Technical Specifications

TYPE: Regional airliner

COUNTRY OF ORIGIN: United States of America

ENGINES:
2 Pratt & Whitney PT6A-67D, Output 1,279 SHP, Inspection Interval 8,000 hrs
Number of Drive Shafts:
1 Compressor (Gas Generator) Shaft
1 Power Turbine Shaft
Compressor Stages and Types:
4 Axial-flow Stages
1 Centrifugal-flow Stage
Combustion Chamber Type:
Annualar
Propeller Manufacturer:
Hartzell Propeller Inc.
Number of Blades and type:
4 constant-speed, full feathering, reversing, counter weighted, hydraulically actuated propsDIMENSIONS

AIRCRAFT DIMENSIONS:
Length: 57.8 ft. (17.62 m)
Height: 15.5 ft. (4.72 m)
Span: 57.9 ft. (17.64 m)
Cabin Dimensions
Length: 25 ft 3 in. (7.69 m)
Height: 5 ft 11 in. (1.80 m)
Width: 4 ft 6 in. (1.37 m)

WEIGHTS
Max Ramp: 17,230 lb. (7,815 kg.)
Max Takeoff: 17,120 lb. (7,766 kg.)
Max Landing: 16,765 lb. (7,605 kg.)
Max Zero Fuel: 15,165 lb. (6,879 kg.)
Basic Operating: 10,790 lb. (4,894 kg.)
Maximum Weight in Baggage Compartments:
Forward: 250 lb. (113kg.)
Aft fwd: 1000 lb. (454 kg.)
Aft aft: 630 lb. (286 kg.)

PERFORMANCE:
Takeoff Field Length: 3,813 ft. (1,162 m) at Max. TO Wt., SL, ISA
Max. Takeoff Weight: 5,235 ft. (1,596 m) at 5,000 ft. elevation, 25°C
Landing Distance: 2,790 ft. (850 m) at Max Landing Wt., SL, ISA
Wing Loading: 54.7 lb./sq. ft.
Power Loading: 6.63 lb./SHP

CAPACITY:
Flight crew of 2
Passenger seating: 19
Max Payload: 4,375 lb. (1,984 kg.)
Useful Load: 6,440 lb. (2,921 kg.)
Max Fuel Capacity: 4,458 lb. (2,022 kg.), (6.7 lb./US gal.), 665 US gal.
Fuel w/max payload: 2,065 lb. (937 kg.)
Cabin Volume
Cockpit: 103 cu. ft. (2.92 cu. m)
Passenger Cabin: 640 cu. ft. (18.12 cu. m)