2007 Bombardier Challenger 605 for sale, Mexico

Service Bulletin Description
SB 605-34-019 REV 3 Installation of Pro-Line 21 Advanced
SB 605-23-008 REV 3 FANS Encryption Key Upload
SB 605-34-030 REV 1 Installation of ADS-B Version 2
SB 605-34-011 REV 4 Install WAAS
SB 605-34-018 Modification TCAS Change 7.1 Upgrade
SB 60534-020 REV 5 Modification Synthetic Vision System (SVS)
SB 605-23-002 REV 5 Install Datalink System
SB 605-23-007 REV 3 Datalink upgrade for Eurocontrols Link 2000+
SB 605-23-011 REV 3 Installation of Iridium SATCOM
SB 605-23-012 Upgrade 3rd VHF to meet Link 2000+ Requirements

The Challenger 605 is equipped with an integrated, Rockwell Collins Pro-Line 21 avionics suite. A general summary of this aircraft’s avionics suite is as follows:

Type of Unit Quantity Description
EFIS (Electronic Flight Instrument System) Four 10x12 LCD Adaptive Flight Displays
ESIS (Electronic Standby Instrument System) Single Integrated Stand-by Instruments
FMS (Flight Management System Dual Collins FMS-6000
IRS (Inertial Reference System) Single Honeywell Laseref V
GPS (Global Positioning System) Dual Collins GPS-4000
ADC (Air Data Computer) Dual Collins ADC-850E
NAV (Navigation Radio) Dual Collins NAV-4000
DME (Distance Measuring Equipment) Dual Collins DME-4000
ADF (Automatic Direction Finder) Dual Collins ADF-400
A/P (Autopilot) Dual Honeywell Autopilot system with Auto-throttle
SVS (Synthetic Vision System) Single
VHF COM (Very High Freq. Communications) Dual Collins HF-4000 VHF
HF COM (High Freq. Communications) Dual Collins HF-9031A with SELCAL
SATCOM (Satellite Communications) Single ICG ICS-200 Iridium System
AFIS (Airborne Flight Information System) Single Integrated Flight Information System
RADAR Single WXR-854 Color Weather Radar
RADAR ALT (Radar Altimeter) Single Collins ALT-4000
XPNDR (Transponder) Dual Collins TDR-94-D with Mode S
GPWS (Ground Proximity Warning System) Single Honeywell Mark V EGPWS w/TAWS
TCAS (Traffic Collision Avoidance System) Single Collins TTR-4000 TCAS II w/Change 7.1
ELT (Emergency Location Transmitter) Single Artex 406 ELT
CVR (Cockpit Voice Recorder) Single L3 Communications CVR
FDR (Flight Data Recorder) Single L3 Communications FDR
3D Map and Long Range Cruise
LDS (Lighting Detection System)
Enhanced Maps on MFD

Description
Number of Passengers Nine (9)
Galley Location Forward
Fwd Cabin Configuration Four (4) place club
Aft Cabin Configuration Three (3) place berthable divan opposite two (2) executive seats
Lavatory Location(s) Aft Fully Enclosed Lavatory
Jumpseat Yes
Removable mid cabin curtain
Refurbished June 2018 (Duncan Aviation)


ENTERTAINMENT
Type of Unit Description
Display/TV Monitor(s) Two 18” monitors
Airshow System Airshow ASX
DVD Player(s) Dual DVD/CD/MP3 Players
Other Notable Features 2 Additional Cabin Outlets & 115V 60Hz Converter

Base Paint Color(s) White
Stripe Color(s) Red and Silver
Last Painted Date June 2018 (Duncan Aviation)

Aft Equipment Storage Box
Additional Magazine Rack
2nd Refuel/Defuel Panel
Main Wheel Storage
Avionics Bay Light
Maintenance Ladder
External Compartments Lights
Entry Light on/Off Switch

WiFi

No