Manufacturer
ACJ TwoTwenty (based on the A220-100)
ACJ319neo
ACJ320neo
ACJ330neo (specifically the ACJ330-800)
ACJ350 (specifically the ACJ350-900 XWB)
BBJ 737 MAX 7 (also known as BBJ MAX 7),
BBJ 737 MAX 8 (BBJ MAX 8)
BBJ 737 MAX 9 (BBJ MAX 9)
Citation XLS Gen2
PC-12 NGX
PC-24
HondaJet Elite II
Alice
Vision Jet SF50 G2+
TBM 960
Kodiak 100 Series III
Kodiak 900
Model Data
M2 GEN2
Cessna Citation M2 Overview
Introduction:
The Citation M2 is a sleek and modern light jet designed as the entry-level model in Cessna’s Citation lineup. It delivers an impressive blend of speed, performance, and comfort while maintaining simplicity for single-pilot operations. Ideal for owner-operators and charter services, the M2 combines cutting-edge avionics, a refined cabin, and operational efficiency to excel in short to medium-range missions.
Length 42 ft 7 in (13.0 m)
DIMENSIONS
| 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) |
CABIN INTERIOR
| 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 |
BAGGAGE CAPACITY
| Weight | 725 lb (329 kg) |
| Volume | 45.6 cu ft (1.29 cu 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 | 8,500 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) |
PERFORMANCE
| 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) |
POWERPLANT
| Manufacturer | Williams International |
| Model | FJ44-1AP-21 |
| Thrust | 1,965 lb (8.74 kN) |
CABIN INTERIOR
| 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 |
Standard
- Garmin FMS with dual WAAS-enabled GPS receivers for navigation
- Garmin Emergency Autoland
- Terrain Avoidance and Warning System (TAWS-B)
- Traffic Collision and Avoidance System (TCAS I)
- Dual Attitude Heading Reference System (AHRS)
- Dual Air Data Computers
- Jeppesen Chartview
- Garmin Safe Taxi
- Digital Audio System
- ADS-B OUT / ADS-B IN
- HSI Map Overlays
- Visual Approach Support
- IFR/VFR Charts in Map
- Full Regime Garmin Autothrottles
- GDL 60 Datalink
- Garmin GWX 8000 StormOptix Weather Radar
- Onboard Maintenance Diagnostics Systems
- Provisions for Cockpit Voice Recorder (CVR)
Optional
- Garmin SVT Synthetic Vision Technology
- Terrain Avoidance and Warning System (TAWS-A)
- Traffic Collision and Avoidance System (TCAS II)
- SiriusXM Satellite Radio and Weather
- Satellite Phone System
- HF-9000 High Frequency Communications
- Enhanced Vision System (EVS)
- FANS-1/A over VHF
- FAA Data Comm
- ATN-B1