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2013 Global 5000 Vision

General

Year:
2013
Manufacturer:
Bombardier
Model:
Global 5000 Vision
Size:
Long range
Serial Number:
2013-tba-Aug Off Market
Asking Price:
$43,995,000
Date Of Spec:
November 2011

Specification

Click here to download the specification for this aircraft (PDF).

Airframe / Engines / APU

Airframe Warranty:
Full Manufacturer Warranty
Registration:
EASA Reg
Aircraft Location:
Montreal, Canada
Total Time:
under 30 hrs
Cycles:
under 20 cycles
Green C Of A Date:
November 2011
Entry Into Service Date:
Est July 2012
Airframe Warranty Expires:
Full Manufacturer
Certified Status:
EASA JAR OPS 1 Certified
Engine Type:
Rolls Royce BR710
Left Engine SN:
TBA
Left Engine Hours:
Under 30 Hrs
Left Engine Cycles:
Under 20
Right Engine SN:
TBA
Right Engine Hours:
Under 30 Hrs
Right Engine Cycles:
Under 20
APU Type:
Allied Signal RE-220
APU SN:
TBA
APU Hours:
Under 30 Hrs

Avionics Options

OVERVIEW

  • Rockwell Collins Pro Line Fusion avionics suite, complete with four 14”x11” landscape active matrix liquid crystal displays (AMLCD) allowing 50/50 split window configuration offering multifunction windows with automatic reversion.
  • Control Tuning Panel (CTP) supported by an Integrated Processing System (IPS) with three single channel Integrated Processing Cabinets (IPC) hosting AFCS
  • Engine Indication and Crew Alerting System (EICAS)
  • Auto Flight via three-axis, active-standby Category II Automatic Flight Control Systems (AFCS)
  • COMM/NAV system uses dual Radio Interface Units (RIU) and operates as the Aircraft Communications Addressing and Reporting System (ACARS) compatible router.

 

COMMUNICATIONS

  • Three Rockwell Collins VHF-4000 COMM radios with 8.33 KHz spacing. One radio with data capability
  • Dual HF
  • Dual SELCAL
  • Datalink with Future Air Navigation System (FANS)
  • Audio System providing individual audio control for COMM/NAV radios, interphone, pilot-to-pilot communications and providing inputs for the aural warnings from TCAS, TAWS, and EICAS.

 

INDICATING & RECORDING

  • Electronic Flight Instrument System (EFIS)
  • Clocks (pilot and co-pilot)
  • Cockpit Voice Recorder (CVR) 120 minutes
  • Flight Data Recorder (FDR) 25 hours
  • Emergency Locator Transmitter (ELT) 121.5 MHz, 243 MHz and 406 MHz frequencies

 

NAVIGATION & SURVEILLANCE

  • Integrated Flight Information System (IFIS) inc. ChartLink™) and Graphical Weather
  • Paperless operation
  • Class II Electronic Flight Bag (EFB) (detachable)
  • Integrated Electronic Standby Instrument for attitude, airspeed and altimeter indication
  • Enhanced Vision System (EVS)
  • Synthetic Vision System (SVS)
  • Head Up Flight Display System (HUD) CAT II
  • Air Data System (ADS) system with three ADC’s
  • Inertial Reference System (IRS)
  • TCAS compliant with Change 7
  • Terrain Awareness and Warning System (TAWS) with windshear detection/alerting.
  • Flight Management System (FMS)
  • Weather Radar with MultiScanTM and OverFlightTM
  • Two VHF navigation receivers / two DME transceivers
  • Two 24 channel GPS WASS receivers

 

SERVICE BULLETINS

  • 700-1A11-11-005 Increased MTOW to 88,700 Lbs
  • 700-1A11-21-005 Addition of Ice Filter Assemblies
  • 700-1A11-23-002 Cabin Communications System (CCS) Aerocom A3000B & ICS 100 Telephone System
  • 700-1A11-27-004 Stick Pusher
  • Rockwell Collins Lightning Sensor System (LSS)
  • Cockpit printer
  • Cabin power bus disconnect
  • Flight observer’s seat audio panel located on cockpit pedestal
  • One power converter (3500 VA/115V/60Hz
  • AC/DC Power distribution
  • 115 VAC GFI electrical outlets: dual outlets in each lavatory and at the galley and LH entrance enclosure
  • single outlet at each single seat grouping and outboard double seats and a single outlet located adjacent to each cockpit seat

 

GLOBAL OFFICE

  • 10/100 Base T Ethernet LAN with connections for laptops and other portable devices
  • Plain paper , fax/printer/scanner
  • RJ-45 LAN interface located at the following locations: cockpit, one (i) in each single seat grouping, one (1) at the double seats
  • Four (4) passenger cabin handsets (cockpit, crew area, RHS #2, and RHS forward divan end cabinet)
  • Wireless Local Area Network (LAN)
  • Dual channel high speed data system. Two (2) HST-2100 provides data transfer up to 128 kbps total (64 Kbps of data transfer rate per channel)

