Cessna Aircraft Company Turboprop Cessna Grand Caravan EX

Spend more time in the air — moving product, moving people, generating revenue — and less time on the ground servicing your aircraft. With the dependable and versatile Grand Caravan EX, you can count on exceptional performance whether you need it for business or personal adventures. Cessna’s Grand Caravan EX was engineered for challenging, rugged missions with high payloads and short, rough runways. This workhorse has the agility of a much smaller aircraft — it can take off with less than 1,399 feet of ground and climb at 1,275 feet per minute, reaching cruise speeds of 185 ktas and traveling distances of up to 904 nautical miles. Standard avionics include: GDU 1040A Pilot & Copilot Primary Flight Display (PFD) GDU 1040A Multifunction Display (MFD) GDC 74A Dual Air Data Computer (ADC) GEA 71 Engine/Airframe Unit GRS 77 Dual Attitude and Heading Reference System (AHRS) GMA 1347 Single Audio System with Integrated Marker Beacon Receiver GTX 33 Mode S Transponder Garmin Relative Terrain/Obstacles Garmin Flight Charts Capable Garmin SafeTaxi Capable KN-63 DME Switch, Avionics Power (Two) (On-Off) Artex ME-406 2-Frequency (Non-Nav Interfaced) ELT with Remote Switch and Monitor Light (Dorsal Fin Installation) Avionics Cooling, (2) Cowl Deck Fans and (3) Display Fans PA System with Aft Cabin Speakers ENGINE INDICATION SYSTEM (EIS) Displayed on MFD During Normal Operations: Engine and System Displays Torque Interstage Turbine Temperature Propeller Speed Gas Generator Speed Oil Pressure Oil Temperature Fuel Quantity Fuel Flow Ammeter/Voltmeter Standby Engine Torque Gauge FAST ™ System Engine Trend Monitoring Detailed Specifications Performance data is based on the standard Grand Caravan EX configuration, operating in International Standard Atmosphere (ISA) conditions with zero wind. Takeoff and landing field lengths are based on a level, hard surface and dry runway. Actual performance will vary with factors such as environmental conditions, aircraft configuration and operational/ATC procedures. Dimensions Length 41 ft 7 in (12.67 m) Height 15 ft 1 in (4.60 m) Wingspan 52 ft 1 in (15.87 m) Wing Wing Area 279 sq ft (25.96 sq m) Wheelbase 13 ft 4 in (4.05 m) Tread 11 ft 8 in (3.56 m) Cabin Interior Height Width Length 54 in (1.37 m) 64 in (1.63 m) 16 ft 9 in (5.10 m) Maximum Passengers 10 - 14 Baggage Capacity Weight Volume 1,410 lb (639.6 kg) 143 cu ft (4.05 cu m) Weights Maximum Ramp Weight 8,842 lb (4,011 kg) Maximum Takeoff Weight 8,807 lb (3,995 kg) Maximum Landing Weight 8,500 lb (3,856 kg) Usable Fuel Capacity Weight Volume 2,246 lb (1,019 kg) 335 gal (1,269 l) Basic Operating Weight 5,330 lb (2,418 kg) Useful Load 3,512 lb (1,593 kg) Maximum Payload 3,170 lb (1,438 kg) Full Fuel Payload 1,266 lb (574 kg) Performance Maximum Cruise Speed 185 ktas (343 km/h) Maximum Range 912 nm (1,689 km) Takeoff Takeoff Distance Ground Roll 2,160 ft (658 m) 1,399 ft (426 m) Landing Landing Distance Ground Roll 1,836 ft (560 m) 1,004 ft (306 m) Maximum Operating Altitude 25,000 ft (7,620 m) Maximum Climb Rate 1,275 fpm (389 mpm) Maximum Limit Speed 175 kias (324 km/h) Stall Speed 61 kcas (113 km/h) Powerplant The powerplant is a Pratt & Whitney Canada PT6A-140 867 SHP turboprop engine mounted in the nose of the aircraft fuselage. Propeller: Hartzell, constant speed, full feathering, reversible pitch, 3 blades, 106-inch diameter Loading: Wing: 31.49 lb/ft2 Power: 10.2 lb/shp