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2003 Bombardier Global Express

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2003 Bombardier Global Express
Aircraft Details
TTAF 5,115 hrs
Serial Number 9115
Year 2003
Interior Color Fabric
Exterior Color Matterhorn White
History N/A

Fully Enrolled on Programs;
Full Batch 3 Avionics w/ ADS-B Out;
Triple FMS and CDU-820;
Head-Up Display;
Increased MTOW to 98,000 lbs.; and
11 Passenger Configuration

AIRFRAME:

Total Time Since New 5,115 Hours (as of Sept. 2017)
Total Landings Since New 1,457 Landings
Entry into Service Date March 20, 2003
Current Location Jet Aviation – Singapore , Seletar Airport
Program Coverage Smart Parts and JSSI Options are Available
Maintenance Tracking CAMP
Certification FAA Part 91

ENGINES:

Left Engine Right Engine  
Description Rolls Royce BR700-710A2-20
Serial Number(s) 12341 12342
Total Hours Since New 5,046 Hours 5,046 Hours
Total Cycles Since New 1,441 Cycles 1,441 Cycles
HSI Due / Overhaul Due On Condition
Program Coverage Rolls-Royce CorporateCare

APU:

Description Honeywell RE220
Serial Number P-216
APU Total Time Since New 3,768 Hours
Program Coverage Honeywell MSP

The Global Express is equipped with an integrated, Honeywell Primus 2000XP avionics suite. A general summary of this aircraft’s avionics suite is as follows:

 

Type of Unit Quantity Unit Description
EFIS (Electronic Flight Instrument System) Six-Tube Honeywell DU-870 Color EFIS Displays
FMS (Flight Management System) Triple Honeywell FMZ-2000 / NZ-2000
CDU (Central Display Unit) Triple Honeywell CD-820
IRS (Inertial Reference System) Triple Honeywell HG2001 (LASEREF IV)
GPS (Global Positioning System) Dual Honeywell HG2021 / GNSSU
ADC (Air Data Computer) Triple Honeywell AZ-840
NAV (Navigation Radio) Dual Honeywell RNZ-851 Integrated NAV Radios
DAU (Data Acquisition Unit) Quad Honeywell DA-810
IAC (Integrated Avionic Computer) Triple Honeywell IC-800 w/ Autopilot & Autothrottle
DME (Distance Measuring Equipment) Dual Honeywell RNZ-851 Integrated NAV Radios
HUD (Head Up Display) Single Thales / Sextant
EFB (Electronic Flight Bag) Dual CMC Electronic CMA-1410E
ADF (Automatic Direction Finder) Dual Honeywell RNZ-851 Integrated NAV Radios
VHF NAV (Very High Freq. Navigation) Dual Honeywell RCZ-851 w/ Mode S (8.33 kHz compliant)
VHF COM (Very High Freq. Communications) Single Honeywell RCZ-833 (8.33 MHz)
HF COM (High Freq. Communications) Dual Rockwell Collins HF-9031A
SATCOM (Satellite Communications) Single Honeywell SDU-600
SELCAL (Selective Calling System) Single Avtech CSD-714
WRADAR (Weather Radar) Single Honeywell Primus WU-880
RADAR ALT (Radar Altimeter) Dual Rockwell Collins ALT-4000
XPNDR (Transponder) Dual Honeywell RNZ-851 Integrated NAV Radios
GPWS (Ground Proximity Warning System) Single Honeywell Mark V
TCAS (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
ELT (Emergency Locator Transmitter) Single ACR Artex 406 w/ NAV Interface
LSS (Lighting Sensor System) Single Honeywell LSZ-860
Number of Passengers Eleven (11)
Galley Location Forward
Forward Cabin Configuration Two (2) Single Seats Facing Forward
Mid Cabin Configuration Four (4) Place Double Club and a One (1) Place Single Seat
Aft Cabin Configuration Two (2) Place Club Opposite a Two (2) Place Conference Group
*** Two Forward Conference Group Seats are Not Certified for Taxi, Take-Off, and Landing
Lavatory Location(s) Forward and Aft
Crew Rest Yes
Jumpseat Yes
Galley Equipment Microwave; High-Temperature Oven; Coffee Maker; and Air Chiller
Other Notable Feature(s) Footrest on Single Seats; and Cabin Humidifier System

ENTERTAINMENT:

Display / TV Monitor(s) Dual 18.0” Bulkhead Monitor and 15.0” Bulkhead Monitor
Airshow System Airshow Genesys
Cabin Management System Baker
Phone System Magnastar C-2000
Other Notable Feature(s) CD / DVD Player
Base Paint Color(s) Matterhorn White
Stripe Color(s) None

MAJOR INSPECTION STATUS:

Inspection Last Performed Next Due
15 Month November 2016 January 2018
30 Month April 2015 January 2018
60 Month July 2013 March 2018
120 Month July 2013 July 2023

OTHER NOTABLE FEATURES:

SB 700-11-016 – Increased Maximum Take-Off Weight to 98,000 lbs.
SB 700-23-003 – Office in the Sky
SB 700-23-005 – Airborne Data Link System
SB 700-31-030 – Batch 3 Software Upgrade
SB 700-34-053 – FANS 1/A+ and RNP 4
SB 700-34-054 – SBAS with LPV Approach Capability
SB 700-34-062 – Automatic Dependent Surveillance – Broadcast Out (ADS-B Out)
ST02406LA – TCAS 7.1
Securaplane 500

 

WEIGHTS:

Gross Weight (Ramp) 98,250 lbs.
Max Takeoff Weight 98,000 lbs.
Max Landing Weight 78,600 lbs.
Empty Weight 49,863 lbs.
Basic Operating Weight 52,500 lbs.