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    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
    1984 CESSNA CITATION SII Used Jet Aircraft1984 CESSNA CITATION SII Used Jet Aircraft
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    1984 CESSNA CITATION SII

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    売主に関する情報

    View Seller Information

    Valor Jets

    お問い合わせ先:Graham Johnson

    電話番号:+1 941-244-2396

    Osprey, Florida, アメリカ

    General

    年式
    1984
    メーカー
    モデル
    シリアル番号
    S550-0013
    Registration #
    N84LG
    状態
    中古
    Based at
    ASL
    説明
    Offered by Valor this 1984 Citation S/II s/n S550-0013.The Citation S/II or Super II is the enhanced version of the Classic Citation II 550, as it gained a supercritical airfoil with swept wing-roots, aileron and flap gap seals, and a fluid deicing system instead of the pneumatic deicing boots used on earlier Citations 500,501,550’s.To further reduce drag, the fuselage and engine nacelle pylons were redesigned, and nacelle fairings were added as well. Fuel capacity was increased by 120 US gal (450 L). The result of the improvements was a cruise speed of 411ktas, and a range of 1,500+ with six passengers and crew with fuel reserve. The improved 2,500lbs thrust JT15D-4B engines have higher temperature-rated components, allowing more thrust at higher altitudes. This aircraft features Garmin COMM/NAV-GPS, XM Datalink, ADS-B Trans, Honeywell MFD, TCAS & TAWS, along with Freon A/C and Increased Gross Weight Mod. Contact us today for more details or to schedule a viewing.

    Airframe

    Total Time
    11,460
    Total Landings
    11,069
    Max Takeoff Weight
    6,849.24 kg

    Engine Program

    Engine 1 Maintenance Program
    None
    Engine(s)
    Hale Aircraft- Turbine HSI/HOTS performed in 2025

    Engine 1

    Engine 1 Make/Model
    PRATT & WHITNEY JT15D-4B
    Engine 1 Serial Number
    PCE71063
    Engine 1 Time
    6,270 SNEW
    Engine 1 TBO
    3500
    Engine 1 Cycles Since Overhaul
    5,852
    Hot Section Time 1
    0
    Engine 1 Notes
    Pratt & Whitney JT15D-4B Left                 Serial Numbers PCE71063  Hours Since New                 6,270              Cycles Since New                3,909 Hours Since HSI/HOTS 0 Hours Since Overhaul           2,774     Overhaul Due TBO 3,500

    Engine 2

    Engine 2 Make/Model
    PRATT & WHITNEY JT15D-4B
    Engine 2 Serial Number
    PCE102026
    Engine 2 Time
    11,286 SNEW
    Engine 2 TBO
    3500
    Engine 2 Cycles Since Overhaul
    10,673
    Hot Section Time 2
    0
    Engine 2 Notes
    Pratt & Whitney JT15D-4B Right  Serial Numbers PCE102026 Hours Since New                 11,286 Cycles Since New                10,673 Hours Since HSI/HOTS 0 Hours Since Overhaul           2,827     Overhaul Due TBO 3,500

    Auxiliary Power Unit

    APU Maintenance Program
    None

    Avionics

    Flight Deck Manufacturer/Model
    COLLINS
    ADS-B Equipped
    はい
    Avionics/Radios
    Collins Pro-Line II ADF: Dual Collins ADF-60 Autopilot: Honeywell SPZ-200 IFCS Communication Radios: Collins VHF-22A/ GNS-530 CVR: Fairchild GA 100 DME: Dual Collins DME42 Flight Director: Honeywell SPZ-200 IFCS GPS: Garmin GNS-530 / King KLN-900 Coupled Navigation Radios: Collins VIR-32/ GNS-530 RMI: Dual Collins RMI-30 Stormscope: BFGoodwrich WX-1000+ SATCOM: Aircell ST-3100 w/ Dual Handsets TAWS: Honeywell KGP-560 EGPWS TCAS: Honeywell TPU-66A TCAS-I Transponder: Dual Garmin GTX-345R Transponder (ADS-B out) Weather Radar: Honeywell ART-2100VP Color Radar

    Additional Equipment

    Additional Equipment
    This Citation SII is equipped with Artex 406 ELT, Garmin GNS-530 COMM/NAV-GPS, GAD-42 Adapter, GDL-49 Data-link, Honeywell KGP-560 EGPWS, Honeywell KDR-510 flight information system w/WX uplink, Teledyne angle of attack, Honeywell KMD-850 multi-function display (Weather-NEXRAD, Traffic, Terrain) Collins audio panels, J.E.T. standby gyro, battery temperature monitor, standby gyro, digital fan speed indicators, dual Davtron clocks, Thrust reversers, gross weight increase mod, improved 8.5 gallon TKS system, Sierra Radome mod, engine fan & turbine synch, baggage compartment mod.

    Exterior

    Year Painted
    2002
    Exterior
    The aircraft is finished in Matterhorn White with Jade-Mist Green, Kelly Green, Kingston Grey, and Dark Grey accent striping. The exterior paint was completed in 2002 by Sky Harbor.

    Interior

    Year Interior
    2002
    Number of Seats
    9
    Galley
    はい
    Galley Configuration
    Forward
    Lavatory
    はい
    Lavatory Configuration
    Aft
    Interior
    Eight-Passenger Executive Cabin This Citation SII features a nine-passenger executive configuration, seating in Light Grey leather, Aft cabin 4-place club with dual executive tables, and a forward 4-place club at entry and a private aft-belted flushing lavatory. Wilsonart Burlwood veneer and trim with aluminum hardware. Matching light grey leather side walls, a light-textured headliner, and grey multi-line stone pile carpeting. Pyramid low-profile storage compartment mid cabin, and 110v outlets in the cabin.

    Inspection Status

    Inspection Status
    Maintenance Tracking via CAMS Phase 1-4 (24m/300-Hour) – C/W In Process Phase 5 (36m/1,200-Hour) – C/W In Process Eng. 1 & Eng. 2 HSI by Hale Aircraft 2025
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