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Posted May 19, 2017 at 12:07 am by Jetcraft

2009 Bombardier Global XRS S/N 9306

2009 Bombardier Global XRS S/N 9306 | 2,328 Hours; 937 Landings | Full Batch 3 Upgrade | HUD/EVS, Increased MTOW

Airframe:

Total Time Since New2,328 Hours (as of 19 June 2016)
Total Landings Since New937 Landings
Entry into service date7 October 2009
Home BaseLuxembourg
Maintenance TrackingCAMP
Program CoverageN/A
CertificationConformed for EASA EU-OPS and FAR Part 91 operations

Engines:

Left EngineRight Engine
DescriptionRolls Royce BR710-A2-20
Serial Number(s)1272912728
Total Hours Since New2,328 Hours2,328 Hours
Total Cycles Since New937 Cycles937 Cycles
Overhaul DueOn Condition
Program Coverage N/A

APU:

DescriptionHoneywell RE220 (GX)
Serial NumberP-431
APU Total Time Since New3,124 Hours
Program CoverageN/A

Avionics:

The Global XRS is equipped with a fully integrated Honeywell Primus 2000XP avionics suite. A general summary of this aircraft’s avionics suite is as follows (Items in bold indicate optional/added equipment):

Type of UnitQuantityDescription
EFIS (Electronic Flight Instrument System)6-TubeDU-870 Color Displays
ESIS (Electronic Standby Instrument System)SingleThales IESI
FMS (Flight Management System)TripleHoneywell FMZ-2000
IRS (Inertial Reference System)TripleHoneywell Laseref
GPS (Global Positioning System)DualHoneywell HG2021Sensor Unit
MADC (Micro Air Data Computer)TripleHoneywell AZ-840
DME (Distance Measuring Equipment)DualHoneywell RNZ-851
EVS (Enhanced Vision System)SingleBombardier EVS
HUD (Head Up Display)SingleThales/Sextant Head Up Display
ADF (Automatic Direction Finder)DualHoneywell RNZ-851
AUTOPILOTSingleHoneywell IC-800
VHF COM (Very High Freq. Communication)DualHoneywell Primus RCZ833K
HF COM (High Freq. Communications)DualCollins HF-9031A
SATCOM (Satellite Communications)SingleCollins SAT-6100
VOR NAV / ILS / MARKERDualHoneywell RNZ-851A
RADARSingleHoneywell WU-880
RADIO ALT (Radio Altimeter)DualCollins ALT-4000
XPNDR (Transponder)DualHoneywell RNZ-851 Mode S
EGPWS (Enhanced Ground Proximity Warning System)SingleHoneywell Mark V w/Windshear
TCAS II (Traffic Collision Avoidance System)SingleHoneywell TCAS 2000 w/ Change 7.1
CVR (Cockpit Voice RecorderSingleAllied Signal SCVR
FDR (Flight Data Recorder)SingleAllied Signal SSFDR

Interior:

Description
Number of PassengersTen (10)
Galley LocationForward
Fwd Cabin ConfigurationThree Place 9G Divan opposite two (2) executive club seats with foldout tables
Mid Cabin Configuration4-place electric Hi-Lo conference group opposite a workstation with narrow seat
Aft Cabin Configuration3-place 16G berthing divan opposite one (1) executive club seat
Lavatory Location(s)Forward crew lavatory and fully enclosed aft lavatory with storage cabinet
Crew AreaForward
JumpseatYes
 
Galley Equipment:TIA WAVEJET microwave oven, TIA high temperature oven, AEROLUX Nespresso

Exterior:

Base Paint Color(s)Overall silver fuselage
Stripe Color(s)Black and White accent stripe running from nose to tail and on the vertical stabilizer
Last Painted DateOriginal

Entertainment:

Type of UnitDescription
Display/TV Monitor(s)Two (2) Bulkhead-mounted 18”  LCD Monitor
Individual MonitorsThree (3) Plug-in 10.4”  touch screen LCD monitors
Airshow SystemInteractive ASXi In-Flight Information System (moving map)
CD/DVD Player(s)Multi-region CD/DVD Players combined unit
Portable Multimedia Input Port (RCA Jack)
Laptop Imagery Display on Bulkhead Monitor
Satellite TVMechanical & Wiring Provision Only (Airshow Tailwind 500)

Range:

Click here to view the online range map. To receive a more detailed custom range report including detailed aircraft comparisons, contact us at +1 919 941 8400 or info@jetcraft.com.

Major Inspection Status:

InspectionLast PerformedNext Due
15 Mo. Check7 MAR 20167 JUN 2017
30 Mo. Check16 NOV 201416 MAY 2017
60 Mo. Check16 NOV 201416 NOV 2019
120 Mo. Check7 OCT 2019

Other Equipment:

Type of UnitType of Unit
Provision for CVR DatalinkWind Shear Escape Guidance & CES software path
Airborne Data Link System (ADLS)Miltope Cockpit Printer
Honeywell LSZ-860 Lightning Sensor System (LSS)Quick Access Recorder (QAR)
Autopilot Emergency Descent ModeSecuraplane 500 w/Camera system and Video Recorder
Dual Electronic Flight Bags (EFBs)Passenger Address (PA) System
Global Office
Refuel/Defuel Control PanelOperations at Airports with Maximum Weight Restrictions
Logo Light, Ext. Baggage Door Lock Override, EICAS “Small Serv Door” Annunciation, Aircraft ID Plate, APU Hour MeterTowbar Assembly
Catwalk Battery AccessHandrail Extension
MEDECO Common Key Panels, Lockable Fuel CapMulti-Purpose Ladder
Aft Equipment Bay Storage BoxAesthetic Side Covers on Main Entry Door
Cabin Bus DisconnectGround Service Cabin Power
One (1) 3500 VA/230VAC/50Hz power converter230V AC 50Hz GFI protected utility outlets

Navigation and Compliance:

RVSMRNP 10
MNPSFM Immunity
RNP 58.33 Com

Weights:

Gross Weight (Ramp)99,750 lbsMax Fuel Capacity45,050 lbs
Max Takeoff Weight99,500 lbsMax Zero Fuel Weight56,000 lbs
Max Landing Weight78,600 lbsBasic Operating Weight52,784 lbs

Connectivity:

Type of UnitDescription
High Speed InternetThree (3) channels Aero H+ (2 voice and 1 Data). Data channel supports ACARS/maintenance functions
Wireless Ethernet LAN
In Flight PhoneSingle-channel ICS-100  Iridium Telephone SystemOne (1) corded and Three (3) Cordless Telephone Handsets
Cabin Printer/FaxPlain Paper

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