C-GVVZ - 1999 LEARJET 45




    Aircraft Summary


    General

    Year
    1999
    Manufacturer
    LEARJET
    Model
    45
    Serial Number
    45-020
    Registration #
    C-GVVZ
    Condition
    Used
    Description
    FEATURES • Enrolled on the Evolve Maintenance Program • Fresh MPIs • Gross Weight and Zero Fuel Weight Increase • FDR Equipped • CVR with RIPS Sentry 120R • Dual UNS 1 EW/LPV FMS • Lifeport Medical Interior Provisions • Concorde Lead Acid Batteries • Belted Lavatory Seat

    Airframe

    Total Time
    9163

    Engine Program

    Engine Maintenance Program
    MSP

    Engine 1

    Engine 1 Manufacturer
    HONEYWELL
    Engine 1 Model
    TFE731-20AR-1B
    Engine 1 Time
    9095.3
    Engine 1 Cycles
    6026
    Engine 1 Notes
    Time Since MPI :100.4 Time to MPI: 3399.6 Time to CZI: 3380.4

    Engine 2

    Engine 2 Manufacturer
    HONEYWELL
    Engine 2 Model
    TFE731-20AR-1B
    Engine 2 Time
    9095.3
    Engine 2 Cycles
    6026
    Engine 2 Notes
    Time Since MPI :100.4 Time to MPI: 3399.6 Time to CZI: 3380.4

    Auxiliary Power Unit

    APU Notes
    Honeywell RE100 APU

    Avionics

    Avionics/Radios
    • Honeywell Primus 1000 Avionics System with EICAS • Dual Micro Data Computers • 4-tube EFIS Display Including MFD • Cockpit Voice Recorder (CVR) with RIPS Sentry 120R • Flight Data Recorder (FDR) -FA2100 • Dual Integrated VHF Comms. UHF / 3rd VHF • Dual Honeywell AHZ-800 AHRS • Dual Integrated VHF Nav’s • Single 2” Standby Altitude Indicator • Single ADF • Single 2” Standby Airspeed Indicator • Aircell • Dual DMEs • Single 2” Standby Altimeter • Dual Mode S Transponders • TCAS II w/Mode S w/Diversity Transponders • Dual Universal UNS 1EW/LPV FMS with SCN 1002.2 • Primary Bendix/King KHF-950 • ARTEX ELT 453-5060 ELT • Honeywell Signal Enhanced EGPWS w/Windshear Alert. • RVSM Certified with 8.33 Spacing and FM Immunity • CMNPS Certified • RNP 5 & 10 Certified

    Additional Equipment

    Additional Equipment
    • GROSS WEIGHT INCREASE 21,500 LBS. ZERO FULL WEIGHT INCREASE 16,500 LBS. • Allied Signal RE-100 APU, • Thrust Reversers, • Triple Rosemont Pitot Static System, • Pulsating Recognition Light System, • Inflatable Quick Donning Crew Oxygen Masks, • Dual Angle of Attack Indicators, • Ice Detection System, • Lighted Chart Holders, • Auxiliary Cockpit Foot Warmers, • Externally Serviced Electronic Flushing Toilet, • Cockpit Sunvisors, • Dual Digital Davtron Clocks, • Clearance Delivery Unit, • Belted Lavatory Seat (16G Certified) Digital Variable Position Spoilers, • Vanity Sink, 40 Amp Ni-cad Batteries, • (4)-110 Volt A/C Outlets in Cabin, Aircraft Locking Package, • Wing Ice Detection Light, Floor Tracking, • Dual 28V Flightbag Outlets • Cabin and galley AC outlets

    Exterior

    Exterior Notes
    • Painted June 2012 • Matterhorn White with red and blue striping

    Interior

    Interior Notes
    • Refurbished in 2012

    Inspection Status

    Inspection Status
    Recent SB Upgrades: • A SB45-27-53 R2 – Aileron inspection • Flight control cable replacement • SB45-27-44 – Improved flight control cable fairleads • SB34-3729 – FMS SCN upgrade to 1002.2 • Aircraft incorporated SB45-5-1 – Evolved Maintenance Program (EMP)


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