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Cessna Aircraft Company Business Jet Citation® X+®

Description
The Citation® X+® jet is the fastest civilian aircraft in the sky today. Astonishingly, it can climb to 51,000 feet and cruise at incredible speeds of up to Mach 0.935. The X+ provides seating for up to 12 people, making it one of the most comfortable cabin environments for work or for recreation. Standard Features Flight Displays Synthetic Vision Technology Touch-screen Control Panels Automatic Flight Control System Attitude Heading Reference Systems (AHRS) Integrated Avionics Units Distance Measuring Equipment Flight Management Systems Weather Radar Traffic Collision Avoidance System (TCAS II) Terrain Awareness Warning System (TAWS) Transponders with ADS-B Out Capability Standby Instrumentation Radio Altimeter Cockpit Voice Recorder Emergency Locator Transmitter Maintenance Diagnostics Installed on Left-Hand Panel (pilot): Touch-screen LCD Control Panel Primary Flight Display (PFD) Secondary PFD Controller Installed on Right-Hand Panel (copilot): Touch-screen LCD Control Panel Primary Flight Display (PFD) Secondary PFD Controller Installed on Center Panel: Multifunction Display (MFD) Dual Touchscreen LCD Control Panels Electronic Standby Flight Display (ESFD) Installed Beneath Glareshield: Flight Guidance Panel (FGP) Installed on Left-Hand Tilt Panel: Electrical Power Panel Installed on Right-Hand Tilt Panel: Anti-Ice/De-Ice Panel Landing Gear Control Panel Installed on Pedestal: Engine Power Levers Flaps Control Pressurization Panel Engine Control/Start Panel Cockpit/Cabin Temperature Panel Fuel, APU, and Hydraulics Detailed Specifications Performance data is based on the standard X 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. Preliminary data, subject to change. Dimensions Length 73 ft 7 in (22.43 m) Height 19 ft 3 in (5.86 m) Wingspan 69 ft 2 in (21.09 m) Wing Wing Area Wing Sweep 527 sq ft (48.96 sq m) 37.0 degrees Wheelbase 29 ft 11 in (9.11 m) Tread 10 ft 7 in (3.23 m) Cabin Interior Height Width Length 68 in (1.73 m) 66 in (1.68 m) 25 ft 2 in (7.67 m) Maximum Passengers 12 Baggage Capacity Weight Volume 1,095 lb (496.7 kg) 104 cu ft (2.93 cu m) Single Pilot Certified No Weights Maximum Ramp Weight 36,900 lb (16,738 kg) Maximum Takeoff Weight 36,600 lb (16,601 kg) Maximum Landing Weight 32,000 lb (14,515 kg) Maximum Zero Fuel Weight 24,978 lb (11,330 kg) Usable Fuel Capacity Weight Volume 12,931 lb (5,865 kg) 1,930 gal (7,306 l) Basic Operating Weight 22,131 lb (10,038 kg) Useful Load 14,769 lb (6,699 kg) Maximum Payload 2,847 lb (1,291 kg) Full Fuel Payload 1,838 lb (834 kg) Performance Maximum Cruise Speed 528 ktas (978 km/h) Maximum Range 3,460 nm (6,408 km) Takeoff Field Length 5,250 ft (1,600 m) Landing Distance 3,330 ft (1,015 m) Maximum Operating Altitude 51,000 ft (15,545 m) Maximum Climb Rate 4,117 fpm (1,255 mpm) Maximum Limit Speed 0.935 Mach (0.935 Mach) Powerplant Two dual-channel FADEC-controlled Rolls-Royce AE3007C2 turbo fan engines power the Citation X+. The AE3007C2 features two spools with a 14-stage axial flow compressor, a two-stage high-pressure turbine, and a three-stage low-pressure turbine. The engine has a bypass ratio of 5:1 and a static takeoff thrust at sea level of 7,034 pounds (31.29 kN) flat rated up to 86°F (30°C). Hydraulically actuated, target-type thrust reversers are attached to each engine. An APU is incorporated for engine start and other benefits. Manufacturer: Rolls-Royce Model: (2) AE3007C2

