AIRFRAME:
6691 Hours Since New (As Of March 2010)
4807 Landings Since New
72-Month Inspection December 2009

GCMP Gulfstream Computerized Maintenance Records Program
No Known Damage History


CERTIFICATIONS:
RVSM (Reduced Vertical Separation Minimums)
RNP-4 & RNP-10 (Required Navigation Performance)
MNPS (Minimum Navigational Performance Specifications)
BRNAV Qualified (Basic Area Navigation)


ENGINES:
Rolls-Royce Spey MK511-8
8000-Hour / 20-Year Overhaul Interval
4000-Hour / 10-Year Mid-Life Inspection Interval

Left:
709 Hours Since Major Overhaul Inspection (September 2006 @ 5898 ETT By Rolls-Royce)
6607 Hours Since New
4724 Cycles Since New
Serial Number 11398

Right:
709 Hours Since Major Overhaul Inspection (September 2006 @ 5866 ETT By Rolls-Royce)
6575 Hours Since New
4713 Cycles Since New
Serial Number 11401


AUXILIARY POWER UNIT:
Honeywell GTCP-36-100
In-Flight Capable
3592 Hours Since New
Serial Number P-361


AVIONICS:
Honeywell EDZ-803 Five-Tube EFIS Electronic Flight Information System
Honeywell SPZ-800 Dual Channel Autopilot
Honeywell Primus 800/MDZ-800 Color Radar With MFD Multi-Function Display
Ryan/3M WX-11J Weather Stormscope
Dual Honeywell ADZ-800 Air Data Computers
Triple Collins VHF-21B Communication Transceivers With 8.33 Spacing
Dual Collins VIR-32 Navigation Receivers With FM Immunity
Dual Collins DME-42 Distance Measuring Equipment
Dual Collins ADF-60 Automatic Direction Finders
Dual Collins TDR-90 Mode S Transponders With Enhanced Surveillance
     (Flight ID)
Dual Collins 628T-2A High Frequency Radios With Motorola
     NA-137 SELCAL
Dual Collins ALT-55B Radio Altimeters
Collins VHF-21B Emergency Transceiver
Dual Honeywell KT-76A Transponders With Mode S / Enhanced Surveillance
Honeywell VA-100 Voice Advisory System
SAT/AFIS Satellite Airborne Flight Information System
Universal TAWS (Class A) Terrain Awareness Warning System
Honeywell CAS-67A TCAS II Traffic Collision Avoidance System
     With Change 7
Dual Universal UNS-1C+ FMS Flight Management System
     With Video Capability And GPS Global Positioning System
Triple Honeywell Laseref II IRS Inertial Reference Systems


ADDITIONAL FEATURES AND MODIFICATIONS:
Artex ELT-406-2 Triple Frequency Emergency Locator Transmitter
Fairchild A-100 CVR Cockpit Voice Recorder
Wiring Provisions For Fairchild FDR Flight Data Recorder
Baker M-1045 Cockpit Audio System
Aero Systems Fuel Management Computer
Dual Honeywell Mach/Airspeed Indicators
Aeromech Standby Airspeed Indicator
Dual Honeywell Vertical Speed Indicators
Dual Honeywell Altimeters
Aeromech Standby Altimeter
IDC Metric Altimeter
Dual Aeronetics RMI Indicators
J.E.T. 2-Inch Emergency Horizon
Dual Davtron Clocks
Portable Emergency Oxygen Bottle
Halon Fire Extinguisher
Electronic Smoke Detector
Pressurized Water Tanks
Crewmember Jumpseat
Airshow 200 Passenger In-Flight Information System
Magnastar C-2000 Direct-Dial Air-To-Ground / Ground-To-Air Digital In-Flight
     Telephone And Communications System, With Three Handsets (1 Cockpit
     And 2 Cabin) And Capability For Voice, Fax And Data Transmissions


INTERIOR:
Seating For Up To Three Crewmembers And 13 Passengers. The Interior Is Completed With A Light Stone Headliner With Camel Beige Leather And Fabric Upholstery, Completed In Tones Of Royal Blue And Gold. All Woodwork Is A Light Oak Finish, Complemented By Stainless Steel Countertops, Custom Made Carpet, And Gold-Plated Hardware.

Large Passenger Coat And Crew Closets Are Conveniently Located In The Entry Vestibule, Along With The Main Cabin Entertainment Systems, Which Consists Of A 10-Disc Compact Disc Stereo, And A Forward 19" Flat Screen Video Monitor Featuring Airshow 200. The Forward Passenger Group Contains Of A Four-Place Divan Opposite A Two Place Seating Group. A Pull-Out Table Is Provided Between The Two Club Chairs.

The Mid-Cabin Area Is Configured As A Work Station With One Large Cabin Chair And Work Desk Opposite A Two-Place Divan.

The Aft Seating Group Consists Of A Four-Place Club With Pull-Out Tables Between The Club Chairs.

Passengers Can Be In Constant Communication With Home And Office Via The Magnastar C-2000 Telephone, Featuring Direct Dial (Voice And Data), Air-To-Ground, Ground-To-Air, Cabin-To-Cockpit, Multiple Call, And Conference Call Features.

The Galley Is Located To The Rear Of The Passenger Cabin And Provides Everything Needed For Preparation Of Meals, Snacks, And Beverages, Including A Microwave Oven, Coffee Pot, Mapco Unit, And Liquor Bottle Storage.

The Private Main Lavatory Is Located To The Rear Of The Galley And Provides Ample Room To Refresh Or Change Clothes. The Main Closet For Passenger Carry-On Items Is Located In This Area, Opposite The Lavatory, And Is Equipped For Hanging Bags And Heavy Luggage.

The Rear Baggage Compartment Can Accommodate Up To 2000 Pounds Of Passenger Luggage Or Other Items. Baggage Is Loaded Through An External Door In The Rear Of The Aircraft But Passengers Can Gain Access To The Baggage Compartment At Any Time During Flight. This Compartment Also Houses Custom Shelving, Hanging Rods, And Storage.


EXTERIOR:
New November 2003 By Gulfstream Aerospace, Savannah, Georgia. Overall Matterhorn White With Gloss Black, Medium Gray, And Chrome Yellow Accent Stripes.