2009 Bombardier Global XRS
Price: Call for Price
- Serial Number: 9276
- Hours: 4,011
- Cycles: 1,373
- 4,011 Hours; 1,373 Landings
- Fully Enrolled on Programs
- DU-875 Display Upgrade
- KA-Band
- Thirteen Passenger Configuration
- Fully Enrolled on Programs
- DU-875 Display Upgrade
- KA-Band
- Thirteen Passenger Configuration
Airframe
Total Hours:
4,011
Total Cycles:
1,373
Maintenance Tracking:
CAMP
Program Coverage: JSSI
Engines
Rolls Royce BR700-710A2-20
Engine Program Coverage:
Rolls Royce Corporate Care Enhanced
Engine 1
Serial Number:
12665
Hours Since New:
3,917
Cycles Since New:
1,344
Engine 2
Serial Number:
12664
Hours Since New:
3,917
Cycles Since New:
1,344
APU
Description:
Honeywell RE220
APU Program Coverage:
MSP
Serial Number:
P-399
Total Time Since New:
5,898
Avionics
The Bombardier Global XRS 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-875
FMS (Flight Management System) Triple Honeywell NZ-2000
CDU (Central Display Unit) Triple Honeywell CD-820
IRS (Inertial Reference System) Triple Honeywell LASEREF IV
GPS (Global Positioning System) Dual Honeywell
MADC (Micro Air Data Computer) Triple Honeywell AZ-950
NAV (Navigation Radio) Dual Honeywell RZ-851
DAU (Data Acquisition Unit) Quad Honeywell DA-810
IAC (Integrated Avionic Computer) Triple Honeywell IC-810
HUD (Head Up Display) Single Bombardier Head Up Display
EVS (Enhanced Vision System) Single Bombardier Enhanced Vision System
VHF COM (Very High Freq. Communications) Triple Honeywell RCZ-833M (Dual) and RCZ-833 (Single)
HF COM (High Freq. Communications) Dual Collins HF-9031A
SATCOM (Satellite Communications) Single Collins SRT-2100
SELCAL (Selective Calling System) Single Avtech CSD-714
WRADAR (Weather Radar) Single Honeywell WU-880
RADAR ALT (Radar Altimeter) Dual Collins ALT-4000
XPNDR (Transponder) Dual Honeywell RZ-851
EGPWS (Enhanced Ground Proximity Warning System) Single Honeywell Mark V EGPWS
TCAS (Traffic Collision Avoidance System) Single ACSS RT-950 TCAS
CVR (Cockpit Voice Recorder) Single
s Honeywell SSCVR
FDR (Flight Data Recorder) Single Honeywell SSFDR
ELT (Emergency Locator Transmitter) Single Artex 406
LSS (Lighting Sensor System) Single Honeywell LP-860
Type of Unit Quantity Unit Description
EFIS (Electronic Flight Instrument System) Six-Tube Honeywell DU-875
FMS (Flight Management System) Triple Honeywell NZ-2000
CDU (Central Display Unit) Triple Honeywell CD-820
IRS (Inertial Reference System) Triple Honeywell LASEREF IV
GPS (Global Positioning System) Dual Honeywell
MADC (Micro Air Data Computer) Triple Honeywell AZ-950
NAV (Navigation Radio) Dual Honeywell RZ-851
DAU (Data Acquisition Unit) Quad Honeywell DA-810
IAC (Integrated Avionic Computer) Triple Honeywell IC-810
HUD (Head Up Display) Single Bombardier Head Up Display
EVS (Enhanced Vision System) Single Bombardier Enhanced Vision System
VHF COM (Very High Freq. Communications) Triple Honeywell RCZ-833M (Dual) and RCZ-833 (Single)
HF COM (High Freq. Communications) Dual Collins HF-9031A
SATCOM (Satellite Communications) Single Collins SRT-2100
SELCAL (Selective Calling System) Single Avtech CSD-714
WRADAR (Weather Radar) Single Honeywell WU-880
RADAR ALT (Radar Altimeter) Dual Collins ALT-4000
XPNDR (Transponder) Dual Honeywell RZ-851
EGPWS (Enhanced Ground Proximity Warning System) Single Honeywell Mark V EGPWS
TCAS (Traffic Collision Avoidance System) Single ACSS RT-950 TCAS
CVR (Cockpit Voice Recorder) Single
s Honeywell SSCVR
FDR (Flight Data Recorder) Single Honeywell SSFDR
ELT (Emergency Locator Transmitter) Single Artex 406
LSS (Lighting Sensor System) Single Honeywell LP-860
Inspections
Inspection Type
Performed
Next Due
15 Month
Performed:
August 2024
Next Due:
October 2025
30 Month
Performed:
August 2024
Next Due:
September 2026
60 Month
Performed:
August 2024
Next Due:
March 2029
120 Month
Performed:
May 2019
Next Due:
March 2029
Additional Equipment/Features
SB700-11-020 – Increased Maximum Take-Off Weight (MTOW) to 99,500 lbs.
SB700-31-034 – Batch 3.3 Avionic Software Upgrade
SB700-34-053 – FANS 1/A+ and RNP 4
SB700-34-054 – Introduction of SBAS with LPV Approach Capability
SB700-34-062 – ADS-B Out (DO-260B)
External Camera System
SB700-31-034 – Batch 3.3 Avionic Software Upgrade
SB700-34-053 – FANS 1/A+ and RNP 4
SB700-34-054 – Introduction of SBAS with LPV Approach Capability
SB700-34-062 – ADS-B Out (DO-260B)
External Camera System
Interior
Number Of Passengers:
13
Forward Galley: Yes
Forward Lavatory: Yes
Aft Lavatory: Yes
Interior Last Refurbished:
2024
Forward Cabin Configuration - Four (4) Place Double Club
Mid Cabin Configuration - Four (4) Place Conference Group Opposite One (1) Single Seat w/ Workstation
Aft Cabin Configuration - One (1) Place Single Seat w/ Entertainment Center Opposite a Three (3) Place Divan (When Bulkhead is removed)
Crew Rest - Forward
Jump Seat - Yes
Mid Cabin Configuration - Four (4) Place Conference Group Opposite One (1) Single Seat w/ Workstation
Aft Cabin Configuration - One (1) Place Single Seat w/ Entertainment Center Opposite a Three (3) Place Divan (When Bulkhead is removed)
Crew Rest - Forward
Jump Seat - Yes
Entertainment
High Speed Internet:
KA-Band
In-Flight Phone:
Iridium ICS-200 System
Exterior
Base Paint Colors:
Matterhorn White & Colonial Blue Belly
Stripe Colors:
Cyber Orange
Last Painted:
2019