Beechcraft Corporation Beechcraft Aircraft King Air® 250

The King Air® 250 is more than just a business icon. The King Air 250 takes the proven and popular Model 200 series to a new level of performance. With an increased gross weight/enhanced payload option, more powerful PT6A-52 engines, composite winglets and composite scimitar propellers, it provides far more mission flexibility. Take your King Air where it’s never been before. Pilot-Tested Refinement The flight deck of the King Air 250 reflects pilot feedback generated during millions of flight hours in all weather conditions. The Rockwell Collins Pro Line 21 avionics suite contributes to the King Air’s record of reliability with advanced situational awareness features such as electronic charts and graphical weather display. Heads Up Placement The strategic heads-up placements on the Flight Director and Autopilot enhance situational awareness. The pilot can make critical altitude, heading and navigational changes without ever looking down. The Collins Flight Guidance System provides accurate and reliable guidance as it locks on to various navigation points and approaches. Enhanced Software The Integrated Flight Information System (IFIS) provides electronic charts software with airport diagrams with aircraft location, approach charts and Notice to Airmen (NOTAMS.) It also includes enhanced map features and intuitively designed clutter-free displays. Standard Features Standard Features Electronic Flight Instrument System (EFIS) Engine Indication System (EIS) Air Data System (ADS) Dual Attitude Heading Reference System (AHRS) Automatic Flight Guidance System (AFGS) Flight Management System (WXR) Dual Navigation and Communication Radios Specifications Dimensions Length 43 ft 10 in (13.36 m) Height 14 ft 10 in (4.52 m) Wingspan 57 ft 11 in (17.65 m) Wing Area 310 sq ft (28.8 sq m) Wheelbase 14 ft 11 in (4.55 m) Tread 14 ft 11 in (4.55 m) Cabin Interior Height 57 in (1.45 m) Width 54 in (1.37 m) Length 16 ft 8 in (5.08 m) Maximum Passengers 10 Baggage Capacity Weight 550 lb (249.5 kg) Volume 55 cu ft (1.57 cu m) Single Pilot Certified Yes Weights Maximum Ramp Weight 12,590 lb (5,711 kg) Maximum Takeoff Weight 12,500 lb (5,670 kg) Maximum Landing Weight 12,500 lb (5,670 kg) Maximum Zero Fuel Weight 11,000 lb (4,990 kg) Usable Fuel Capacity Weight 3,645 lb (1,653 kg) Volume 544 gal (2,059 l) Basic Operating Weight 8,790 lb (3,987 kg) Useful Load 3,800 lb (1,724 kg) Maximum Payload 2,210 lb (1,002 kg) Full Fuel Payload 155 lb (70 kg) Performance Maximum Cruise Speed 310 ktas (574 km/h) Maximum Range 1,726 nm (3,197 km) Takeoff Distance 2,111 ft (643 m) Landing Distance 2,845 ft (867 m) Maximum Operating Altitude 35,000 ft (10,668 m) Maximum Climb Rate 2,450 fpm (747 mpm) Maximum Limit Speed 259 kias (480 km/h) Powerplant Manufacturer P&WC Type PT6A-52 Power Rating 850 shp (634 kW)