 

LIGHTING

  • Light Emitting Diode (LED) interior lighting
  • Wing tip taxi lights
  • Wheel well maintenance lights
  • Pulse landing light system
  • Illuminated ordinance signs
  • Exterior ground service panel lights (pylon lights)
  • External service panel lighting

 

Additional Options

LOOSE EQUPMENT/SPARES (ADDITIONAL)

  • Two plug-in 10.4in touch screen LCD monitors in leather pouches
  • Single and double seats armrest covers
  • Eight throw pillows
  • One spare carpet (FS250 to FS799)

 

AIRCRAFT MISCELLANEOUS INSTALLATIONS

  • Addition of refuel/de-fuel control panel in the entrance enclosure
  • Common keyed locks (external door panels)
  • Airstair forward handrail extension
  • External baggage door lock override
  • Catwalk battery access
  • Aft equipment bay storage box with max weight capacity 60 lbs
  • Tow bar assembly and tow bar storage provisions (tow bar is loose equipment)
  • Multi-purpose aft equipment bay access ladder
  • Two seven-inch gear pin storage boxes in Airstair
  • Semi-recessed Jeppesen manual storage box at cockpit entrance

Floorplan

Interior

INTERIOR 2012

PASSENGERS 13 passenger executive fire blocked interior

 

ENTRY AREA

  • RH forward lavatory with vacuum sanitation system, vanity and storage cabinets
  • LHS entrance enclosure with coat rod and flight observer seat
  • RHS forward
  • LHS galley annex with 10.4 touch screen
  • Forward cabin bulkheads with LH sliding pocket door

FORWARD CABIN

  • Four berthable single wide seats with footrests, berthing/recline, track and swivel and electric inflatable lumbar support
  • Two bi-fold pull-out side ledge tables
  • 2 magazine racks

MID CABIN

  • RHS credenza with fax, printer and storage
  • LHS hi-low manual conference table
  • LHS two sets of double seats feature recline (swivel on inboard chairs only) and electric lumbar support
  • Low cabinet under emergency exit
  • Mid-cabin bulkhead with LHS sliding pocket door and removable RH upper bulkhead for FAR Part 135 & JAR Ops 1

AFT CABIN

  • RHS three-place berthable divans with two end cabinets inc. drinks holder and storage.
  • LHS two seats in club arrangment
  • Bulkheads and hinged door separating cabin from aft lavatory

AFT LAVATORY ZONE AND BAGGAGE COMPARTMENT

  • Aft vacuum lavatory, wardrobe, vanity and storage cabinets
  • 158 cu ft with adjustable and 2 fold-down shelving, coat rods, 2 hang-up bars and restraint net

CABIN SUPPORT SYSTEMS

  • Two therapeutic oxygen outlets in passenger cabin and oxygen drop boxes as required in main cabin, galley, lavatories and at flight observer seat
  • Master passenger control of two cabin temperature zones
  • Entry area heater
  • Re-circulating water system with dual pumps and UV filtration
  • Heated hose assemblies for freeze protection
  • 24.7 US gallon water tank
  • 16 gallon waste tank servicing forward and aft lavatories

Interior Options

EMERGENCY EQPT FOR JAR-OPS 1

  • Bilingual exit sign
  • Smoke detector in each lavatory, in aft wardrobe and in baggage (factory installed)
  • Life rafts (inc. 406MHz ELT) life vests, PBEs, fire extinguishers and first aid kit as required
  • Engraved Maglite flash light (in addition to two (2) cockpit flash lights)

 

GALLEY EQUIPMENT

  • One AEROLUX ESPRESSO Manual fill coffee maker
  • One 0.7 cu ft microwave oven (TIA)
  • One air chiller unit to cool selected galley areas
  • One (1) divided ice drawer with overboard drain
  • One TIA (1543-3) high temperature oven
  • Note: The china, crystal and flatware will be customer supplied

 

MAINTENANCE & DIAGNOSTICS

  • Central maintenance function for applicable integrated cabin systems
  • Diagnostic reports viewable on the galley touch screen monitor or other connected devices.

Entertainment System

ENTERTAINMENT SYSTEM

  • Two multi-region CD/DVD players
  • Two bulkhead-mounted LCD video monitors in passenger cabin
  • High quality cabin speaker/sub-woofer arrangement
  • Airshow ASXi
  • Air Data System (ADS) system with three ADC’s
  • Passenger headphone distribution system
  • Six receptacles for plug-in monitors installed in the passenger area
  • Power Distribution of aircraft AC and DC power

 

CABIN UTILITIES / CONTROL & DISPLAY

  • One 10.4 inch galley touch screen control monitor
  • Two 8.4 inch cockpit touch screen equipment (pilot & co-pilot side)
  • Wireless passenger control units (PCU), entertainment switch panel and local switch panels

 

CABIN SERVICES

  • Cabin/lavatory call system
  • Passenger address system
  • ICG ICS-100 Iridium telephone system
  • Passenger briefing system

Downloads