Cessna Aircraft Company Business Jet Citation® CJ4®

Description
The Citation® CJ4® jet redefines versatility for a light jet. The CJ4 has added speed, range and cabin size over its predecessor without incurring midsize jet operating costs.The Collins Pro Line 21™ avionics suite allows a single pilot to safely and effectively operate the CJ4. Features such as single point refueling, an externally serviceable lavatory and excellent range deliver what crew and cabin passengers appreciate. Standard Features Dual Primary Flight Displays Dual Multifunction Displays Single Flight Management System with GPS Navigation Integrated Flight Guidance System Crew Alerting System Integrated Electronic Checklists Electronic Jeppesen Charts Dual Attitude Heading Reference Systems XM Broadcast Graphical Weather MultiScan Weather Radar Mark VIII Enhanced Ground Proximity Warning System TCASII Optional avionics include: Mark V Enhanced Ground Proximity Warning System with Runway Awareness Dual Flight Management System High-Frequency Radio with SELCAL 88-Parameter Flight Data Recorder ACARS Data Link Installed in Center Glareshield Panel: LH and RH Master Warning/Master Caution Lights LH and RH Display Control Panel CVR Microphone LH and RH Engine Fire Control Switches Flight-Guidance Panel Reversion Controls Installed on Instrument Panel (left to right): LH Digital Audio Control Panel Avionics/Electrical Power Panel LH Primary Flight Display (PFD) LH Multifunction Display (MFD) Electronic Standby Instrument System Landing-Gear Control Module RH Multifunction Display (MFD) RH Primary Flight Display (PFD) RH Digital Audio Control Panel Cockpit Voice Recorder Controller Database Loading Unit (DBU) Installed on Tilt Panel (left to right): Oxygen Controls Cockpit Temperature Controls Fuel Controls Manual Ignition Control FADEC Switches Pressurization Controls Ice-Protection Switches Curser Control Panels (CCP) Collins FMS-3000 Control Display Unit (CDU) Push-to-Talk Switch Cockpit Speaker Mute Switch Event Switch Cabin Temperature Controls ELT Remote Switch Flight Hour Meter Installed on Pedestal: Lighting and Dimming Controls Engine Power Levers Flap-Control Handle Speed Brake Control Handle Engine Start Control Aileron Trim Control Rudder Trim Control Secondary Elevator Trim Control Installed Beneath Tilt Panel: Emergency Brake Handle Control Lock Parking Brake Handle Installed in Floor Aft of Center Pedestal: Emergency Gear Extension Handle Detailed Specifications Performance data is based on the standard CJ4 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 53 ft 4 in (16.26 m) Height 15 ft 5 in (4.69 m) Wingspan 50 ft 10 in (15.49 m) Wing Wing Area Wing Sweep 330 sq ft (30.66 sq m) 12.5 degrees Wheelbase 21 ft 2 in (6.45 m) Tread 12 ft 4 in (3.76 m) Cabin Interior Height Width Length 57 in (1.45 m) 58 in (1.47 m) 17 ft 4 in (5.28 m) Maximum Passengers 10 Baggage Capacity Weight Volume 1,040 lb (471.7 kg) 77 cu ft (2.18 cu m) Single Pilot Certified Yes Weights Maximum Ramp Weight 17,230 lb (7,815 kg) Maximum Takeoff Weight 17,110 lb (7,761 kg) Maximum Landing Weight 15,660 lb (7,103 kg) Maximum Zero Fuel Weight 12,500 lb (5,670 kg) Usable Fuel Capacity Weight Volume 5,828 lb (2,644 kg) 870 gal (3,293 l) Basic Operating Weight 10,254 lb (4,651 kg) Useful Load 6,976 lb (3,164 kg) Maximum Payload 2,246 lb (1,019 kg) Full Fuel Payload 1,148 lb (521 kg) Performance Maximum Cruise Speed 451 ktas (835 km/h) Maximum Range 2,170 nm (4,019 km) Takeoff Field Length 3,190 ft (972 m) Landing Distance 2,740 ft (835 m) Maximum Operating Altitude 45,000 ft (13,716 m) Maximum Climb Rate 3,854 fpm (1,175 mpm) Maximum Limit Speed 0.77 Mach (0.77 Mach) Powerplant Two, dual-channel, FADEC-controlled, Williams FJ44-4A turbofan engines are installed on the CJ4. This engine is a medium-bypass, twin-spool design with four compression stages and three turbine stages. It produces 3,621 pounds (16.11kN) of takeoff 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) FJ44-4A Thrust: 3,621 lbf Time Between Overhaul: 5,000 hrs
