2005 CESSNA CITATION XLS

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    Vliegtuig locatie:Guilford, Connecticut, VS

    Verkopersinformatie

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    Mikolay Jet Group

    Contactpersoon:Mike Mikolay

    Telefoon:+1 203-887-2309

    Guilford, Connecticut, VS

    +1 203-887-2309

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    Omschrijving

    Aircraft is enrolled on an engine monitoring program that extends the TBO to 5,500 hours APU is currently undergoing the 4,000 Cycle Rotor Overhaul Many desirable options that include: - WIFI (GoGo AVANCE L5) - WAAS - ADS-B Out - Garmin GMX-200 MFD w/ XM Weather - Garmin GDL-69 - RAAS (Runway Awareness & Advisory System)

    Specificaties

    Jaar2005
    FabrikantCESSNA
    ModelCITATION XLS
    Serienummer560-5581
    Registratie #N577PS
    ConditieGebruikt
    Gebaseerd opGMU
    Totale tijd4,770
    Totale landingen3,876
    Bereik1,989 Nm
    Max. hellingsgewicht9,253.28 kg
    Maximaal startgewicht9,162.57 kg
    Maximaal landingsgewicht8,482.18 kg
    Maximaal nul brandstofgewicht6,849.24 kg
    Basis leeggewicht5,701.91 kg
    Onderhoud bijhoudenCamp
    Engine 1 Maintenance ProgramGeen
    Motor 1 OpmerkingenEnrolled on Trend Monitoring Program which extends TBO to 5500
    Engine 1 Make/ModelPRATT & WHITNEY PW545B
    Motor 1 serienummerPCE-DD0171
    Engine 1 Time4,770 SNEW
    Motor 1 TBO5500
    Motor cycli3,879
    Motor 1 OpmerkingenEnrolled on Trend Monitoring Program which extends TBO to 5500
    Engine 2 Make/ModelPRATT & WHITNEY PW545B
    Motor 2 serienummerPCE-DD0170
    Engine 2 Time4,770 SNEW
    Motor 2 TBO5500
    Engine 2 Cycles Since Overhaul3,879
    Motor 2 OpmerkingenEnrolled on Trend Monitoring Program which extends TBO to 5500
    APUJa
    APU-tijd2,135
    APU-onderhoudsprogrammaGeen
    APU-notitiesAPU is currently undergoing the 4,000 Cycle Rotor Overhaul
    Flight Deck Manufacturer/ModelHONEYWELL
    ADS-B uitgerustJa
    WAASJa
    Avionics/radio'sAvionics: Honeywell Primus 1000 Suite Flight Displays: Three Honeywell Primus 1000 Liquid Crystal Displays ‍Global Positioning System: Dual Universal UNS 1ESPW FMS w/ GPS Communications: Dual Honeywell 850 Integrated Comms Navigation: Dual Honeywell 850 Navs Cockpit Voice Recorder: Fairchild FA2100 CVR (120 minute) Flight Management System: Dual Universal UNS 1ESPW FMS w/ GPS Attitude Heading Reference Unit: Honeywell LCR-93 AHRS ‍Distance Measuring Equipment: Dual Honeywell DM 850 DME‍ Autopilot System: Honeywell Primus 1000 IFCS‍ Transponders: Dual Honeywell XS 850 / Mode S Transponders w/ ADS-B Out and Enhanced Surveillance ‍ Traffic Alert and Collision Avoidance System: Honeywell TPU-678 TCAS II‍ Weather Radar: Honeywell WU-880 Weather Radar‍ Terrain Awareness Warning System: Honeywell Mark V TAWS‍ Radio Altimeter: Honeywell ALT-55B Radio Altimeter‍ Emergency Locator Transmitter: Artex 406-N ELT w/ navigation interface‍ SATCOM: AirCell ST-3100 Iridium w/ dual cordless handsets‍ High Frequency Radio: Honeywell HF 1050 w/ SELCAL