Suppliers

Company
Product
Description
Supplier Links
Business Jet - Citation® X+® - Cessna Aircraft Company
Wichita, KS, USA
Business Jet
Citation® X+®
Business Jet Citation® X+®
The Citation® X+® jet is the fastest civilian aircraft in the sky today. Astonishingly, it can climb to 51,000 feet and cruise at incredible speeds of up to Mach 0.935. The X+ provides seating for up to 12 people, making it one of the most comfortable cabin environments for work or for recreation. Standard Features Flight Displays Synthetic Vision Technology Touch-screen Control Panels Automatic Flight Control System Attitude Heading Reference Systems (AHRS) Integrated Avionics Units Distance Measuring Equipment Flight Management Systems Weather Radar Traffic Collision Avoidance System (TCAS II) Terrain Awareness Warning System (TAWS) Transponders with ADS-B Out Capability Standby Instrumentation Radio Altimeter Cockpit Voice Recorder Emergency Locator Transmitter Maintenance Diagnostics Installed on Left-Hand Panel (pilot): Touch-screen LCD Control Panel Primary Flight Display (PFD) Secondary PFD Controller Installed on Right-Hand Panel (copilot): Touch-screen LCD Control Panel Primary Flight Display (PFD) Secondary PFD Controller Installed on Center Panel: Multifunction Display (MFD) Dual Touchscreen LCD Control Panels Electronic Standby Flight Display (ESFD) Installed Beneath Glareshield: Flight Guidance Panel (FGP) Installed on Left-Hand Tilt Panel: Electrical Power Panel Installed on Right-Hand Tilt Panel: Anti-Ice/De-Ice Panel Landing Gear Control Panel Installed on Pedestal: Engine Power Levers Flaps Control Pressurization Panel Engine Control/Start Panel Cockpit/Cabin Temperature Panel Fuel, APU, and Hydraulics Detailed Specifications Performance data is based on the standard X 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. Preliminary data, subject to change. Dimensions Length 73 ft 7 in (22.43 m) Height 19 ft 3 in (5.86 m) Wingspan 69 ft 2 in (21.09 m) Wing Wing Area Wing Sweep 527 sq ft (48.96 sq m) 37.0 degrees Wheelbase 29 ft 11 in (9.11 m) Tread 10 ft 7 in (3.23 m) Cabin Interior Height Width Length 68 in (1.73 m) 66 in (1.68 m) 25 ft 2 in (7.67 m) Maximum Passengers 12 Baggage Capacity Weight Volume 1,095 lb (496.7 kg) 104 cu ft (2.93 cu m) Single Pilot Certified No Weights Maximum Ramp Weight 36,900 lb (16,738 kg) Maximum Takeoff Weight 36,600 lb (16,601 kg) Maximum Landing Weight 32,000 lb (14,515 kg) Maximum Zero Fuel Weight 24,978 lb (11,330 kg) Usable Fuel Capacity Weight Volume 12,931 lb (5,865 kg) 1,930 gal (7,306 l) Basic Operating Weight 22,131 lb (10,038 kg) Useful Load 14,769 lb (6,699 kg) Maximum Payload 2,847 lb (1,291 kg) Full Fuel Payload 1,838 lb (834 kg) Performance Maximum Cruise Speed 528 ktas (978 km/h) Maximum Range 3,460 nm (6,408 km) Takeoff Field Length 5,250 ft (1,600 m) Landing Distance 3,330 ft (1,015 m) Maximum Operating Altitude 51,000 ft (15,545 m) Maximum Climb Rate 4,117 fpm (1,255 mpm) Maximum Limit Speed 0.935 Mach (0.935 Mach) Powerplant Two dual-channel FADEC-controlled Rolls-Royce AE3007C2 turbo fan engines power the Citation X+. The AE3007C2 features two spools with a 14-stage axial flow compressor, a two-stage high-pressure turbine, and a three-stage low-pressure turbine. The engine has a bypass ratio of 5:1 and a static takeoff thrust at sea level of 7,034 pounds (31.29 kN) flat rated up to 86°F (30°C). Hydraulically actuated, target-type thrust reversers are attached to each engine. An APU is incorporated for engine start and other benefits. Manufacturer: Rolls-Royce Model: (2) AE3007C2

The Citation® X+® jet is the fastest civilian aircraft in the sky today. Astonishingly, it can climb to 51,000 feet and cruise at incredible speeds of up to Mach 0.935. The X+ provides seating for up to 12 people, making it one of the most comfortable cabin environments for work or for recreation.

