2014 CESSNA CITATION M2


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    Aircraft Summary


    General

    Year
    2014
    Manufacturer
    CESSNA
    Model
    CITATION M2
    Condition
    New
    Description
    2014 Delivery; Choose your Colors & Options! The M2 is equipped with a fully digital, dual-channel autopilot system (AP) equipped with many features for added safety, redundancy, and reliability. Integrating data from the avionics system, the AP is built to inspire confidence while ensuring optimum smoothness and comfort.

    Airframe

    Total Time
    0.0
    Airframe Notes
    The M2 is equipped with a fully digital, dual-channel autopilot system (AP) equipped with many features for added safety, redundancy, and reliability. Integrating data from the avionics system, the AP is built to inspire confidence while ensuring optimum smoothness and comfort. The system is powered by the Garmin GFC 700 scalable architecture and uses prestored airspeed-limit data along with autopilot gains that are scheduled to optimize performance to offer excellent stability and control. The AP maximizes aircraft performance with precise lateral and vertical navigation guidance for all phases of flight. It can maintain attitude, altitude, airspeed, vertical speed, and heading, in addition to flying VNAV descent profiles, automated Takeoff/Go-Around procedures, and more. 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 sq m) • 0.0 degrees Cabin Interior • Height • Width • Length • 57 in (1.45 m) • 58 in (1.47 m) • 11 ft (3.35 m) • Seating Capacity • 7 - 7 Baggage Capacity • Weight • Volume • 725 lb (329 kg) • 46 cu ft (1.29 cu m) • Single Pilot Certified • Yes Wingspan – 47 ft 3 in (14.40 m) Height 13 ft 11 in (4.24 m) Length – 42 ft 7 in (12.98 m) 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) • Weight • Volume • 3,309 lb (1,501 kg) • 494 gal (1,870 l) • Basic Operating Weight • 6,991 lb (3,171 kg) • Useful Load • 3,809 lb (1,728 kg) • Maximum Payload • 1,409 lb (639 kg) • Full Fuel Payload • 500 lb (227 kg) Performance • Maximum Cruise Speed • 400 ktas (741 km/h) • Range • 1,300 nm (2,408 km) • Takeoff Distance • 3,250 ft (991 m) • Landing Distance • 2,640 ft (805 m) • Maximum Operating Altitude • 41,000 ft (12,497 m) • Maximum Climb Rate • N/A fpm (N/A mpm) • Maximum Limit Speed • 0.710 Mach

    Engine Program

    Engine Program Notes
    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: 4,000 hr

    Avionics

    Avionics/Radios
    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 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: GTC 570 (2) each 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

    Additional Equipment

    Additional Equipment
    OPTIONS 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

    Interior

    Interior Notes
    Choose Your Floorplan optional 4 or 5 Passenger Interiors! The M2 cabin is equipped with indirect overhead LED lighting, as well as LED reading lights above each passenger seat. Each seat is also equipped with adjustable air vents for comfort. The headliner and valance design give passengers ample seated headroom while eight large windows heighten the sense of spaciousness. Six distinctive color selections are available for the interior furnishings as part of the base price of the aircraft: Pearl, Raffia, Mink, Citrus, Frost, and Carbon. Each interior design selection offers a complementary blend of the finest fabrics, leathers, tailored carpet, and high-durability painted coatings.


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