N999AD - 1991 CESSNA CITATION V


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    Aircraft Summary


    General

    Year
    1991
    Manufacturer
    CESSNA
    Model
    CITATION V
    Serial Number
    0136
    Registration #
    N999AD
    Condition
    Used
    Description
    Previous Registration Numbers: N772AA & N501T Maximum Ramp Weight: 16,500 pounds Maximum Takeoff Weight: 16,300 pounds Maximum Landing Weight: 15,200 pounds Maximum Zero Fuel Weight: 12,200 pounds Basic Operating Weight: 10,000 pounds Fuel Capacity: 5,814 pounds 2 owners since new, Honeywell/Collins equipped, EROS oxygen masks, thrust reversers, no damage history

    Airframe

    Total Time
    6361.0
    Airframe Notes
    Total Cycles: 4337

    Engine Program

    Engine Program Notes
    LEFT ENGINE Year 1991 Manufacturer Pratt & Whitney Type JT15D-5A S/N PC-E108272 Total Time 6,211 hours Total Cycles 4,222 TBO 3,500 hours RIGHT ENGINE Year 1991 Manufacturer Pratt & Whitney Type JT15D-5A S/N PC-E108281 Total Time 6,287.9 hours Total Cycles 4,279 TBO 3,500 hours All engine overhauls and hot section inspection performed by Pratt & Whitney.

    Engine 1

    Engine 1 Time
    2727
    Engine 1 Time Since
    SMOH

    Engine 2

    Engine 2 Time
    2827
    Engine 2 Time Since
    SMOH

    Avionics

    Avionics/Radios
    Honeywell EDZ-605 EFIS (5-tube installation) Honeywell MC-800 MFD Controller with Electronic Checklists and Armrest Joysticks Honeywell SPZ-500 AFCS (Autopilot) Honeywell AZ-810 Digital Air Data Computer (DADC) Honeywell VN-800 VNAV Computer/Altitude Controller Honeywell Dual FZ-500 Flight Directors and MS-205 Mode Selectors Honeywell Primus 870 Color Weather Radar with WC-870 Controller Dual C14D Directional Gyros Dual VG-14A Vertical Gyros Dual Collins VHF-22A Comms Dual Collins VIR-32 Navs Dual Collins RMI-36 Dual Collins DME-42 Collins TDR-94 Transponders Collins ADF-462 Collins ALT-55B Radar Altimeter JET AI-804 Standby Gyro Sundstrand Mark II GPWS GA-100 CVR Fairchild F-1000 FDR Universal UNS-1K/GPS FMS, Enroute & Instrument Approach Approval, Panel Data Loader

    Additional Equipment

    Additional Equipment
    Cessna 12,200 pound Zero Fuel Weight Cessna 400 pound Gross Weight Increase (16,300 pound Takeoff Weight) Cessna Zephyr Freon Air Conditioning EROS Oxygen masks B&D Cockpit Display B&D Cabin Display Flitefone VI with Cockpit and Cabin Handsets Precise Flight Pulse Lights 2 Cabin AC Power Outlets Tail Logo Lights 4 Seat Belt Extenders (36") 4 Seat Slip Covers Cloth Engine Covers Right Hand Landing Gear Handle Placement Radome Quick Release Mod Cabin Temperature Indicator ELT with Cockpit Control Switch Fire Bell Installation Monorail Sun Visor Thrust Reversers Thrust Reverser Locks Jack Pads Locking Fuel Cap

    Exterior

    Year Painted
    2002
    Exterior Notes
    Matterhorn white (570-535), no stripes, new paint August 2002, wing & tail deice boots replaced in 1999.

    Interior

    Year Interior
    2002
    Interior Notes
    Interior completely refurbished, August 2002, seven seats plus aft lavatory with vanity (lavatory seat not approved for takeoff and landing). Center club configuration with left-hand forward refreshment center and forward right-hand cabinet. Seats, Panels, & Drink Rails "Buff" Leather Seat Padding Confor Foam Headliner "Seashell" Carpet Duraweave "Natural" Cabinet and Table Edging Natural Wood Cabinetry Laminate "Congo Spruce" Seat Belts "Fawn" Privacy Curtain "Cornsilk" Baggage Area Carpet Beige Gross Point

    Inspection Status

    Inspection Status
    CESCOM Computerized Mainteance Tracking System since new. All Airworthiness Directives complied with. All mandatory and recommended Cessna Service Bulletins and Letter complied with. All mandatory and recommended Pratt & Whitney Service Bulletins and Letters complied with. All major maintenance performed at Cessna Citation Service Centers. Phase 1-5 (5801.9 total time) completed March 2001 at the Wichita Cessna Citation Service Center. Phase 1-4 (6359.5 total time) completed June 2002 at the Orlando Cessna Citation Service Center.


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