Posted May 18, 2017 at 7:40 pm by Jetcraft

2009 Bombardier Challenger 605 SN 5726

2009 Bombardier Challenger 605 S/N 5726 | 2,550 Hours; 1,108 Cycles | Engines & APU on Programs | RVSM Certification, TCAS 7.1

Airframe:

Total Time Since New 2,672 hours    (As of June 25th,, 2017)
Total Landings Since New 1,156 landings
Entry into Service Date 09 March 2009
Maintenance Tracking CAMP
Certification Currently Operated – EU OPS1

Engines:

Left Engine Right Engine
Description General Electric CF-34-3B
Serial Numbers 950605 950606
Total Hours Since New 2,672 hours 2,672 hours
Total Cycles Since New 1,156 cycles 1,156 cycles
HSI Due/Overhaul Due On Condition
Program Coverage JSSI

APU:

Description Honeywell GTCP 36-150(CL)
Serial Number P-176
APU Total Time Since New 2,906 hours
HSI Due/Overhaul Due On Condition
Program Coverage JSSI

Avionics:

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 (Unit Descriptions in bold indicate optional/added equipment):

Type of Unit Quantity Unit Description
EFIS (Electronic Flight Instrument System) Four 10” x 12” Flight Displays
ESIS (Electronic Standby Instrument System) Single Integrated Stand-by Instruments
FMS (Flight Management System) Dual Collins FMC-6000 w/ 3D Map/Long Range Cruise
IRS (Inertial Reference System) Triple Honeywell Laseref V
GPS (Global Positioning System) Dual Collins GPS-4000A
CDU (Control Display Unit) Dual Collins CDU-6200
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-462
A/P (Autopilot) Dual Honeywell Autopilot system w/ Auto-throttle
VHF COM (Very High Freq. Communication) Triple Collins VHF-4000
HF COM (High Freq. Communications) Dual Collins HF-9031A w/ Selcal
SATCOM (Satellite Communications) Single ICG ICS-200 Iridium System
AFIS (Airborne Flight Information System) Single Collins Pro Line 21
RADAR Single Collins RTA-854
RADAR ALT (Radar Altimeter) Single Collins ALT-4000
XPNDR (Transponder) Dual Collins TDR-94D
EGPWS (Ground Proximity Warning System) Single Honeywell Mark V w/ RAAS
TCAS (Traffic Collision Avoidance System) Single Collins TCAS-4000 w/ Change 7.1
ELT (Emergency Locator Transmitter) Single Artex C406-N
CVR (Cockpit Voice Recorder) Single L3 Communications
FDR (Flight Data Recorder) Single L3 Communications

Interior:

Description
Number of Passengers Ten (10) Passengers
Galley Location Forward
Forward Cabin Configuration Four (4) place Club
Aft Cabin Configuration Tow (2) place Club opposite a four (4) place partial berthing Divan
Lavatory Location Aft
Jumpseat Yes
 
Galley Equipment:
Microwave TIA Microwave Oven
High Temp Oven TIA High Temperature Oven
Coffee/Espresso Maker Nespresso Coffee Maker
Other Notable Features Redi Hot Dispenser, Water Heater

Exterior:

Base Paint Color Matterhorn White
Stripe Colors Silver (metallic) & Aristo Blue
Last Painted Date August 2011

Entertainment:

Type of Unit Description
Display/TV Monitors 2 x 20” Monitors
Airshow System Airshow 410
DVD Player Dual Audio International Multi-standard DVD Player
CD Player Multi-disk (10 disk) CD Player
CMS (Cabin Management System) Audio International w/ Generation II Switch Panel Series

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:

Inspection Last Performed Next Due
12 month check 11 April 2017 11 April 2018
24 month check 11 April 2017 09 March 2019
48 month check 11 April 2017 09 March 2021
96 month check 11 April 2017 09 March 2025

Other Equipment:

Type of Unit Type of Unit
EFB (Electronic Flight Bag) – Class 2 2nd Refuel Defuel Panel
LDS (Lightning Detection System) Avionics Bay Light
Avionica micro QAR Therapeutic Oxygen Outlet in Cabin
Aft Equipment Bay Storage Box & Catwalk Rosen Sunvisor System

Navigation and Compliance:

RVSM RNP 10
P-RNAV RNP 4
B-RNAV (RNP 5) NAT MNPS

Weights:

Gross Weight (Ramp) 48,300 lbs Max Zero Fuel Weight 32,000 lbs
Max Takeoff Weight 48,200 lbs Max Payload 4,085 lbs
Max Landing Weight 38,000 lbs Current Basic Operating Weight 26,419 lbs

Connectivity:

Type of Unit Description
In Flight Phone ICS-200 Two-Channel Iridium Satellite Telephone System
Other Notable Features 1 x Wireless Handset in Cabin

On map

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