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    2000 DASSAULT FALCON 900EX N-NUMBER N66FJ2000 DASSAULT FALCON 900EX N-NUMBER N66FJ
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    N66FJ - 2000 DASSAULT FALCON 900EX

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    Aircraft Summary

    General
    Year
    2000
    Manufacturer
    DASSAULT
    Model
    FALCON 900EX
    Serial Number
    66
    Registration #
    N66FJ
    Condition
    Used
    Description
     5213 Landings. on JSSI – 100% coverage, dual Honeywell Primus 2000
    Airframe
    Total Time
    8244.0
    Engine Program
    Engine Program Notes
    Engines: Honeywell TFE731-60 (on JSSI – 100% coverage). 

#1 Engine s/n P112313: 7438 TT, Cycles: 4745, TSMPI: 743, TSCZI: 3243. 

#2 Engine s/n P112312: 7847 TT, Cycles: 4994, TSMPI: 743, TSCZI: 3243. 

#3 Engine s/n P112311: 7847 TT, Cycles: 4994, TSMPI: 743, TSCZI: 3243. 

APU s/n P370:
Garrett GTCP-150F (on JSSI), 2105 hours.

    Engine 1
    Engine 1 Time
    7438
    Engine 1 Time Since
    SNEW
    Engine 2
    Engine 2 Time
    7847
    Engine 2 Time Since
    SNEW
    Engine 3
    Engine 3 Time
    7847
    Engine 3 Time Since
    SNEW
    Avionics
    Avionics/Radios
    Flight Director: dual Honeywell Primus 2000, Autopilot/Auto Throttle: Honeywell Primus 2000, Flight Management System: triple Honeywell FMZ-2000 (software 6.0 with TOLD), Global Positioning System (GPS): dual Honeywell GNSSU (12 channel), Communication (VHF) Transceivers: dual Collins VHF-422C (8.33 spacing), Navigation (VHF) Receivers: dual Collins VIR-432 (FM Immunity),      Automatic Direction Finders: dual Collins ADF-462, Distance Measuring Equipment: dual Collins DME-442, ATC, Transponder: dual Collins TDR-94D, Color Weather Radar: Honeywell Primus 880 w/dual Controllers, TCAS II: Collins TCAS-94 (Change 7), Radar Altimeter: dual Honeywell AA-300, Inflight Telephone: Teledyne Controls Magnastar C-2000, SATCOM (Aero-I): Sextant JetSat (5 channel), High Frequency Communication: dual Collins HF-9000 w/ Coltech SELCAL (2 Channel), AFIS:  Honeywell (VHF & SATAFIS) with Sky printer, Heads-Up Guidance System (HGS): Flight Dynamics HGS-2850 (Full Provisions only), Inertial Reference System: triple Honeywell Laseref IV, Enhanced GPWS: AlliedSignal Mk-V (Enhanced Flight ID), Cockpit Voice Recorder: AlliedSignal SSCVR, Flight Data Recorder: AlliedSignal SSFDR.
    Additional Equipment
    Additional Equipment
    Triple Baker B1045 Flightdeck Audio, Socata ELT 97-406 MHz, 115 cu. ft. oxygen bottle, Devore “Tel-Tail” two light recognition system, Toshiba TF-471Fax/CopierPrinter, Airshow 400, two Baker DVD/CD players, 18 inch LCD monitor, 8.4 inch Rosen LCD side-ledge monitors and receptacles, TIA: Wave Jet Microwave oven, Hi-Temp. oven, Coffee Maker.
    Exterior
    Exterior Notes
    Overall Off White fuselage with Blue tail protruding through underbelly accented with Red stripe (Repainted 2005).
    Interior
    Interior Notes
    Taupe leather seats & divan, Taupe and Black fleck carpet, Pommele Sapele veneer with high gloss, Papyrus Ultra-leather lower sidewall, Bone Ultra-suede headliner, Antique Brass plating (Partial Refurb 2006). 

Seating: 12 passenger; 4 forward club seats, 4-place mid-cabin dining group with opposing credenza, removable cabin divider, 3-place aft divan, aft executive work station, aft lavatory, Erda third crewmember seat.
    Inspection Status
    Inspection Status
    CAMP. Inspections Due: A & A+ August 12, 2009. B, 2B, & 3B at 9600 hours. C April 19, 2012. IT at 8393 hours or July 16, 2009 (Code 275021). RVSM, MNPS, BRNAV (RNP-5).


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