Cessna Aircraft Company Business Jet Citation Longitude

Our entry into the super midsize jet category is going straight to the top. With a 4,000 nm range, a Mach.86 cruising speed and a 45,000 foot maximum cruising altitude , the Citation Longitude delivers far more performance than other midsize jets far more efficiently. Performance is not the only bar-raising characteristic of the Longitude. It also sets a new standard in private business travel for cabin efficiency, technology and comfort. Standard Features: Flight Displays Synthetic Vision Technology Touch-screen Control Panels Automatic Flight Control System Inertial Reference Systems (IRS) 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 Longitude 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 87 ft (26.52 m) Height 26 ft (7.92 m) Wingspan 86 ft (26.21 m) Wing Wing Area Wing Sweep N/A 30.0 degrees Wheelbase N/A Tread N/A Cabin Interior Height Width Length 72 in (1.83 m) 77 in (1.96 m) 28 ft 11 in (8.81 m) Maximum Passengers 12 Baggage Capacity Weight Volume N/A 100 cu ft (2.83 cu m) Single Pilot Certified No Weights Maximum Ramp Weight N/A Maximum Takeoff Weight N/A Maximum Landing Weight N/A Maximum Zero Fuel Weight N/A Usable Fuel Capacity Weight Volume N/A N/A Basic Operating Weight N/A Useful Load N/A Maximum Payload N/A Full Fuel Payload N/A Performance Maximum Cruise Speed 490 ktas (907 km/h) Maximum Range 4,000 nm (7,408 km) Takeoff Field Length 5,400 ft (1,646 m) Landing Distance N/A Maximum Operating Altitude 45,000 ft (13,716 m) Maximum Climb Rate N/A Maximum Limit Speed 0.86 Mach (0.86 Mach) Powerplant The Snecma Silvercrest™ SC-2C is the next generation business jet engine and is making its debut in the Citation Longitude. With Silvercrest, Snecma gives Citation its best-in-class technologies, based on its long-standing expertise in military aircraft engines, as well as 36 years of experience within the CFM joint venture (GE and Snecma) for the best selling CFM56 commercial aero-engine. Manufacturer: Snecma Silvercrest® SC-2C Thrust: Over 11,000 lbf each at takeoff Fuel burn: 15% lower than engines with similar thrust Noise level: Up to 20 EPNdB vs. Stage 4 Emission: 50% margin vs. CAEP/6