Cessna Aircraft Company Business Jet Citation® Mustang®

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Business Jet - Citation® Mustang® - Cessna Aircraft Company
Wichita, KS, USA
This single pilot aircraft combines the comfort of a large business jet with the freedom to roam of a light aircraft. The speed and range inspired performance of the Citation® Mustang® jet will tackle the sky like a jet, while delivering the efficiency of a lighter aircraft. The aerodynamic design and advanced technology of the Mustang make for exceptional short-field performance and the ability to cruise over the weather. Standard avionics include: Garmin FMS with dual WAAS-enabled GPS for navigation Weather-avoidance radar Terrain-avoidance warning system Traffic information system Dual altitude heading reference system Dual air data computers Optional avionics include: Jeppesen ChartView Garmin Synthetic Vision Technology Honeywell’s Traffic Advisory System SiriusXM Satellite Radio and Weather TCAS II CDVR Citation Mustang avionics detailed component specifications: Dual 10.4-inch (diagonal) TFT LCD control display units with integrated terrain-awareness system (TAWS B) utilized as primary flight displays (PFD) — Garmin GDU 1040A Single 15-inch (diagonal) TFT LCD control display unit with integrated terrain-awareness system (TAWS B) utilized as a multifunction display (MFD) — Garmin GDU 1500 Dual engine/airframe interface units — Garmin GEA 71 Dual digital air data computers (ADC) — Garmin GDC 74B Dual digital attitude heading reference systems (AHRS) — Garmin GRS 77 Dual magnetometers — Garmin GMU 44 Dual integrated avionics units with VHF Nav/Com, GPS receivers, flight directors, and aural warning generator — Garmin GIA 63W Dual digital audio control panels — Garmin GMA 1347D Single remote flight management system (FMS) / MFD control keyboard — Garmin GCU 475 Three-axis automatic flight control system (AFCS) with integrated pitch trim — Garmin GFC 700 with Garmin GMC 710 Mode Controller Dual Mode S Diversity Transponders with Enhanced Surveillance and Traffic Information System (TIS) — Garmin GTX 33D Four-color weather-avoidance radar — Garmin GWX 68 Satellite data link weather transceiver — Garmin GDL 69A Electric standby attitude indicator — Mid Continent Instruments 4200 Electromechanical standby airspeed Indicator -—Aerosonic 261440 Electromechanical Standby Altimeter — Aerosonic 162350 Emergency locator transmitter (ELT) — Artex C406-N Pilot-selectable Flight Path Scan narrows the scan range to ±10, 20, or 30 degrees and increases the scan rate. Ground mapping depicts terrain features with a separate color scheme from the weather modes Installed on center glare shield panel: LH and RH master caution/master warning lights LH and RH engine fire control switches Flight director/autopilot controller Electronic standby instrument system LH and RH display control units Installed on instrument panel (left to right): LH primary flight display (PFD) Multifunction display (MFD) RH primary flight display (PFD) Installed on tilt panel (left to right): Electrical power panel Pressurization controls Ice protection controls Windshield anti-ice controls Fuel controls Engine start control Ignition controls Landing gear control module Lighting controls Flight hour meter ELT remote switch Environmental controls Installed on pedestal: Engine power levers Flap control handles Speed brake control Elevator trim control and indicator Takeoff/Go-Around button Rudder trim control Aileron trim control Emergency gear release Installed beneath the instrument panel: Emergency brake handle Parking brake handle Detailed Specifications Performance data is based on the standard Mustang 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 40 ft 7 in (12.37 m) Height 13 ft 5 in (4.09 m) Wingspan 43 ft 2 in (13.16 m) Wing Wing Area Wing Sweep 210 sq ft (19.51 sq m) 11.0 degrees Wheelbase 14 ft 4 in (4.37 m) Tread 11 ft 10 in (3.61 m) Cabin Interior Height Width Length 54 in (1.37 m) 55 in (1.40 m) 9 ft 9 in (2.97 m) Maximum Passengers 5 Baggage Capacity Weight Volume 718 lb (325.7 kg) 63 cu ft (1.78 cu m) Single Pilot Certified Yes Weights Maximum Ramp Weight 8,730 lb (3,960 kg) Maximum Takeoff Weight 8,645 lb (3,921 kg) Maximum Landing Weight 8,000 lb (3,629 kg) Maximum Zero Fuel Weight 6,750 lb (3,062 kg) Usable Fuel Capacity Weight Volume 2,580 lb (1,170 kg) 385 gal (1,457 l) Basic Operating Weight 5,600 lb (2,540 kg) Useful Load 3,130 lb (1,420 kg) Maximum Payload 1,150 lb (522 kg) Full Fuel Payload 550 lb (249 kg) Performance Maximum Cruise Speed 340 ktas (630 km/h) Maximum Range 1,200 nm (2,222 km) Takeoff Field Length 3,110 ft (948 m) Landing Distance 2,380 ft (725 m) Maximum Operating Altitude 41,000 ft (12,497 m) Maximum Climb Rate 3,010 fpm (917 mpm) Maximum Limit Speed 0.63 Mach (0.63 Mach) Powerplant Two dual-channel, FADEC-controlled, Pratt & Whitney Canada™ PW615F-A turbofan engines are installed on the Mustang. The engine is a 2.8:1 bypass ratio, counter-rotating, twin-spool design with three compression stages and two turbine stages. It produces 1,460 pounds (6.49 kN) of thrust at sea level, static conditions, flat-rated up to 77°F (25°C). The FADEC system also provides time-limited dispatch, diagnostics and engine synchronization according to switch position. Manufacturer: Pratt & Whitney Model: (2) PW615F-A Thrust: 1,460 lbf Time between overhaul: 3,500 hr

