Global 5000

1100 hours, manufactured in 2006

ASA Consulting

São Paulo - New York in less than 9 hours in a very comfortable cabin.

Range: 5,200 NM

Maximum speed: 520 Knots

Maximum certified altitude: 51.000 feet

Characteristics

Highlights
  • Total Time Airframe 1000 Hours (425 Landings)
  • Left Engine 1000 Hours (BR710A2-20) – Cycles:418
  • Right Engine 1000 Hours (BR710A2-20) – Cycles: 418
  • APU 663 Hours (RE 220GX) – Cycles: 892
  • Rolls Royce Corporate Care
  • Smart Plus
  • Manufacturer`s Warranties (started on December 1st. 2006)
  • 20 years or 20,000 hours aircraft Primary Metal Structured
  • 5 years or 5,000 hours airframe and systems (excluding completion work)
  • 5 years or 5,000 hours green avionics
  • 6 years or 3,000 hours APU Parts
  • 5 Yeas or 5,000 Hours APU Labor
  • 2 Years or 2,000 hours Paint and Completion work
Entrance Area
  • RH forward lavatory: vacuum toilet, vanity and sink
  • LH entrance enclosure: cockpit flight observer seat (jumpseat), coat rod, storage areas and crew oxygen mask.
  • RH galley: refer to list below for specifics of equipment
  • LH galley annex with:10.4” Touch screen control panel, refer to list below for specifics of equipment
  • Forward cabin bulkheads with LH sliding pocket door (separates entrance area from cabin)
Forward Cabin
  • RH side (zone 1A): One (1) pull – out table and two (2) wide, low back, single executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar
  • LH side (zone 1B): One (1) pull-out table and two (2) wide, low back, single executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar
  • Two (2) magazine racks-one (1) on each RHS & LHS fwd bulkheads
Mid Cabin
  • RH Side (zone 2A): Credenza cabinet including entertainment and FAX/printer. Low cabinet under emergency exit including miscellaneous storage
  • LH side (zone 2B): One (1) manually-operated hi-low conference table and two (2) sets of low back, double seats that feature: integral headrest, recline, track & swivel ( swivel on inboard chairs only), and electric inflatable lumbar
  • Mid cabin bulkhead on LHS, LHS pocket door and RHS removable bulkhead.
Aft Cabin
  • RH side (Zone 3A): 3-place 16G divan (forward seat position can be occupied when RH mid cabin bulkhead is removed) that also features: berthing and storage. Two (2) end cabinets, each features: (2) drink holders, storage, and CME interface
  • LH side (Zone 3B): One (1) pull-out table and two (2) wide, low back, single executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar
Aft Lavatory Zone
  • Aft cabin bulkheads and hinged door
  • Vacuum toilet
  • Vanity cabinet with miscellaneous storage
  • Wardrobe and storage cabinet featuring adjustable and fixed shelving
Baggage Compartment Area
  • Approximately 145 cu. Ft.
  • Two (2) fold-down shelves
  • Two (2) hang-up bars (one swings down to stow)
Soundproofing
  • Bombardier vibro-acoustic soundproofing package tailored to the layout, and finishing trims
  • Enhanced acoustic package.
Environmental Control System (ECS)
  • Passenger control of two cabin temperature zones (+/- 2 deg. C) around master control setting
  • Entry area heater
Oxygen System
  • Factory-installed EROS MF-10 full-face masks are retained for the pilot and co-pilot
  • Puritan Bennett “Sweep-On” 2000 half masks for pilot and co-pilot
  • Eros MC-20 half mask and MXG goggles at flight observer seat.
  • Oxygen drop boxes as required in main cabin as well as galley, lavatories and at jumpseat
  • Two (2) therapeutic oxygen outlets in passenger cabin.
Avionics/Electrical Systems
  • Satellite Communication System and High Speed Link (SAT-6100) IMT44304001
  • Thales/Sextant Head-up Flight Display System (HFDS) CAT II operations (Factory/Completion installed)
  • Central Aircraft – Information Maintenance System (CAIMS) – Installation of the CAIMS “ Report – to – printer “ switch
  • Teledyne Datalink System (ACARS)IMT23234001
  • Honeywell RCZ-833 Third VHF Communication System IMT23114001
  • Honeywell LSZ-860 Lightning Sensor System (LSS)IMT34474001
  • 3rd Honeywell Single Global Positioning (GPS) system
