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2010 Bombardier Challenger 605

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2010 Bombardier Challenger 605
Aircraft Details
TTAF 2,739 hrs
Serial Number 5811
Year 2010
Interior Color Leather
Exterior Color Matterhorn White
History N/A

Fully Programmed

CASP Avionics Coverage

WAAS/LPV (Collins STC ST01505WI-D)

Aircell ATG 5000 Gogo Biz / Text & Talk

12 Passenger Executive Floorplan 2

AIRFRAME:

Total Time Since New 2,739.4 Hours   (as of 18 August 2017 )
Total Landings Since New 2,354 Landings
Entry into Service Date 8 April 2010
Home Base West Mifflin, PA USA (KAGC)
Program Coverage Smart Parts Plus
Maintenance Tracking Flight Docs
Certification Currently Operated FAR Part 91

ENGINES:

Left Engine Right Engine  
Description General Electric CF34-3B
Serial Number(s) 950841 950842
Total Hours Since New 2,739.4 Hours 2,739.4 Hours
Total Cycles Since New 2,359 Cycles 2,358 Cycles
HSI Due / Overhaul Due On Condition
Program Coverage GE OnPoint

APU:

Description Honeywell GTCP 36-150
Serial Number P-256
APU Total Time Since New 2,749 Hours
HSI Due / Overhaul Due On Condition
Program Coverage MSP

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 Unit Description
EFIS (Electronic Flight Instrument System) 4-Tube Four (4) 10×12” LCD Collins Pro-Line 21
FMS (Flight Management System) Dual Collins FMS-6000
CDU (Central Display Unit) Single
IRS (Inertial Reference System) Triple Honeywell Laseref V
GPS (Global Positioning System) Dual Collins WAAS Capable GPS
ADC (Air Data Computer) Dual Digital ADC’s
NAV (Navigation Radio) Dual VOR/ILS/MKR Nav Systems
DAU (Data Acquisition Unit) Single
DME (Distance Measuring Equipment) Dual 3-Channel DME Systems
HUD (Head Up Display) Single Collins HGS 6605
EVS (Enhanced Vision System) Single Bombardier Enhanced Vision System
ADF (Automatic Direction Finder) Dual Digital ADF Systems
AFS (Auto Flight System) Dual Honeywell Dual Channel AFS w/ Autothrottle
VHF COM (Very High Freq. Communications) Dual 8.33kHz Spacing
HF COM (High Freq. Communications) Dual Digital HF Communication System
SATCOM (Satellite Communications) Single Collins SRT 2100
SELCAL (Selective Calling System) Single
GPWS (Ground Proximity Warning System) Single Honeywell Mark V w/ TAWS
WRADAR (Weather Radar) Single Dual-scan Digital Color Radar
RADIO ALT (Radio Altimeter) Dual
XPNDR (Transponder) Dual Enhanced Surveillance Mode-S Transponders
TCAS (Traffic Collision Avoidance System) Single TCAS II
CVR (Cockpit Voice Recorder) Single 120 Minute CVR
FDR (Flight Data Recorder) Single 25 Hour FDR
ELT (Emergency Locator Transmitter) Single 406 MHz ELT
Number of Passengers Twelve (12) Passenger Executive Floorplan 2
Galley Location Forward
Forward Cabin Configuration Four (4) Place Club
Aft Cabin Configuration Four (4) Place Conference Group Opposite Four (4) Place Divan
Lavatory Location Aft
Jumpseat Track and Swivel Jumpseat
Galley Equipment Espresso Maker, Microwave Oven, Two Pullout Work Surfaces, Auxiliary Heater
Other Notable Feature(s) Berthing Mattress for Conference Group, Aft Cabin Bulkhead Pocket Door, Crystal Showcase, Two (2) Flip-Down Hang-Up Bars in Baggage Compartment, Additional Magazine Rack
Last Refurbished Date Original with Touch-up at Duncan August 2017
Base Paint Colors Matterhorn White and Royal Blue Split Base
Stripe Color Gamma Grey
Last Painted Date Original with Wings Painted at Duncan August 2017

ENTERTAINMENT:

Display / TV Monitor(s) Two (2) 21” Cabin Monitors
Airshow System Collins Moving Map Equipment (MME)
Cabin Management System Collins CES Cabin System
Other Notable Feature(s) Airborne Office Suite, Two (2) Cockpit and Five (5) Cabin Power Outlets

CONNECTIVITY:

High Speed Internet Aircell ATG 5000 Gogo Biz / Text & Talk
Phone System Aircell ICG ST3100
Other Satcom SRT2100

NAVIGATION AND COMPLIANCE:

WAAS/LPV (Collins STC ST01505WI-D)
   Dual Electronic Flight Bags (EFB’s)/Cockpit Touch Screen
DBU – 5000 Data Loader

OTHER EQUIPMENT:

3D Map and Long Range Cruise Pilot Awareness & Productivity Package
Lightning Detection System External Compartment Lights
Datalink with Inmarsat Satcom Interface 3M Erosion Boots on Winglets
Enhanced Maps on MFD Additional Carpet Set
Cockpit Touchscreen Monitors Cockpit Writing Tables
Second Refuel/Defuel Panel Crew Seat Integrated Headrests
Avionics Bay Light Entry Light On/Off Switch
Medeco Common Keyed Locks Landing Gear Undercarriage Paint
Aft Equipment Storage Box Polished Kidney Panels
Mainwheel Storage Box Additional 40 Cubic Foot Oxygen Bottle
Maintenance Ladder Fly-Away Kit (Maintenance Runner, Seat Covers)
Portable Tow Bar

WEIGHTS:

Max Weight (Ramp) 48,300 lbs.
Max Takeoff Weight 48,200 lbs.
Max Landing Weight 38,000 lbs.
Max Zero Fuel Weight 32,000 lbs.
Empty Weight 25,815 lbs.
Basic Operating Weight 27,373 lbs.