This single pilot aircraft combines the comfort of a large business jet with the freedom to roam of a light aircraft. The speed and range inspired performance of the Citation® Mustang® jet will tackle the sky like a jet, while delivering the efficiency of a lighter aircraft. The aerodynamic design and advanced technology of the Mustang make for exceptional short-field performance and the ability to cruise over the weather.

Standard avionics include:

  • Garmin FMS with dual WAAS-enabled GPS for navigation
  • Weather-avoidance radar
  • Terrain-avoidance warning system
  • Traffic information system
  • Dual altitude heading reference system
  • Dual air data computers

Optional avionics include:

  • Jeppesen ChartView
  • Garmin Synthetic Vision Technology
  • Honeywell’s Traffic Advisory System
  • SiriusXM Satellite Radio and Weather
  • TCAS II
  • CDVR

Citation Mustang avionics detailed component specifications:

  • Dual 10.4-inch (diagonal) TFT LCD control display units with integrated terrain-awareness system (TAWS B) utilized as primary flight displays (PFD) — Garmin GDU 1040A
  • Single 15-inch (diagonal) TFT LCD control display unit with integrated terrain-awareness system (TAWS B) utilized as a multifunction display (MFD) — Garmin GDU 1500
  • Dual engine/airframe interface units — Garmin GEA 71
  • Dual digital air data computers (ADC) — Garmin GDC 74B
  • Dual digital attitude heading reference systems (AHRS) — Garmin GRS 77
  • Dual magnetometers — Garmin GMU 44
  • Dual integrated avionics units with VHF Nav/Com, GPS receivers, flight directors, and aural warning generator — Garmin GIA 63W
  • Dual digital audio control panels — Garmin GMA 1347D
  • Single remote flight management system (FMS) / MFD control keyboard — Garmin GCU 475
  • Three-axis automatic flight control system (AFCS) with integrated pitch trim — Garmin GFC 700 with Garmin GMC 710 Mode Controller
  • Dual Mode S Diversity Transponders with Enhanced Surveillance and Traffic Information System (TIS) — Garmin GTX 33D
  • Four-color weather-avoidance radar — Garmin GWX 68
  • Satellite data link weather transceiver — Garmin GDL 69A
  • Electric standby attitude indicator — Mid Continent Instruments 4200
  • Electromechanical standby airspeed Indicator -—Aerosonic 261440
  • Electromechanical Standby Altimeter — Aerosonic 162350
  • Emergency locator transmitter (ELT) — Artex C406-N
  • Pilot-selectable Flight Path Scan narrows the scan range to ±10, 20, or 30 degrees and increases the scan rate.
    Ground mapping depicts terrain features with a separate color scheme from the weather modes
    Installed on center glare shield panel:
  • LH and RH master caution/master warning lights
  • LH and RH engine fire control switches
  • Flight director/autopilot controller
  • Electronic standby instrument system
  • LH and RH display control units
    Installed on instrument panel (left to right):
  • LH primary flight display (PFD)
  • Multifunction display (MFD)
  • RH primary flight display (PFD)
    Installed on tilt panel (left to right):
  • Electrical power panel
  • Pressurization controls
  • Ice protection controls
  • Windshield anti-ice controls
  • Fuel controls
  • Engine start control
  • Ignition controls
  • Landing gear control module
  • Lighting controls
  • Flight hour meter
  • ELT remote switch
  • Environmental controls
    Installed on pedestal:
  • Engine power levers
  • Flap control handles
  • Speed brake control
  • Elevator trim control and indicator
  • Takeoff/Go-Around button
  • Rudder trim control
  • Aileron trim control
  • Emergency gear release
    Installed beneath the instrument panel:
  • Emergency brake handle
  • Parking brake handle

