Crew: 2
Passengers: up to 8
External
Length: 58.69 ft 17.89 m
Wingspan: 43.79 ft 13.35 m
Wing area (basic): 264.5 ft ² 24.57 m ²
Height overall: 14.56 ft 4.44 m
Internal
Cabin length: 17.67 ft 5.39 m
(From cockpit divider to end
of pressurized compartment)
Cabin maximum width: (Centerline) 5.95 ft 1.81 m
Cabin width: (Floorline) 3.9 ft 1.19 m
Cabin height: 5.71 ft 1.74 m
Floor area: (Excluding cockpit) 68.9 ft ² 6.40 m ²
Total volume: 453 ft ³ 12.80 m ³
(From cockpit divider to end
of pressurized compartment)
Weights
A. Maximum ramp weight: 23,750 lb 10,773 kg
B. Maximum takeoff weight: 23,500 lb 10,659 kg
C. Maximum landing weight: 19,500 lb 8,845 kg
D. Maximum zero fuel weight: 17,000 lb 7,711 kg
E. Typical basic operating weight: 14,772 lb 6,700 kg
F. Maximum fuel weight: 7,910 lb 3,588 kg
Maximum payload (D-E): 2,228 lb 1,011 kg
Payload – full fuel (A-E-F): 1,068 lb 484 kg
Fuel with maximum payload: 6,750 lb 3,062 kg
Range
Maximum range: 2,493 NM
2,869 SM
4,617 km
(IFR Reserves, ISA, with 4 pax/2 crew)
Speed Mach kts mph km/h
High-speed cruise 0.81 464 534 859
Typical cruise speed 0.79 457 526 846
Long-range cruise speed 0.74 422 486 782
Airfield Performance
Balanced field length: 5,450 ft 1,661 m
(SL, ISA, MGTOW)
Landing distance
(SL, ISA, MLW): 3,420 ft 1,042 m
Ceiling
Maximum operating altitude: 51,000 ft 15,545 m
Climb to cruise altitude of 41,000 ft 18 min, 30 sec
(12,497 m) after MGTOW departure:
Noise Level Takeoff
Approach
Sideline
EPNdB 78.9
87.7
83.2
Engines
Pratt & Whitney Canada PW305A turbofans
Thrust: 4,600 pounds (20.46 kN) thrust at takeoff
Flat-rating: ISA + 17°C (90°F)
Avionics
All-Digital Rockwell Collins Pro Line 4 four-tube EFIS
Dual Attitude Heading Reference Systems (AHRS)
WXR-840 Weather Radar
Dual nav/comm systems
Dual UNS-1C FMS
Traffic Collision Avoidance System (TCAS 2000)
Enhanced Ground Proximity Warning System (EGPWS)
Emergency Locator Transmitter (ELT)