Potable Water System (PWS)
  • Re-circulating water system with dual pumps (for redundancy) and UV filter system
  • 24.7 Gallon water tank
Cabin Electronic Systems (CES)
  • Global Office:
  • 10/100 Base T Ethernet LAN with connections for lap tops and portable devices
  • Plain paper: NT compatible FAX/Printer/Scanner
  • RJ-45 LAN interface at each single, outboard double seat and in the cockpit
  • Wireless LAN
  • Cabin Utilities/Control and Display:
  • One (1) 10.4 inch galley touch screen control monitor
  • One (1) Cockpit Touch Screen Equipment (co-pilot side).
  • Passenger control switch panels, entertainment switch panel and local switch panels
  • Two (2) IR remote controls
  • Power Distribution of aircraft AC and DC power
  • Entertainment:
  • Two (2) multi-region DVD players
  • One (1) multi-disk CD player
  • Two (2) bulkhead-mounted 21.3-inch LCD video monitors
  • High Quality Cabin Speaker/Subwoofer Arragement (10 speakers & 4 suwoofers)
  • Eight (8) receptacles for plug in monitors (4 plug in monitors are included)
  • Passenger headphone distribution
  • Airshow moving map
  • Cabin Services
  • Cabin/Lavatory Call System
  • Passenger Address System
  • Telephone system (PBX)
  • Passenger briefing system
  • ICG ICS-200 Iridium Telephone system
  • Maintenance and Diagnostics:
  • Central maintenance function for applicable integrated cabin systems
  • Diagnostic report viewing on the galley touch screen monitor
Other Avionics/Electrical System
  • Satellite Communication System (SATCOM):
  • Three (3) channel Aero H+ (INMARSAT) System (2 voice channels and I data channel). Data channel supports ACARS/ maintenance functions.
  • One (1) single-channel Iridium based airborne telephone system
  • PBX (Aerocom 3000B) integrates two systems allowing common access from handset
  • Four (4) passenger cabin hansets (one is cordless). One handset in cockpit
  • Single channel high speed data system (HST- 2100) offers data transfer of up to 64 KBPS
  • Cabin power bus disconnect
  • Ground service cabin power
  • One (1) power converter (3500VA/115V/60Hz) IMT24264001
  • Additional TRU
  • EICAS: “Door open” annunciation
  • 115VAC GFI electrical outlets located as follows:
  • A dual outlet in each lavatory and at RH galley, LH galley annex, credenza, and LH entrance enclosure
  • A single outlet at each single chair and each outboard double chair
Lighting
  • LED interior lighting
  • Exterior ground service lights (pylon lights)
  • Wing tip taxi lights IMT33424001
  • Pulse landing light system
  • Wheel-well maintenance lights(factory installed)
  • Logo lights
  • Services lights timer override
  • Exterior service panel lighting
Miscellaneous Installations And Equipment
  • Aircraft miscellaneous installations:
  • Additional refuel-defuel panel IMT28234001
  • Forward handrail extension
  • Common keyed panel locks
  • Aft equipment bay storage box (30lb. maximum)
  • Crew plaque
  • Semi recessed Jeppesen manual storage box at cockpit entrance
  • Towbar and assembly storage (towbar is loose equipment)
  • Cockpit miscellaneous equipment
  • Two (2) engraved Maglite rechargeable flaslights
  • Two (2) roller screens
  • Two (2) writing pad holders
  • Thale Integrated Standby Instrument (ISIS)
  • Galley miscellaneous equipment:
  • 10-cup, manual fill coffeemaker (TIA Model 1603)
  • Aerolux Nespresso manual fill coffee maker (AL –EX15-200E-17)
  • Chiller-cooled cold food storage
  • One divided ice drawer with overboard drain
  • High temp oven with digital controller (TIA Model) 1545-3
  • 0.7 cu ft. microwave oven (TIA)
  • Passenger cabin miscellaneous equipment:
  • Electrically operated accordion style window shades
  • Eight (8) ledge storage boxes one at each single and double seat location
  • Additional Aft cabin window (S/B 700-56 -001 FS 788 RHS)
Emergency Equipment
  • Smoke detector in each lavatory, in aft wardrobe and in baggage (factory-installed)
  • Life rafts, life vests, PBEs, fire extinguishers, and first aid kit as required
  • Engraved Maglite flashlight (in addition to (2) cockpit flashlights)
Production-Installed Avionics
