Cessna Aircraft Company Business Jet Citation® CJ3+®

Description
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

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Business Jet Citation® CJ3+®
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

  • 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
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Technical Specifications

  Cessna Aircraft Company
Product Category Aircraft
Product Number Citation® CJ3+®
Product Name Business Jet
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