N577PS - 2005 CESSNA CITATION XLS




    Aircraft Summary


    General

    Year
    2005
    Manufacturer
    CESSNA
    Model
    CITATION XLS
    Serial Number
    560-5581
    Registration #
    N577PS
    Condition
    Used
    Based at
    GMU
    Description
    Available for immediate delivery 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)

    Airframe

    Total Time
    4770
    Total Landings
    3876
    Range
    1,989 NM
    Max Ramp Weight
    20,400 lb
    Max Takeoff Weight
    20,200 lb
    Max Landing Weight
    18,700 lb
    Max Zero Fuel Weight
    15,100 lb
    Basic Empty Weight
    12,570.56 lb
    Maintenance Tracking
    CAMP

    Engine Program

    Engine Maintenance Program
    None

    Engine 1

    Engine 1 Manufacturer
    PRATT & WHITNEY
    Engine 1 Model
    PW545B
    Engine 1 Serial Number
    PCE-DD0171
    Engine 1 Time
    4770
    Engine 1 Time Since
    SNEW
    Engine 1 TBO
    5500
    Engine 1 Cycles
    3879
    Engine 1 Notes
    Enrolled on Trend Monitoring Program which extends TBO to 5500

    Engine 2

    Engine 2 Manufacturer
    PRATT & WHITNEY
    Engine 2 Model
    PW545B
    Engine 2 Serial Number
    PCE-DD0170
    Engine 2 Time
    4770
    Engine 2 Time Since
    SNEW
    Engine 2 TBO
    5500
    Engine 2 Cycles
    3879
    Engine 2 Notes
    Enrolled on Trend Monitoring Program which extends TBO to 5500

    Auxiliary Power Unit

    APU
    Yes
    APU Time
    2135
    APU Maintenance Program
    None
    APU Notes
    APU is currently undergoing the 4,000 Cycle Rotor Overhaul

    Avionics

    Flight Deck Manufacturer
    HONEYWELL
    ADS-B Equipped
    Yes
    WAAS
    Yes
    Avionics/Radios
    Avionics: 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

    Additional Equipment

    Wifi
    Yes
    Additional Equipment
    WIFI (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)

    Exterior

    Year Painted
    2015
    Exterior Notes
    Overall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)

    Interior

    Year Interior
    2018
    Number of Seats
    9
    Galley Configuration
    Forward
    Interior Notes
    The 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

    Inspection Status

    Inspection Status
    Operated & 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
    Airworthy
    Yes


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