Global Express MSN 9111

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• New to market!!!

• 2003 vintage GLEX

• Single Fortune 500 owner

• Impeccable maintenance condition with Batch 3 Avionics

• Pristine exteriors and interiors


Total Time Since New 7557 Hours (as of 13 Sep 17)
Total Landings Since New 4440 Landings
Entry into service date 27-May-2003
Home Base Mumbai, INDIA
Maintenance Tracking ARMS
Program Coverage Smart Parts Program
Certification EASA, FAA, DGCA Certified




Left Engine Right Engine
Description Rolls Royce BR710-A2-20 Rolls Royce BR710-A2-20 Rolls Royce BR710-A2-20 Rolls Royce BR710-A2-20
Serial Number(s) 12334 12333
Total Hours Since New 6956 Hours 6774 Hours (As on 13 Sep 17)
Total Cycles Since New 4118 Cycles 3966 Cycles (As on 13 Sep 17)
Overhaul Due On Condition
Program Coverage Rolls Royce Corporate Care Program




Description Honeywell RE220 (GX)
Serial Number P-221
APU Total Time Since New 7860 Hours (As on 8 Sep 17)
Program Coverage N/A



This Global Express is equipped with a fully integrated Honeywell Primus 2000XP avionics suite.

Type of Unit Quantity Description
EFIS (Electronic Flight Instrument System) 6-Tube DU-875 Primus Elite LCD Displays
ESIS (Electronic Standby Instrument System) Single Thales IESI
FMS (Flight Management System) Triple Honeywell FMZ-2000
IRS (Inertial Reference System) Triple Honeywell
GPS (Global Positioning System) Dual Honeywell HG2021Sensor Unit
MADC (Micro Air Data Computer) Triple Honeywell
DME (Distance Measuring Equipment) Dual Honeywell RNZ-851
HUD (Head Up Display) Single Thales Head Up Display
ADF (Automatic Direction Finder) Dual Honeywell RNZ-851
AUTOPILOT Dual Honeywell IC-800
VHF COM (Very High Freq. Communication) Triple Honeywell Primus RCZ 833
SATCOM (Satellite Communications) Single Honeywell MCS 6000
VOR NAV / ILS / MARKER Dual Honeywell RNZ-851
RADAR Single Honeywell Primus 880, WU-880
RADIO ALT (Radio Altimeter) Dual Collins ALT- 4000
XPNDR (Transponder) Dual Honeywell RCZ-833, Mode S
EGPWS (Enhanced Ground Proximity Warning System) Single Honeywell Mark V w / Windshear
TCAS II (Traffic Collision Avoidance System) Single Honeywell TCAS 2000 w/ Change 7.1
CVR (Cockpit Voice Recorder Single Honeywell SSCVR
FDR (Flight Data Recorder) Single Honeywell SSFDR
Telelink Datalink ——- Teledyne TL-608



Number of Passengers Sixteen (16)
Galley Location Forward
Fwd Cabin Configuration Four Place 9G Single Club Seats with foldout tables
Mid Cabin Configuration Six-Place 9G Single Seat conference group with conference table
Aft Cabin Configuration Six-place 16G Bed divan LH and RH (3 place each)
Lavatory Location(s) One Forward crew lavatory and One Aft fully enclosed lavatory with storage cabinet
Crew Area Forward
Jumpseat Yes



Base Paint Color(s) Overall White fuselage
Stripe Color(s) Golden and Blue accent stripe running from nose to tail and on the vertical stabilizer
Last Painted Date October 2013



Type of Unit Description
Display/TV Monitor(s) Three (3) Bulkhead-mounted 18” LCD Monitor
Individual Monitors Two (2) Plug-in 10” touch screen LCD monitors
Airshow System Rockwell Collins Flight Information System (Moving Map)
CD/DVD Player(s) Multi-region CD/DVD Players combined unit



Inspection Last Performed Next Due
15 Mo. Check 15 Aug 2017 14 Nov 2017
30 Mo. Check 10 JUNE 2016 9 DEC 2018
60 Mo. Check 21 DEC 2013 20 DEC 2018
120 Mo. Check 21 DEC 2013 20 DEC 2023




Type of Unit Type of Unit
Provision for CVR Datalink Cockpit Printer
Airborne Data Link System (ADLS) Passenger Address (PA) System
Honeywell LSZ-860 Lightening Sensor System (LSS) ACARS Data Support
Global Office Operations at Airports with Maximum Weight Restrictions
Cockpit Refuel/Defuel Control Panel Towbar Assembly
Logo Light, Ext. Baggage Door Lock Override, EICAS “Small Serv Door” Annunciation, Aircraft ID Plate, APU Hour Meter Handrail Extension
Battery Access Multi-Purpose Ladder
Common Key Panels, Lockable Fuel Cap Aesthetic Side Covers on Main Entry Door
Aft Equipment Bay Storage Box Ground Service Cabin Power
Cabin Bus Disconnect 230V AC 50Hz GFI protected utility outlets
One (1) 3500 VA/230VAC/50Hz power converter Batch 3 Avionics Upgrade
ADSB Upgrade Package Magnastar C-2000 ARTU Cabin Communication System
CAIMS Information System CPDLC Support capability



RNAV 5 FM Immunity



Gross Weight (Ramp) 96,250 lbs Max Fuel Capacity 43,538 lbs
Max Takeoff Weight 96,000 lbs Max Zero Fuel Weight 56,000 lbs
Max Landing Weight 78,600 lbs Basic Operating Weight 45,000 lbs



Type of Unit Description
High Speed Internet(Wi-Fi) Three (3) channels Aero H+ (2 voice and 1 Data). Data channel supports ACARS/maintenance functions
Wireless Ethernet LAN -
In Flight Phone Via Satcom Single-channel ICS-100 Iridium Telephone SystemThree (3) corded and One (1) Cordless Telephone Handsets
Cabin Cabin Printer/Fax Plain Paper
ACARS Data Support -



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