2005 BOMBARDIER GLOBAL 5000 SERIAL NUMBER 9154 EQUUS GLOBAL AVIATION +1 (954)

Transcription

1 2005 BOMBARDIER GLOBAL 5000

2 2005 BOMBARDIER GLOBAL 5000 UPDATED HONEYWELL PRIMUS ELITE 875 LCD DISPLAY PACKAGE - FULL HONEYWELL BROCHURE AVAILABLE UPON REQUEST A new product designed to meet exisfng requirements with planned growth funcfonality to support future situafonal awareness enhancements and CNS/ATM progression

3 2005 BOMBARDIER GLOBAL 5000 ONLY 3443 HOURS 1144 LANDINGS ENGINES: ROLLS ROYCE BR710- A2-20 LEFT ENGINE: 3443 HOURS RIGHT ENGINE: 3443 HOURS APU: HONEYWELL RE- 220 (GX) 3694 HOURS 1144 CYCLES 1144 CYCLES 3516 CYCLES SINCE NEW 8C INSPECTION & LANDING GEAR OVERHAUL CURRENTLY IN PROCESS BAS SINGAPORE BATCH III COMPLIED WITH UPDATED COCKPIT WITH HONEYWELL PRIMUS ELITE 875 LCD DISPLAY PACKAGE

4 2005 BOMBARDIER GLOBAL 5000 THE GLOBAL 5000 IS UNIQUELY EQUIPPED WITH AN INTEGRATED HONEYWELL PRIMUS 2000XP AVIONICS SUITE FEATURING THE LATEST PRIMUS ELITE 875 ENHANCEMENT PACKAGE. TYPE OF UNIT QUANTITY DESCRIPTION EFIS (Electronic Flight Instrument System) 6- Tube Honeywell Primus Elite Color Displays ESIS (Electronic Standby Instrument System) Single Integrated Electronic Standby Instruments FMS (Flight Management System) Dual Honeywell NZ w/ CD 820 IRS (InerFal Reference System) Triple Honeywell LASEREF IV GPS (Global PosiFoning System) Dual Honeywell 12 Channel MADC (Micro Air Data Computer) Triple Honeywell AZ- 840 DME (Distance Measuring Equipment) Dual Honeywell RM- 855 Radio Management Units NAV (NavigaFon Radio) Dual Honeywell RM- 855 Radio Management Units ADF (AutomaFc DirecFonal Finder) Dual Honeywell RM- 855 Radio Management Unit RA (Radio AlFmeters) Dual Collins ALT HUD (Head Up Display) Single Thales/Sextant LSS (Lightning Sensor System) Single Honeywell LSZ- 860 EICAS (Engine IndicaFon/Crew AlerFng System) Single Honeywell Primus AUDIO Triple Audio Control Panel AV- 850A VHF COM (Very High Freq. CommunicaFon) Triple Primus II w/8.33 spacing HF COM (High Freq. CommunicaFons) Dual Collins HF SELCAL (SelecFve Calling) Single Coltech CSD- 714 SELCAL SATCOM (Satellite CommunicaFons) Single SAT System HIGH SPEED LINK Single SAT System RADAR Single Honeywell Primus 880 Weather Radar

5 2005 BOMBARDIER GLOBAL 5000 AVIONICS CONTINUED RADAR ALT (Radar AlFmeter) Dual Honeywell ALT RADAR (Weather Radar) Single Honeywell Primus 880 XPNDR (Transponder) Dual Honeywell w/ Mode S EGPWS (Enhanced Ground Proximity Warning System) Single Honeywell Mark V TCAS (Traffic Collision Avoidance System) Single Collins TCZ- 910 with Change 7 CVR (Cockpit Voice Recorder) Single Allied Signal SSCVR FDR (Flight Data Recorder) Single Allied Signal SSFDR ACARS Single Teledyne Datalink System (ACARS) CAIMS Single Central Aircrae- InformaFon (6) 8X7 COLOR CRT DISPLAY UNITS - 2 Primary Display, 2 MulFfuncFon Display, 1 EICAS & 1 System SynopFc Display. (3) IC- 800 INTEGRATED AVIONICS COMPUTERS for the I/O processor, ASCB controller, Electronic Display System EDS, Flight Management Computer, Autothrohle control, & Flight Guidance Computer FGC. TRIPLE LONG- RANGE NAVIGATION via Dual integrated NZ- 2000,(1) DL- 900 data loader and (1) Lasertrack (NDU). SATELLITE COMMUNICATION SYSTEM (SATCOM) Three (3) channel Aero H+ (Inmarsat) system (2 voice channels and 1 data channel). Data channel supports ACARS/ maintenance funcfons (reference SB 700A XX above) One (1) single- channel Iridium based airborne telephone system PBX (Aerocom 3000B) integrates two systems allowing common access from handsets Four (4) passenger cabin handsets (one is cordless). One handset in cockpit Single channel high speed data system (HST- 2100) offers data transfer of up to 64 KBPS

