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Major Price Reduction: $41,000,000  $38,995,000

   Why buy a Global XRS?

   Longer Range
   Cabin is 20 feet longer than a
      Challenger
   Maximum Range of 6,250 nm
      with all seats filled
   Separate Crew Rest Area
   Why buy THIS Global XRS?

   Always registered and based in
      the U.S. = easy sale process
   Excellent Pedigree and Condition
   Delivered enrolled on RRCC
   HUD/EVS/Triple FMS
   High Speed Data with Wireless LAN
   Tailwind 500 Satellite TV
   CES (Collins) Software 7 Upgrade
   High Service Bulletin Compliance

      
Watch a video produced by JMCJSI about this exciting aircraft
Click here to watch



Watch a Rockwell Collins video for the software upgrade
Click here to watch


Read a recent JMCJSI Blog Post by Josh Mesinger
"
Pedigree"
Click here to read

      

Download a printable Acrobat PDF version of this photos
Global XRS, SN 9203.pdf 2,561 kb      Need Acrobat?


 Aircraft Location:
This outstanding aircraft is based in Hillsboro, OR and may be viewed by appointment. 

 Airframe:
TTAF: 1,701 hrs
Landings: 700

 Engines:
Plan: Delivered enrolled on Rolls-Royce Corporate Care
Type: BR700-710A2-20
   #1 (left)  #2 (right)
S/N: 12517 12518 
TSN: 1,701 hrs 1,701 hrs
CSN: 700 700
Next O/H Due:  On Condition On Condition
Next HOT Due: On Condition On Condition

 APU:
Type: Honeywell RE-220
S/N: P-330 
TSN: 1,199 APU hours
O/H Frequency: On Condition
HOT Frequency: On Condition

 Weight & Balance:
Empty: 51,258 lbs
Basic Operating: 52,971 lbs
Max Takeoff: 99,500 lbs (SB 700-11-020)
Max Landing: 78,600 lbs
Max Zero Fuel: 56,000 lbs
Full Fuel: 45,050 lbs
Max Ramp:: 99,750 lbs (SB 700-11-020)

 Maintenance / Inspections:
On CAMP maintenance tracking program
1A Check complied with 8/17/10 @ 1,456 hours, next due 12/12/11 or 2,000 hours
2A Check complied with 6/12/09 @ 1,006 hours, next due @ 2,000 hours
3A Check complied with 8/17/10 @ 1,465 hours, next due @ 3,000 hours
450 Landing Check complied with 10/21/09 @ 450 landings, next due @ 900 landings
6A Check due @ 3,000 hours
900 Landing Check due @ 900 landings
9A Check due at 4,500 hours
1C Check complied with 3/31/11 @ 1,663 hours, next due 6/15/12
2C Check complied with 1/6/10 @ 1,160 hours, next due 6/15/12
4C Check due 6/16/12
8C Check due 6/15/17

 Remaining Warranty Dates:
Airframe & Airframe systems (excluding completion) until June 15, 2012 or 5,000 hrs
Aircraft Primary Metal Structures until June 15, 2027 or 20,000 hrs
Green Aircraft Avionics until June 15, 2012 or 5,000 hrs
BMW Rolls-Royce Engines until June 15, 2012 or 2,500 hrs or cycles
APU Parts until June 15, 2013 or 3,000 hrs
APU Labor until June 15, 2012 or 5,000 hrs

 Avionics:
COM: Dual Honeywell RCZ 833K with optional 3rd RCZ 833 unit installed
NAV: Dual Honeywell RNZ 851
FDS: Honeywell Primus 2000XP
A/P: Honeywell GP 400 Guidance Panel
XPNDR: Dual Honeywell RCZ 833K Mode S with Enhanced Flight ID
ADF: Dual Honeywell RNZ 851
DME: Dual Honeywell RNZ 85
ADC: Triple Honeywell AZ 840 MADC
FMS: Triple Honeywell NZ 2000 with CDU 820s and 5.8 Software
GPS: Dual Honeywell GPS 550 HG2021GD03
AFIS: Teledyne Controls Tele link Unit (ADLU)
SATCOM: ICS 100 Iridium, Collins SAT 6100 with SRT 2100 High Speed Data
HFCOM: Dual Collins HF 9000 (HF9031A)
FFONE: ICG Aerocom 3000, 2 cordless handsets and 3 corded handsets
EFIS: Six DU 870 Displays (2 PFD, 2 EICAS, 2 MFD)
RADAR: Honeywell WU 880 with LSZ 860 Lightning Sensor (SB 700-34-003)
SELCAL: Single Coltech CSD 714
TCAS: Honeywell TCAS 2000 RT 950 with Change 7
RADALT: Dual Honeywell ALT 4000
EGPWS: Honeywell Mark V with RAAS (218-218 software)
LRNAV: Triple Honeywell Laseref IV (HG2001GD03)
FDR: Honeywell SSFDR 980-4700-041
CVR: Honeywell SSCVR 980-6022-001
ELT: Artex B406-4
Audio Panels: Triple Honeywell AV850A

