Beschreibung
Turn-key Part 135 Citation Ultra with 2023 paint and interior, Maintained with an open checkbook, flying over 500 hours a year on charter, and ready to keep working from day one.
1991 Cessna Citation V | S/N 560-0109 | N480RL | Based at HOU
N480RL is a well-equipped Citation V that’s ready to fly. It has a 2023 interior and exterior refurbishment (photos show current condition), and avionics upgraded for today’s airspace. It has been maintained with an open-checkbook maintenance policy: every item is addressed when it comes arises.
Airframe
17,605.8 hours total time / 12,153 landings
Enrolled on CESCOM
Phases 1–5 complied with April–May 2026
RVSM recertified April 2026
Engines: Pratt & Whitney Canada JT15D-5A (3,500-hour TBO)
Engine 1: 2,226.8 hours since overhaul (May 2021); hot section inspection February 2026
Engine 2: 2,105.7 hours since overhaul (April 2021); hot section inspection February 2026
More than 1,270 hours left on both engines before overhaul
Avionics: ADS-B Out, WAAS and RVSM
Honeywell 5-tube EFIS with dual FZ-500 flight directors
Garmin GTN 625 GPS/COM/NAV (WAAS)
Primus 870 weather radar
TCAS II
Sandel ST3400 TAWS
KHF-950 HF radio
8.33 kHz COM
This is a cost-effective, mission-capable light jet that’s fully maintained and ready to go to work, for an owner-operator or a charter fleet. Records are available for review. Contact us today to schedule a viewing.Spezifikation
Jahr1991
HerstellerCESSNA
ModellCITATION V
Seriennummer560-0109
Registration #N480RL
ZustandGebraucht
FlightRulesIFR
Based atKHOU
Total Time17,605
Total Landings12,153
Range1,300 Nm
Max Ramp Weight7,484.27 kg
Max Takeoff Weight7,393.56 kg
Max Landing Weight6,894.6 kg
Maintenance TrackingCamp
AirframeAIRFRAME: 17,605.8 hrs total time / 12,153 landings (as of 12-Oct-2026).
Enrolled on CAMP. Phases 1-5 complied with April/May 2026. RVSM recertified 28-Apr-2026.
Engine 1 Maintenance ProgramKeine
Engine 1 Make/ModelPRATT & WHITNEY JT15D-5A
Engine 1 Serial NumberPCE-100067
Engine 1 Time2,226.8 SOH
Engine 1 TBO3500
Engine 1 Cycles10,384
Hot Section Time 1 430.9
Engine 1 NotesTotal time 12,423.2 hrs / 10,384 cycles. Overhauled 13-May-2021 at 15,379.0 airframe hrs; 1,273.2 hrs remaining to 3,500-hr TBO. HSI 27-Feb-2026.
Engine 2 Make/ModelPRATT & WHITNEY JT15D-5A
Engine 2 Serial NumberPCE-100068
Engine 2 Time2,105.7 SOH
Engine 2 TBO3500
Engine 2 Cycles10,381
Hot Section Time 2427.6
Engine 2 NotesTotal time 12,423.2 hrs / 10,381 cycles. Overhauled 16-Apr-2021 at 15,500.1 airframe hrs; 1,394.3 hrs remaining to 3,500-hr TBO. HSI 27-Feb-2026.