Detailed Specifications

Performance data is based on the standard Mustang 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
  • 40 ft 7 in (12.37 m)
  • Height
  • 13 ft 5 in (4.09 m)
  • Wingspan
  • 43 ft 2 in (13.16 m)
    Wing
  • Wing Area
  • Wing Sweep

  • 210 sq ft (19.51 sq m)
  • 11.0 degrees
    Wheelbase
  • 14 ft 4 in (4.37 m)
    Tread
  • 11 ft 10 in (3.61 m)
    Cabin Interior
  • Height
  • Width
  • Length

  • 54 in (1.37 m)
  • 55 in (1.40 m)
  • 9 ft 9 in (2.97 m)
  • Maximum Passengers
  • 5
    Baggage Capacity
  • Weight
  • Volume

  • 718 lb (325.7 kg)
  • 63 cu ft (1.78 cu m)
  • Single Pilot Certified
  • Yes

Weights

  • Maximum Ramp Weight
  • 8,730 lb (3,960 kg)
  • Maximum Takeoff Weight
  • 8,645 lb (3,921 kg)
  • Maximum Landing Weight
  • 8,000 lb (3,629 kg)
  • Maximum Zero Fuel Weight
  • 6,750 lb (3,062 kg)
    Usable Fuel Capacity
  • Weight
  • Volume

  • 2,580 lb (1,170 kg)
  • 385 gal (1,457 l)
  • Basic Operating Weight
  • 5,600 lb (2,540 kg)
  • Useful Load
  • 3,130 lb (1,420 kg)
  • Maximum Payload
  • 1,150 lb (522 kg)
  • Full Fuel Payload
  • 550 lb (249 kg)

Performance

  • Maximum Cruise Speed
  • 340 ktas (630 km/h)
  • Maximum Range
  • 1,200 nm (2,222 km)
  • Takeoff Field Length
  • 3,110 ft (948 m)
  • Landing Distance
  • 2,380 ft (725 m)
  • Maximum Operating Altitude
  • 41,000 ft (12,497 m)
  • Maximum Climb Rate
  • 3,010 fpm (917 mpm)
  • Maximum Limit Speed
  • 0.63 Mach (0.63 Mach)

Powerplant

Two dual-channel, FADEC-controlled, Pratt & Whitney Canada™ PW615F-A turbofan engines are installed on the Mustang. The engine is a 2.8:1 bypass ratio, counter-rotating, twin-spool design with three compression stages and two turbine stages. It produces 1,460 pounds (6.49 kN) of thrust at sea level, static conditions, flat-rated up to 77°F (25°C). The FADEC system also provides time-limited dispatch, diagnostics and engine synchronization according to switch position.

  • Manufacturer: Pratt & Whitney
  • Model: (2) PW615F-A
  • Thrust: 1,460 lbf
  • Time between overhaul: 3,500 hr
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Technical Specifications

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