| POWERPLANTS |
| Manufacturer |
Pratt
& Whitney |
| Model |
PT6A-60A |
| Shaft-
Horsepower per Engine |
1050
SHP |
| PROPELLERS |
| Manufacturer |
Hartzell |
| No.
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 |
| |
| ACCOMMODATIONS |
| Crew
Seats (One Pilot Required) |
02 |
| Passenger
Seats (Typical) |
09 |
| Baggage
Volume (Accessible In Flight) |
550
lb 55.3 cu ft |
| |
| DESIGN
WEIGHTS |
| Maximum
Ramp Weight |
15100
lb |
| Maximum
Take-Off Weight |
15000
lb |
| Maximum
Landing Weight |
15000
lb |
| Maximum
Zero Fuel Weight |
12500
lb |
| Basic
Operating Weight (std BEW Plus One
Crew @ 200 |
9526
lb |
| Maximum
Fuel Capacity |
539
U.S. Gal |
| Maximum
Fuel Capacity Weight |
3611
lb |
| Useful
Load (Standard Airplane) |
5574
lb
|
| |
| RANGE |
| (Maximum
Range Power, FL 350, NBAA IFR
Reserve 100 mm Alt) |
|
| 4
PAssengers / 800 Lb Payload |
1765
nm |
| 8
Passengers / 1600 Lb Payload |
1670
nm |
| |
| TAKE-OFF
FIELD LENGTH |
| Sea
Level, ISA, 15000 LB, Flaps Approach |
3300
ft |
| 300
Nm 8 Passengers Mission, Sea Level,
ISA NBAA IFR Reserve, 100 nm Alt |
2659 |
| Maximum
Cruise Speed |
312
KTAS |
| |
| RATE
OF CLIMB |
| All-Engine
(Sea Level, Flaps Up, 15000 Lb) |
2731
ft / min |
| One-Engine
(Sea Level, Flaps Up, 15000 Lb) |
780
ft / min |
| |
| CEILINGS |
| Maximum
Certified Altitude |
35000
ft |
| All-Engine
Service Ceiling |
35000
ft |
| Engine-Out |
21500
ft |