Global 5000

1100 hours, manufactured in 2006

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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)