Cessna Aircraft Company Business Jet Citation® XLS+®

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Business Jet - Citation® XLS+® - Cessna Aircraft Company
Wichita, KS, USA
Business Jet Citation® XLS+®
Textron Aviation has given the best selling business jet in the world a series of improvements to take it to a whole new level. The Citation® XLS+® jet combines transcontinental range, first-class cabin comfort for up to 12 passengers and remarkable performance efficiency in a beautiful midsize jet. Loaded with features generally reserved for a large, commercial aircraft, the XLS+ will take your business global. Sit back and enjoy the ride. The heart of your travel The pilot needs to know different flight-critical information at various times during each phase of the flight, which is why the XLS+ is equipped with the Collins Pro Line 21™. This line of avionics provides weather navigation systems, airport diagrams, detailed flight status data, checklists, diagnostic systems and are directly in the crew’s line of sight. Angled control panels and four tilted eight by ten inch displays show flight information in simple, clear readouts. Your digital weatherman Your XLS+ will give you instant, accurate and up-to-date weather information for your flight path via the XM WX Satellite Weather® Data Service. This long-range, comprehensive weather detection system provides sharp situational awareness for both pilots and copilots. With upgraded software, pilots can view satellite imagery with NEXRAD overlays, see Temporary Flight Restrictions (FSR) both in graphical and textual formats, view winds aloft and view cloud-to cloud lightning with strikes data refreshed every five minutes. Images and data are available at any altitude and are processed through a receiver supplied on a Head-Up Display (HUD) technologies which are then stored in the file server unit (FSU) for immediate access. Uncompromising safety The XLS+ is equipped with a traffic collision avoidance system (TCAS) powered by the Collins TCAS-4000. The system tracks all other aircraft within a 35-nautical-mile radius. The system will select and display only the aircraft traffic that poses a collision threat along with audible traffic alerts and resolution advisories to assist pilots in maneuvering around potential hazards. If the other aircraft detected in the system is also equipped with TCAS technology, each system will coordinate complementary maneuvers to correct the situation. A partial list of standard equipment: Dual 8 x 10-inch Primary Flight Displays Dual 8 x 10-inch Multifunction Displays Electronic Flight Information System Crew Alerting System Flight Guidance System Dual Air Data Computers XM Broadcast Weather (U.S.) Emergency Descent Mode Dual Attitude Heading Reference System Integrated Electronic Checklists Electronic Charts Flight Management System Global Positioning System Terrain Awareness Warning System Traffic Collision Avoidance System (TCAS II) Maintenance Diagnostic System Available optional equipment: Interactive Graphical Weather Lightning Detection Stormscope Mark V EGPWS with Runway Awareness and Advisory System High-Frequency Communications with SELCAL Equipment Details Installed on Left-Hand Panel (pilot): Pilot’s digital audio control panel Master warning/master caution lights Primary flight display Display control panel (DCP) Battery temperature gauge Digital clock Installed on Right-Hand Panel (copilot): Master warning/master caution lights Display control panel (DCP) Primary flight display Copilot’s digital audio control panel APU fire annunciator APU system annunciators APU ammeter Installed on Center Panel: TAWS switches and annunciators Electronic standby flight display Electronic standby horizontal situation indicator Standby engine display with N1, N2, ITT Multifunction displays Installed in Glareshield: Flight guidance panel Thrust reverser indications and engine fire control switches Angle of attack indexer (pilot’s side) Installed on Left-Hand Tilt Panel: FADEC switches Electrical power control Avionics power control Fuel transfer control Pilot’s AHRS control Oxygen pressure indicator Cockpit speaker mute switch Pilot’s AHRS and ADC reversion switches Oxygen mask switch Microphone selector switch Installed on Right-Hand Tilt Panel: Copilot’s AHRS control Anti-ice/de-ice controls Cockpit speaker mute switch Landing gear control and indicators Cabin altitude and differential pressure indicator Cabin pressurization system controller Cabin rate of climb Cabin bleed air source selection control Manual pressurization control Microphone selector switch Copilot's AHRS and ADC reversion switches Cockpit and cabin temperature controls Emergency cabin pressure dump control Installed on Pedestal: Rotary test switch Engine start and ignition control Pulse light switches Exterior lights control Cockpit and instrument lighting controls Landing/recognition/ taxi light controls Flight deck lighting controls Cockpit voice recorder (CVR) control panel Event switch DC voltmeter Left and right generator load ammeters Standby radio tuning control Engine power levers Flap control Flap position indicator Speed brake control (on throttle knobs) Engine synchronizer switch Collins FMS-3000 Control Display Units (CDU) Cursor control panels (CCP) Elevator trim control and indicator Aileron trim control and indicator Rudder trim control and indicator Maintenance diagnostic system download ports Database Loading Unit (DBU-5000) Display reversionary control panel Dimensions Length 52 ft 6 in (16.00 m) Height 17 ft 2 in (5.23 m) Wingspan 56 ft 4 in (17.17 m) Wing Wing Area Wing Sweep 370 sq ft (34.35 sq m) 0.0 degrees Wheelbase 21 ft 11 in (6.68 m) Tread 14 ft 11 in (4.55 m) Cabin Interior Height Width Length 68 in (1.73 m) 66 in (1.68 m) 18 ft 6 in (5.64 m) Maximum Passengers 9 Baggage Capacity Weight Volume 800 lb (362.9 kg) 90 cu ft (2.55 cu m) Single Pilot Certified No Weights Maximum Ramp Weight 20,400 lb (9,253 kg) Maximum Takeoff Weight 20,200 lb (9,163 kg) Maximum Landing Weight 18,700 lb (8,482 kg) Maximum Zero Fuel Weight 15,100 lb (6,849 kg) Usable Fuel Capacity Weight Volume 6,740 lb (3,057 kg) 1,006 gal (3,808 l) Basic Operating Weight 12,860 lb (5,833 kg) Useful Load 7,540 lb (3,420 kg) Maximum Payload 2,240 lb (1,016 kg) Full Fuel Payload 800 lb (363 kg) Performance Maximum Cruise Speed 441 ktas (817 km/h) Maximum Range 2,100 nm (3,889 km) Takeoff Field Length 3,560 ft (1,085 m) Landing Distance 3,180 ft (969 m) Maximum Operating Altitude 45,000 ft (13,716 m) Maximum Climb Rate 3,500 fpm (1,067 mpm) Maximum Limit Speed 0.75 Mach (0.75 Mach) Powerplant Two, dual-channel FADEC-controlled Pratt & Whitney Canada™ PW545C turbofan engines are installed on the XLS+. The PW545C produces a static takeoff thrust of 4,119 pounds (18.32kN) at sea level, up to 77˚F (25˚C) and has a bypass ratio of 3.8:1. Hydraulically actuated, target-type thrust reversers are attached to each engine. An APU is incorporated for engine start and other benefits. Manufacturer: Pratt & Whitney Model: (2) PW545C Thrust: 4,119 lbf Time Between Overhaul: 5,000 hrs