 Additional Equipment and Features:
RVSM Capable
MNPS Capable
FM Immunity Compliant
8.33 Spacing Compliant
TAWS Compliant
Rockwell Collins Cabin Electronic system (CES) version 7 upgrade
Thales HFDS Heads-Up Flight Display System (SB 700-34-002)
Bombardier Enhanced Vision System BEVS (SB 700-34-033 Rev. 1)
Triple Honeywell IC 800 Integrated Avionics Computers
(4) Honeywell DA 810 Data Acquisition Units
Honeywell 3rd FMS with Cabin Video Feed (SB 700-34-004)
Honeywell IAC -009 Software Upgrade (SB700-31-001)
Honeywell LSS Lightning Sensor (SB 700-34-030)
Honeywell NZ 2000 Upgrade to CD 820 Displays (SB 700-34-047)
Honeywell Quick Access Recorder Installation QAR (SB 700-31-026)
Teledyne Controls G-624E P7.0G Sky Printer Cockpit Printer
EMS Technologies AMT 50 SATCOM Antenna Assembly
EVAS Enhanced Vision Assurance Systems
Dual APE 4190 Digital Cockpit Clocks
Logo Lights System (SB 700-33-001 Rev. 1)
CAIMS Central Aircraft Information Maintenance System with PMAT Display
Auto Throttle System
Maximum Take-Off Weight Increase to 99,500 lbs (SB 700-11-020)
Autopilot Emergency Decent Mode (SB 700-22-003)
Wiring Provisions for XM Weather System (by 337)
Baggage Door Internal T Handle Installation (SB 700-52-033)
Addition of Refuel/Defuel Control Panel in Flight Compartment (SB 700-28-002 Rev. 1)
Certification for Operations at Airports with Maximum Weight Restrictions (SB 700-11-018)
Modifications to Permit Zero Flap Take Off Capability (SB 700-27-059 A, B and C)
Pulse Landing lights

 Interior:

This aircraft has a 13 passenger fireblocked interior plus a crew rest area and one crew jump seat. The forward section of the aircraft features a crew rest area adjacent to the galley. The forward cabin features four single chairs in club configuration with two stowing work tables. The mid cabin includes a four place conference group with a two position manual table. The aft cabin includes a 16g divan (three place with bulkhead removed, two place with bulkhead installed) on the right hand side opposite two chairs in club configuration with a stowing work table. The club BEAerospace individual seats and the divan are all berthable. There is a solid swing door from the galley into the forward cabin, a solid electric door from mid to aft cabin and a solid electric door from aft into lav.

The forward galley is equipped with a Hi-Temp oven, microwave oven, dual coffee maker, hot cup, sink with swivel and folding faucet, drain switch, chilled storage with removable shelves and soda storage, clean ice and bottle storage with drainage, wine and liquor storage, china, flatware, utensils, linen and dirty dish bin and crystal storage, (4) 115 VAC 60 HZ outlets. The middle tambour door has a microswitch that deactives the water system and the two forward doors have a microswitch that deactivates the galley utility outlets. There is a 10.4” touchscreen in the upper galley that provides control for all galley and cabin systems.

The entertainment and cabin systems feature the Rockwell Collins Cabin Electronic system (CES) version 7 upgrade, (2) units of dual DVD players (4 total DVD players), (1) VCP, (1) CD with MP3 capability and the following Ethernet monitors: (1) 21.3” on left forward bulkhead, (1) 18” (fixed mounted) on the credenza, (1) 24” on right aft bulkhead, (2) fixed mounted in crew rest and galley respectively and (1) portable 10.4” plug in for (4) defined individual seat locations. The entertainment and cabin systems also features the Tailwind 500 Satellite TV System, an Airshow Interactive system, ICS100 Iridium Phone system, Collins SAT 6100 SATCOM with SRT 2100 with (2) 64K HSD data channels and a wireless Ethernet LAN, AEROCOM 3000 with (3) corded handsets and (2) cordless, RJ 45 jacks, 115VAC 60 HZ outlets, fax / printer machine installed in mid cabin credenza, Securaplane CAM-11 and CMX 03-X External camera system with (4) video cameras (2 color and 2 black and white).

Forward and Aft fully flushing chemical lavs (8 gallons), externally serviced toilets, each lav includes vanity cabinets with a sink and faucet, soap dispenser, facial tissue dispenser, toilet paper dispenser, concealed power outlet, exhaust fans, storage and switches for both the water heater and floor mat. The aft lav also has a lighted cosmetic mirror.

Additional Interior Information:
BEAerospace seats all have fold up leg rests, flip up armrests with stowage and electronic controls for lumbar support, flex wing headrests, full swivel capability, full berthing and reclining capability and an audio jack in the lower inboard armrest. The 16g divan has a frame length of 80” take-off and landing certification for 2 with the FWD bulkhead installed and 3 with it removed (it is easily removable by the crew anytime) and it is fully berthable and has (3) shoulder harnesses installed. The double chairs on either side of the 4-place conference group fully recline and each seat has lumbar support.

The credenza in main cabin includes a small cold storage/ Ice drawer which is both removable and insulated.

Interior Coverings:
Chairs are tan leather with fabric inserts
Headliner is biscuit
Divan is a fabric in a Sapphire color
Wood is Fig Walnut Gloss
Metal finish is Smoke Nickel Satin
Counter tops are a Blue Pearl Tiled Granite
Cabin sidewalls were recovered by Bombardier Dallas on 2/1/2008


 Exterior Colors:
Overall Jet Glo White with Charcoal Gray Metallic and Evening Sky Stripes.
Stripes repainted on 6/7/2011 by Westar Aviation.

 Additional Information:

For more information about our services please call us at:
Phone: +1 303-444-6766 Fax: +1 303-444-6866
3025 47th Street, Suite D2
Boulder, Colorado 80301 USA

Or E-mail sales@jetsales.com


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Specifications as of 5/16/12.  Specifications are subject to verification upon inspection
and should not provide a basis for reliance or create any other binding obligation.  Information has been provided by Seller and has not been independently verified by JMCJSI.  Presenting these aircraft specifications does not constitute the registration of a client by JMCJSI.

J. Mesinger Corporate Jet Sales, Inc.



 
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Jay Mesinger
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