2016 Bombardier Global 6000
Price: $27,500,000
- Serial Number: 9751
- Tail Number: N18CZ
- Hours: 3,425
- Cycles: 1,287
• 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)
• 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)
Airframe
Total Hours:
3,425
Total Cycles:
1,287
Home Base:
TEB
Airframe:
3,425 Hours 1,288 Landings
Date of Manufacture (CofA):
December 21, 2015
Entry into Service: June 29, 2016
3,425 Hours 1,288 Landings
Date of Manufacture (CofA):
December 21, 2015
Entry into Service: June 29, 2016
Engines
Rolls-Royce BR700-710A2-20
Engine Program Coverage:
Rolls Royce Corporate Care (RRCC)
Engine 1
Serial Number:
22631
Hours Since New:
3,425
Cycles Since New:
1,294
Engine 2
Serial Number:
22630
Hours Since New:
3,425
Cycles Since New:
1,294
APU
Description:
Honeywell RE220-GX
APU Program Coverage:
MSP Gold
Serial Number:
P-878
Total Time Since New:
1,773
Total Cycles Since New:
2,430
Avionics
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:
o Flight Guidance
o Autothrottle
o Autopilot
o Yaw Damper
o 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:
o Dual Transponder Functionality
o TCAS II Change 7.1
o 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)
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:
o Flight Guidance
o Autothrottle
o Autopilot
o Yaw Damper
o 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:
o Dual Transponder Functionality
o TCAS II Change 7.1
o 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)
Inspections
Inspection Type
Performed
Next Due
15 Mo
Performed:
August 2024
@
3,008 Hours
Next Due:
February 2026
30 Mo
Performed:
August 2024
@
3,008 Hours
Next Due:
May 2027
60 Mo
Performed:
August 2021
@
1,641 Hours
Next Due:
June 2026
120 Mo
Next Due:
June 2026
500 Hr
Performed:
August 2024
@
3,008 Hours
Next Due:
3,558 Hours
750 Hr
Performed:
August 2024
@
3,008 Hours
Next Due:
3,808 Hours
1000 Hr
Performed:
June 2023
@
2,435 Hours
Next Due:
3,485 Hours
1500 Hr
Performed:
August 2023
@
2,532 Hours
Next Due:
4,082 Hours
2250 Hr
Performed:
August 2022
@
2,081 Hours
Next Due:
4,381 Hours
3000 Hr
Performed:
August 2024
@
3,008 Hours
Next Due:
6,000 Hours
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
Additional Equipment/Features
• 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
• 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
Interior
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 divan in coordinating charcoal fabric, complemented by a custom Tai Ping 100% wool light and dark gray patterned carpet (plus cut never used spare carpet ready for installation). The interior woodwork and cabinetry is finished in a Dark Recon Wenge gloss veneer. All exposed cabin functional and decorative metal surfaces are plated in a satin nickel finish. The private aft lavatory and dressing area features a mirrored, lighted vanity, sink, central vacuum style flushing toilet, ample closet and storage areas, and in-flight accessibility to the spacious walk-in aft baggage compartment. Multiple universal GFCI 115VAC electrical outlets are located throughout the cockpit, vestibule, lavatories, and cabin, for crew and passenger use.
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.
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 divan in coordinating charcoal fabric, complemented by a custom Tai Ping 100% wool light and dark gray patterned carpet (plus cut never used spare carpet ready for installation). The interior woodwork and cabinetry is finished in a Dark Recon Wenge gloss veneer. All exposed cabin functional and decorative metal surfaces are plated in a satin nickel finish. The private aft lavatory and dressing area features a mirrored, lighted vanity, sink, central vacuum style flushing toilet, ample closet and storage areas, and in-flight accessibility to the spacious walk-in aft baggage compartment. Multiple universal GFCI 115VAC electrical outlets are located throughout the cockpit, vestibule, lavatories, and cabin, for crew and passenger use.
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.
Exterior
Completed June 2016 @ Bombardier – Montreal, QC
Overall Matterhorn White with Gloss Cumulus Gray Pearl and Gloss Titanium Pearl stripes.
Overall Matterhorn White with Gloss Cumulus Gray Pearl and Gloss Titanium Pearl stripes.
Weights
Max Takeoff Weight:
99,500.00
Max Landing Weight:
78,600.00
Max Zero Fuel Weight:
58,000.00
Empty Weight:
51,053.00
Basic Operating Weight:
52,398.00
Ramp Weight:
99,750.00