The Citation® CJ3+® jet delivers superior unparalleled reliability without sacrificing productivity and comfort. With upgraded Intrinzic™ flight deck power by Garmin® G3000™, operating this single-pilot certified jet is so intuitive; it’s fueling the passion for flight in pilots and passengers alike.
Standard Features:
Garmin FMS with dual WAAS-enabled GPS receivers for navigation
Weather Avoidance Radar
Terrain Avoidance Warning System (TAWS-B)
Traffic Collision and Avoidance System (TCAS II)
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
Cabin Briefer
Satellite phone system
Domestic and International Internet
XM Satellite Weather and Radio
HF-9000 High Frequency Communications 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 Center 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 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
Decision Height Warning
Detailed Specifications
Performance data is based on the standard CJ3+ 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.
Dimensions
Length
51 ft 2 in (15.59 m)
Height
15 ft 2 in (4.62 m)
Wingspan
53 ft 4 in (16.26 m) Wing
Wing Area
Wing Sweep
294 sq ft (27.32 sq m)
0.0 degrees Wheelbase
20 ft (6.10 m) Tread
16 ft (4.88 m) Cabin Interior
Height
Width
Length
57 in (1.45 m)
58 in (1.47 m)
15 ft 8 in (4.78 m)
Maximum Passengers
9 Baggage Capacity
Weight
Volume
1,000 lb (453.6 kg)
65 cu ft (1.84 cu m)
Single Pilot Certified
Yes
Weights
Maximum Ramp Weight
14,070 lb (6,382 kg)
Maximum Takeoff Weight
13,870 lb (6,291 kg)
Maximum Landing Weight
12,750 lb (5,783 kg)
Maximum Zero Fuel Weight
10,510 lb (4,767 kg) Usable Fuel Capacity
Weight
Volume
4,710 lb (2,136 kg)
703 gal (2,661 l)
Basic Operating Weight
8,540 lb (3,874 kg)
Useful Load
5,530 lb (2,508 kg)
Maximum Payload
1,970 lb (894 kg)
Full Fuel Payload
820 lb (372 kg)
Performance
Maximum Cruise Speed
416 ktas (770 km/h)
Maximum Range
2,040 nm (3,778 km)
Takeoff Field Length
3,180 ft (969 m)
Landing Distance
2,770 ft (844 m)
Maximum Operating Altitude
45,000 ft (13,716 m)
Maximum Climb Rate
4,478 fpm (1,365 mpm)
Maximum Limit Speed
0.737 Mach (0.737 Mach)
Powerplant
Two, dual-channel FADEC-controlled, Williams FJ44-3A turbofan engines are installed on the CJ3+. The engine is a medium-bypass, twin-spool design with five compression stages and three turbine stages. It produces 2,820 pounds (12.54kN) of thrust at sea level, static conditions, flat-rated up to 79˚F (26˚C.) The FADEC system also provides time-limited dispatch, diagnostics and engine synchronization.
Manufacturer: Williams International
Model: (2) FJ44-3A
Thrust: 2,820 lbf
Time Between Overhaul: 4,000 hrs
The Citation® CJ3+® jet delivers superior unparalleled reliability without sacrificing productivity and comfort. With upgraded Intrinzic™ flight deck power by Garmin® G3000™, operating this single-pilot certified jet is so intuitive; it’s fueling the passion for flight in pilots and passengers alike.
Standard Features:
- Garmin FMS with dual WAAS-enabled GPS receivers for navigation
- Weather Avoidance Radar
- Terrain Avoidance Warning System (TAWS-B)
- Traffic Collision and Avoidance System (TCAS II)
- 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
- Cabin Briefer
- Satellite phone system
- Domestic and International Internet
- XM Satellite Weather and Radio
- HF-9000 High Frequency Communications
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 Center 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 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
- Decision Height Warning
Detailed Specifications
Performance data is based on the standard CJ3+ 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.
Dimensions
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Wing
- Wing Area
- Wing Sweep
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- 294 sq ft (27.32 sq m)
- 0.0 degrees
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Cabin Interior
- Height
- Width
- Length
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- 57 in (1.45 m)
- 58 in (1.47 m)
- 15 ft 8 in (4.78 m)
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Baggage Capacity
- Weight
- Volume
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- 1,000 lb (453.6 kg)
- 65 cu ft (1.84 cu m)
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Weights
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Usable Fuel Capacity
- Weight
- Volume
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- 4,710 lb (2,136 kg)
- 703 gal (2,661 l)
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Performance
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- Maximum Operating Altitude
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Powerplant
Two, dual-channel FADEC-controlled, Williams FJ44-3A turbofan engines are installed on the CJ3+. The engine is a medium-bypass, twin-spool design with five compression stages and three turbine stages. It produces 2,820 pounds (12.54kN) of thrust at sea level, static conditions, flat-rated up to 79˚F (26˚C.) The FADEC system also provides time-limited dispatch, diagnostics and engine synchronization.
- Manufacturer: Williams International
- Model: (2) FJ44-3A
- Thrust: 2,820 lbf
- Time Between Overhaul: 4,000 hrs