Cessna Aircraft Company Business Jet Citation® Latitude®

Fly farther in the widest Citation in the sky. The Citation® Latitude® jet boasts the most spacious, most refined cabin environment in the midsize jet category. At 77 inches wide, six feet tall and more than 21 feet long with a flat floor, stand up cabin, the Latitude was built for comfort. We surrounded the Citation Latitude’s clean, contemporary design in an aircraft built to our rigorous standards. Standard Features Flight Displays Synthetic Vision Technology Touch-screen Control Panels Automatic Flight Control System Attitude Heading Reference Systems (AHRS) Integrated Avionics Units Distance Measuring Equipment Flight Management Systems Weather Radar Traffic Collision Avoidance System (TCAS II) Terrain Awareness Warning System (TAWS) Transponders with ADS-B Out Capability Standby Instrumentation Radio Altimeter Cockpit Voice Recorder Emergency Locator Transmitter Maintenance Diagnostics Installed on Left-Hand Panel (pilot): Touch-screen LCD Control Panel Primary Flight Display (PFD) Secondary PFD Controller Installed on Right-Hand Panel (copilot): Touch-screen LCD Control Panel Primary Flight Display (PFD) Secondary PFD Controller Installed on Center Panel: Multifunction Display (MFD) Dual Touch-screen LCD Control Panels Electronic Standby Flight Display (ESFD) Installed Beneath Glareshield: Flight Guidance Panel (FGP) Installed on LH Tilt Panel: Electrical Power Panel Installed on RH Tilt Panel: Anti-Ice/De-Ice Panel Landing Gear Control Panel Installed on Pedestal: Engine Power Levers Flaps Control Switch in Throttle Lever Pressurization Panel Engine Control/Start Panel Cockpit/Cabin Temperature Panel Fuel, APU, and Hydraulics Detailed Specifications Performance data is based on the standard Latitude 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. Preliminary data, subject to change. Dimensions Length 62 ft 3 in (18.97 m) Height 20 ft 11 in (6.38 m) Wingspan 72 ft 4 in (22.05 m) Wing Wing Area Wing Sweep 543 sq ft (50.4 sq m) 12.7 degrees Wheelbase 27 ft (8.23 m) Tread 10 ft (3.05 m) Cabin Interior Height Width Length 72 in (1.83 m) 77 in (1.96 m) 21 ft 9 in (6.63 m) Maximum Passengers 9 Baggage Capacity Weight Volume 1,245 lb (564.7 kg) 127 cu ft (3.6 cu m) Single Pilot Certified No Weights Maximum Ramp Weight 31,050 lb (14,084 kg) Maximum Takeoff Weight 30,800 lb (13,971 kg) Maximum Landing Weight 27,575 lb (12,508 kg) Maximum Zero Fuel Weight 21,200 lb (9,616 kg) Usable Fuel Capacity Weight Volume 11,394 lb (5,168 kg) 1,700 gal (6,435 l) Basic Operating Weight 18,656 lb (8,462 kg) Useful Load 12,394 lb (5,622 kg) Maximum Payload 2,544 lb (1,154 kg) Full Fuel Payload 1,000 lb (454 kg) Performance Maximum Cruise Speed 446 ktas (826 km/h) Maximum Range 2,700 nm (5,000 km) Takeoff Field Length 3,668 ft (1,118 m) Landing Distance 2,681 ft (817 m) Maximum Operating Altitude 45,000 ft (13,716 m) Maximum Climb Rate N/A Maximum Limit Speed 0.80 Mach (0.80 Mach) Powerplant Two Pratt & Whitney Canada™ PW306D1 turbofan engines are installed on the Citation Latitude. The engine is a twin-spool design with a damage-resistant wide chord fan. Behind the fan, four axial and one centrifugal compressor stages lead to a high-efficiency, low-emission, through-flow combustion and five turbine stages. Two-stage variable inlet guide vanes and bleed-off valves are controlled by the FADEC to optimize compressor and engine performance. Manufacturer: Pratt & Whitney Canada Model: (2) PW306D1 Thrust: 5,760 lb Time Between Overhaul: 6,000 hrs