    WifiJa
    Extra uitrustingWIFI (GoGo AVANCE L5) WAAS ADS-B Out Garmin GMX-200 MFD w/ XM Weather Garmin GDL-69 Datalink HF Radio w/ SELCAL 2nd UNS 1ESPW FMS Cockpit Speaker Mute Switch RAAS (Runway Awareness & Advisory System)
    Jaar geschilderd2015
    BuitenkantOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
    Jaar interieur2018
    Aantal zitplaatsen9
    Kombuis configuratieForward
    InterieurThe 9-passenger executive interior with new carpet in 2018 and wood veneers refinished in 2015 and is configured as follows: Entryway: Two-place side-facing divan Cabin: Mid-cabin double club and two forward-facing seats in the aft cabin portion of the aircraft Aft Lavatory: Lavatory with externally serviceable flushing toilet and aft closet storage Left Hand Forward Refreshment Center: Insulated ice drawer, trash compartment, and storage
    InspectiestatusOperated & Maintained per FAR §135 Date of Manufacture: 2005 Certification Date: September 24, 2005 Maintenance tracked by CAMP Engines Enrolled on Trend Monitoring Inspection Doc. Description Last Completed Next Due Date (Date/Hours) Document 1 (12 M) Nose, Cockpit, Fuselage May 23, 2025 April 30, 2026 Document 3 (24 M) Cabin, Lavatory, Windshields, Windows May 23, 2025 April 30, 2027 Document 6 (48 M) Complete Inspection May 19, 2023 April 30, 2027 Document 8 (2400 Hrs) Complete Inspection 3,955.9 6,355.9 Document 11 (48 M) Flight Control Inspection April 28, 2025 April 30, 2027 Document 13 (72 M) CVR, Hydraulic, Cockpit, Empennage April 21, 2021 April 30, 2027 Document 16 (96 M) Nose, Cabin, Cockpit, Horizontal, Vertical May 19, 2023 May 31, 2031 Document 17 (6000 Hrs) Vertical Stabilizer Pivot Fitting n/a 6,000.0 Engine 1 & 2 Inspection 4,732.4 / 4,732.4 5,532.4 / 5,532.4 Engine 1 & 2 Overhaul Inspection n/a 5,500.0
    LuchtwaardigJa
    Jaar2005|
    FabrikantCESSNA|
    ModelCITATION XLS|
    Serienummer560-5581|
    Registratie #N577PS|
    ConditieGebruikt|
    Gebaseerd opGMU|
    Totale tijd4,770|
    Totale landingen3,876|
    Bereik1,989 Nm|
    Max. hellingsgewicht9,253.28 kg|
    Maximaal startgewicht9,162.57 kg|
    Maximaal landingsgewicht8,482.18 kg|
    Maximaal nul brandstofgewicht6,849.24 kg|
    Basis leeggewicht5,701.91 kg|
    Onderhoud bijhoudenCamp|
    Engine 1 Maintenance ProgramGeen|
    Motor 1 OpmerkingenEnrolled on Trend Monitoring Program which extends TBO to 5500|
    Engine 1 Make/ModelPRATT & WHITNEY PW545B |
    Motor 1 serienummerPCE-DD0171|
    Engine 1 Time4,770 SNEW |
    Motor 1 TBO5500|
    Motor cycli3,879|
    Motor 1 OpmerkingenEnrolled on Trend Monitoring Program which extends TBO to 5500|
    Engine 2 Make/ModelPRATT & WHITNEY PW545B |
    Motor 2 serienummerPCE-DD0170|
    Engine 2 Time4,770 SNEW |
    Motor 2 TBO5500|
    Engine 2 Cycles Since Overhaul3,879|
    Motor 2 OpmerkingenEnrolled on Trend Monitoring Program which extends TBO to 5500|
    APUJa|
    APU-tijd2,135|
    APU-onderhoudsprogrammaGeen|
    APU-notitiesAPU is currently undergoing the 4,000 Cycle Rotor Overhaul|