Textron Aviation has given the best selling business jet in the world a series of improvements to take it to a whole new level. The Citation® XLS+® jet combines transcontinental range, first-class cabin comfort for up to 12 passengers and remarkable performance efficiency in a beautiful midsize jet. Loaded with features generally reserved for a large, commercial aircraft, the XLS+ will take your business global. Sit back and enjoy the ride.

The heart of your travel

The pilot needs to know different flight-critical information at various times during each phase of the flight, which is why the XLS+ is equipped with the Collins Pro Line 21™. This line of avionics provides weather navigation systems, airport diagrams, detailed flight status data, checklists, diagnostic systems and are directly in the crew’s line of sight. Angled control panels and four tilted eight by ten inch displays show flight information in simple, clear readouts.

Your digital weatherman

Your XLS+ will give you instant, accurate and up-to-date weather information for your flight path via the XM WX Satellite Weather® Data Service. This long-range, comprehensive weather detection system provides sharp situational awareness for both pilots and copilots.

With upgraded software, pilots can view satellite imagery with NEXRAD overlays, see Temporary Flight Restrictions (FSR) both in graphical and textual formats, view winds aloft and view cloud-to cloud lightning with strikes data refreshed every five minutes. Images and data are available at any altitude and are processed through a receiver supplied on a Head-Up Display (HUD) technologies which are then stored in the file server unit (FSU) for immediate access.

Uncompromising safety

The XLS+ is equipped with a traffic collision avoidance system (TCAS) powered by the Collins TCAS-4000. The system tracks all other aircraft within a 35-nautical-mile radius. The system will select and display only the aircraft traffic that poses a collision threat along with audible traffic alerts and resolution advisories to assist pilots in maneuvering around potential hazards. If the other aircraft detected in the system is also equipped with TCAS technology, each system will coordinate complementary maneuvers to correct the situation.

A partial list of standard equipment:

  • Dual 8 x 10-inch Primary Flight Displays
  • Dual 8 x 10-inch Multifunction Displays
  • Electronic Flight Information System
  • Crew Alerting System
  • Flight Guidance System
  • Dual Air Data Computers
  • XM Broadcast Weather (U.S.)
  • Emergency Descent Mode
  • Dual Attitude Heading Reference System
  • Integrated Electronic Checklists
  • Electronic Charts
  • Flight Management System
  • Global Positioning System
  • Terrain Awareness Warning System
  • Traffic Collision Avoidance System (TCAS II)
  • Maintenance Diagnostic System

Available optional equipment:

  • Interactive Graphical Weather
  • Lightning Detection Stormscope
  • Mark V EGPWS with Runway Awareness and Advisory System
  • High-Frequency Communications with SELCAL