APU Maintenance ProgramKeine
GPS 1 HerstellerGARMIN
GPS 1 ModellGTN 625
Transponder 1 HerstellerGARMIN
Transponder 1 ModellGTX335R
Transponder 2 HerstellerGARMIN
Transponder 2 ModellGTX335R
ADS-B EquippedJa
WAASJa
Avionics/RadiosHoneywell 5-tube EFIS (factory option): pilot and copilot PFD / ND displays plus MFD, dual symbol generators and MFD symbol generator
Honeywell Primus II integrated radio system (SRZ-850 factory package) with dual RNZ-850 integrated nav units, dual VHF comm, dual radio management units
ADS-B Out compliant: dual Garmin GTX 335R transponders and Garmin GTN 625 GPS / COM / NAV (STC ST01691WI)
Honeywell Primus 650 weather radar
Sandel ST3400 TAWS / RMI
TCAS with top and bottom antennas and TCAS control unit
Universal UNS-1ESP flight management system (per complied SL560-34-30) with GPS
RVSM modification complied (SB 560-34-97 R01) with RVSM air data computer altimeter; 91.411 / 91.413 checks current to 30-Apr-2028
Dual Honeywell flight director computers with dual vertical gyros and dual directional gyros
Bendix/King KHF 950 HF communication system with large control head (factory option)
Garmin GMA 35 audio panel
Allied Flitefone VI cabin and cockpit telephone
Cockpit voice recorder with DK120 underwater locator beacon (ULB battery expires 30-Nov-2029)
Safe Flight angle-of-attack / stall warning system with pilot AOA indexer
Year Painted2023
Year Interior2023
Number of Seats7
GalleyJa
Galley ConfigurationForward
LavatoryJa
Lavatory ConfigurationAft
InteriorInterior Refurb 2023
AirworthyJa
Jahr1991|
HerstellerCESSNA|
ModellCITATION V|
Seriennummer560-0109|
Registration #N480RL|
ZustandGebraucht|
FlightRulesIFR|
Based atKHOU|
Total Time17,605|
Total Landings12,153|
Range1,300 Nm|
Max Ramp Weight7,484.27 kg|
Max Takeoff Weight7,393.56 kg|
Max Landing Weight6,894.6 kg|
Maintenance TrackingCamp|
AirframeAIRFRAME: 17,605.8 hrs total time / 12,153 landings (as of 12-Oct-2026).
Enrolled on CAMP. Phases 1-5 complied with April/May 2026. RVSM recertified 28-Apr-2026.|
Engine 1 Maintenance ProgramKeine|
Engine 1 Make/ModelPRATT & WHITNEY JT15D-5A |
Engine 1 Serial NumberPCE-100067|
Engine 1 Time2,226.8 SOH |
Engine 1 TBO3500|
Engine 1 Cycles10,384|
Hot Section Time 1 430.9|
Engine 1 NotesTotal time 12,423.2 hrs / 10,384 cycles. Overhauled 13-May-2021 at 15,379.0 airframe hrs; 1,273.2 hrs remaining to 3,500-hr TBO. HSI 27-Feb-2026.|
Engine 2 Make/ModelPRATT & WHITNEY JT15D-5A |
Engine 2 Serial NumberPCE-100068|
Engine 2 Time2,105.7 SOH |
Engine 2 TBO3500|
Engine 2 Cycles10,381|
Hot Section Time 2427.6|
Engine 2 NotesTotal time 12,423.2 hrs / 10,381 cycles. Overhauled 16-Apr-2021 at 15,500.1 airframe hrs; 1,394.3 hrs remaining to 3,500-hr TBO. HSI 27-Feb-2026.|
APU Maintenance ProgramKeine|
GPS 1 HerstellerGARMIN|
GPS 1 ModellGTN 625|
Transponder 1 HerstellerGARMIN|
Transponder 1 ModellGTX335R|
Transponder 2 HerstellerGARMIN|
Transponder 2 ModellGTX335R|
ADS-B EquippedJa|
WAASJa|
Avionics/RadiosHoneywell 5-tube EFIS (factory option): pilot and copilot PFD / ND displays plus MFD, dual symbol generators and MFD symbol generator
Honeywell Primus II integrated radio system (SRZ-850 factory package) with dual RNZ-850 integrated nav units, dual VHF comm, dual radio management units
ADS-B Out compliant: dual Garmin GTX 335R transponders and Garmin GTN 625 GPS / COM / NAV (STC ST01691WI)
Honeywell Primus 650 weather radar
Sandel ST3400 TAWS / RMI
TCAS with top and bottom antennas and TCAS control unit
Universal UNS-1ESP flight management system (per complied SL560-34-30) with GPS
RVSM modification complied (SB 560-34-97 R01) with RVSM air data computer altimeter; 91.411 / 91.413 checks current to 30-Apr-2028
Dual Honeywell flight director computers with dual vertical gyros and dual directional gyros
Bendix/King KHF 950 HF communication system with large control head (factory option)
Garmin GMA 35 audio panel
Allied Flitefone VI cabin and cockpit telephone
Cockpit voice recorder with DK120 underwater locator beacon (ULB battery expires 30-Nov-2029)
Safe Flight angle-of-attack / stall warning system with pilot AOA indexer|
Year Painted2023|
Year Interior2023|
Number of Seats7|
GalleyJa|
Galley ConfigurationForward|
LavatoryJa|
Lavatory ConfigurationAft|
InteriorInterior Refurb 2023|
AirworthyJa|
