Cessna Aircraft Company Single Engine Aircraft Cessna Turbo Stationair®

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Single Engine Aircraft - Cessna Turbo Stationair® - Cessna Aircraft Company
Wichita, KS, USA
Single Engine Aircraft Cessna Turbo Stationair®
The Turbo Stationair® is designed to fit your mission needs. Choose from five different seating options designed for any mission. From the relaxing club seating to the one seat trainer configuration with a clear view of the instrument panel, each cabin configuration allows for maximum flexibility with seat tracks that run the length of the cabin. From takeoff to touchdown, you’ll be smiling Enhanced situational awareness for pilots means enhanced safety for all. The leading technology of the Garmin G1000 all-glass avionics suite integrates the functionality and reliability needed to fly with confidence. The Turbo Stationair’s flight deck is a proven system that reduces workload with added features and capabilities such as graphical weather radar, electronic charts, Synthetic Vision Technology (SVT™), engine sensor data, autopilot functionality, and more. The G1000 flight deck is standard on our Caravan and Citation Mustang models as well, so your transition between aircraft will be smoother when you upgrade. Virtual landscapes Synthetic Vision Technology enhances visual orientation in darkness, fog, haze, rain or any solid IFR conditions that keep you from seeing clearly. Graphics modeling technology recreates a 3D virtual rendering of the surrounding landscape on both of the PFDs. The resulting picture depicts a dimensional graphic of ground and water, airports, obstacles and air traffic all shown relative to the aircraft. Infrared technology The optional enhanced vision system (EVS) is a perfect complement to the G1000’s SVT, providing an infrared view outside the cockpit that turns night into day and improves vision through smoke and haze. The EVS provides a real-time moving image of the outside environment and illuminates possible hazards. You have the option of showing the EVS feed on the MFD in large format, which is handy during approach. Once on the ground, the view can be reduced and displayed beside the airport map to support ground navigation. There is virtually no weight added to the Turbo Stationair with integration of the EVS, and its value in situational awareness is immeasurable. Garmin G1000 Avionics Package: GMA-1347 Digital Audio Panel with Marker Beacon/Intercom GTX-33 Transponder-Mode S w-TIS GIA-63W NAV/COM/GPS/WAAS with GS #1 GIA-63W NAV/COM/GPS/WAAS with GS #2 GDU-1044B Primary Flight Display (PFD) GDU-1044B Multifunction Display (MFD) GEA-71 Engine/Airframe Computer GRS-77 AHRS GDC-74A Air Data Computer with OAT Probe GMU-44 Magnetometer Garmin SafeTaxi & FliteCharts GFC-700 Autopilot Go-Around Switch Electric Trim A/P Disconnect Control Wheel Steering Button Electronic Checklists C406-N Three-Frequency Emergency Locator Transmitter Emergency Locator Transmitter Remote Mounted Switch Backup Attitude Gyro, Altimeter and Airspeed Indicator Control Wheel Push-To-Talk Switch-Pilot/Copilot Mic & Phone Jacks-Pilot/Copilot/ Passengers Auxiliary Stereo Input Jack Antennas: Marker Beacon Antenna Transponder Antenna VHF/GPS Antenna (2)` XM Antenna NAV Antenna Emergency Locator Transmitter External Antenna Stormscope Antenna Pitot System — Heated Static System Handheld Microphone Alternate Static Source Compass Detailed Specifications Performance data is based on the standard Turbo Stationair 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 28 ft 3 in (8.61 m) Height 9 ft 4 in (2.83 m) Wingspan 36 ft (10.97 m) Wing Wing Area 174 sq ft (16.17 sq m) Wheelbase 5 ft 9 in (1.76 m) Tread 8 ft 1 in (2.46 m) Cabin Interior Height Width Length 50 in (1.26 m) 43 in (1.08 m) 12 ft 1 in (3.68 m) Maximum Passengers 6 Baggage Capacity Weight Volume 180 lb (81.6 kg) 11 cu ft (0.31 cu m) Weights Maximum Ramp Weight 3,617 lb (1,641 kg) Maximum Takeoff Weight 3,600 lb (1,633 kg) Maximum Landing Weight 3,600 lb (1,633 kg) Maximum Zero Fuel Weight N/A Usable Fuel Capacity Weight Volume 522 lb (237 kg) 87 gal (329 l) Basic Operating Weight 2,336 lb (1,060 kg) Useful Load 1,281 lb (581 kg) Maximum Payload 1,264 lb (573 kg) Full Fuel Payload 759 lb (344 kg) Performance Maximum Cruise Speed 164 ktas (304 km/h) Maximum Range 703 nm (1,302 km) Takeoff Takeoff Distance Ground Roll 1,740 ft (530 m) 910 ft (277 m) Landing Landing Distance Ground Roll 1,395 ft (425 m) 735 ft (224 m) Maximum Operating Altitude 25,000 ft (7,620 m) Maximum Climb Rate 1,050 fpm (320 mpm) Maximum Limit Speed 182 kias (337 km/h) Stall Speed 54 kcas (100 km/h) Powerplant With its 310 horsepower turbocharged powerplant, the Turbo Stationair serves up more muscle and better climb, so you can soar at greater speeds in higher altitudes. And not only that, but this phenomenal aircraft also delivers legendary payload capacity and additional safety margins, especially during high-hot operations. Smooth, quick climbs to altitudes as high as 27,000 feet mean less traffic and terrain, along with more favorable winds. Turbo Stationair Powerplant Manufacturer: Textron Lycoming Model: (1) TIO-540-AJ1A Power Output: 310 hp Propeller Manufacturer: McCauley Description: 3-blade metal, constant speed
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Technical Specifications

  Cessna Aircraft Company
Product Category Aircraft
Product Number Cessna Turbo Stationair®
Product Name Single Engine Aircraft
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