Cessna Aircraft Company Turboprop Cessna Caravan

The Caravan’s speed and range capabilities are unusually high for a cargo hauler. Its reliability and versatility in all weather conditions and terrains have made the Caravan famous for its rugged utility and flexibility. This durable workhorse will take to the sky from rough, unprepared, and short airstrips. Its reliability even in remote areas, at high altitudes, and in hot climates is unbeatable. Standard avionics include GDU 1040A Pilot and 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 Safe Taxi 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 Gas Generator Speed Propeller Speed Oil Pressure Oil Temperature Fuel Quantity Fuel Flow Ammeter/Voltmeter Standby Engine Torque Gauge Altair Digital ADAS Engine Trend Monitoring System Detailed Specifications Performance data is based on the standard Caravan 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 37 ft 7 in (11.46 m) Height 14 ft 11 in (4.53 m) Wingspan 52 ft 1 in (15.87 m) Wing Wing Area 279 sq ft (25.96 sq m) Wheelbase 11 ft 8 in (3.54 m) Tread 11 ft 8 in (3.56 m) Cabin Interior Height Width Length 54 in (1.37 m) 64 in (1.63 m) 12 ft 9 in (3.88 m) Maximum Passengers 10 - 14 Baggage Capacity Weight Volume 325 lb (147.4 kg) 32 cu ft (0.89 cu m) Weights Maximum Ramp Weight 8,035 lb (3,645 kg) Maximum Takeoff Weight 8,000 lb (3,629 kg) Maximum Landing Weight 7,800 lb (3,538 kg) Usable Fuel Capacity Weight Volume 2,224 lb (1,009 kg) 332 gal (1,257 l) Basic Operating Weight 4,705 lb (2,134 kg) Useful Load 3,330 lb (1,510 kg) Maximum Payload 3,095 lb (1,404 kg) Full Fuel Payload 1,106 lb (502 kg) Performance Maximum Cruise Speed 186 ktas (344 km/h) Maximum Range 1,071 nm (1,983 km) Takeoff Takeoff Distance Ground Roll 2,055 ft (626 m) 1,160 ft (354 m) Landing Landing Distance Ground Roll 1,625 ft (495 m) 715 ft (218 m) Maximum Operating Altitude 25,000 ft (7,620 m) Maximum Climb Rate 1,234 fpm (376 mpm) Maximum Limit Speed 175 kias (324 km/h) Stall Speed 61 kcas (113 km/h) Powerplant The Pratt & Whitney Canada PT6A-114A turboprop engine is flat-rated to 675 shaft horsepower at 1,900 rpm. Engine operation is monitored by the engine indication system, which shows numeric readouts of critical engine fuel and electrical indications for torque, propeller speed, fuel flow and others. A wet type standby engine torque gauge is also installed. Manufacturer: Pratt & Whitney Canada Model: (1) PT6A-114A Power Output: 675 shp Propeller Manufacturer: McCauley Description: 3 blade metal, constant speed, full feathering