For Sale: 2010 BOMBARDIER GLOBAL XRS
Jet Aircraft
Recently Completed 180-Month Inspection, Starlink Install and New Carpet – c/w in May 2025 by West Star Aviation
Engines Enrolled on Rolls Royce Corporate Care
APU Enrolled on JSSI
HUD & EVS
Synthetic Vision System
Batch 3.4 FMS Upgrade
KA-Band Internet
Increased MTOW 99,500 LBS
Certification Date March 2010
Primus Elite DU-875 Avionics Upgrade including ADS-B, FANS 1A, & WAAS
Detailed Information
Airframe
Total Time Since New: 5,065.4 Hours
Total Landings Since New: 1,694 Cycles
Engines
E N G I N E D E T A I L S
Engines Enrolled on Rolls Royce Corporate Care
| Engine | Model | Serial Number | Time Since New | Cycles Since New |
|---|---|---|---|---|
| Left | Rolls Royce BR-700-710A2-20 | 12791 | 5,065.4 Hours | 1,696 Cycles |
| Right | Rolls Royce BR-700-710A2-20 | 12790 | 5,065.4 Hours | 1,697 Cycles |
A U X I L I A R Y P O W E R U N I T
APU Enrolled on JSSI
Honeywell RE-220 (GX)
Serial Number: P-465
Total Time Since New: 4,636 Hours
Interior Details
ADS-B Out: Automatic Dependent Surveillance – Broadcast Out
CPDLC: Controller Pilot Data Link Communications
FANS 1/A: Future Air Navigation System
WAAS: Wide Area Augmentation System
MNPS: Minimum Navigation Performance Specifications
RNP 4: Require Navigation Performance 4
RVSM: Reduced Vertical Separation Minimum
Exterior Details
New Paint – October 2020
Matterhorn White with Medium Gray and Granite Accents
Avionics
EFIS (Electronic Flight Instrument System): Six Tube Honeywell DU-875 Color Displays w/ Jeppesen Charts & Maps
FMS (Flight Management System): Triple Honeywell CD-820
FLT DIR (Flight Director): Primus 2000XP IFCS w/ Triple IC-800
GPS (Global Positioning Device): Dual Honeywell HG-2021
EFB (Electronic Flight Bag): Dual Class II
Navigation Radio: Dual Honeywell RNZ-851
SVS (Synthetic Vision System): Dual Honeywell
EVS (Enhanced Vision System): GT546-001-7
HUD (Heads-Up Display): GT546-001-7
Autopilot: Dual Honeywell IC-800
VHF Com (Very High Frequency Communication): Triple Honeywell RCZ-833M
HF Com (High Frequency Communication): Dual Rockwell Collins HF-9031A w/ SELCAL CSD-714
ELT (Emergency Locator Transmitter): Artex 406 ELT
Radar: Honeywell Primus WU-880
EGPWS (Enhanced Ground Proximity Warning System): Honeywell
TCAS (Traffic Collision Avoidance System): ACSS TCAS-2000 w/ Change 7.1
LSS (Lighting Sensor System): Honeywell LP-860
CVR (Cockpit Voice Recorder): Honeywell 980-6022-001
FDR (Flight Data Recorder): Honeywell 980-4700-041
Fuel Capacity
WEIGHTS:
Max Take Off Weight: 99,500 lbs.
Max Landing Weight: 78,600 lbs.
Basic Operating Weight: 52,653 lbs.
Max Fuel Weight: 44,716 lbs.
Payload at Max Fuel: 2,408 lbs.
Condition
MAINTENANCE STATUS:
180-Month Inspection c/w May 2025
Batch 3.4 FMS Upgrade
Engines enrolled on Rolls Royce Corporate Care
APU enrolled on Honeywell JSSI
Maintenance tracked by CAMP
120-Month Next Due August 2030
240-Month Next Due August 2030
500 Hour Check Next Due at 5202 Hours
750 Hour Check Next Due at 5575 Hours
1000 Hour Check Next Due at 5683 Hours
1500 Hour Check Next Due at 3233 Hours
2250 Hour Check Next Due at 5983 Hours
3000 Hour Check Next Due at 5969 Hours
4500 Hour Check Next Due at 8991 Hours
Equipment
ADS-B Out: Automatic Dependent Surveillance – Broadcast Out
CPDLC: Controller Pilot Data Link Communications
FANS 1/A: Future Air Navigation System
WAAS: Wide Area Augmentation System
MNPS: Minimum Navigation Performance Specifications
RNP 4: Require Navigation Performance 4
RVSM: Reduced Vertical Separation Minimum
