Posted May 18, 2017 at 8:31 pm by Jetcraft

2010 Bombardier Challenger 605 S/N 5816

2010 Bombardier Challenger 605 S/N 5816 | 1,285 Hours; 499 Cycles | 12 Passenger Configuration | ADS-B Out & RAAS Enabled


Total Time Since New1,312Hours (As of February 3, 2017)
Total Landings Since New511 Cycles
Entry into service date12 June 2010
Home BaseHong Kong, Hong Kong
Maintenance TrackingCAMP
CertificationFAR Part 91


Left EngineRight Engine
DescriptionGeneral Electric CF34-3B
Serial Number(s)950851950852
Total Hours Since New1,312 Hours1,312 Hours
Total Cycles Since New511 Cycles511 Cycles
Program CoverageGE Aviation GE OnPoint


DescriptionHoneywell GTCP36-150 (CL)
Serial NumberP-262
APU Total Time Since New2,426 Hours


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 UnitQuantityDescription
EFIS (Electronic Flight Instrument System)FourAFD 5022 Adaptive Flight Displays
ESIS (Electronic Standby Instrument System)SingleIntegrated Stand-by Instruments
FMS (Flight Management SystemDualFMC-6000 Flight Management Systems
IRS (Inertial Reference System)DualHoneywell Laseref V
GPS (Global Positioning System)DualCollins GPS-4000 Navigation Units
ADC (Air Data Computer)DualCollins ADC-850E Air Data Computers
NAV (Navigation Radio)DualCollins NAV-4000
DME (Distance Measuring Equipment)DualCollins DME-4000
ADF (Automatic Direction Finder)DualCollins ADF-462
A/P (Autopilot)DualHoneywell Autopilot system with Auto-throttle
VHF COM (Very High Freq. Communication)TripleCollins HF-4000 VHF Communication System
HF COM (High Freq. Communications)DualCollins HF-9031A with SELCAL
SATCOM (Satellite Communications)SingleICG ICS-200 Iridium System
AFIS (Airborne Flight Information System)SingleIntegrated Flight Information System
RADARSingleCollins RTA-854
RADAR ALT (Radar Altimeter)SingleCollins ALT-4000 Radio Altimeter
XPNDR (Transponder)Dual Collins TDR-94-D Mode S Transponders
EGPWS (Enhanced Ground Proximity Warning System)SingleHoneywell Mark V EGPWS w/TAWS
RAAS (Runway Awareness and Advisory System)SingleHoneywell Mark V
TCAS (Traffic Collision Avoidance System)SingleCollins TTR-4000 TCAS
CVR (Cockpit Voice RecorderSingleL3 Communications CVR
FDR (Flight Data Recorder)SingleL3 Communications FDR
ELT (Emergency Location Transmitter)SingleArtex 406


Number of PassengersTwelve (12)
Galley LocationForward
Forward Cabin ConfigurationFour (4) Place Double Club w/ Pull-Out Tables
Aft Cabin ConfigurationFour (4) Place Conference Grouping Opposite a Four (4) Place Divan
Lavatory Location(s)Aft w/ Inflight Access to Baggage
Galley EquipmentTIA Microwave Oven; TIA Convection Oven; and TIA Coffee Maker
Other Notable Feature(s)Iridium ICG ICS-200 In Flight Phone System


Base Paint Color(s)Overall Matterhorn White
Stripe Color(s)Astra Blue and Sapphire Blue Accent


Display / TV Monitor(s)Dual Bulkhead LCD Monitors
Airshow SystemInflight Entertainment System
Other Notable Feature(s)Dual DVD / CD / MP3 Player; 115VAC Outlets; and Multi-Function Printers


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

Major Inspection Status:

InspectionLast PerformedNext Due
400 Hour Inspection1,196 hours1,596 hours
600 Hour Inspection1,035 hours1,635 hours
800 Hour Inspection713 hours1,513 hours
1,600 Hour Inspection0 Hours1,600 Hours
24 Month InspectionJune 2016June 2018
36 Month InspectionJune 2016June 2019
48 Month InspectionJune 2014June 2018
96 Month InspectionJune 2010June 2018

Other Equipment:

Engine Instrument / Crew Alerting System (“EICAS”)
3D Mapping and Long Range Cruise
Lightning Detection System (“LDS”)


Gross Weight (Ramp)48,300 lbs.Max Zero Fuel Weight32,000 lbs.
Max Takeoff Weight48,000 lbs.Empty Weight26,299 lbs.
Max Landing Weight38,000 lbs.Typical Basic Operating Weight32,000 lbs.


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