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Airframe
3443 HOURS
1144 LANDINGS
Engine(s)
ROLLS ROYCE BR710--A2--20
LEFT ENGINE: 3443 HOURS / 1144 CYCLES
RIGHT ENGINE: 3443 HOURS / 1144 CYCLES
APU: HonEYWELL RE--220 (GX)
3694 HOURS / 3516 CYCLES SINCE NEW
Avionics/Radios
THE GLOBAL 5000 IS UNIQUELY EQUIPPED WITH AN INTEGRATED HonEYWELL PRIMUS 2000XP AVIonICS SUITE FEATURING THE LATEST PRIMUS ELITE 875 ENHANCEMENT PACKAGE.
-- FULL HonEYWELL BROCHURE AVAILABLE UPON REQUEST –
A new product designed to meet existing requirements with planned growth functionality to support future situational awareness enhancements and CNS/ATM progression.
TYPE OF UNIT QUANTITY DEscriptION
EFIS (Electronic Flight Instrument System) 6--Tube Honeywell Primus Elite --875 Color Displays
ESIS (Electronic Standby Instrument System) Single Integrated Electronic Standby Instruments
FMS (Flight Management System) Dual Honeywell NZ--2000 w/ CD 820
IRS (Inertial Reference System) Triple Honeywell LASEREF IV
GPS (Global Positioning 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 (Navigation Radio) Dual Honeywell RM--855 Radio Management Units
ADF (Automatic Directional Finder) Dual Honeywell RM--855 Radio Management Unit
RA (Radio Altimeters) Dual Collins ALT--4000
HUD (Head Up Display) Single Thales/Sextant
LSS (Lightning Sensor System) Single Honeywell LSZ--860
EICAS (Engine Indication/Crew alerting System) Single Honeywell Primus
AUDIO Triple Audio Control Panel AV--850A
VHF COM (Very High Freq. Communication) Triple Primus II w/8.33 spacing
HF COM (High Freq. Communications) Dual Collins HF--9000
SELCAL (selecive Calling) Single Coltech CSD--714 SELCAL
SATCOM (Satellite Communications) Single SAT--6100 System
HIGH SPEED link Single SAT--6100 System
RADAR Single Honeywell Primus 880 Weather Radar
RADAR ALT (Radar Altimeter) Dual Honeywell ALT--4000
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 (Tra?c 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 Aircraft--Information
(6) 8X7 COLOR CRT DISPLAY UNITS -- 2 Primary Display, 2 Multifunction Display, 1 EICAS & 1 System Synoptic Display.
(3) IC--800 INTEGRATED AVIonICS COMPUTERS for the I/O processor, ASCB controller, Electronic Display System EDS, Flight Management Computer, Autothrottle 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 functions (reference SB 700A11--23--XX above)
One (1) single--channel Iridium based airborne telephone system
PBX (Aerocom 3000B) integrates two systems allowing common access fro handsets Four (4) passenger cabin handsets (one is cordless). One handset in cockpit
Single channel high speed data system (HST--2100) o?ers data transfer of up to 64 KBPS
Cabin power bus disconnect
Ground service cabin power
Power converter
Additional TRU
EICAS “door open” annunciation.
16 Electrical outlets installed
Additional Equipment
LIGHTING:
LED interior lighting
Pulse landing light system
Logo lights
Exterior (pylon lights)
Wheel--well maintenance lights
Wing tip taxi lights
Service lights timer override
Soundproo?ng: Bombardier vibro--acoustic soundproo?ng package tailored to the layout, and ?nishing 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 ?ight observer seat. Oxygen dro boxes as required in main cabin as well as galley, lavatories and at jumpseat, Two (2) therapeutic oxygen outlets in passenger cabin
Environmental Control System (ECS): Passenger control of two cabin temperature zones (+/-- 2 deg. C) around master control setting Entry area heater
Potable Water System (PWS): Re--circulating water system with dual pumps (for redundancy) and UV ?lter system
24.7 Gallon water tank
Interior
INTERIOR ConFIGURATION
Entrance Area: RH forward lavatory with vacuum toilet, vanity and sink
LH entrance enclosure: cockpit ?ight observer seat (jumpseat), coat rod, storage areas and crew oxygen mask.
RH galley with: a manual--?ll Aerolux Nespresso machine, a Tia manual--?ll carafe co?ee 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 ft 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 executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric in?atable 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 in?atable 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 in?atable 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 operating rules. A removable curtain and permanent curtain track.
A[ 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 (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 executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric in?atable lumbar
A[ Lavatory Zone: Aft cabin bulkheads and hinged door, Vacuum toilet and vanity cabinet with miscellaneous storage Wardrobe and storage cabinet featuring adjustable and ?xed shelving
Baggage Compartment Area: Approximately 145 cu. ft. with (2) Fold--down shelves and (2) hang--up bars
CABIN ELECTRonIC SYSTEMS
Global O?ce -- 10/100 base T Ethernet LAN
Plain paper, NT compatible FAX/ Printer/ Scanner
RJ--45 LAN interface at each single and outboard double seat 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
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 Arrangement, Eight (8) receptacles for plug--in monitors (plug--in monitors not included). Airshow moving map