Equipment Details

    Installed on Left-Hand Panel (pilot):
  • Pilot’s digital audio control panel
  • Master warning/master caution lights
  • Primary flight display
  • Display control panel (DCP)
  • Battery temperature gauge
  • Digital clock
    Installed on Right-Hand Panel (copilot):
  • Master warning/master caution lights
  • Display control panel (DCP)
  • Primary flight display
  • Copilot’s digital audio control panel
  • APU fire annunciator
  • APU system annunciators
  • APU ammeter
    Installed on Center Panel:
  • TAWS switches and annunciators
  • Electronic standby flight display
  • Electronic standby horizontal situation indicator
  • Standby engine display with N1, N2, ITT
  • Multifunction displays
    Installed in Glareshield:
  • Flight guidance panel
  • Thrust reverser indications and engine fire control switches
  • Angle of attack indexer (pilot’s side)
    Installed on Left-Hand Tilt Panel:
  • FADEC switches
  • Electrical power control
  • Avionics power control
  • Fuel transfer control
  • Pilot’s AHRS control
  • Oxygen pressure indicator
  • Cockpit speaker mute switch
  • Pilot’s AHRS and ADC reversion switches
  • Oxygen mask switch
  • Microphone selector switch
    Installed on Right-Hand Tilt Panel:
  • Copilot’s AHRS control
  • Anti-ice/de-ice controls
  • Cockpit speaker mute switch
  • Landing gear control and indicators
  • Cabin altitude and differential pressure indicator
  • Cabin pressurization system controller
  • Cabin rate of climb
  • Cabin bleed air source selection control
  • Manual pressurization control
  • Microphone selector switch
  • Copilot's AHRS and ADC reversion switches
  • Cockpit and cabin temperature controls
  • Emergency cabin pressure dump control
    Installed on Pedestal:
  • Rotary test switch
  • Engine start and ignition control
  • Pulse light switches
  • Exterior lights control
  • Cockpit and instrument lighting controls
  • Landing/recognition/taxi light controls
  • Flight deck lighting controls
  • Cockpit voice recorder (CVR) control panel
  • Event switch
  • DC voltmeter
  • Left and right generator load ammeters
  • Standby radio tuning control
  • Engine power levers
  • Flap control
  • Flap position indicator
  • Speed brake control (on throttle knobs)
  • Engine synchronizer switch
  • Collins FMS-3000 Control Display Units (CDU)
  • Cursor control panels (CCP)
  • Elevator trim control and indicator
  • Aileron trim control and indicator
  • Rudder trim control and indicator
  • Maintenance diagnostic system download ports
  • Database Loading Unit (DBU-5000)
  • Display reversionary control panel

Dimensions

  • Length
  • 52 ft 6 in (16.00 m)
  • Height
  • 17 ft 2 in (5.23 m)
  • Wingspan
  • 56 ft 4 in (17.17 m)
    Wing
  • Wing Area
  • Wing Sweep

  • 370 sq ft (34.35 sq m)
  • 0.0 degrees
    Wheelbase
  • 21 ft 11 in (6.68 m)
    Tread
  • 14 ft 11 in (4.55 m)
    Cabin Interior
  • Height
  • Width
  • Length

  • 68 in (1.73 m)
  • 66 in (1.68 m)
  • 18 ft 6 in (5.64 m)
  • Maximum Passengers
  • 9
    Baggage Capacity
  • Weight
  • Volume

  • 800 lb (362.9 kg)
  • 90 cu ft (2.55 cu m)
  • Single Pilot Certified
  • No

Weights

  • Maximum Ramp Weight
  • 20,400 lb (9,253 kg)
  • Maximum Takeoff Weight
  • 20,200 lb (9,163 kg)
  • Maximum Landing Weight
  • 18,700 lb (8,482 kg)
  • Maximum Zero Fuel Weight
  • 15,100 lb (6,849 kg)
    Usable Fuel Capacity
  • Weight
  • Volume

  • 6,740 lb (3,057 kg)
  • 1,006 gal (3,808 l)
  • Basic Operating Weight
  • 12,860 lb (5,833 kg)
  • Useful Load
  • 7,540 lb (3,420 kg)
  • Maximum Payload
  • 2,240 lb (1,016 kg)
  • Full Fuel Payload
  • 800 lb (363 kg)

Performance

  • Maximum Cruise Speed
  • 441 ktas (817 km/h)
  • Maximum Range
  • 2,100 nm (3,889 km)
  • Takeoff Field Length
  • 3,560 ft (1,085 m)
  • Landing Distance
  • 3,180 ft (969 m)
  • Maximum Operating Altitude
  • 45,000 ft (13,716 m)
  • Maximum Climb Rate
  • 3,500 fpm (1,067 mpm)
  • Maximum Limit Speed
  • 0.75 Mach (0.75 Mach)

Powerplant

Two, dual-channel FADEC-controlled Pratt & Whitney Canada™ PW545C turbofan engines are installed on the XLS+. The PW545C produces a static takeoff thrust of 4,119 pounds (18.32kN) at sea level, up to 77˚F (25˚C) and has a bypass ratio of 3.8:1. Hydraulically actuated, target-type thrust reversers are attached to each engine. An APU is incorporated for engine start and other benefits.

  • Manufacturer: Pratt & Whitney
  • Model: (2) PW545C
  • Thrust: 4,119 lbf
  • Time Between Overhaul: 5,000 hrs
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Technical Specifications

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