    Flight Deck Manufacturer/ModelHONEYWELL|
    ADS-B uitgerustJa|
    WAASJa|
    Avionics/radio'sAvionics: Honeywell Primus 1000 Suite Flight Displays: Three Honeywell Primus 1000 Liquid Crystal Displays ‍Global Positioning System: Dual Universal UNS 1ESPW FMS w/ GPS Communications: Dual Honeywell 850 Integrated Comms Navigation: Dual Honeywell 850 Navs Cockpit Voice Recorder: Fairchild FA2100 CVR (120 minute) Flight Management System: Dual Universal UNS 1ESPW FMS w/ GPS Attitude Heading Reference Unit: Honeywell LCR-93 AHRS ‍Distance Measuring Equipment: Dual Honeywell DM 850 DME‍ Autopilot System: Honeywell Primus 1000 IFCS‍ Transponders: Dual Honeywell XS 850 / Mode S Transponders w/ ADS-B Out and Enhanced Surveillance ‍ Traffic Alert and Collision Avoidance System: Honeywell TPU-678 TCAS II‍ Weather Radar: Honeywell WU-880 Weather Radar‍ Terrain Awareness Warning System: Honeywell Mark V TAWS‍ Radio Altimeter: Honeywell ALT-55B Radio Altimeter‍ Emergency Locator Transmitter: Artex 406-N ELT w/ navigation interface‍ SATCOM: AirCell ST-3100 Iridium w/ dual cordless handsets‍ High Frequency Radio: Honeywell HF 1050 w/ SELCAL|
    WifiJa|
    Extra uitrustingWIFI (GoGo AVANCE L5) WAAS ADS-B Out Garmin GMX-200 MFD w/ XM Weather Garmin GDL-69 Datalink HF Radio w/ SELCAL 2nd UNS 1ESPW FMS Cockpit Speaker Mute Switch RAAS (Runway Awareness & Advisory System)|
    Jaar geschilderd2015|
    BuitenkantOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)|
    Jaar interieur2018|
    Aantal zitplaatsen9|
    Kombuis configuratieForward|
    InterieurThe 9-passenger executive interior with new carpet in 2018 and wood veneers refinished in 2015 and is configured as follows: Entryway: Two-place side-facing divan Cabin: Mid-cabin double club and two forward-facing seats in the aft cabin portion of the aircraft Aft Lavatory: Lavatory with externally serviceable flushing toilet and aft closet storage Left Hand Forward Refreshment Center: Insulated ice drawer, trash compartment, and storage|
    InspectiestatusOperated & Maintained per FAR §135 Date of Manufacture: 2005 Certification Date: September 24, 2005 Maintenance tracked by CAMP Engines Enrolled on Trend Monitoring Inspection Doc. Description Last Completed Next Due Date (Date/Hours) Document 1 (12 M) Nose, Cockpit, Fuselage May 23, 2025 April 30, 2026 Document 3 (24 M) Cabin, Lavatory, Windshields, Windows May 23, 2025 April 30, 2027 Document 6 (48 M) Complete Inspection May 19, 2023 April 30, 2027 Document 8 (2400 Hrs) Complete Inspection 3,955.9 6,355.9 Document 11 (48 M) Flight Control Inspection April 28, 2025 April 30, 2027 Document 13 (72 M) CVR, Hydraulic, Cockpit, Empennage April 21, 2021 April 30, 2027 Document 16 (96 M) Nose, Cabin, Cockpit, Horizontal, Vertical May 19, 2023 May 31, 2031 Document 17 (6000 Hrs) Vertical Stabilizer Pivot Fitting n/a 6,000.0 Engine 1 & 2 Inspection 4,732.4 / 4,732.4 5,532.4 / 5,532.4 Engine 1 & 2 Overhaul Inspection n/a 5,500.0|
    LuchtwaardigJa|
    Als Paragraaf Weergeven

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