Standard Features

  • Flight Displays
  • Synthetic Vision Technology
  • Touch-screen Control Panels
  • Automatic Flight Control System
  • Attitude Heading Reference Systems (AHRS)
  • Integrated Avionics Units
  • Distance Measuring Equipment
  • Flight Management Systems
  • Weather Radar
  • Traffic Collision Avoidance System (TCAS II)
  • Terrain Awareness Warning System (TAWS)
  • Transponders with ADS-B Out Capability
  • Standby Instrumentation
  • Radio Altimeter
  • Cockpit Voice Recorder
  • Emergency Locator Transmitter
  • Maintenance Diagnostics
    Installed on Left-Hand Panel (pilot):
  • Touch-screen LCD Control Panel
  • Primary Flight Display (PFD)
  • Secondary PFD Controller
    Installed on Right-Hand Panel (copilot):
  • Touch-screen LCD Control Panel
  • Primary Flight Display (PFD)
  • Secondary PFD Controller
    Installed on Center Panel:
  • Multifunction Display (MFD)
  • Dual Touchscreen LCD Control Panels
  • Electronic Standby Flight Display (ESFD)
    Installed Beneath Glareshield:
  • Flight Guidance Panel (FGP)
    Installed on Left-Hand Tilt Panel:
  • Electrical Power Panel
    Installed on Right-Hand Tilt Panel:
  • Anti-Ice/De-Ice Panel
  • Landing Gear Control Panel
    Installed on Pedestal:
  • Engine Power Levers
  • Flaps Control
  • Pressurization Panel
  • Engine Control/Start Panel
  • Cockpit/Cabin Temperature Panel
  • Fuel, APU, and Hydraulics

Detailed Specifications

Performance data is based on the standard X 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.

Preliminary data, subject to change.

Dimensions

  • Length
  • 73 ft 7 in (22.43 m)
  • Height
  • 19 ft 3 in (5.86 m)
  • Wingspan
  • 69 ft 2 in (21.09 m)
    Wing
  • Wing Area
  • Wing Sweep

  • 527 sq ft (48.96 sq m)
  • 37.0 degrees
    Wheelbase
  • 29 ft 11 in (9.11 m)
    Tread
  • 10 ft 7 in (3.23 m)
    Cabin Interior
  • Height
  • Width
  • Length

  • 68 in (1.73 m)
  • 66 in (1.68 m)
  • 25 ft 2 in (7.67 m)
  • Maximum Passengers
  • 12
    Baggage Capacity
  • Weight
  • Volume

  • 1,095 lb (496.7 kg)
  • 104 cu ft (2.93 cu m)
  • Single Pilot Certified
  • No

Weights

  • Maximum Ramp Weight
  • 36,900 lb (16,738 kg)
  • Maximum Takeoff Weight
  • 36,600 lb (16,601 kg)
  • Maximum Landing Weight
  • 32,000 lb (14,515 kg)
  • Maximum Zero Fuel Weight
  • 24,978 lb (11,330 kg)
    Usable Fuel Capacity
  • Weight
  • Volume

  • 12,931 lb (5,865 kg)
  • 1,930 gal (7,306 l)
  • Basic Operating Weight
  • 22,131 lb (10,038 kg)
  • Useful Load
  • 14,769 lb (6,699 kg)
  • Maximum Payload
  • 2,847 lb (1,291 kg)
  • Full Fuel Payload
  • 1,838 lb (834 kg)

Performance

  • Maximum Cruise Speed
  • 528 ktas (978 km/h)
  • Maximum Range
  • 3,460 nm (6,408 km)
  • Takeoff Field Length
  • 5,250 ft (1,600 m)
  • Landing Distance
  • 3,330 ft (1,015 m)
  • Maximum Operating Altitude
  • 51,000 ft (15,545 m)
  • Maximum Climb Rate
  • 4,117 fpm (1,255 mpm)
  • Maximum Limit Speed
  • 0.935 Mach (0.935 Mach)

Powerplant

Two dual-channel FADEC-controlled Rolls-Royce AE3007C2 turbo fan engines power the Citation X+. The AE3007C2 features two spools with a 14-stage axial flow compressor, a two-stage high-pressure turbine, and a three-stage low-pressure turbine. The engine has a bypass ratio of 5:1 and a static takeoff thrust at sea level of 7,034 pounds (31.29 kN) flat rated up to 86°F (30°C). Hydraulically actuated, target-type thrust reversers are attached to each engine. An APU is incorporated for engine start and other benefits.

  • Manufacturer: Rolls-Royce
  • Model: (2) AE3007C2
Supplier's Site

Technical Specifications

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