2016 BOMBARDIER GLOBAL 6000

$23,860,000

Category:

Description

AIRFRAME

Total Time Since New 1,646 Hours (As of June 29, 2022)
Total Landings Since New 612 Landings
Entry Into Service Date November 2016
Home Base Paris Le Bourget
Maintenance Tracking CAMP
Certification EASA Part NCC (Private Ops)
Program Coverage Bombardier Smart Parts Plus

ENGINES

  Left Engine Right Engine
Description Rolls Royce BR700-710A2-20
Serial Numbers 22621 22620
Total Hours Since New 1,646 Hours 1,646 Hours
Total Cycles Since New 616 Cycles 616 Cycles
Program Coverage Rolls-Royce Corporate Care

APU

Description Honeywell RE220
Serial Number P-877
APU Total Time Since New 815 Hours
Program Coverage Honeywell MSP Gold

 

AVIONICS

The Global 6000 is equipped with an integrated Collins Pro Line Fusion 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-LCD Collins AFD-6520
GPS (Global Positioning System) Dual Collins GPS-4000S
IRS (Inertial Reference System) Triple Honeywell LASERF VI
NAV (Navigation Radio) Dual Collins NAV-4000
DME (Distance Measuring Equipment) Dual Collins DME-4000
EVS (Enhanced Vision System) Single Bombardier
HGS (Head Up Guidance System) Single Bombardier
SVS (Synthetic Vision System) Single Collins SVM-6110H
VHF COM (Very High Freq. Communication) Triple Collins VHF-4000
HF COM (High Freq. Communications) Dual Collins HF-9031A
SATCOM (Satellite Communications) Single Collins SDU-2200
WX RADAR (Weather Radar) Single Collins RTA-4118
RAD ALT (Radio Altimeter) Dual Collins ALT-4000
XPNDR (Transponder) Single Collins TDR-94D
TSS (Traffic Surveillance System) Single Collins TSS-4100
TAWS (Terrain Awareness and Warning System) Single Collins TPM-6000
CVR (Cockpit Voice Recorder) Single L3 Harris FA2100
FDR (Flight Data Recorder) Single L3 Harris FA2100
LSS (Lighting Sensor System) Single Collins WX-1000
ELT (Emergency Locator Transmitter) Single Artex B406-4
QAR (Quick Access Recorder) Single Collins QAR-100

INTERIOR

Description
Number of Passengers Fourteen (14)
Galley Location Forward
Forward Cabin Configuration Four (4) Place Club
Mid Cabin Configuration Four (4) Place Conference Group Opposite Single (1) Executive Seat With Work Station
Aft Cabin Configuration Two (2) Place Club Opposite Three (3) Place Divan (Certified for Three (3) when RH removable bulkhead is removed for taxi, take-off, and landing)
Crew Rest Yes
Jump Seat Yes
Lavatory Locations Forward Crew Lavatory and Aft Executive
Last Refurbishment Original Completion
Galley Equipment Expresso Maker, High-Temperature Oven, Microwave Oven, Ice Drawer, Pull-Out Work Surface, Waste Container

ENTERTAINMENT SYSTEM

Monitors One (1) 24-Inch HD Monitor on RH FWD Bulkhead
One (1) 24-Inch HD Monitor on LH AFT Bulkhead
Airshow Yes
Plug-In Tablet-Arm Receptacles Ten (10)
Connectivity Dual (2) Blu Ray Players, USB Jack, Media Streamer, R-45 Ethernet Port (Gigabit), HDMI Jack (3)
Bluetooth Receivers Yes

 EXTERIOR

Base Paint Color Overall Matterhorn White
Stripe Colors Navy Blue, Light Blue, Orange
Last Paint Original Completion

 

Range

 

MAJOR INSPECTION STATUS

Inspection Last Performed Next Due
15 Month August 2021 February 2023
30 Month August 2021 May 2024
60 Month August 2021 November 2026
120 Month N.A. November 2026

CONNECTIVITY

Type of Unit Description
High Speed Internet KA-Band
Satellite Communications Collins ARINC 781 SATCOM
Phone System Airborne Telephone System (ATS)

NAVIGABILITY

Class II Electronic Flight Bag (EFB) System – EASA STC 10038659 Rev 2 (TCCA and FAA Approved)

SB 700-11-6002 – Increased Maximum Take-Off Weight (MTOW) to 99,500lbs

SB 700-23-6017 – Honeywell JetWave KA-Band Radome Fairing

SB 700-31-6001 – Quick Access Recorder (QAR)

SB 700-34-6001 – Surface Management System (SMS) − Activation of SMS /Take−off and Landing Alert Function. (scheduled in August 2022)

SB 700-34-6004 – Installation of Head-Up Display (HUD) System

SB 700-34-6005 – Installation of Enhanced Vision System (EVS)

SB 700-34-6016 – Activation of Steep Approach Option – Glidepath Angles From 4.5 To 5.5 Degrees

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