2006 BOMBARDIER GLOBAL 5000
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- Audrey McGee
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1 Serial number 9190 Registration PR-XDN Specifications & Pictures
2 WARRANTY Total Time Airframe: 1000 hours. Total Landings: 425 Left and Right Engine: 1000 hours (BR710A2-20) Total Cycles: 418 APU Total Time: 663 hours (RE 220GX). APU Total Cycles: 892 Rolls Royce Corporate Care, Smart Plus. Manufacturer s Warranties (started on Dec. 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 years or 5,000 APU Labor.- 2 years or 2,000 hours Paint and Completion work INTERIOR CONFIGURATION Entrance Area:.- RH forward lavatory: vacuum toilet, vanity and.- LH entrance enclosure: cockpit flight observer seat (jumpseat), coat rod, storage areas and crew oxygen masks.- RH galley.- LH galley: annex with: 10.4 Touch Screen Control Panel.- Forward cabin bulkheads with LH sliding pocket doors (separate entrance area from cabin)
3 INTERIOR CONFIGURATION Forward Cabin.- RH side: One pull-out table and two wide, look back, single executive seats that feature integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar.- LH side: One pull-out table and two wide, low back, single executive seats that feature integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar.- Two magazine racks-one on each RHS & LHS fwd bulkheads Mid Cabin.- RH side: Credenza cabinet including entertainment and fax/printer. Low cabinet under emergency exit including miscellaneous storage.- LH side: One manually-opearted hi-low conference table and two 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 bulkheads. Aft Cabin.- RH side: 3-place 16G divan (forward seat position can be occupied when RH mid cabin bulkhead is removed) that also features berthing and storage. Two end cabinets, each features two drink holders, storage, and CME interface.- LH side: One pull-out table and two wide, low back, single executive seats featuring 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 fold-down shelves.- Two hang-up bars (one swings down to stow).
4 AVIONICS/ELECTRICAL SYSTEM.- Satellite Communication System and High Speed Link (SAT-6100) IMT Thales/Sextant Head-up Flight Display System (HFDS) CAT II operations (Factory/Completion Installed).- Central Aircraft - Information Maintenance System (CAIMS) - Installation of the CAIMS Reportto-printer switch.- Teledyne Datalink System (ACARS) IMT Honeywell RCZ-833 Third VHF Communication System (LSS) IM Honeywell LSZ-860 Lightning Sensor System (LSS) IMT rd Honeywell Single Global Positioning (GPS) System.- Satellite Communication System (SATCOM).- Three channel Aero H+ (INMARSAT) System (2 voice channels and I data channel). Data channel supports ACARS/maintenance functions.- One single-channel Iridium based airborne telephone system.- PBX (Aerocom 3000B) integrates two systems allowing common access from handset.- Four passenger cabin handsets (one is cordless). One handset in cockpit.- Single channel high speed data system (HST-2100) offers data transfer up to 64 KBPS.- Cabin power bus disconnected.- Ground service cabin power.- One power converter.- 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. CABIN ELECTRONIC SYSTEM (CES).- Global Office including: 10/100 Base T Ethernet LAN with connections for laptops and portable devices. Plain paper NT compatible fax/printer/scanner. RJ-45 LAN interface at each single, outboard double seat and cockpit. Wireless LAN
5 CABIN ELECTRONIC SYSTEM (CES).- Cabin Utilities/Control and Display featuring: One 10.4 inch galley touch screen control monitor, one cockpit touch screen equipment (co-pilot side). Passenger control switch panels, entertainment switch panel and local switch panels. Two IR remote controls. Power Distribution of aircraft AC and DC power.- Entertainment: Two multi-region DVD players, one multi-disk CD player, two bulkhead-mounted 21.3 inch LCD video monitors. High quality cabin speaker/subwoofer arrangement (10 speakers & 4 subwoofer). Eight receptacles for plug in monitors (4 plug in are included). Passenger headphone distribution, airshow moving map, cabin services, cabin/lavatory call system. Phone system (PBX), passenger briefing system. ICG ICS-200 Iridium telephone system..- Maintenance and diagnostics: Central maintenance function for applicable integrated cabin systems and diagnostic report viewing on the galley touch screen monitor. MISCELLANEOUS INSTALLATIONS.- Aircraft miscellaneous: Additional refuel-defuel panel IMT Forward handrail extension, common keyed panel locks, aft equipment bay storage box (30lb max.) Crew plaque, semi recessed Jeppesen manual storage box at cockpit entrance. Towbar and assembly storage (towbar is loose equipment).- Cockpit miscellaneous equipment: Two engraved Magnalite rechargeable flashlights. Two roller screens, two writing pad holders, Thale Integrated Standby Instrument (ISIS).- Galley miscellaneous equipment: 10 cup manual-fill cofeemaker, chiller-cooled cold food storage, one divided ice drawer with overboard drain. High temp. oven with digital controller, 0.7 cu ft. microwave oven..- Passenger cabin miscellaneous: Electrically operated accordion style window shades, eight ledge storage boxes one at each single and double seat location. Additional aft cabin window.
6 PRODUCTION-INSTALLED AVIONICS.- Honeywell Primus 2000XP Integrated Avionics System.- Six 8x7 inch color CRT Display Units.- Three IC-800 Integrated Avionics Computers (IAC).- Triple long-range navigation sources.- Dual 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 Refernce System (IRS).- Dual Primus II Nav/Com system with 25 Khz or 8.33 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 Allert and Collision Avoidance System with change 7 software upgrade.- Triple Global Positioning System (GPS).- EGPWS.- FDR.- SSCVR.- Dual ALT 4000 radio altimeter system.- Dual HF-9000 Hig Frecuency communications system.- Coltech CSD-714 Selective Calling System (SELCAL.- Artex ELT with NAV interface unit.- External service panel lightning. Specifications are subject to verification by purchaser
7 PICTURES
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10 PICTURES ASKING PRICE: MAKE OFFER For more information, contact us at Pacific Point Aviation
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