2001 Global Express s/n 9050
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4,600 Hours     2,065 Landings

CofA Date

March 31, 2000

Entry into Service Date

July 28, 2001


Rolls-Royce BR700-710A2-20     

Left:     Ser #: 12231       4,600 Hours     2065 Cycles  

Right:     Ser #: 12206   4,600 Hours     2065 Cycles


Honeywell GTC RE220-GX     S/N: P-146     4,750 Hours     2,981 Cycles

Major Aircraft Enhancements & Upgrades

  • IAC BATCH 3 Software Upgrade (SB 700-31-030 Rev 3):  FMS 6.1, RNP 0.3, Vertical Glide Path (VGP) mode (LNAV/VNAV) and activation of FANS 1/A+, WAAS (SBAS)/LPV and RNP 4.
  • FANS 1/A+ / RNP 4 30/30 (SB 700-34-053 Rev 2:  FMS modification to FANS 1/A+ and RNP 4 operational capability to 30nm/30nm separation.
  • SBAS – LPV (SB 700-34-054 Rev 1):  GPS Modification & Introduction of SBAS/LPV Approach Capability.
  • ADS-B Out (SB 700-34-062 Rev 3)
  • TCAS 7.1 (AD 2012-02-08)
  • Honeywell HD-710 Swift Broadband High Speed Data System (Inmarsat SATCOM) interfaced with Aircell Gogo Business Aviation ATG-5000 Hi-Speed Broadband Internet & Wi-Fi System

Honeywell Primus 2000XP (Honeywell DU-870) 6-Tube EFIS Integrated Avionics Suite

Honeywell DL 1000 Data Loader
Triple NZ-2000 Integrated FMS w/ 6.1 Software & Dual GPS
Triple Honeywell LASEREF IV Inertial Reference System (IRS)
Dual Honeywell AZ-840 Micro Air Data Computers
Quad Ameteck Data Acquisition Units (DAU)
Triple IC-800 Integrated Avionics Computers (IAC)
Primus 880 Color Weather Radar
Triple VHF Honeywell RCZ-833 COMM Units
Dual Honeywell RCZ-833 Enhanced Mode S Transponders w/ ADS-B Out
Dual Primus II RM-855 Radio Management Units
Dual Honeywell RNZ-851 Integrated NAV Units w/ VOR/ILS/MKR/ADF/DME (8.33 kHz Spacing & FM Immunity)
Dual Collins ALT-4000 Radio Altimeters
Dual Collins HF-9000 HF Comm System
Coltech CSD-714 SELCAL System
Honeywell Mark V EGPWS w/ Wind Shear
Honeywell TCAS II 2000 w/ Change 7.1
Honeywell Cockpit Voice Recorder (SSCVR)
Honeywell Flight Data Recorder (SSFDR)
Avionica Mini QAR MR11 Quick Access Recorder (FDR) – 750 hrs. recording time
Full Authority Digital Engine Control System (FADEC)
Engine Indication/Crew Alerting System (EICAS)
Dual Honeywell Autopilots w/ Autothrottles
Central Aircraft Information Maintenance System (CAIMS)
Honeywell VHF/SAT AFIS
ACARS Teledyne Datalink

Additional Features

Currently Operated Part 135
Office in the Sky Option (SB 700-23-003)
HD-710 Swift Broadband High Speed Data
6 Channels (5 Voice, 1 Data)
Magnastar C-2000 Flight Phone (6 Handsets)
Artex 406Hz Emergency Location Transmitter w/ Navigation Interface
WSI AV-300 Weather System
406 Hz ELT’s in all 3 Life Rafts
2 DVD/CD Players in Cabin
Airshow Flight Information System
115VAC 60Hz Power Outlets throughout the cabin
Backup Fuel Panel Control in the Cockpit


3A (1500 Hr), 1C (15 Mo), 2C (30 Mo), 4C (60 Mo), & 8C (120 Mo) Checks Completed August 2011 at 3,019 Hrs. by Bombardier – Ft. Lauderdale, FL.

2A (1000 Hr), 2C (30 Mo), 4C (60 Mo), & 12C (180 Mo) Checks Completed June 2016 at 3,780 Hrs. by Jet Aviation – Basel, Switzerland.

Maintenance Tracked on Traxxall

Airframe Enrolled on Smart Parts + (HAPP Included)


Last Weighed June 27, 2016

Gross Weight (Ramp):     96,250 lbs.

Max Takeoff Weight:     96,000 lbs.

Max Landing Weight:     78,600 lbs.

Max Zero Fuel:     56,000 lbs.

Basic Empty Weight:     50,052 lbs.

Basic Operating Weight:     51,924 lbs.


Major Refurbishment June 2016 @ Jet Aviation – Basel, Switzerland

Completed at the Bombardier Completion Center, Montreal Canada, July 2001. 

13 passenger, fireblocked, interior features an entry area that includes a crew jump seat, left-side crew rest area, right-side forward crew vacuum lavatory, right-side forward main galley, with an aft main vacuum lavatory, and aft baggage compartment.  The entry area and forward cabin are separated by a pocket door.  The interior features a 3-zone cabin with a forward cabin 4-place club with 2 manually operated executive tables between the opposing club chairs, a mid-cabin 4-place conference group opposite a credenza, followed by dual aft 3-place berthable divans (left-side certified 2 TTOL and right-side certified 3 TTOL) separated from the main-cabin by a curtain.  The main cabin is capable of comfortably berthing 5 passengers.  Club and conference group chairs are covered in a light cream leather and the divans in a coordinating burgundy fabric.  The carpeting is burgundy cut pile wool and the wood/cabinetry is a gloss finished, medium-toned veneer complemented by gold plating. Cabin entertainment includes Airshow and Dual DVD/CD players that can be viewed on one (1) 18″ LCD monitor mounted on left forward bulkhead, plug-in 10.4″ touchscreen LCD monitors, and one (1) 10.4″ touchscreen LCD cabin management monitor in the galley.  The forward galley includes a microwave oven, Nespresso machine, air chiller unit for cold storage, sink with potable water, and ample storage for glassware, china, catering trays and additional supplies. 

June 2016 Interior Upgrades

Replaced carpet in the main cabin and aft lavatory; reupholstered 4 club chairs, 4 conference group chairs, and 2 divans; reupholstered window panels, dado panels, and sidewalls; curtains in the crew rest area, main cabin door, and mid-cabin were replaced.


New Paint (Complete Strip & Paint) October 2011 @ Bombardier – Tucson, AZ

Overall Light Ivory Lower Fuselage and Burgundy Upper Fuselage with a Burgundy stripe.


Aircraft is Located at Long Island MacArthur Airport (ISP) in Ronkonkoma, NY, USA.