IV C | ||
| Required Crew: |
||||
| VFR | 1 pilot | |||
| IFR | 2 pilots | |||
| Passengers | 18 | |||
| ROTOR BLADES |
||||
| Main |
5 | |||
| Tail |
4 | |||