  • Business Jet - Citation® CJ4® - Cessna Aircraft Company
    Cessna Aircraft Company
Description
The Citation® CJ4® jet redefines versatility for a light jet. The CJ4 has added speed, range and cabin size over its predecessor without incurring midsize jet operating costs.The Collins Pro Line 21™ avionics suite allows a single pilot to safely and effectively operate the CJ4. Features such as single point refueling, an externally serviceable lavatory and excellent range deliver what crew and cabin passengers appreciate. Standard Features Dual Primary Flight Displays Dual Multifunction Displays Single Flight Management System with GPS Navigation Integrated Flight Guidance System Crew Alerting System Integrated Electronic Checklists Electronic Jeppesen Charts Dual Attitude Heading Reference Systems XM Broadcast Graphical Weather MultiScan Weather Radar Mark VIII Enhanced Ground Proximity Warning System TCASII Optional avionics include: Mark V Enhanced Ground Proximity Warning System with Runway Awareness Dual Flight Management System High-Frequency Radio with SELCAL 88-Parameter Flight Data Recorder ACARS Data Link Installed in Center Glareshield Panel: LH and RH Master Warning/Master Caution Lights LH and RH Display Control Panel CVR Microphone LH and RH Engine Fire Control Switches Flight-Guidance Panel Reversion Controls Installed on Instrument Panel (left to right): LH Digital Audio Control Panel Avionics/Electrical Power Panel LH Primary Flight Display (PFD) LH Multifunction Display (MFD) Electronic Standby Instrument System Landing-Gear Control Module RH Multifunction Display (MFD) RH Primary Flight Display (PFD) RH Digital Audio Control Panel Cockpit Voice Recorder Controller Database Loading Unit (DBU) Installed on Tilt Panel (left to right): Oxygen Controls Cockpit Temperature Controls Fuel Controls Manual Ignition Control FADEC Switches Pressurization Controls Ice-Protection Switches Curser Control Panels (CCP) Collins FMS-3000 Control Display Unit (CDU) Push-to-Talk Switch Cockpit Speaker Mute Switch Event Switch Cabin Temperature Controls ELT Remote Switch Flight Hour Meter Installed on Pedestal: Lighting and Dimming Controls Engine Power Levers Flap-Control Handle Speed Brake Control Handle Engine Start Control Aileron Trim Control Rudder Trim Control Secondary Elevator Trim Control Installed Beneath Tilt Panel: Emergency Brake Handle Control Lock Parking Brake Handle Installed in Floor Aft of Center Pedestal: Emergency Gear Extension Handle Detailed Specifications Performance data is based on the standard CJ4 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 53 ft 4 in (16.26 m) Height 15 ft 5 in (4.69 m) Wingspan 50 ft 10 in (15.49 m) Wing Wing Area Wing Sweep 330 sq ft (30.66 sq m) 12.5 degrees Wheelbase 21 ft 2 in (6.45 m) Tread 12 ft 4 in (3.76 m) Cabin Interior Height Width Length 57 in (1.45 m) 58 in (1.47 m) 17 ft 4 in (5.28 m) Maximum Passengers 10 Baggage Capacity Weight Volume 1,040 lb (471.7 kg) 77 cu ft (2.18 cu m) Single Pilot Certified Yes Weights Maximum Ramp Weight 17,230 lb (7,815 kg) Maximum Takeoff Weight 17,110 lb (7,761 kg) Maximum Landing Weight 15,660 lb (7,103 kg) Maximum Zero Fuel Weight 12,500 lb (5,670 kg) Usable Fuel Capacity Weight Volume 5,828 lb (2,644 kg) 870 gal (3,293 l) Basic Operating Weight 10,254 lb (4,651 kg) Useful Load 6,976 lb (3,164 kg) Maximum Payload 2,246 lb (1,019 kg) Full Fuel Payload 1,148 lb (521 kg) Performance Maximum Cruise Speed 451 ktas (835 km/h) Maximum Range 2,170 nm (4,019 km) Takeoff Field Length 3,190 ft (972 m) Landing Distance 2,740 ft (835 m) Maximum Operating Altitude 45,000 ft (13,716 m) Maximum Climb Rate 3,854 fpm (1,175 mpm) Maximum Limit Speed 0.77 Mach (0.77 Mach) Powerplant Two, dual-channel, FADEC-controlled, Williams FJ44-4A turbofan engines are installed on the CJ4. This engine is a medium-bypass, twin-spool design with four compression stages and three turbine stages. It produces 3,621 pounds (16.11kN) of takeoff 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) FJ44-4A Thrust: 3,621 lbf Time Between Overhaul: 5,000 hrs

