N404EL - 2005 LEARJET 40XR


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    Aircraft Summary


    General

    Year
    2005
    Manufacturer
    LEARJET
    Model
    40XR
    Serial Number
    2033
    Registration #
    N404EL
    Condition
    Used
    FlightRules
    IFR
    Description
    US Certificate of Airworthiness dated August 15, 2005 Aircraft Warranty Start Date of September 2005 Gross Weight Increase Mod (SB 40-11-01) complied with BR Engine Upgrade (SB 40-72-01) complied with One US Based Owner Since New No Damage History All maintenance has been performed at a Bombardier Learjet Service Center Aircraft Enrolled on Bombardier Smart Parts Plus Program Maintained under FAR Part 91 Since New CAMPS Airframe Maintenance Tracking Program Full Maintenance History available upon request Reduced Vertical Separation Minimum (RVSM) Please contact Jim Blakey for further details at (281) 989-5660 or [email protected]

    Airframe

    Total Time
    1509.1
    Airframe Notes
    Status as of 08/21/09 TTSN: 1509.1 Landings: 1404

    Engine Program

    Engine Program Notes
    Honeywell TFE-731-20BR-1B Left Engine: SN - 116630, 1509.1 TTSN, 1404 Cycles Right Engine: SN - 116630, 1509.1 TTSN, 1404 Cycles Engines are enrolled on Honeywell MSP Jet-Care Trending & Spectro Oil Analysis Since New

    Avionics

    Avionics/Radios
    Honeywell DU-870 Primus 1000 - Four Tube EFIS Package Dual Honeywell IC-600 Autopilot Computers Dual Honeywell AZ-850 Air Data Computers Dual Honeywell AHZ-800 AHRS Computers Engine Instrument/Crew Alerting System (EICAS) Dual Honeywell Primus II Nav / Comm systems with 8.33 Spacing & FM Immunity Dual Honeywell Primus II - RNZ-851 DME Dual Honeywell Primus II - RM-851 Mode S Transponders Honeywell Primus II - RNZ-851 ADF Honeywell Primus II - KHF-950 HF with SELCAL Honeywell RT-300 Radio Altimeter Honeywell Primus 660 Color Weather Radar Honeywell Traffic Collision Avoidance System TCAS-II (TCAS 2000) with Change 7 Honeywell MK V EGPWS with Windshear Detection & Terrain Display Dual Universal UNS-1E Flight Management Systems (FMS) Software 802.4 with GPS Artex C406-2 Emergency Locator Transmitter (ELT) OPTIONAL EQUIPMENT FMS Advanced Performance Database Dual Angle of Attack (AOA) Indicators Iridium ICS-100/200 SATCOM System 4 - 110 Volt AC Outlets Microwave Oven Aircraft Locking Package Pulse Light System Tail Illumination Package - LOGO Lights Lighted Control Wheel Chart Holders Pedestal Mounted Data Transfer Unit (DTU) XM Satellite Weather Dual Fujitsu FG-7000 Electronic Flight Bags (EFB) Entertainment System with Dual DVD, 10 Player CD Airshow 4000 with 1-Forward Monitor, 1-Aft Monitor and 2 Rosen 7" Side Mounted Monitors

    Additional Equipment

    Additional Equipment
    2 Inch Standby IAS/ATT/ALT Indicators Dual Concorde 38 Amp Hour Lead Acid Batteries Keith Vapor Cycle Air Conditioning System with Auxiliary Heater Honeywell SSCVR Cockpit Voice Recorder (CVR) Dual DAVTRON Clocks

    Exterior

    Year Painted
    2005

    Interior

    Year Interior
    2005
    Number of Seats
    7
    Interior Notes
    Executive Configuration with Forward 4 Place Club, 2 Forward Facing Seats, Aft Belted Lavatory Six Lateral Tracking Seats upholstered in light tan leather with light tan carpeting Aft Lav with Flushing Toilet, Sink, Lighted Vanity Mirror & Belted Lav Seat Galley Jump Seat (Non-belted) High-Gloss Wood Veneer Cabinetry Slimline Tables

    Inspection Status

    Inspection Status
    Inspection - C/W - DATE - C/W - BY - DUE Phase A-300 Hour - 1500 Hours - 08/2009 - Bombardier - 1,800 Hours Phase B-600 Hour - 1200 Hours - 05/2008 - Learjet Wichita - 1,800 Hours Phase C-1,200 Hour - 1200 Hours - 05/2008 - Learjet Wichita - 2,400 Hours Phase D-2,400 Hour - NA - NA - NA - 2,400 Hours


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