  • Honeywell Primus 2000XP Integrated Avionics System
  • Production-Installed Avionics
  • Six 8×7 inch color CRT Display Units (DU-870) – 2 Primary Flight Display PFD, 2 Multifunction Display MFD, 1 EICAS and I System Synoptic Display
  • Three IC-800 Integrated Avionics Computers (IAC), each responsible for the following functions: I/O processor, ASCB controller, Electronic Display System EDS, Flight Management Computer, Autothrottle Control, Flight Guidance Computer FGC
  • Triple long-range navigation sources:
  • Triple integrated NZ-2000 Flight Management System with CD-820 CDUs
  • One DL – 800 data loader
  • One Lasertrack Navigation Data Unit (NDU)
  • Triple LASERREF IV Inertial Reference System (IRS)
  • Dual Primus II Nav/Com system with 25 KHz or 8.33 KHz channel spacing
  • Triple AZ-840 Micro Air Data Computers (MADC)
  • Dual Automatic Flight Control System (AFCS)
  • Primus 880 weather radar with dual Weather Radar Controllers
  • Dual full flight regime autothrottle
  • TCAS II TCZ-910 Traffic Alert and Collision Avoidance System with change 7 software upgrade
  • Triple Global Positioning System (GPS)
  • Central Aircraft Information and Maintenance System (CAIMS)
  • Other Honeywell Systems (formally Allied Signal):
  • Enhance Ground Proximity Warning System (EGPWS)
  • Flight Data Recorder (FDR – 57 parameters part 91 only)
  • Solid State Cockpit Voice Recorder (SSCVR) – 4 channel recording with 2 hour duration
  • Collins Systems:
  • Dual ALT-4000 radio altimeter systems
  • Dual HF-9000 High Frequency (HF) communications system
  • Coltech System:
  • Coltech CSD-714 Selective Calling System (SELCAL)
  • Other:
  • Artex ELT with NAV interface unit
  • External service panel lighting
  • Specification Subject to Verification Upon Inspection
  • Subject to Prior Sale or Removal From the Market Without Notice
Capacity
  • Crew (min/typical): 2-3
  • Passengers: 8-19
  • (business/high-density interior)
Avionics
  • Honeywell Primus 2000xp avionics suite
  • Central Aircraft Information Maintenance System (CAIMS)
  • Advanced diagnostic and troubleshooting tools integrated with major aircraft systems
  • Available both on the ground and in flight, CAIMS minimizes troubleshooting workload and reduces aircraft downtime
  • Head – up flight display system
  • TCAS 2000, EGPWS, GPS
  • SATCOM, telephone/fax, datalink, on-board local area network, single channel high-speed data
Engines
  • Rolls-Royce Deutschland BR710A2-20 turbofans
  • Thrust: 14,750 pounds (65.6 kN) thrust at takeoff
  • Flat-rating: ISA + 20ºC (95º F)
Range
  • Maximum range
  • At M 0.85: 4,800 NM 5,524SM 8,889 km (NBAA IFR Reserves, ISA, with 8 pax/3 crew)
Airfield Performance
  • Balance field length
  • (SL,ISA, MGTOW): 5,000 ft (1,524 m )
  • Landing distance (SL, ISA, MLW): 2,700 ft (823 m)
Speed
  • High-speed cruise 0.89 Match 513 kts 590 Mph 950 Km/h
  • Typical cruise speed 0.85 Match 488 kts 562 Mph 904 Km/h
Ceiling
  • Maximum operating altitude: 51,000 ft (15,545 m)
  • Climb to cruise altitude of 43,000 ft (13,106 m): 23.2 min
External
  • Length: 96.75 ft (29.49 m)
  • Wingspan: 94 ft (28.65 m)
  • Wing area: 1,022 ft (94.94 m)
  • (basic)
  • Height overall: 24.83 ft (7.57 m)
Internal
  • Cabin length: 42.47 ft (12.94 m)
  • (from start of forward lavatory to end of pressurized compartment)
  • Cabin maximum width: 8.17 ft (2.49 m) (centerline)
  • Cabin width: 6.92 ft (2.11) (floorline)
  • Cabin height: 6.25 ft (1.91m)
  • Floor Area: 294 ft (27.31 m) (excluding cockpit)
  • Total volume: 1,882 ft3 (53.29 m) (from start of forward lavatory to end of pressurized compartment)
Weights
  • A. Maximum ramp weight: 89,900 lb (40,778 kg)
  • B. Maximum takeoff weight: 89,700 lb (40,687 kg)
  • C. Maximum landing weight: 78,.600 lb (35,652 kg)
  • D. Maximum zero fuel weight: 56,000 lb (25,401 kg)
  • E. Typical basic operating weight: 50,830 lb (23,054 kg)
  • F. Maximum fuel weight: 36,000 lb (16,329 kg)
  • Maximum payload (D-E): 5,170 lb (2,345 kg)
  • Payload – full fuel (A-E-F): 3,070 lb (1,392 Kg)
  • Fuel with 8 pax/3 crew: 35,520 lb (16,111 kg)