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Description
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Business Jet - Citation® CJ4® - Cessna Aircraft Company
Cessna Aircraft Company
Wichita, KS, USA
Business Jet
Citation® CJ4®
Business Jet Citation® CJ4®
The Citation® CJ4® jet redefines versatility for a light jet. The CJ4 has added speed, range and cabin size over its predecessor without incurring midsize jet operating costs.The Collins Pro Line 21™ avionics suite allows a single pilot to safely and effectively operate the CJ4. Features such as single point refueling, an externally serviceable lavatory and excellent range deliver what crew and cabin passengers appreciate. Standard Features Dual Primary Flight Displays Dual Multifunction Displays Single Flight Management System with GPS Navigation Integrated Flight Guidance System Crew Alerting System Integrated Electronic Checklists Electronic Jeppesen Charts Dual Attitude Heading Reference Systems XM Broadcast Graphical Weather MultiScan Weather Radar Mark VIII Enhanced Ground Proximity Warning System TCASII Optional avionics include: Mark V Enhanced Ground Proximity Warning System with Runway Awareness Dual Flight Management System High-Frequency Radio with SELCAL 88-Parameter Flight Data Recorder ACARS Data Link Installed in Center Glareshield Panel: LH and RH Master Warning/Master Caution Lights LH and RH Display Control Panel CVR Microphone LH and RH Engine Fire Control Switches Flight-Guidance Panel Reversion Controls Installed on Instrument Panel (left to right): LH Digital Audio Control Panel Avionics/Electrical Power Panel LH Primary Flight Display (PFD) LH Multifunction Display (MFD) Electronic Standby Instrument System Landing-Gear Control Module RH Multifunction Display (MFD) RH Primary Flight Display (PFD) RH Digital Audio Control Panel Cockpit Voice Recorder Controller Database Loading Unit (DBU) Installed on Tilt Panel (left to right): Oxygen Controls Cockpit Temperature Controls Fuel Controls Manual Ignition Control FADEC Switches Pressurization Controls Ice-Protection Switches Curser Control Panels (CCP) Collins FMS-3000 Control Display Unit (CDU) Push-to-Talk Switch Cockpit Speaker Mute Switch Event Switch Cabin Temperature Controls ELT Remote Switch Flight Hour Meter Installed on Pedestal: Lighting and Dimming Controls Engine Power Levers Flap-Control Handle Speed Brake Control Handle Engine Start Control Aileron Trim Control Rudder Trim Control Secondary Elevator Trim Control Installed Beneath Tilt Panel: Emergency Brake Handle Control Lock Parking Brake Handle Installed in Floor Aft of Center Pedestal: Emergency Gear Extension Handle Detailed Specifications Performance data is based on the standard CJ4 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 53 ft 4 in (16.26 m) Height 15 ft 5 in (4.69 m) Wingspan 50 ft 10 in (15.49 m) Wing Wing Area Wing Sweep 330 sq ft (30.66 sq m) 12.5 degrees Wheelbase 21 ft 2 in (6.45 m) Tread 12 ft 4 in (3.76 m) Cabin Interior Height Width Length 57 in (1.45 m) 58 in (1.47 m) 17 ft 4 in (5.28 m) Maximum Passengers 10 Baggage Capacity Weight Volume 1,040 lb (471.7 kg) 77 cu ft (2.18 cu m) Single Pilot Certified Yes Weights Maximum Ramp Weight 17,230 lb (7,815 kg) Maximum Takeoff Weight 17,110 lb (7,761 kg) Maximum Landing Weight 15,660 lb (7,103 kg) Maximum Zero Fuel Weight 12,500 lb (5,670 kg) Usable Fuel Capacity Weight Volume 5,828 lb (2,644 kg) 870 gal (3,293 l) Basic Operating Weight 10,254 lb (4,651 kg) Useful Load 6,976 lb (3,164 kg) Maximum Payload 2,246 lb (1,019 kg) Full Fuel Payload 1,148 lb (521 kg) Performance Maximum Cruise Speed 451 ktas (835 km/h) Maximum Range 2,170 nm (4,019 km) Takeoff Field Length 3,190 ft (972 m) Landing Distance 2,740 ft (835 m) Maximum Operating Altitude 45,000 ft (13,716 m) Maximum Climb Rate 3,854 fpm (1,175 mpm) Maximum Limit Speed 0.77 Mach (0.77 Mach) Powerplant Two, dual-channel, FADEC-controlled, Williams FJ44-4A turbofan engines are installed on the CJ4. This engine is a medium-bypass, twin-spool design with four compression stages and three turbine stages. It produces 3,621 pounds (16.11kN) of takeoff 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) FJ44-4A Thrust: 3,621 lbf Time Between Overhaul: 5,000 hrs

