1990 BOMBARDIER CHALLENGER 601-3AER S/N 5074

Price

Price On Request

Description

HIGHLIGHTS

120M Inspection Completed June 2020
Enrolled on Engine & Avionic Programs
Extended Range Mod
APU -150 Upgrade
ADS-B Out Compliant V1
10 Passenger and with FWD Galley Configuration

 

AIRFRAME

Total Time Since New 10,791 Hours (as of April 30, 2021)
Total Landings Since New 6,094 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 350376
Total Hours Since New 10,385 Hours 10,470 Hours
Total Cycles Since New 6,408 Cycles 6,420 Cycles
Program Coverage General Electric OnPoint

 

APU

Description Honeywell GTCP 36-150
Serial Number P-361C
APU Total Time Since New 6,491 Hours

 

AVIONICS

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

 

OTHER NOTABLE FEATURES

SB-601-0262 – Fuel Storage – Tail Cone Fuel Tank
STC-ST0246SE – ADS-B Out V1
Previously Operated under FAR Part 91

 

MAJOR INSPECTION STATUS

Inspection Last Performed Next Due
12 Month July 2020 In Progress
24 Month April 2019 In Progress
36 Month April 2019 April 2022
48 Month April 2019 April 2023
60 Month July 2020 May 2025
120 Month June 2020 June 2030
Landing Gear Overhaul June 2020 June 2030

 

COMPLIANCE

RVSM RNP 2
RNP 10 RNAV 5
RNP 1 ADS-B Out V1
TCAS 7.1

 

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

 

INTERIOR

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)

 

EXTERIOR

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)

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Contact

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