2002 Global Express
Description
The Bombardier Global Express XRS is a long-range, intercontinental business jet manufactured by Bombardier Aerospace. The XRS was the second variant of the Global Express, following the original Global Express model. It was introduced in 2002, and featured an improved wing design, a higher maximum takeoff weight, and an increased range of 7,400 nautical miles. The XRS also features more powerful and fuel efficient engines, and a redesigned interior layout. Additionally, the XRS is capable of landing at shorter runways than the original Global Express. The Global Express XRS has been used by many governments, corporations, and wealthy individuals for long-distance travel.
Features
- Total Time: 8017 hrs
- Engine(s)
- Rolls Royce BR700-710A2-20
- TTSN: 7,915 / 8,017
- TSOH: 582 / 8,017
- SN: 12265 / 12264
- Engines on Condition
- Engines enrolled on Rolls-Royce Corporate Care
- Avionics
- AIRCRAFT COMMUNICATION ADDRESSING & RECORDING SYSTEM: Teledyne ACARS Airborne Data Link
- AIR DATA COMPUTERS: Triple Honeywell AZ-840 Micro Air Data Computers
- CONTROL DISPLAY UNITS: Triple Honeywell CDU 820’s, upgraded with video graphic capability
- CENTRAL AIRCRAFT INFORMATION MAINTENANCE SYSTEM: CAIMS version 7.1
- COCKPIT VOICE RECORDER: Honeywell SSCVR (120 minutes)
- COMMUNICATIONS: Dual Honeywell RCZ-833K and 3rd RCZ-853 VHF transceivers
- ELECTRONIC FLIGHT INSTRUMENT SYSTEM: Triple Honeywell IC-800 Integrated Avionics Computers (IAC) with
- six (6) 8” x 7” DU-870 color EFIS displays
- EMERGENCY LOCATOR TRANSMITTER: Artex 406 MHz ELT
- FLIGHT DATA RECORDER: Honeywell DFDR digital flight data recorder (256 wps)
- FLIGHT MANAGEMENT SYSTEM: Triple Honeywell FMS
- GLOBAL POSITIONING SYSTEM: Dual Honeywell GPS
- HIGH FREQUENCY: Dual Collins HF-9031A with SELCAL
- LIGHTNING DETECTION: Honeywell LSZ-860 Lightning Sensor System
- LONG RANGE NAVIGATION: Triple Honeywell Laseref IV
- NAVIGATION: Dual Honeywell RNZ-851 Integrated VHF Navigation radios with VOR/ILS/MKR/ADF/DME and FM
- Immunity
- RADIO ALTIMETERS: Dual Rockwell Collins ALT-4000 radio altimeters
- STANDBY INSTRUMENT: L3 GH-3000 Emergency standby indicator system
- TERRAIN AWARENESS AND WARNING: Honeywell Mark V EGPWS
- TRANSPONDERS: Dual Honeywell RCZ-833K Transponders with enhanced Mode S
- TRAFFIC COLLISION ALERT AVOIDANCE SYSTEM: Honeywell/ACSS RT-950 (TCAS II)
- WEATHER RADAR: Honeywell Primus 880 Color Radar
- Maintenance Status
- Batch 3.4 complied with November 26, 2019
- APU enrolled on Honeywell MSP
- Engines enrolled on Rolls Royce Corporate Care
- Date of Manufacture: December 2000
- Certification Date: January 30, 2002
- Completed at Bombardier Montreal: January 2002
- Current and operational on FAR §135
- Operated per FAR §91
- Maintenance tracked by CAMP
- CAIMS (version 7.1) with in-flight printing
- Features/Options
- ADS-B Out
- TCAS 7.1
- WAAS / LPV
- CPDLC
- ADS-C
- RVSM
- PRNAV
- RNP 4
- RNP 10
- Fans 1/A
- MNPS
- 8.33 Spacing / FM Immunity
- Optional Cabin Window
- Logo Lights
- Pilot and Co-pilot vision safe emergency vision assurance system (EVAS)
- Securaplane 450 Security System
- Liebherr Cabin Humidification System
- Bombardier Second Refuel Control Panel in the flight compartment
- Rechargeable Maglite flashlights
- Pilot and Co-pilot footrests
- 26 Gallon aft water tank
- Aft ultra violet water filter system
- Jumpseat audio panel
- New jumpseat installation 06/2014
Location
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