The Citation® CJ4® jet redefines versatility for a light jet. The CJ4 has added speed, range and cabin size over its predecessor without incurring midsize jet operating costs.The Collins Pro Line 21™ avionics suite allows a single pilot to safely and effectively operate the CJ4. Features such as single point refueling, an externally serviceable lavatory and excellent range deliver what crew and cabin passengers appreciate.

Standard Features

  • Dual Primary Flight Displays
  • Dual Multifunction Displays
  • Single Flight Management System with GPS Navigation
  • Integrated Flight Guidance System
  • Crew Alerting System
  • Integrated Electronic Checklists
  • Electronic Jeppesen Charts
  • Dual Attitude Heading Reference Systems
  • XM Broadcast Graphical Weather
  • MultiScan Weather Radar
  • Mark VIII Enhanced Ground Proximity Warning System
  • TCASII

Optional avionics include:

  • Mark V Enhanced Ground Proximity Warning System with Runway Awareness
  • Dual Flight Management System
  • High-Frequency Radio with SELCAL
  • 88-Parameter Flight Data Recorder
  • ACARS Data Link
    Installed in Center Glareshield Panel:
  • LH and RH Master Warning/Master Caution Lights
  • LH and RH Display Control Panel
  • CVR Microphone
  • LH and RH Engine Fire Control Switches
  • Flight-Guidance Panel
  • Reversion Controls
    Installed on Instrument Panel (left to right):
  • LH Digital Audio Control Panel
  • Avionics/Electrical Power Panel
  • LH Primary Flight Display (PFD)
  • LH Multifunction Display (MFD)
  • Electronic Standby Instrument System
  • Landing-Gear Control Module
  • RH Multifunction Display (MFD)
  • RH Primary Flight Display (PFD)
  • RH Digital Audio Control Panel
  • Cockpit Voice Recorder Controller
  • Database Loading Unit (DBU)
    Installed on Tilt Panel (left to right):
  • Oxygen Controls
  • Cockpit Temperature Controls
  • Fuel Controls
  • Manual Ignition Control
  • FADEC Switches
  • Pressurization Controls
  • Ice-Protection Switches
  • Curser Control Panels (CCP)
  • Collins FMS-3000 Control Display Unit (CDU)
  • Push-to-Talk Switch
  • Cockpit Speaker Mute Switch
  • Event Switch
  • Cabin Temperature Controls
  • ELT Remote Switch
  • Flight Hour Meter
    Installed on Pedestal:
  • Lighting and Dimming Controls
  • Engine Power Levers
  • Flap-Control Handle
  • Speed Brake Control Handle
