HP-JRJ - 2020 BOMBARDIER GLOBAL 5500

2020

BOMBARDIER

GLOBAL 5500

60007

HP-JRJ

Used

DEAL PENDING Low Hours Engines and APU on program EASA certified Two 3-place divan in aft cabin

1999

595

JSSI

Engine Model: Rolls Royce PEARL 15

1202

APU Model : Honeywell RE220 (GX)

The Aircraft is equipped with the Bombardier Vision Flight Deck Avionics Suite, complete with Four (4) 14”x11” Landscape Active Matrix Liquid Crystal Displays (AMLCD). OPTIONS INSTALLED: Datalink Graphical Weather System Quick Access Recorder AUTO FLIGHT: Dual three-axis, Category II Automatic Flight Control Systems (AFCS) is provided with pitch and roll channels and an independent linear actuator for the yaw axis. The AFCS includes computations for Flight guidance; Autothrottle; Autopilot; Yaw damper; and Automatic pitch trim. The flight director modes include Emergency Descent Mode which will automatically turn and dive the Aircraft down to 15,000 ft when the system senses pressurization issues and pilots do not take action within a specific amount of time. COMMUNICATIONS The communication system provides equipment designed to supply communication in the Aircraft, between different aircraft, and between the Aircraft and ground stations. The Aircraft communication system includes: Three (3) VHF communication radios; Two (2) HF transceivers; One (1) dual SELCAL system capable of monitoring three (3) VHF and two (2) HF radios; One (1) handset using the cabin satellite airborne telephone system; One (1) data communication channel (ACARS), which in conjunction with the VHF meets the requirements of Future Air Navigation System (FANS 1/A+) including Airline Operational Control (AOC), Air Traffic Services (ATS), Facilities Notifications (AFN), Automatic Dependent Surveillance - Contract (ADS-C), and Controller Pilot Datalink Communication (CPDLC); and One (1) dual channel interphone system with hand-held microphones and individual controls for pilot, co-pilot and flight observer seat. INDICATING / RECORDING SYSTEM: Electronic Flight Instrument System (EFIS); Engine Indication and Crew Awareness System (EICAS); Synchronized digital GPS Clock; Cockpit Voice Recorder (CVR); Flight Data Recorder (FDR); and Emergency Locator Transmitter (ELT). NAVIGATION Two (2) Integrated Flight Information Systems (IFIS)2 with dual File Server Unit; One (1) Head-Up Display (HUD) System; One (1) Enhanced Vision System (EVS); One (1) Synthetic Vision System (SVS); One (1) Electronic Integrated Standby Instrument (ISI); One (1) Air Data System (ADS) composed of three (3) Air Data Computers (ADC); One (1) Auto-tilt Weather Radar; Three (3) Inertial Reference Systems (IRS); Two (2) GPS WAAS receivers; Two (2) VHF navigation receivers; Two (2) ADF receivers; Two (2) DME transceivers; One (1) Traffic Surveillance System and One (1) standalone Transponder capable of: Dual transponder functionality; TCAS II change 7.1; and ADS-B Out. Two (2) Radio Altimeter systems; One (1) Terrain Awareness and Warning System (TAWS); and Three (3) Flight Management Systems (FMS).

2020

2020

14

Yes

Forward

Yes

Forward and Aft

14 Passenger configuration – certified for 13 pax during take off and landing Forward Cabin: Four (4) Place Club Seats Mid Cabin: Four (4) Place Conference Group opposite a Credenza Aft Cabin: Two (2) 16G 3- Place Divan Forward and Aft Lavatory

OPTIONS INSTALLED: Quick Access Recorder Datalink Graphical Weather System EU Air OPS Part CAT operations Take-off and Landing Awareness Function (TLAF) Surface Management System Aft Cabin equipped with two (2) 16G 3-Place Divan Provision Installation for KA Band High Speed Connectivity including Software only (Radome not included)