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Engines Enrolled on Rolls Royce Corporate Care, APU on MSP, 2009 Paint, HUD, EVS, High Speed Data, Office in the Sky, 10/12 Passenger Convertible executive interior, crew rest area, executive shower in aft lavatory.
Airframe total time: 4,804 hours
Engine Program: Rolls-Royce Corporate Care
Engine #1: 4,804 hours / 1,719 Cycles
Engine #2: 4,804 hours / 1,719 Cycles
APU: 2,773 Hours / 3,621 Cycles
6 Tube EFIS DU-870 / Engine Instrument and Crew Advisory System (EICAS)Dual Fail-Operational (automatic switching) Auto-PilotDual CD-820 FMS with Video Capability (optional third CD-820 FMS is installed)Triple Long-Range Nav SourceDual Full Flight Regime Auto-ThrottleTriple IAC-800 Integrated Avionics Computers (IAC)
Triple AZ840 Micro Air Data Computers (MADC) (RVSM compliant)Triple Honeywell Laseref IVQuad Ameteck DA-810 Data Acquisition Units (DAU)Primus 880 Color Weather Radar - Dual Control HeadsDual Primus II Integrated Nav/Com/Ident. Radios; Compliance with European 8.33 kHz Channel Spacing RequirementsCentralized Aircraft Information System (CAIMS) and Portable Access Maintenance Terminal (PMAT)TCAS 2000 Traffic Alert and Collision Avoidance SystemGPS (with optional second Honeywell GPS installed)
Mark-5 EGPWSCockpit Voice Recorder (CVR)Flight Data Recorder (FDR)DL-950 USB Data LoaderDual ALT-4000 Collins Radio AltimetersDual Collins HF-9000 HF Radios
Artex 406 MHz Emergency Locator Transmitter (ELT)
Magnastar C200 Airborne Telephone System "Office in the Sky"
SecuraPlane Security System
Honeywell GP550 #2 (2nd) Global Positioning System (GPS)
CAIMS In Flight Capability
Teledyne TL-608 Airborne Data-Link
3rd VHF Transceiver
Lightning Sensor System (LSS)
Thales Heads-Up Flight Display System (HUD)
Honeywell 3rd FMS
Honeywell MCS 7000 Satellite Communication System (Satcom)
Honeywell CD-810 Control Display Units Replaced with CD-820
Enhanced Vision System (EVS)
Flight Data Recording System "Quick Access Recorder"
Additional Refuel / De-fuel Panel
Logo Lighting System
Passenger Door Aesthetic Side Covers
Cabin Management System (CMS) (Dual MHT, DVD, 3 Cabin Monitors, 8 Channel XM Radio, Dual High Speed Data)
Appointed with a unique Ten(10) / Twelve (12) passenger convertible executive interior. Configuration (A) accommodates ten (10) passengers featuring a forward four (4) place club followed by a four (4) place conference group opposite a large credenza. Aft cabin features two (2) single place place seats opposite a berthable divan. Configuration (B) accommodates twelve (12) passengers by adding two additional single place executive seats opposite on another when the aft divan is removed.
The aircraft is equipped with a forward crew rest area as well as forward crew lavatory and aft passenger lavatory with executive shower. The forward galley features a high temp oven, microwave, and coffee maker.
Desothane Matterhorn White with Burgundy, Alpine Green and Gold Stripes. New Paint in October 2009.
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Year: 2003 |
S/N: 9116 |
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