Global 5000 (vendido)
1100 horas totais, ano 2006
São Paulo - Nova York com folga e muito conforto.
Autonomia: 9.630km
Velocidade máxima: 963 km/h
Teto operacional máximo: 51.000 pés
(Preço: Consultar)
Destaques
- 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
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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
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
Baggage Compartment Area
- Approximately 145 cu. Ft.
- Two (2) fold-down shelves
- Two (2) hang-up bars (one swings down to stow)
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.
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Potable Water System (PWS)
- Re-circulating water system with dual pumps (for redundancy) and UV filter system
- 24.7 Gallon water tank
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
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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
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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)
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
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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
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)
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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)
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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 Lavatory Zone
- Aft cabin bulkheads and hinged door
- Vacuum toilet
- Vanity cabinet with miscellaneous storage
- Wardrobe and storage cabinet featuring adjustable and fixed shelving
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
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
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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
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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)
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Production-Installed Avionics
- Honeywell Primus 2000XP Integrated Avionics System
- Production-Installed Avionics
- Six 8x7 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
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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 )
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)
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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)
VER TODOS
