Description of the engines:
Engines enrolled in MSP
APU enrolled in MSP
Airframe enrolled in EEC enhanced
Avionics:
ROCKWELL COLLINS PRO LINE FUSION
Synthetic Vision System (SVS) with full-screen presentation
RNP AR 0.3
Three frequency Emergency Locator Transmitter ELT / NAV
Single ADF
Third VHF communication transceiver
Single HF plus SELCAL
ACARS Datalink
ACARS over Iridium
CPDLC over ATN (EASA Link 2000 )
FANS 1A CPDLC
Datalink Graphical Weather
Lightning Detection System
Surface Management System
Reactive Windshear
Radio altimeter
Traffic Surveillance System (Integrated TCAS II and Enhanced
Mode S Transponder System)
Second Enhanced Mode S Transponder
Terrain Awareness and Warning System class A (TAWS-A)
OnboardMaintenance system (OMS)
Electronic checklist
Autothrottle system
Dual Air Data System RVSM compatible
Dual Flight Management System (FMS) with Take-off and Landing
performance calculation capability (TOLD)
Dual Global Positioning System (GPS) with SBAS/WAAS
Navigation charts capability - Integrated Flight Information
System (IFIS)
Cockpit Voice Recorder (CVR)
Flight Data Recorder (FDR)
ADS-B out
Equipment:
High Altitude Landing and Take-off (HALTO)
Iridium Satellite Phone
Swift Broadband High Speed Data
Enhanced Cabin Management System (19 HD Monitors)
High Power Outlets 115V
HEPA Filter
Observer Seat
Pilot Tables
Logo Light
Auto Brake
Exterior:
Embraer Demo Scheme
Interior:
9 Passengers Configuration with 6 Enhanced Seats and a RHS 3
Place Divan in the aft Cabin
Belted Toilet
Observer Seat
Cockpit Galley Curtain
Cabin/Lavatory Pocket Door
Galley/Cabin Pocket Door
Main Door Thermo-Acoustic Curtain
Microwave Oven and Refrigerator
Provisions for Coffee Machine
Stone floor on galley and lavatory floors / Stone veneer on countertops
Other comments:
Engines enrolled in MSP
APU enrolled in MSP
Airframe enrolled in EEC enhanced
Steep Approach Capability
CAT-II
