2005 CESSNA CITATION XLS

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    Posizione dell' Aereomobile:Guilford, Connecticut, Stati Uniti

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    Mikolay Jet Group

    Contatto:Mike Mikolay

    Telefono:(203) 887-2309

    Guilford, Connecticut, Stati Uniti

    (203) 887-2309

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    Descrizione

    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)

    Specifiche

    Anno2005
    ProduttoreCESSNA
    ModelloCITATION XLS
    Numero di serie560-5581
    Registrazione #N577PS
    CondizioneUsati
    FondataGMU
    Tempo totale4,770
    Sbarchi totali3,876
    Autonomia1,989 Nm
    Peso massimo della rampa9,253.28 kg
    Peso massimo al decollo9,162.57 kg
    Peso massimo di atterraggio8,482.18 kg
    Peso massimo del carburante zero6,849.24 kg
    Peso vuoto di base5,701.91 kg
    Monitoraggio di mantenimentoCamp
    Engine 1 Maintenance ProgramNessuna
    Engine 1 Make/ModelPRATT & WHITNEY PW545B
    Motore 1 - Numero di seriePCE-DD0171
    Engine 1 Time4,770 SNEW
    Motore 1 TBO5500
    Engine 1 Cycles Since Overhaul3,879
    Motore 1 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500
    Engine 2 Make/ModelPRATT & WHITNEY PW545B
    Motore 2 - Numero di seriePCE-DD0170
    Engine 2 Time4,770 SNEW
    Motore 2 TBO5500
    Engine 2 Cycles Since Overhaul3,879
    Motore 2 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500
    APUSi
    Durata unità di potenza ausiliaria2,135
    Programma APUNessuna
    Note APUAPU is currently undergoing the 4,000 Cycle Rotor Overhaul
    Flight Deck Manufacturer/ModelHONEYWELL
    Sistema ADS-BSi
    WAASSi
    Avionica/RadioAvionics: 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
    WifiSi
    Attrezzature aggiuntiveWIFI (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)
    Anno dipinto2015
    EsterioreOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
    Anno Interno2018
    Numero di posti a sedere9
    Configurazione della cambusaForward
    InterioreThe 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
    Stato di ispezioneOperated & 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
    Idoneo alla navigazione aereaSi
    Anno2005|
    ProduttoreCESSNA|
    ModelloCITATION XLS|
    Numero di serie560-5581|
    Registrazione #N577PS|
    CondizioneUsati|
    FondataGMU|
    Tempo totale4,770|
    Sbarchi totali3,876|
    Autonomia1,989 Nm|
    Peso massimo della rampa9,253.28 kg|
    Peso massimo al decollo9,162.57 kg|
    Peso massimo di atterraggio8,482.18 kg|
    Peso massimo del carburante zero6,849.24 kg|
    Peso vuoto di base5,701.91 kg|
    Monitoraggio di mantenimentoCamp|
    Engine 1 Maintenance ProgramNessuna|
    Engine 1 Make/ModelPRATT & WHITNEY PW545B |
    Motore 1 - Numero di seriePCE-DD0171|
    Engine 1 Time4,770 SNEW |
    Motore 1 TBO5500|
    Engine 1 Cycles Since Overhaul3,879|
    Motore 1 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500|
    Engine 2 Make/ModelPRATT & WHITNEY PW545B |
    Motore 2 - Numero di seriePCE-DD0170|
    Engine 2 Time4,770 SNEW |
    Motore 2 TBO5500|
    Engine 2 Cycles Since Overhaul3,879|
    Motore 2 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500|
    APUSi|
    Durata unità di potenza ausiliaria2,135|
    Programma APUNessuna|
    Note APUAPU is currently undergoing the 4,000 Cycle Rotor Overhaul|
    Flight Deck Manufacturer/ModelHONEYWELL|
    Sistema ADS-BSi|
    WAASSi|
    Avionica/RadioAvionics: 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|
    WifiSi|
    Attrezzature aggiuntiveWIFI (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)|
    Anno dipinto2015|
    EsterioreOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)|
    Anno Interno2018|
    Numero di posti a sedere9|
    Configurazione della cambusaForward|
    InterioreThe 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|
    Stato di ispezioneOperated & 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|
    Idoneo alla navigazione aereaSi|
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