Global Express MSN 9111 AVAILABLE FOR SALE-MAKE OFFER
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DESCRIPTION
• New to market!!!
• 2003 vintage GLEX
• Single Fortune 500 owner
• Impeccable maintenance condition with Batch 3 Avionics
• Pristine exteriors and interiors
AIRFRAME
| 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 |
ENGINES
| 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 |
APU
| Description | Honeywell RE220 (GX) |
| Serial Number | P-221 |
| APU Total Time Since New | 7860 Hours (As on 8 Sep 17) |
| Program Coverage | N/A |
AVIONICS
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 |
INTERIOR
| 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 |
EXTERIOR
| 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 |
ENTERTAINMENT
| 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 |
MAJOR INSPECTION STATUS
| 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 |
OTHER / ADDITIONAL EQUIPMENT
| 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 |
NAVIGATION & COMPLIANCE
| RVSM | RNAV 10 (RNP 10) |
| MNPS | RNAV 1 & 2 |
| RNAV 5 | FM Immunity |
WEIGHTS
| 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 |
CONNECTIVITY
| 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 | – |