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GENERAL AIRCRAFT SPECIFICATIONS*

ENGINES

Manufacturer

Model

Shaft-Horsepower per Engine  

Pratt & Whitney Canada

PT6A-135A

650 (Flat Rated)

EXTERNAL

DIMENSIONS

Wing Span

Length

Height

Wing Area

58.20 ft (17.74 m)

41.67 ft (12.70 m)

15.52 ft (4.73 m)

329.38 ft² (30.60 m²)

PROPELLERS

Manufacturer

Number of Blades

MT-Propeller

5

INTERNAL

DIMENSIONS

Cabin Length

Cabin Height

Cabin Width

Total Cabin Volume (Incl. Baggage)

13.12 ft (4.00 m)

4.53 ft (1.38 m)

5.35 ft (1.63 m)

347.20 ft³ (9.86 m³)

ACCOMMODATIONS  

Crew Seats (One Pilot Required)

Passenger Seats

Baggage Capacity

2

0-12

397 lb (180kg)

WEIGHTS

Approx. Basic Empty Weight

(Stand. Config. 9 Cabin Seat)

Maximum Ramp Weight

Maximum Take-off Weight

Approx. Useful Load        

Maximum Landing Weights  

Land

Water

8,375 lb (3,800 kg)

11,351 lb (5,150 kg)

11,240 lb (5,100 kg)

2,865 lb (1,300 kg)

10,689 lb (4,850 kg)

11,020 lb (5,000 kg)

FUEL CAPACITY

Useable

363 U.S. gal (1,375 l)

SPEEDS

Maximum Cruise Speed                            

Stall Speed (Landing  Configuration, Land)        

180 KTAS

66 KCAS

RATE OF CLIMB

Two Engines at MTOW, SL

One Engine at MTOW, SL

1,079 ft/min (329 m/min)

392 ft/min (120 m/min)

CEILING  

Maximum Operating Altitude

15,000 ft (4,573 m)

TAKE-OFF

DISTANCES

Sea Level, ISA, (Over 35  ft/10.66 m Obstacle) Land

Water      

2,244 ft (684 m)

3,445 ft (1,050 m)

LANDING

DISTANCES

Sea Level, ISA, (Over 50  ft/15.24 m Obstacle)

Land

Wate

2,621 ft (799 m)

2,795 ft (852 m)

*PRELIMINARY DESIGN DATA; subject to changewithout any notice

*Alldata and information’s published within this website are preliminary and subject to change without anynotice.