| Engines |
| Manufacturer |
Pratt & Whitney |
| Model |
PT6A-60A |
| Shaft-Horsepower per Engine |
1,050 SHP |
| |
| Propellers
|
| Manufacturer |
Hartzell |
| Number of Blades |
4 |
| |
| External Dimensions |
| Overall Length |
46 ft 8 in |
| Overall Height |
14 ft 4 in |
| Wing Span |
57 ft 11 in |
| Wing Area |
310 sq ft |
| |
| Internal Dimensions |
| Cabin Length |
19 ft 6 in |
| Cabin Height |
4 ft 9 in |
| Cabin Width Maximum |
4 ft 6 in |
| Floor Width |
4 ft 1 in |
| Cabin Volume |
355 cu ft |
| Cockpit Volume |
85 cu ft |
| |
| Accomodations |
| Crew Seats (One Pilot Required) |
2 |
| Passenger Seats (Typical) |
9 |
| Baggage Volume (Accessible in Flight) |
550 lb 55.3 cu ft |
| |
| Design Weights |
| Maximum Ramp Weight |
15,100 lb |
| Maximum Takeoff Weight |
15,000 lb |
| Maximum Landing Weight |
15,000 lb |
| Maximum Zero Fuel Weight |
12,500 lb |
Basic Operating Weight
(Std BEW Plus One Crew @ 200 lb) |
9,526 lb |
| Maximum Fuel Capacity |
539 U.S. Gal |
| Maximum Fuel Capacity Weight |
3,611 lb |
| Useful Load (Standard Airplane) |
5,574 lb |
| |
| Range |
| (Maximum Range Power, FL350, NBAA IFR Reserve 100 nm Alt) |
| 4 Passenger / 800 lb Payload |
1765 nm |
| 8 Passenger / 1,600 lb Payload |
1670 nm |
| |
| Takeoff Field Length |
|
| Sea Level, ISA, 15,000 lb, Flaps Approach |
3,300 ft |
| 300 nm 8 Passenger Mission, Sea Level, ISA NBAA IFR Reserve, 100 nm Alt |
2,659 ft |
|
| Maximum Design Speeds |
| Maximum Cruise Speed |
312 KTAS |
| |
| Rate of Climb |
All-Engines
(Sea Level, Flaps Up, 15,000 lb) |
2,731 ft / min |
One-Engine
(Sea Level, Flaps Up, 15,000 lb) |
780 ft / min |
| |
| Ceilings |
| Maximum Certified Altitude |
35,000 ft |
| All-Engine Service Ceiling |
35,000 ft |
| Engine-Out Service Ceiling |
21,500 ft |
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