CITATION S/II

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GALLERY

OVERVIEW

Valor is pleased to present this 1988 Citation S/II, serial number S550-0151, a refined and enhanced version of the Classic Citation II 550. Designed for superior efficiency and performance, the Super II incorporates a supercritical airfoil with swept wing roots, aileron and flap gap seals, and an advanced fluid deicing system that replaces the pneumatic boots found on earlier models. Aerodynamic refinements, including redesigned fuselage and engine nacelle pylons with added fairings, contribute to reduced drag. An increased fuel capacity of 120 additional gallons enables a cruise speed of 411 KTAS and a range of 1,419 miles with reserves. The upgraded JT15D-4B engines deliver 2,500 lbs of thrust with higher temperature-rated components, providing greater performance at higher altitudes.

This aircraft is equipped with an advanced Garmin avionics suite, including dual GTN-750/650 COMM/NAV, WAAS capabilities, Garmin ADS-B In & Out transponders with Flight ID and Traffic, and Flight Map 796. Available for immediate delivery. Contact us today for more details or to schedule a viewing.

Highlights

  • 475hrs SINCE HSI/HOTS
  • Garmin GTN-750/650 (WAAS/LPV)
  • Garmin GDL-Datalink | Garmin MAP 796
  • ADS-B In & Out | TCAS/TAWS

Airframe

  • Hours Since New 14,119
  • Landings Since New 10,722

Engines

Pratt & Whitney JT15-4B Left Right
Serial Numbers PCE102071 PCE102069
Hours Since New 15,491 15,090
Cycles Since New 12,244 11,414
Hours Since HSI/HOTS 475 475
Hours Since Overhaul 2,200 2,300
Overhaul Due TBO 3,500 3,500

 

Inspection

On CESCOM Maintenance Tracking
Phase 1-4 / 24M-300HR – C/W 01/2025
Phase 5 / 36M-1,200HR – C/W 01/2025
Phase 21 / 24M RVSM Calibration – C/W 01/2025

Avionics

AVIONICS

Honeywell & Garmin

  • Autopilot: Honeywell SPZ-500 IFCS
  • Communication Radios: Garmin GTN-750/650 (WAAS)
  • CVR: Fairchild GA100
  • DME: Collins DME-42
  • Flight Director: Honeywell SPZ-500 IFCS
  • FMS: Garmin GTN-750/650 (WAAS/LPV)
  • GPS: Garmin w/ MAP 796
  • Navigation Radios: Garmin GTN-750/650 (WAAS)
  • Radar Altimeter: Collins ALT-55
  • Stormscope: BFGoodrich WX-1000
  • TAWS: King KGP-560 EGPWS
  • TCAS: BFGoodrich SKY-497
  • Transponder: Dual Garmin GTX-345R & 335 w/Flight ID (ADS-B In & Out)
  • Weather Radar: Honeywell Primus 800 (Color)

CAPABILITIES

  • RVSM
  • ADS-B In & Out
  • WAAS/LPV
  • TAWS | TCAS
  • Intergraded COMM/ NAV
  • Electronic Chart View

Additional Information

INTERIOR

Executive Cabin with Modern Refinements. This executive nine-passenger interior is finished in Honey Wheat leather, offering both style and comfort. The forward cabin features a two-place divan, transitioning into a mid-cabin four-place club configuration with dual executive pull-out tables. The aft section includes two forward-facing seats and a private, belted flushing lavatory, enclosed by pocket doors for added privacy.

Dark Burlwood veneer cabinetry and bulkheads, with nickel hardware. Coordinating Honey Wheat leather sidewalls and arm-rails, faux suede headliner, and desert sand carpeting.

For convenience, the forward LH refreshment center includes a dual liquid dispenser, ice bin, liquor and drink cabinet, multiple storage compartments, and a solid surface working area. USB dual ports at each main cabin seat and Freon A/C with climate control.

This interior was refurbished in 2015, including seats, sidewalls, carpet, and woodwork.

 

EXTERIOR

The exterior features overall Matterhorn White with Black Velvet, Castle Silver and
Gold accent striping. Refurbished in 2000.

 

ADDITIONAL EQUIPMENT

This aircraft is equipped with an ELT 406C-2, Garmin avionics suite, including the GTN750 & GTN-650 for COMM, NAV, and GPS functionality. It also features a GDL-69A Datalink with XM Weather & MAP-796. The remote Garmin GMA-35C Audio Panel enhances communication efficiency. For passenger convenience, USB ports, and dual Davtron clocks. Performance and safety features include thrust reversers, Freon air conditioning, Bravo style entry steps, a Sierra quick-release radome, Nose baggage pneumatic lifts, Cleveland wheels and brakes.

 

INSPECTION OVERVIEW

On CESCOM Maintenance Tracking

  • Phase 1-4 / 24M-300HR – C/W 01/2025
  • Phase 5 / 36M-1,200HR – C/W 01/2025
  • Phase 21 / 24M RVSM Calibration – C/W 01/2025

 

WEIGHTS / CAPACITY

  • Maximum Gross Takeoff Weight (MGTOW): 15,100 lbs
  • Maximum Ramp Weight: 15,300 lbs
  • Maximum Zero Fuel Weight (ZFW): 11,200 lbs
  • Maximum Landing Weight: 14,400 lbs
  • Usable Fuel Capacity: 5,775 lbs
    (862 U.S. gallons)

INQUIRE

Download the Brochure for this Jet

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