Specifications

Description

Aircraft Detail Airframe TT4,150 Landings1,396 ProgramEmbraer Executive Care Standard Engine(s) TT14,334 Cycles10,668 On Engine ProgramNo APU APU under Embraer Executive Care Standard Program Maintenance Certification: EASA Interior Details Nineteen seat (19) Passenger configuration over 5 zones Zone 1 - Club Four opposite 2 Club seats Electric Pocket door between zone 1 and zone 2 Zone 2 - Club Four Seating Zone 3 - Four place Divan opposite credenza with 42” HD Wide screen monitor Zone 4 - Club Four opposite 2 Club seats Zone 5 - Electric Pocket door access to Master Suite VIP Lavatory with walk in shower with stone flooring Baggage compartment Full service forward Galley Credenza in entry area Espresso Coffee Maker lacobucci Nespresso Additional Coffee maker lacobucci Hi-Fly American model Refrigerator/Freezer Additional Oven Foldable Trolley Stone Flooring Safe Compartment Honeywell Jetwave KA Band Connectivity iPod dock, HD Blu-Ray/DVD players - zone 3 and 5 Surround Audio - zone 5 Additional Master Control Touch Screen Panel Additional 24” HD Wide screen LCD Monitor - Zone 2 and 4 Upgraded 32” HD Wide screen LCD Monitor - Zone 5 Upgraded 42” HD Wide screen LCD Monitor - Zone 3 Exterior Details Pearlescent White, Light Blue and Dark Blue contouring stripes join a sweeping blue design across the body of the aircraft finishing with the Embraer logo Avionics Honeywell Primus Epic Flight Control System Honeywell Primus Epic with 5 LCD Electronic Displays Dual Monitor Warning Function (MWF) System Graphics Generation Function (GGF) hosted in the display units Dual System Utilities Function System Dual Flight Management System (FMS) Central Maintenance System Data Acquisition Function Dual Automatic Direction Finder (ADF) Dual Distance Measurement System (DME) Triple Air Data System (ADS) Dual Mode S Enhanced Transponder System Dual VHF Digital Radio Dual VHF Omnidirectional Range (VOR) System Dual Instrument Landing System (ILS, composed of Localizer (LOC) and Glideslope (GS) Dual Global Positioning System (GPS) Enhanced Ground Proximity Warning System (EGPWS) Windshear Detection and Guidance System - hosted in the EGPWS Dual Inertial Reference System (IRS) P-880 Weather Radar with turbulence detection Traffic Alert and Collision Avoidance System (TCAS) Dual Radio Altimeter System Dual Digital Voice Data Recorder (DVDR) Dual Multifunctional Control and Display Unit (MCDU) Emergency Locator Transmitter (ELT) with Positioning Report System Three Audio Control Panels (ACP) Electronic Clock System Integrated Electronic Standby (IES) Display System Standby Magnetic Compass Dual Cursor Control Devices (CCD) Dual Guidance Panel (GP) Controller Quick Access Recorder (QAR) SELCAL System Dual High Frequency HF Communication System ADS-B Out DO-260B CPDLC over ATN FANS 1/A Avionic Load 27.4 Autobrake capability Additional Details • CMF (ACARS) with 3rd VHF Mode 2 • Cockpit Printer Communications over Aeronautical Telecommunications Network LSS - Lightning Sensor System ECL - Electronic Checklist EFB - Electronic Flight Bag DMU - Data Management Unit Gray Water Tank RAAS - Runway Awareness and Advisory System Steep Approach Capability - EASA only