2004 Gulfstream G-450 s/n 4005

Serial Number:4005TTAF:1350 Hrs.Number of landings:610Engine(s) Manufacturer:Rolls-Royce Tay 611-8CEngine 1: Time since new:S/N: 85013 - 1350 Hrs.Engine 2: Time since new:S/N: 85010 - 1350 Hrs.Engine 1 Cycles:610Engine 2 Cycles:610Auxiliary Power Unit:Honeywell GTCP 36-150GIV (S/N: P-105) 1010 hours, 1080 cyclesMaintenance Information: Aircraft: • Entry into service: June 2005 • Completion Center : Savannah • Last inspections: 1A, 1C, 5C in March 2010 • Next inspections: 1A, 1C, 2C, 3C, 6C, 72/72 Month • No damage history Engines: • Not affected by Stage 7 Stator Vane issue • Fan Cases replaced for Ice Impact Tray Service Bulletin • Inspection program: Hard Time • Rolls-Royce warranty until June 2012 Engine Maintenance Plan:Hard Time:: Avionics ::  Honeywell Primus Epic / Gulfstream PlaneView Four 14 inch LCD Display Units Three Modular Avionics Units One Honeywell GP-500 Guidance Panel Two Honeywell DC-884 Display Controllers Three Honeywell MC-850 Multifunction Control Display Units Two side - mounted Cursor Control Devices Three Honeywell Laseref V Inertial Reference Units Three Honeywell A]-200 Air Data Modules Three Honeywell AV-900 Audio Control Panels Two Honeywell MRC-855 Modular Radio Cabinets_ each with DF-855 ADF, DM-855 DME, NV-875A Nav, TR-866B Comm, XS-857A Transponder One Honeywell NC-860A Nav / Comm Unit Two Honeywell RT-300 Radio Altimeters Two Rockwell Collins HF-9034A High Frequency Radios ACSS RT-951 TCAS 2000 Honeywell Primus 880 Weather Radar Visual Guidance System with Kollsman EVS Camera and Honeywell Overhead Unit Goodrich EBDI-4000 Standby Bearing and Distance Indicator Goodrich GH-3100 Standby Attitude Indicator Miltope Cockpit Printer Honeywell MCS-7000 Satcom Magnastar C-2000 Radio Telephone Honeywell LS]-860 Lightning Sensor Artex 406 ELT Honeywell FDR, CVR Securaplane 500 Security System Rockwell Collins Airshow 4000 :: Special Features ::  Modifications and upgrades: Brother MFC 440CN Fax / Printer installation Airshow 4000 processor Mods P, T ATG window shade improvements and are functional on Ground Service Bus Water tank shutoff valve access door ECS pack heat exchanger gaskets replaced per Honeywell Service Bulletin Trim air valves modified to -3 standard Nose taxi lights, nose tie down rings and stair light bezels chromed TCAS processor modification B ACMS ADB upgrade to dual power supply unit All flight control actuators replaced in August 2009 Tail navigation and logo light socket improvement Fuel quantity connector improvement Forward bulkhead monitor upgraded to 20 inch, individual seat monitors upgraded to 7 inch Wiring provisions for satellite TV Glass cockpit side windows Cockpit 60 Hz outlet installed Cockpit book holder installed Wire protective tubing installation for Canadian certification Spare Parts: Two main wheels with tires APU ignitor and ignition box Main gear axle Iack adapter Baggage door seal Fax / printer Full spare carpet including cockpit and baggage areas Spare material and leather for seats, sidewalls, headliner and decorative panels AD Compliance: All applicable, including AD 2007-26-19 for engine ice impact panels CB Compliance: All applicable, including: CB 59B Part II Horizontal Stabilizer replacement CB 91 Flight Spoiler Pushrod End Replacement
::interior::Aft galley Forward and aft lavatories with vacuum waste system Vestibule crew refreshment center Galley features expanded gasper cooled compartment plus modifications to improve storage Additional mirror in aft lavatory Cabin reading and table lights changed to ewarmf white Two coat hooks each in vestibule and aft lavatory Aft lavatory door Iamb incorporates breakaway modification One double size and three individual size Jet Rest self-inflating mattresses included Thirty gallon water system with ultraviolet sterilizer