6 2005 BOMBARDIER GLOBAL 5000 AVIONICS & ELECTRICAL SYSTEMS CONTINUED Cabin power bus disconnect Ground service cabin power Power converter AddiFonal TRU EICAS door open annunciafon. 16 Electrical outlets installed CABIN ELECTRONIC SYSTEMS Global Office - 10/100 Base T Ethernet LAN Plain paper, NT compafble FAX/ Printer/ Scanner RJ- 45 LAN interface at each single and outboard double seat Wireless LAN Cabin UFliFes / Control and Display One (1) 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 Entertainment - Two (2) mulf- region DVD players, One (1) mulf- disk CD player, Two (2) bulkhead- mounted inch LCD video monitors, High Quality Cabin Speaker/Subwoofer Arrangement, Eight (8) receptacles for plug- in monitors (plug- in monitors not included). Airshow moving map LIGHTING LED interior lighfng Exterior (pylon lights) Wing Fp taxi lights Pulse landing light system Wheel- well maintenance lights Service lights Fmer override Logo lights.

7 2005 BOMBARDIER GLOBAL 5000 INTERIOR CONFIGURATION Entrance Area: RH forward lavatory with vacuum toilet, vanity and sink LH entrance enclosure: cockpit flight observer seat (jumpseat), coat rod, storage areas and crew oxygen mask. RH galley with: a manual- fill Aerolux Nespresso machine, a Tia manual- fill carafe coffee maker and an air chiller unit for cold food storage area, one divided ice drawer with overboard drain. LH galley annex with: 10.4 Touch screen control panel, a 0.7 cu e microwave and a Tia high temp oven with digital controller. 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 execufve 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 execufve seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar. (2)magazine racks - one (1) on each RHS & LHS fwd bulkheads Mid Cabin: RH side (Zone 2A): Credenza cabinet including entertainment equipment and fax/printer. Low cabinet under emergency exit. 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. A conversion kit will be included to disable the door, as a requirement to comply with FAR PART 135 operafng rules. A removable curtain and permanent curtain track.

8 2005 BOMBARDIER GLOBAL 5000 INTERIOR CONFIGURATION CONTINUED A[ Cabin: RH side: 3- place 16G divan (forward seat posifon 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: One (1) pull- out table and two (2) wide, low back, single execufve seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar A[ Lavatory Zone: Ae cabin bulkheads and hinged door, Vacuum toilet and vanity cabinet with miscellaneous storage Wardrobe and storage cabinet featuring adjustable and fixed shelving Baggage Compartment Area: Approximately 145 cu. e. with (2) Fold- down shelves and (2) hang- up bars EQUIPMENT AND SYSTEMS Soundproofing: Bombardier vibro- acousfc soundproofing package tailored to the layout, and finishing trims Oxygen System: Factory- installed EROS MF- 10 full- face masks are retained for the pilot and co- pilot. 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) therapeufc oxygen outlets in passenger cabin Environmental Control System (ECS): Passenger control of two cabin temperature zones (+/- 2 deg. C) around master control sesng Entry area heater Potable Water System (PWS): Re- circulafng water system with dual pumps (for redundancy) and UV filter system 24.7 Gallon water tank

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