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1990 Bombardier Challenger 601-3AER

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1990 Bombardier Challenger 601-3AER
Aircraft Details
TTAF 10,516 hrs
Serial Number 5074
Year 1990
Interior Color Leather
Exterior Color White
History N/A

Enrolled on GE OnPoint and HAPP;
Extended Range Mod;
Triple VHF Comm. and IRU;
APU -150 Upgrade;
ADS-B Out Compliant; and
10 Passenger and FWD Galley Configuration.

AIRFRAME:

Total Time Since New 10,516 Hours (as of October 2, 2017)
Total Landings Since New 5,891 Landings
Certification Date July 6, 1990
Home Base Essendon, Melbourne
Avionics Program Honeywell HAPP
Maintenance Tracking CAMP
Certification CASR Part 91

ENGINES:

Left Engine Right Engine  
Description General Electric CF=34
Serial Number(s) 350367 35376
Total Hours Since New 10,111 Hours 10,195 Hours
Total Cycles Since New 6,205 Cycles 6,217 Cycles
Program Coverage General Electric OnPoint

APU:

Description Honeywell GTCP 36-150
Serial Number P-361C
APU Total Time Since New 6,136 Hours

The Bombardier Challenger 601-3A is equipped with an integrated, Honeywell SPZ-8000 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) Five-Tube Honeywell SPZ-8000
FMS (Flight Management System) Dual Honeywell FMZ-2000 w/ LPV (Software 5.2)
CDU (Central Display Unit) Dual Honeywell CD-810
IRS (Inertial Reference System) Triple Honeywell IRU II and MS-300 Mode Selector
GPS (Global Positioning System) Dual Honeywell GNSSU, 12 Channel
ADC (Air Data Computer) Dual Honeywell AZ-810
NAV (Navigation Radio) Dual Honeywell Integrated System
DME (Distance Measuring Equipment) Dual Rockwell Collins DME-42
EFB (Electronic Flight Bag) Single Pilot View CMA 1100
ADF (Automatic Direction Finder) Dual Rockwell Collins ADF-462
A/P (Autopilot) Dual Honeywell DFZ-800
VHF COM (Very High Freq. Communications) Triple Rockwell Collins VHF-22C w/ 8.33 Spacing
HF COM (High Freq. Communications) Dual Rockwell Collins HF-9000 w/ SELCAL
SATCOM (Satellite Communications) Single Aircell Axxess II ST-4200 (Iridium) Dual Channel
WRADAR (Weather Radar) Single Honeywell Primus 880
RADAR ALT (Radar Altimeter) Single Honeywell RT-300
XPNDR (Transponder) Dual Rockwell Collins TDR-94D Mode S and ADS-B
GPWS (Ground Proximity Warning System) Single Honeywell EGPWS MK V
TCAS (Traffic Collision Avoidance System) Single Honeywell TCAS II w/ Change 7.1
CVR (Cockpit Voice Recorder) Single L3 Technologies A100S
FDR (Flight Data Recorder) Single L3 Technologies F1000
ELT (Emergency Locator Transmitter) Single ACR Artex C406-2
LSS (Lighting Sensor System) Single Honeywell LP-850
Number of Passengers Ten (10) Passenger
Galley Location Forward
Forward Cabin Configuration Four (4) Place Double Club
Aft Cabin Configuration Four (4) Place Conference Group Opposite Two (2) Place Club
Lavatory Location(s) Aft
Jumpseat Yes
Galley Equipment High-Temp Oven; Microwave; and Coffee / Espresso Maker
Other Notable Feature(s) Dual Life Raft; and Logo Light
Last Refurbished Date(s) February 2006 (General Dynamic Aviation Services)
June 2010 (West Star Aviation)

ENTERTAINMENT:

Display / TV Monitor(s) Dual 20.0” Bulkhead Monitors
Airshow System Airshow 410
Other Notable Feature(s) CD / DVD Player; and USB Data Loader
Base Paint Color(s) Matterhorn White
Stripe Color(s) Blue and Titanium
Last Painted Date(s) February 2006 (General Dynamic Aviation Services)
August 2017 (Paint Protection)

MAJOR INSPECTION STATUS:

Inspection Last Performed Next Due
12 Month May 2017 May 2018
24 Month April 2017 April 2019
36 Month April 2016 April 2019
48 Month May 2015 May 2019
60 Month May 2015 May 2020
120 Month June 2015 June 2020
Landing Gear Overhaul June 2020

OTHER NOTABLE FEATURES:

SB-601-0262 – Fuel Storage – Tail Cone Fuel Tank
RVSM, RNP 10, RNP 2, RNP 1, and RNAV 5 Compliant
Previously Operated under FAR Part 91

WEIGHTS:

Gross Weight (Ramp) 45,250 lbs.
Max Takeoff Weight 45,100 lbs.
Max Landing Weight 36,000 lbs.
Max Zero Fuel Weight 31,000 lbs.
Empty Weight 25,965 lbs.
Basic Operating Weight 26,977 lbs.