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  • Alert Me Name: Bombardier Challenger 604
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Bombardier Challenger 604
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    United States - CA, North America + Canada
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Aircraft Highlights

Fully Programmed

Aircell ATG-5000 WiFi

Precision Plus Avionics Upgrade

Two Interior Configurations (10 or 12 Passengers)

ADS-B Out // WAAS Installation Scheduled for August 2018


Total Time Since New 7,669.3 Hours (As of 2 July 2018)
Total Landings Since New 4,370 Landings
Entry into Service Date December 1999
Program Coverage Smart Parts Plus
Maintenance Tracking CAMP
Certification Currently Operated FAR Part 135


Left Engine Right Engine
Description General Electric CF-34-3B
Serial Number(s) 872543 872544
Total Hours Since New 7,669.3 Hours 7,619.6 Hours
Total Cycles Since New 4,371 Cycles 4,345 Cycles
HSI Due/Overhaul Due On Condition
Program Coverage GE OnPoint


Description Honeywell GTCP 36-150 (CL)
Serial Number P-615C
APU Total Time Since New 5,844.2 Hours
HSI Due/Overhaul Due On Condition
Program Coverage MSP


Gross Weight (Ramp) 48,300 lbs Max Zero Fuel Weight 32,000 lbs
Max Takeoff Weight 48,200 lbs (Increased) Empty Weight 27,849 lbs
Max Landing Weight 38,000 lbs Basic Operating Weight 28,300 lbs
Inspection Last Performed Next Due
36 Month Scheduled for August 2018 August 2021
48/96/192/240 Month August 2015 See CAMP
The Challenger 604 is equipped with an integrated, Rockwell Collins Pro Line 4 (with Precision Plus upgrade) 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 EFD 4077 EFIS/MFD Displays
FMS (Flight Management System) Dual Collins FMC-6000
GPS (Global Positioning System) Dual GPS-4000
IRS (Inertial Reference System) Dual Litton LTN-101
DCU (Data Concentrator Unit) Single Collins DCU 4000
ADC (Air Data Computer) Dual ADC-850E
NAV (Navigation Radios) Dual Collins VIR 432 Nav. System w/ FM Immunity
DME (Distance Measuring Equipment) Dual Collins DME 442
ELT (Emergency Locator Transmitter) Single Artex 406 ELT
ADF (Automatic Direction Finder) Dual Collins ADF 462
EICAS (Engine Instrument/Crew Alerting System) Single
VHF COM (Very High Freq. Communication) Dual Collins VHF-422B w/ 8.33 Spacing
HF COM (High Freq. Communications) Dual Collins HF-9031 HF w/ SELCAL
SATCOM (Satellite Communications) Single Collins 906 Six-Channel SATCOM System
RADAR (Weather Radar) Single Collins WXP 4220 Split Scan Weather Radar w/ Dual Controllers
RADIO ALT (Radio Altimeter) Single ALT-55B
XPNDR (Transponder) Dual Dual Collins TDR-94D Mode S Transponders (Enhanced Surveillance)
EGPWS (Enhanced Ground Proximity Warning System) Single Honeywell MK-V (Enhanced Version)
TCAS (Traffic Collision Avoidance System) Single Collins TTR-920 TCAS II w/ Change 7.1
CVR (Cockpit Voice Recorder) Single Fairchild A-100S
FDR (Flight Data Recorder) Single Fairchild F-1000
Type of Unit Description
WiFi Aircell ATG-5000 WiFi
Airshow Airshow 400
Cabin Entertainment System Audio International (CD Changer, DVD & VCR)
Display/TV Monitor(s) Fwd/Aft Mounted 20” Monitors;
Four (4) 8.4” Plug-in Monitors

Number of Passengers Twelve (12) OR Ten (10) Passenger
Galley Location Forward
Fwd Cabin Configuration Four (4) Place Executive Club
Aft Cabin Configuration A. 12 Passenger Configuration: Four (4) Place Conference Group with Hi-Lo Table Opposite Four (4) Place Divan

B. 10 Passenger Configuration: Aircraft Will Deliver with Optional Two (2) Place Club which may be Installed Opposite Four (4) Place Divan
Lavatory Location Aft (Small)
Baggage Aft Large L-Shaped Compartment
Jumpseat Forward
Other Notable Features Fireblocked; 115 VAC/60 Hz Standard US Outlets; Microwave and Convection Ovens
Last Interior Date Original Completion; Interior Recovered December 2011

Base Paint Color(s) Overall Matterhorn White
Stripe Color(s) Blue and Red Accent Stripes
Last Painted Date March 2008

Bombardier Challenger 604

Make Offer
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    United States - CA, North America + Canada
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