  • Engine Start Control
  • Aileron Trim Control
  • Rudder Trim Control
  • Secondary Elevator Trim Control
    Installed Beneath Tilt Panel:
  • Emergency Brake Handle
  • Control Lock
  • Parking Brake Handle
    Installed in Floor Aft of Center Pedestal:
  • Emergency Gear Extension Handle

Detailed Specifications

Performance data is based on the standard CJ4 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
  • 53 ft 4 in (16.26 m)
  • Height
  • 15 ft 5 in (4.69 m)
  • Wingspan
  • 50 ft 10 in (15.49 m)
    Wing
  • Wing Area
  • Wing Sweep

  • 330 sq ft (30.66 sq m)
  • 12.5 degrees
    Wheelbase
  • 21 ft 2 in (6.45 m)
    Tread
  • 12 ft 4 in (3.76 m)
    Cabin Interior
  • Height
  • Width
  • Length

  • 57 in (1.45 m)
  • 58 in (1.47 m)
  • 17 ft 4 in (5.28 m)
  • Maximum Passengers
  • 10
    Baggage Capacity
  • Weight
  • Volume

  • 1,040 lb (471.7 kg)
  • 77 cu ft (2.18 cu m)
  • Single Pilot Certified
  • Yes

Weights

  • Maximum Ramp Weight
  • 17,230 lb (7,815 kg)
  • Maximum Takeoff Weight
  • 17,110 lb (7,761 kg)
  • Maximum Landing Weight
  • 15,660 lb (7,103 kg)
  • Maximum Zero Fuel Weight
  • 12,500 lb (5,670 kg)
    Usable Fuel Capacity
  • Weight
  • Volume

  • 5,828 lb (2,644 kg)
  • 870 gal (3,293 l)
  • Basic Operating Weight
  • 10,254 lb (4,651 kg)
  • Useful Load
  • 6,976 lb (3,164 kg)
  • Maximum Payload
  • 2,246 lb (1,019 kg)
  • Full Fuel Payload
  • 1,148 lb (521 kg)

Performance

  • Maximum Cruise Speed
  • 451 ktas (835 km/h)
  • Maximum Range
  • 2,170 nm (4,019 km)
  • Takeoff Field Length
  • 3,190 ft (972 m)
  • Landing Distance
  • 2,740 ft (835 m)
  • Maximum Operating Altitude
  • 45,000 ft (13,716 m)
  • Maximum Climb Rate
  • 3,854 fpm (1,175 mpm)
  • Maximum Limit Speed
  • 0.77 Mach (0.77 Mach)

Powerplant

Two, dual-channel, FADEC-controlled, Williams FJ44-4A turbofan engines are installed on the CJ4. This engine is a medium-bypass, twin-spool design with four compression stages and three turbine stages. It produces 3,621 pounds (16.11kN) of takeoff 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) FJ44-4A
  • Thrust: 3,621 lbf
  • Time Between Overhaul: 5,000 hrs
Supplier's Site

Technical Specifications

  Cessna Aircraft Company
Product Category Aircraft
Product Number Citation® CJ4®
Product Name Business Jet
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