Aircraft Highlights

One Owner Since New

Delivered with 96 Month Inspection Done

TCAS II w/ Change 7.1

10-Passenger Configuration

Operated EU OPS

AIRFRAME / ENGINES / APU / WEIGHT

AIRFRAME

Total Time Since New 4,286 Hours (as of June 11, 2019)
Total Landings Since New 1,835 Landings
Entry into Service Date February 2012
Maintenance Tracking CAMP
Certification Currently Operated EU OPS

ENGINES

Left Engine Right Engine
Description Honeywell AS907-1-1A/HTF7000
Serial Numbers P118810 P118811
Total Hours Since New 4,286 Hours 4,286 Hours
Total Cycles Since New 1,849 Cycles 1,846 Cycles
HSI Due/Overhaul Due On Condition

APU

Description Honeywell 36-150 (BD)
Serial Number P-447
APU Total Time Since New 4,187 Hours
HSI Due/Overhaul Due On Condition

Maintenance & Inspections

Inspection Last Performed Next Due
12-Month February 2019 March 2020
24-Month March 2018 March 2020
36-Month January 2017 January 2020
48-Month March 2016 Undergoing
96-Month February 2012 Undergoing

AVIONICS & CONNECTIVITY

The Challenger 300 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) Four-Tube AFD-5220
FMS (Flight Management System) Dual CSU-3100
ELT (Emergency Locator Transmitter) Single C406-N
GPS (Global Positioning System) Dual GPS-4000A
NAV (Navigation Radio) Dual NAV-4000
DME (Distance Measuring Equipment) Dual DME-4000
ADF (Automatic Direction Finder) Dual NAV-4000
A/P (Autopilot) Dual FGC-3002
VHF COM (Very High Freq. Communication) Triple VHF-4000
HF COM (High Freq. Communications) Dual HF-9031A
SATCOM (Satellite Communications) Single ICS-200
RADAR Single RTA-844
RADAR ALT (Radar Altimeter) Single ALT-4000
XPNDR (Transponder) Dual TDR-94 (Mode S)
EGPWS (Enhanced Ground Proximity Warning System) Single MK VIII
TCAS (Traffic Collision Avoidance System) Single TTR-4000 w/ Change 7.1
CVR (Cockpit Voice Recorder) Single CVR L3 COMM
FDR (Flight Data Recorder) Single RIPS CVR

Interior & Entertainment

Description
Number of Passengers Ten (10) Passengers
Galley Location Forward
Forward Cabin Configuration Four (4) Place Club Seating
Aft Cabin Configuration Three (3) Place Divan Opposite Two (2) Single Club Seats
Lavatory Locations Aft, 16G Belted Lavatory

Galley Equipment:
Microwave WaveJet Microwave Oven
Coffee/Espresso Maker Coffee/Espresso Maker as Loose Equipment

CONNECTIVITY
Type of Unit Description
In Flight Phone Iridium Airborne Telephone System

ENTERTAINMENT
Type of Unit Description
Display/TV Monitors Two (2) 20” LCD Bulkhead Monitors
Airshow System Airshow 410
DVD Player One (1) DVD/CD Player
Other Notable Features Seven (7) 115V Electrical Outlets