Citation M2

Maximum Range

1,550 nm

Maximum Cruise Speed

404 ktas

Maximum Passengers


Useful Load

3,810 lb

Takeoff Field Length

3,210 ft

Engine Model


Bold Move

The CESSNA CITATION M2 jet is the ultimate combination of beauty and efficiency. The M2 is the entry level jet that pilots have been asking for. Speed, control, range and comfort complete the aircraft providing you with serious jet performance.

Perfect for corporate, charter or private use, the M2 features in-cabin technology, touch-controlled avionics suited for a single pilot and two powerful Williams FJ44 engines, facilitating cruising speed of up to 404 knots. A GARMIN G3000 flight deck provides an ideal flying experience.

The Citation M2 jet delivers fast, efficient trips with exceptional range at 1,550 nm. The interior is finished with category-leading craftsmanship and room for up to seven passengers. A wireless cabin management system and LED lighting finish off the design.

Striking Style

The Citation M2’s aluminum airframe was engineered with multiple structural load paths, system redundancies, and optimal aerodynamics.
Connectivity and Control
The optional cabin management system, moving map, and in-flight entertainment system keep you connected and in control.
Traveling and style and comfort
The interior layout provides seatings for up to seven passengers to work and relax comfortably with eight large windows to emphasize the spaciousness of the cabin
Elegant cabin design

The M2 offers a wide selection of custom configurations with an all-new interior, in-cabin technologies, climate control and adjustable lighting



Improved speed and clarity describe the new GARMIN G3000 avionics suite in the CESSNA CITATION M2 jet. Brand new hardware and software mean significant speed and resolution enhancements. Not only is the display resolution greatly improved for operators, but the system boots up, processes and loads databases faster than ever before.
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.

Reliability and Awareness

The CJ3+ is equipped with a fully digital, dual-channel autopilot (AP) system equipped with many features for added redundancy and reliability. Integrating data from the avionics system, the AP is built to inspire confidence while ensuring smoothness and comfort. The system is powered by the Garmin® GFC™ 700, a control system that has a flight director, autopilot, yaw damper, and features that provide top-level performance. The GFC 700 allows for outstanding flight automation and precision. The AP maximizes aircraft performance with precise lateral and vertical navigation guidance for all phases of flight. It can maintain altitude, airspeed, vertical speed, and heading, in addition to flying VNAV descent profiles, automated Takeoff/Go-Around procedures, and more. The CJ3+ has an AP system that is simple and straightforward to operate yet sophisticated and state-of-the-art, which makes flying the CJ3+ easier, safer, more consistent, and more enjoyable.

Length 42 ft 7 in (13.0 m)

Height 13 ft 11 in (4.2 m)

Wingspan 47 ft 3 in (14.39 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)

New Standered Features 


HSI Map Overlays

Visual Approach Support

IFR/VFR Charts in Map


Flight Stream 510 (No Cost Option)


FAA Data Comm

XM Weather Animation

Standard Features 

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


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

Equipment details 


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


Electrical Power Panel

Left-Hand Primary Flight Display (PFD)

Multifunction Display (MFD)

Right-Hand Primary Flight Display (PFD)


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


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


Emergency Brake Handle

Parking Brake Handle

Emergency Gear Release

Control Locks

Rain Removal levers

Height 57 in (1.4 m)

Width 58 in (1.47 m)

Length 11 ft (3.4 m)

Maximum Passengers 7

Single Pilot Certified Yes


Weight 725 lb (329 kg)

Volume 45.6 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 8,500 lb (3,856 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 1,510 lb (685 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)