The Bombardier Global Express XRS cor...
Challenger 300 For Sale
2007 Challenger 300 For Sale
AIRFRAME: Total Time: 1185.0 Hrs.
Total Landings: 470
ENGINES: Honeywell HTF-7000
L Engine: 1185.0 TSN, 478 CSN
R Engine: 1185.0 TSN, 478 CSN
APU: Honeywell GTCP36-150BD: 1130.0 TSN
Four-screen display, all EFIS, Collins Pro Line 21 avionics suite
The Bombardier Challenger 300 is a super-mid-sized jet capable of traversing transcontinental distances. The forward cabin features a cabin pocket door between the galley and seating area. Forward four place leather club. Aft left side three place divan opposite 2 single leather seats. Forward right side galley with sink, microwave & coffee maker. Entertainment center features Dual 20” monitors, Dual CD/ DVD Players & Airshow with superior soundproofing. Aft belted lav.
Communications & Navigation
Dual VHF Communications Radio (8.33 KHz channel
spacing)
Third VHF Communication Option
Dual Mode S Transponder
Dual Cockpit Audio Control Panel
Third Audio System
Triple Cockpit Audio Jack Panel
Dual Cabin/Ground/Crew Audio Jack Panel
Dual Cockpit Speakers
Dual VOR/ILS/MKR Navigation Receivers
Single DME Transceiver
Second Distance Measuring Equipment (DME)
Single ADF Receiver
Second Automatic Direction Finder (ADF)
Single GPS Receiver
Second Global Positioning System (GPS)
Dual Radio Interface Unit
Dual HF Communication with SELCAL
Displays/Core Elements
Single Integrated Avionics Processing Cabinet
Four Tube Cockpit Display Unit
Single Clock
Single Integrated Standby Instrument
Dual Display Selection Panel
Single Reversion Control Panel
EICAS
Single Data Concentrator Unit
Single Remote Data Concentrator
Single EICAS Control Panel
ELT
Single Emergency Locator Transmitter (121.5, 243.0
and 406.025 MHz)
Flight Control
Dual Automatic Flight Control Function
Single Flight Guidance Panel
Triple Servos
Datalink with Weather Maps
Datalink with Selective Calling Option, Universal
Weather for IFIS
IFIS
Dual IFIS with Enhanced Map Graphics on MFD
Electronic Charts
Universal Weather
DBU 5000
IFIS and Rockwell Collins Dataload
Flight Management
Single FMS Function
Second Flight Management System (FMS)
Dual FMS V-Speed
Maintenance System
Single Maintenance Function
Radio Altimeter
Single Radio Altimeter
Dual Radio Altimeter Antenna
Recording Systems
Single Cockpit Voice Recorder (120 minutes)
Flight Data Recorder (FDR)
Sensors
Dual Air Data Computers
Single Pitot Probe
Dual Pitot Static Probes
Dual Attitude Heading Reference Units
Dual Flux Detectors
Single Standby Compass
Single Enhanced GPWS
Dual Static Ports
TCAS
Single TCAS II (Change 7.0) Receiver/Transmitter
System
WXR
Single 14” WXR Transmitter/Receiver w/dual scan
Others
Single Stall Computer
Dual Stick Shaker
Single Stick Pusher
Dual AOA Vanes
Over Water Flight Kit
Cockpit Writing Tables
Exterior Equipment Package
Airborne Telephone System: A dual channel SATCOM telephone system including one (1) wireless handset with
base located in the cabin (at the right hand forward facing seat and one (1) spare handset, and one (1) wired handset
installed in the cockpit..
The navigation system includes the following components:
· Air Data System (ADS) – Two (2) digital air data computers are installed. The air data computer uses pitot static
and temperature measurements to compute operating parameters such as pressure altitude, altitude rate, indicated
airspeed, Mach number, vertical speed, maximum operating speed, current barometric correction, and true
airspeed.
· Datalink with Weather Maps - Provides flight crews with graphical weather capability in addition to
the Datalink system, which provides textual information utilizing the Aircraft Addressing and
Reporting System (ACARS) network. The graphical weather products available are: NEXRAD,
NEXRAD with echo tops and movement, weather depiction, wind and temperature forecasts, icing
forecasts and turbulence forecasts. Three different Datalink plans are available from the service
provider.
· Integrated Flight Instrument System (IFIS) –The dual FSU configuration provides the redundancy
required for a chartless capable cockpit. Each FSU enables independently displayed electronic
charts on each MFD. The FSU IFIS can present ground reference information, approach charts,
standard instrument departures (SIDs), standard terminal arrival routes (STARs) and airport surface
charts.
· Enhanced Map Overlays - Provides the display symbology for geo-political boundaries (state and
country boundaries, major water surfaces), airways (high and low altitude) and restricted airspaces
on the two Multi-Function Displays (MFDs). A database subscription, supplied by Rockwell
Collins, is required in order to maintain an up-to-date Enhanced Map Overlays database. The
Geographical (World Wide Coverage) database is updated every 2nd year. The Airspace/Airways
(World Wide Coverage) database is updated every 28 days
· Electronic Flight Instrument System (EFIS) –The EFIS fully integrates the EICAS functions (engine
instrument, crew alerting and synoptic pages).
· Weather Radar – Color weather radar is installed. The radar also provides a ground mapping function.
Enhanced Weather Radar (exchange)
· Radio Altimeter – One (1) radio altimeter is installed with data displayed on the PFD.
· Attitude And Heading Reference System (AHRS) – Two (2) independent Attitude and Heading Reference
Systems (AHRS) are installed. Each system is able to provide aircraft attitude, rate and acceleration information
to the EFIS, AFCS and other systems.
· Very High Frequency (VHF) Navigation – Two (2) VOR/ILS VHF navigation receivers are installed in the
aircraft. Both systems are tuned by the integrated radio tuning system. Dual HF Communication with SELCAL
· Automatic Direction Finder (ADF) – A single Automatic Direction Finder (ADF) is installed. The receiver is
tuned via the integrated tuning system. Second Automatic Direction Finder (ADF)
· Distance Measuring Equipment (DME) – A single Distance Measuring Equipment (DME) transponder is
installed. The DME is tuned via the integrated radio tuning system.
· Global Positioning System (GPS) – A single GPS sensor, meeting the requirements of TSO c129, Class B1
requirements, is installed. Second Global Positioning System (GPS)
· Flight Management System (FMS) – A single Flight Management System (FMS) is installed. A single data
loader is provided. The FMS is able to load information from, and download information to, the data loader.
Major functions of the FMS include:
Second Flight Management System (FMS)
Dual FMS V-Speed
Fully coupled lateral and vertical navigation (with interface to the flight director)
Flight planning (with worldwide database)
Blended radio navigation (GPS, VOR, DME, etc.)
Fuel performance computing
Remote radio tuning
ACARS management and display (option)
Interior:
Floorplan 4 - Divan in Aft Left-Hand Position
Premium Carpet
Real Wood Veneer
16 G Belted Toilet Seat
L/H Forward Pyramid Cabinet
R/H Aft Pyramid Cabinet
Forward Partition with Sliding Door
Dado Storage Boxes (6)
