2009 BOMBARDIER GLOBAL EXPRESS XRS

2009

BOMBARDIER

GLOBAL EXPRESS XRS

9276

Used

Engines Enrolled on Rolls-Royce CorporateCare DU-875 Display Upgrade KA-Band Thirteen Passenger Configuration

4104

1404

Entry into Service Date March 30, 2009 Program Coverage SmartParts Available Maintenance Tracking CAMP

CorporateCare Enhanced

12665

4010

SNEW

1375

Rolls Royce BR700-710A2-20

12664

4010

SNEW

1375

Rolls Royce BR700-710A2-20

Yes

Description Honeywell RE220 Serial Number P-399 APU Total Time Since New 6,045 Hours

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 Honeywell SSCVR FDR (Flight Data Recorder) Single Honeywell SSFDR ELT (Emergency Locator Transmitter) Single Artex 406 LSS (Lighting Sensor System) Single Honeywell LP-860

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

Base Paint Color(s) Matterhorn White and Colonial Blue Belly Stripe Color(s) Cyber Orange Last Painted May 2019 at Duncan Aviation

Number of Passengers Thirteen (13) Galley Location Forward 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) Lavatory Location(s) Forward Crew and Aft Executive Crew Rest Forward Jump Seat Yes Last Refurbishment August 2024 (Curtain and Lav Bulkhead) ENTERTAINMENT Display / TV Monitor(s) Single 31.5” Entertainment Monitor and Dual 24.0” Bulkhead Monitors Airshow System Collins Airshow w/ Moving Maps CONNECTIVITY Phone System Iridium ICS-200 System Internet KA-Band

Inspection Last Performed Next Due 15 Month Inspection November 2025 November 2026 30 Month Inspection August 2024 September 2026 60 Month Inspection August 2024 March 2029 120 Month Inspection May 2019 March 2029