Cessna Aircraft Company Single Engine Aircraft Cessna Skyhawk®

The Cessna Skyhawk® is the ultimate training aircraft and the most popular single-engine aircraft ever built. With the Garmin® G1000™ and GFC 700 autopilot, it delivers an intuitive cockpit experience matched with a highly durable air-frame with forgiving flying characteristics. This superior platform is ideally suited to learn the skills needed to become a true pilot in command. Accept nothing less than excellence Our engineering team designed the Skyhawk’s cockpit with the latest in avionic technology and the most advanced application of ergonomic sciences available. The flight deck is powered by the Garmin G1000® avionics suite, including optional integrated Garmin Synthetic Vision Technology (SVT™) and an automatic flight control system. Two 10.4-inch, high-resolution liquid crystal displays show flight instrumentation, traffic data, digital altitude, moving maps, navigation, communication, and other real-time flight-critical data. See the future The Skyhawk’s flight deck can include the optional Garmin Synthetic Vision Technology (SVT™), which offers sophisticated graphics modeling of terrain, traffic, and obstacles in the flight path. The system looks at the entire flight path via satellite and renders a three-dimensional “virtual reality” landscape, which is displayed on one or both primary flight displays. This technology prepares you for what lies ahead in plenty of time to plan for it and gives you a clear visual of any traffic around your aircraft, even in solid IFR (instrument flight rules) or nighttime VFR (visual flight rules) conditions. Digital weather radar With the optional GDL 69A data link receiver and a subscription to XM WX Satellite Weather, you will see a high-resolution representation of the weather along your flight path on your high-resolution primary flight display. The GDL 69 offers NEXRAD, METARs, TAFs, lightning, and more that you can layer directly over optional Jeppesen or standard topographic map databases. Global weather information is available through the optional GSR 56, which connects you to the Iridium satellite network. Voice and text messaging connectivity as well as position reporting and digital color radar data are included. The following list of equipment is included on the standard Skyhawk with the Garmin 1000 Avionics Package and does not reflect optional equipment: 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 Electronic Checklists 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/Passen gers Auxiliary Stereo Input Jack Antennas: Marker Beacon Antenna Transponder Antenna VHF/GPS Antenna (2) NAV Antenna Emergency Locator Transmitter External Antenna Pitot System — Heated Static System Handheld Microphone Alternate Static Source Detailed Specifications Performance data is based on the standard Skyhawk 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 27 ft 2 in (8.28 m) Height 8 ft 11 in (2.72 m) Wingspan 36 ft 1 in (11.00 m) Wing Wing Area 174 sq ft (16.17 sq m) Wheelbase 5 ft 5 in (1.65 m) Tread N/A Cabin Interior Height Width Length 48 in (1.22 m) 40 in (1.00 m) 11 ft 10 in (3.61 m) Maximum Passengers 4 Baggage Capacity Weight Volume 120 lb (54.4 kg) 30 cu ft (0.85 cu m) Weights Maximum Ramp Weight 2,558 lb (1,160 kg) Maximum Takeoff Weight 2,550 lb (1,157 kg) Maximum Landing Weight 2,550 lb (1,157 kg) Maximum Zero Fuel Weight N/A Usable Fuel Capacity Weight Volume 318 lb (144 kg) 53 gal (201 l) Basic Operating Weight 1,640 lb (744 kg) Useful Load 918 lb (416 kg) Maximum Payload 910 lb (413 kg) Full Fuel Payload 600 lb (272 kg) Performance Maximum Cruise Speed 124 ktas (230 km/h) Maximum Range 640 nm (1,185 km) Takeoff Takeoff Distance Ground Roll 1,630 ft (497 m) 960 ft (293 m) Landing Landing Distance Ground Roll 1,335 ft (407 m) 575 ft (175 m) Maximum Operating Altitude 14,000 ft (4,267 m) Maximum Climb Rate 730 fpm (223 mpm) Maximum Limit Speed 163 kias (302 km/h) Stall Speed 48 kcas (89 km/h) Powerplant Lycoming piston-aircraft engines currently power more than half the world’s general aviation fleet and are known for reliability and durability. This horizontally opposed, air-cooled, four-cylinder, fuel-injected aircraft engine provides the power of 180 horses. Manufacturer: Textron Lycoming Model: (1) IO-360-L2A Power Output: 180 hp Propeller Manufacturer: McCauley Description: 2-blade metal, fixed pitch