Date of manufacturer: Dec-2004
Entry into service: July 2005
Airframe:
1,884 Total Hours
835 Landings
Engines: Rolls Royce BR-710A2-20
#1 & #2
1,904 Hours Since New
845 Cycles Since New
APU: Allied Signal RE-220 (GX)
1,540 Hours Since New
996 Cycles Since New
Recent 4C (60 month) Inspection at Standard Aero May-2010
Securaplane Alarm System
One Owner Since New
Impeccable Condition Inside & Out
Optional Equipment
Collins Tailwind 500 Direct TV (Configured for U.S. Coverage)
High Speed Data System: Dual HST 2100 providing 128knps data transfer for email / internet
HUD
Dual Channel Iridium Satellite Telephone
Third Honeywell Flight Management System
Additional Cabin telephone wired handsets (3)
Ten (10) 115VAC Outlets
Dual 21.3” Forward and Aft Cabin Bulkhead Mounted Monitors
Six (6) 10.4” Cabin Seat Armrest Monitors
Interior
The Entertainment center is located in the center cabin credenza and features the Tailwind 500 Direct TV System, Airshow Network, Fax/Printer/Scanner, multi-region DVD players and a multi-disc CD Player. Passengers enjoy cabin entertainment on six (6) 10.4” individual armrest monitors and dual 21.3” bulkhead monitors. The forward galley includes an espresso machine, oven, a microwave, chiller and a coffee maker. The aircraft is equipped with expanded forward crew lavatory and cabin attendant jump seat.
Exterior Matterhorn White with Two Blue & One Red Accent Stripe(s).
Avionics
Honeywell Integrated Avionics System
Six (6) Tube 8"x 7" DU-870 Color Electronic Flight Instrument System (EFIS) Displays/2 PFD / 2
EICAS / 2 MFD
Triple NZ-2000 Integrated Flight Management System w/ Dual 12 Channel GPS
Dual Full Regime Auto Throttle System
Triple IC-800 Integrated Avionics Computers (IAC) with Batch-2 upgrade
Triple AZ-840 Micro Air Data Computers (MADC)
Triple LASEREF IV Inertial Reference Systems
Three Ameteck DA-810 Data Acquisition Units (DAU)
Primus WC-880 Color Weather Radar w/ Dual Controls
Dual Primus II RM-855B Integrated NAV/COM/Ident Radios w/ VOR/ILS/MKR/ADF/DME/VHF Comm/Mode
“S” Diversity
Central Aircraft Information Maintenance System (CAIMS)
TCAS II Traffic Alert and Collision Avoidance System (Change 7 Incorporated)
Dual ALT-4000 Radio Altimeters
Coltech CSD-714 SELCAL
Allied Signal SSCVR Cockpit Voice Recorder
Allied Signal SSFDR Flight Data Recorder
Artex 406 MHz Emergency Location Transmitter (ELT) with NAV interface
MCS-6100 6 – Channel SATCOM
Dual Collins HF-9031A HF Communication System
Enhanced Ground Proximity Warning System (GPWS) w/ Windshear Detection System
8.33 kHz Channel Spacing/FM Immunity Compliant
Full Authority Digital Engine Control System (FADEC)
Engine Indication/Crew Alerting System (EICAS)
Teledyne ACARS Datalink
Triple FMS 810 CDU's
Weights
Gross Weight (Ramp) 88,000 lbs
Max Take off Weight 87,700 lbs
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