Airframe: 
9464 Hours, 5983 Cycles

Engine Specs:
Rolls Royce CAE 300 7C ON ROLLS ROYCE CORPORATE CARE
Left:    S/N:  CAE-330139  9673.8 hrs, 5964 cycles
Righ:  S/N:  CAE-330168  8002.5 hrs, 5096 cycles

Avionics/Radios:
Honeywell Primus 2000 Dual Flt Dir/Dual A/P System,
Honeywell Primus 2000 5 tube EFIS System,
Dual Integrated Honeywell NZ2000 Flight Management System with Dual GPS,
Dual Honeywell Air Data Computer,
Dual Primus II Radio System,
Dual RCZ 851E Integrated Comm Transceiver (non 8.33 kHz)
VHF Comm/Mode A, C, S Transponder,
Dual RCZ 850 Integrated Nav Receiver
ADF/VOR/MKR BCN/ILS Dual DME Indicator,
Dual RM-855 Radio Management Units,
Dual Honeywell AV850A Audio Panel,
Dual Honeywell KHF-950 High Frequency Radio System with SELCAL,
Honeywell VHF AFIS,
Honeywell Primus 880 Weather Radar,
Honeywell MKV Enhanced Ground Proximity Warning System with Windshear,
Dual Honeywell Attitude and Heading Reference Unit,
L-3 (Goodrich) Standby Attitude Indicator,
Standby Airspeed and Altimeter Indicator,
Standby HSI (Aeronetics),
L-3 Standby PS835C Battery pack,
Cockpit Voice Recorder – A200S 120 minute Solid State unit from L-3,
Honeywell A-300 Radio Altimeter System,
Litton ELT, triple frequency,
MagnaStar C2000 Telephone System, 1 Cockpit Handset, 2 Cabin Handsets,
Honeywell CAS67A TCAS II with Change 7.0 software

Additional Equipment:
Airframe is RVSM approved
Dual VisionSafe EVAS installation
CD Player
VHS Video Cassette Player
Collins Airshow Genesis system
Six (6) Side Ledge Monitor Receptacles
Cabin 110VAC outlets

Exterior:
Painted February, 2006 by Duncan, Lincoln, NE. Overall Matterhorn White with Slate Gray, Charcoal and Raspberry striping.

Interior:
Cabin seats refurbished February, 2006 by Duncan Aviation, Lincoln, NE. Interior layout is a double club configuration with a forward right hand galley.

Inspection Status:
On Cescom