One U.S. Owner Since New and Always Hangared
Global Vision Flight Deck
Engines Enrolled on Rolls-Royce CorporateCare
APU enrolled on MSP Gold
Honeywell Jetwave Ka-Band High Satellite Data System
FANS 1/A+ CPDLC
ATN CPDLC
WAAS (SBAS) / LPV
Venue Cabin Management System (CMS)
Price $27,500,000
Global Vision Flight Deck
Rockwell Collins Pro Line Fusion Avionics Suite Version 5.5.1
Four 14” x 11” Active Matrix LCD EFIS Screens
Dual 3-Axis CAT 2 Automatic Flight Control Systems (AFCS) Includes Computations for:
Flight Guidance
Autothrottle
Autopilot
Yaw Damper
Automatic Pitch Trim
Two (2) Integrated Flight Information Systems (IFIS) w/ Dual File Server Unit
One (1) Head-Up Display (HUD) System
One (1) Enhanced Vision System (EVS)
One (1) Synthetic Vision System (SVS)
One (1) Electronic Integrated Standby Instrument (ISI)
One (1) Air Data System (ADS) Composed of Three (3) Air Data Computers (ADC)
One (1) Auto-Tilt Weather Radar
Three (3) Inertial Reference Systems (IRS)
Two (2) GPS WAAS Receivers
Two (2) VHF Navigation Receivers
Two (2) ADF Receivers
Two (2) DME Transceivers
One (1) Traffic Surveillance System & One (1) Standalone Transponder Capable of:
Dual Transponder Functionality
TCAS II Change 7.1
ADS-B Out (DO-260B Compliant)
Two (2) Radio Altimeter Systems
One (1) Terrain Awareness and Warning System (TAWS)
Three (3) Flight Management Systems (FMS)
Three (3) VHF Communication Radios
Two (2) HF Transceivers
One (1) Dual SELCAL System Capable of Monitoring Three (3) VHF & Two (2) HF Radios
One (1) Handset Using the Cabin Satellite Airborne Telephone System Voice Communication Channel Interfacing Directly w/ the Cockpit Audio Integrated System
One (1) Data Communication Channel (ACARS), which in Conjunction w/ the VHF Meets the Requirements of Future Air Navigation System (FANS 1/A+) Including Airline Operational Control (AOC), Air Traffic Services (ATS), Facilities Notifications (AFN), Automatic Dependent Surveillance – Contact (ADS-C), & Link 2000+ Controller Pilot Datalink Communication
One (1) Dual Channel Interphone System w/ Hand-Held Microphones & Individual Controls for Pilot, Co-Pilot & Flight Observer Seat
Electronic Flight Instrument System (EFIS)
Engine Indication & Crew Awareness System (EICAS)
Synchronized Digital GPS Clock
Cockpit Voice Recorder (CVR)
Flight Data Recorder (FDR)
Emergency Locator Transmitter (ELT)
Completed June 2016 @ Bombardier – Montreal, QC
Thirteen (13) Passenger Forward Galley with Forward Crew Rest Interior features a crew jump seat, forward crew vacuum lavatory, forward crew rest area, forward main galley, and aft main lavatory. The entry area includes the Right-Hand Side forward crew lavatory, Left-Hand Side forward crew rest area, and the Right-Hand Side full-service main galley. The entry area and forward cabin are separated by an electric pocket door. The interior features a 3-zone cabin with a forward cabin 4-place club with stowable executive writing and dining tables between the opposing club chairs, a mid-cabin Left-Hand Side 4-place conference group opposite a credenza, followed by an aft cabin with a Left-Hand Side 2-place club opposite a 3-place berthable divan when the removable bulkhead is removed (2-place TTOL when the removable bulkhead is installed) separated from the main-cabin by a bulkhead with an electric pocket door. The club and conference group chairs are upholstered in a Excel Cowhide dove colored leather, the di
Cabin entertainment includes a Dual Blu-ray/CD/DVD/MP3 Player which can be viewed on One (1) 24” HD LCD Monitor in the Right-Hand Fwd Cabin Bulkhead, One (1) 24” HD LCD Monitor in the Left-Hand Aft Cabin Bulkhead, and One (1) 24″ HD LCD Pop-Up Monitor with Electric Lift and Swivel Mounted in the Right-Hand Credenza. Connectivity via Honeywell Jetwave Ka-Band High Satellite Data System.
The Forward Right-Hand Side full-service main galley features a china storage drawers, crystal showcase, inserts to accommodate china, crystal and flatware sets, flight attendant HD touchscreen, 2 pull-out work surfaces, high temp oven, microwave oven, manual fill coffee capsule machine, air chiller, insulated chilled area with a drawer and perforated pull-out removable shelves, chilled drawer with 2 rows of soda cans, drawer for wine bottle and tray storage, stainless ice drawer with divider, small clean ice basket and drainage, dirty dish bin drawer, sealed waste drawer, stainless steel sink with strainer, faucet and sink cover with cutting board on reverse side, and Corian countertop.
Completed June 2016 @ Bombardier – Montreal, QC
Overall Matterhorn White with Gloss Cumulus Gray Pearl and Gloss Titanium Pearl stripes.
Engines are On Condition (Task Oriented) & Enrolled on Rolls-Royce CorporateCare
APU Enrolled on Honeywell MSP Gold
Maintenance Tracked on CAMP Computerized Maintenance Program
On MSG-3 Maintenance Program
WEIGHTS:
Max Ramp Weight: 99,750 lbs.
Max Gross Takeoff Weight: 99,500 lbs.
Max Landing Weight: 78,600 lbs.
Max Zero Fuel Weight: 58,000 lbs.
Basic Empty Weight: 51,053 lbs.
Basic Operating Weight: 52,398 lbs.
Quick Access Recorder (QAR)
Take-Off & Landing Awareness Function (TLAF) Surface Management System
XM Graphical Weather System
Datalink Graphical Weather System
Crew Force Measurement System (CFMS)
FAR Part 135 Operations – Three (3) Pilot Crew for up to 12 Hours
Flight Crew Emergency Vision Assurance System (EVAS)
Second Datalink System
Floormat Heaters (Entrance Area & Forward Cabin Zones)
Automatic Switch on Main Passenger Door
24″ Pop-Up HD Monitor (Credenza)
SATCOM Data Router
GlobalVT Software Key
Dual Channel Swift Broadband
Dual Channel Iridium Telephone System
Inmarsat SATCOM System
Cockpit Certified Printer
RVSM, MNPS, BRNAV, Basic RNP-1, RNP-4, RNP-5, RNP-10, P-RNAV, US-RNAV, RNP APCH, RF Legs, RNP AR Approach w/ RF Legs Capable
Frank Janik
