Cessna Aircraft Company Business Jet Citation® M2®

The Citation® M2® jet is the ultimate combination of beauty and efficiency. The M2 is the entry level jet that pilots have been asking for. Perfect for corporate, charter or private use, the M2 features a redesigned interior with excellent in-cabin technologies, updated touch-controlled avionics suited for a single pilot and two powerful Williams FJ44 engines, facilitating cruising speed of up to 400 knots. Standard avionics include: Garmin FMS with dual WAAS-enabled GPS receivers for navigation Weather Avoidance Radar Terrain Avoidance Warning System (TAWS-B) Garmin Traffic Collision and Avoidance System (TCAS I) Dual Altitude Heading Reference System Dual Air Data computers Jeppesen ChartView Garmin Safe Taxi Digital Audio System Optional avionics include: Garmin SVT™ Synthetic Vision Technology Terrain Awareness Warning System Class A (TAWS-A) SiriusXM Satellite Radio Garmin TCAS II Garmin Surface Watch TAWS-A Cabin Briefer Satellite phone system Domestic and International Internet Installed on Center Glareshield Panel: LH and RH Master Caution/Master Warning Lights LH and RH Engine Fire Control Switches Reversionary and Dimming Controls Flight Director / Autopilot Controller Electronic Standby Instrument System LH and RH Display Control Units Installed on Instrument Panel (left to right): Electrical Power Panel Left-Hand Primary Flight Display (PFD) Multifunction Display (MFD) Right-Hand Primary Flight Display (PFD) Installed on Tilt Panel (left to right): Pressurization Controls Ice Protection Controls Windshield Anti-ice Controls Fuel Controls Ignition Controls Landing Gear Control Module Lighting Controls Emergency Communications Switch Event Marker Cockpit Voice Recorder Controller Flight Hour Meter ELT Remote Switch Installed on Pedestal: Garmin Touch Screen Controllers Engine Start Control Engine Power Levers Flap Control Handles Speed Brake Control Elevator Trim Control and Indicator Takeoff/Go-Around Button Rudder Trim Control Aileron Trim Control Installed Beneath the Instrument Panel: Emergency Brake Handle Parking Brake Handle Emergency Gear Release Control Locks Rain Removal levers Detailed Specifications Performance data is based on the standard M2 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 42 ft 7 in (12.98 m) Height 13 ft 11 in (4.24 m) Wingspan 47 ft 3 in (14.40 m) Wing Wing Area Wing Sweep 240 sq ft (22.3 sq m) 0.0 degrees Wheelbase 15 ft 4 in (4.67 m) Tread 13 ft (3.96 m) Cabin Interior Height Width Length 57 in (1.45 m) 58 in (1.47 m) 11 ft (3.35 m) Maximum Passengers 7 Baggage Capacity Weight Volume 725 lb (328.9 kg) 46 cu ft (1.29 cu m) Single Pilot Certified Yes Weights Maximum Ramp Weight 10,800 lb (4,899 kg) Maximum Takeoff Weight 10,700 lb (4,853 kg) Maximum Landing Weight 9,900 lb (4,491 kg) Maximum Zero Fuel Weight 8,400 lb (3,810 kg) Usable Fuel Capacity Weight Volume 3,296 lb (1,495 kg) 492 gal (1,862 l) Basic Operating Weight 7,004 lb (3,177 kg) Useful Load 3,796 lb (1,722 kg) Maximum Payload 1,396 lb (633 kg) Full Fuel Payload 500 lb (227 kg) Performance Maximum Cruise Speed 404 ktas (748 km/h) Maximum Range 1,540 nm (2,852 km) Takeoff Field Length 3,210 ft (978 m) Landing Distance 2,590 ft (789 m) Maximum Operating Altitude 41,000 ft (12,497 m) Maximum Climb Rate 3,698 fpm (1,127 mpm) Maximum Limit Speed 0.71 Mach (0.71 Mach) Powerplant Two Williams FJ44 turbofan engines are installed on the Citation M2. This engine is a 2.58:1 bypass, twin-spool design with three compression stages and three turbine stages and produces 1,965 pounds (8.74 kN) of takeoff thrust at sea level, static conditions, flat-rated up to 72° F (22° C). Dual-channel full authority digital engine controls (FADECs) provide automation and efficiency in engine management. Manufacturer: Williams International Model: (2) FJ44-1AP-21 Thrust: 1,965 lbf Time Between Overhaul: 3,500 hr