• Maximum Range

    1,550 nm

  • Maximum Cruise Speed

    404 ktas

  • Maximum Occupants


  • Useful Load

    3,810 lb

  • Takeoff Field Length

    3,210 ft

Achieve new heights

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.


Striking Style

The Citation M2’s aluminum airframe was engineered with multiple structural load paths, system redundancies, and optimal aerodynamics.

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Treat Yourself To Comfort

  • Standard
  • Side-Facing Seat

Select Your Personal Touches

  • Carbon

    Dark and sleek sophistication with bright, metallic accents gives the Carbon Collection a sporty, classic feel.

  • Citrus

    Crisp, textural fabrics combine with deep, warm tones to create an atmosphere of lively, elegant style.

  • Frost

    A modern blend of light vinyl, silks, and soft leathers contrasted with darker trims and carpet comprise the powerful Frost Collection.

  • Mink

    Rich, dimensional textures and smooth, silky finishes create the refined and polished artistry of the Mink collection.

  • Pearl

    Inspired by the polished, soft ivory of pearls, the Pearl Collection features lighter textured fabrics and deeper toned leathers for an open, airy feel.

  • Raffia

    The stylish Raffia Collection weaves together subtle earth tones offset with darker accents for an elegant and soothing professional atmosphere.


Precision At Your Command

User-friendly touch screens powered by Garmin® G3000™ avionics make for intuitive control, while Synthetic Vision Technology (SVT™) provides a clear, concise picture of your flying environment.

The M2 is equipped with a fully digital, dual-channel autopilot system 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 uses pre-stored airspeed-limit data along with autopilot gains that are scheduled to optimize performance to offer excellent stability and control. The autopilot maximizes aircraft performance with precise lateral and vertical navigation guidance for all phases of flight.

The autopilot system is simple and straightforward to operate yet sophisticated and state-of-the-art, which makes flying the M2 easier, consistent and more enjoyable.

Real-time Diagnostics. Real-time answers.

LinxUs is compatible on the Citation M2 when equipped with the Garmin GDL™59 (Wi-Fi Datalink) and Garmin GSR™56 (Iridium Satellite Receiver). LinxUs technology saves time and money. Working with the Central Diagnostics Maintenance system (CDMS) LinxUs and LinxUs Air, both function as a fault-isolation system that monitors the aircraft 100 percent of the time. In the event of an onboard issue, actionable answers are provided in real time, resulting in faster turnaround to get the aircraft back in the air.

LinxUs – reports issues upon landing with a Wifi connection.
LinxUs Air – reports issues in flight via satellite (For aircraft equipped with GSR56).

  • 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 Attitude Heading Reference System
  • Dual Air Data computers
  • Jeppesen ChartView
  • Garmin Safe Taxi
  • Digital Audio System
Optional Avionics Include
  • Garmin SVT™ Synthetic Vision Technology
  • Domestic and International Internet
  • XM Satellite Weather and Radio
  • Traffic Collision Avoidance System (TCAS II)
  • Terrain Awareness Warning System Class A (TAWS-A)
  • Cabin Briefer
  • Satellite phone system
  • HF-9000 High Frequency Communications
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 on Pedestal
  • Emergency Brake Handle
  • Parking Brake Handle
  • Emergency Gear Release
  • Control Locks
  • Rain Removal levers



42 ft 7 in (12.98 m)


13 ft 11 in (4.24 m)


47 ft 3 in (14.40 m)


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 Area 240 sq ft (22.3 sq m)
Wing Sweep 0.0 degrees
Wheelbase 15 ft 4 in (4.67 m)
Tread 13 ft (3.96 m)

Cabin Interior

Height 57 in (1.45 m)
Width 58 in (1.47 m)
Length 11 ft (3.35 m)
Maximum Occupants 7
Single Pilot Certified Yes

Baggage Capacity

Weight 725 lb (328.9 kg)
Volume 46 cu ft (1.29 cu m)


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 Weight 3,296 lb (1,495 kg)
Usable Fuel Volume 492 gal (1,862 l)
Basic Operating Weight 6,990 lb (3,171 kg)
Useful Load 3,810 lb (1,728 kg)
Maximum Payload 1,410 lb (640 kg)
Full Fuel Payload 514 lb (233 kg)


Maximum Cruise Speed 404 ktas (748 km/h)
Maximum Range 1,550 nm (2,871 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)


Manufacturer Williams International
Model FJ44-1AP-21
Thrust 1,965 lb (8.74 kN)