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Flight Display System - Pro Line 21 system with two (2) AFD-3010 and one (1) AFD-3010E adaptive flight displays (pilot's PFD, MFD and copilot's PFD); incorporates an Engine Indicating (EI) system.
Comm 1 - Collins VHF-4000 transceiver (118.000 to 136.975 MHz with 8.33 KHz increments), tuning through CDU or Collins RTU-4200.
Comm 2 - Collins VHF-4000 transceiver (118.000 to 136.975 MHz with 8.33 KHz increments), tuning through CDU or Collins RTU-4200.
Nav 1 - Collins NAV-4000 VOR/LOC/GLS/ADF/Marker Beacon receiver, tuning through CDU or RTU.
Nav 2 - Collins NAV-4500 VOR/LOC/GLS/Marker Beacon receiver, tuning through CDU or RTU.
AHRS - dual Collins AHC-3000 attitude heading reference system including dual FDU-3000 fl ux detector units, slaved and DG heading modes are provided.
GPS - Collins GPS-4000S Global Positioning System.
DBU-5000 data base unit for all database loading.
ADC - Dual Collins ADC-3010 air data computers.
ADF - Collins NAV-4000 with ADF, including antenna.
Transponders - Dual Rockwell Collins (Mode S) TDR-94D "Diversity" transponders with enhanced surveillance and Flight ID, controlled through CDU or RTU.
Transponder ATC Ident button on pilot's and copilot's control wheels.

DME - Collins DME-4000 with DME information displayed on PFD's.
Audio system - dual dB 700/dB 800 systems.
CVR - L3 Communications FA2100-1020-00 cockpit voice recorder with 120 minute recording time.
Flight Guidance System - dual Rockwell Collins FGC-3000 flight guidance computers, single autopilot system with yaw damper.
FMS - Rockwell Collins FMS-3000 fl ight management system with single CDU-3000 and navigational inputs from GPS receivers, Navigation receivers, and DME. FMS 4.0 software provides LPV approach capability,
IFIS - Rockwell Collins Integrated Flight Information System (IFIS) with IFIS 6.0 software provides enhanced map features to traditional displays (e.g. rivers, lakes, national boundaries, airway and airspace depictions). A File Server Unit (FSU) is connected to an Ethernet capable MFD and provides the control interface using a Cursor Control Panel (CCP).
Collins ECH-5000 Electronic Charts software depicting NOTAMS, airport diagrams with aircraft location and approach charts (GPS/ILS). The charts are integrated into IFIS and preloads the electronic charts to match the FMS fl ight plan.
Subscriptions services are required for the following functions:
Jeppesen electronic charts; Collins enhanced map overlays; Collins navigational database. First 12 months of subscription service for owner's home region is provided.
SFDS - Secondary Flight Display System Meggitt Mark II provides back-up attitude, heading, airspeed, altitude, and Nav with backup battery.
Weather radar - Collins TWR-850 Turbulence Weather Radar incorporates the Doppler principle of frequency shift to detect and display precipitation-related turbulence (up to a 50 nm range). It also features an auto-tilt function target alert mode.
Radio altimeter - Collins ALT-4000 radio altimeter, measures altitude up to 2,500 feet AGL, displayed on PFD.
Maintenance Diagnostics Computer - Collins MDC-3110 maintenance diagnostics computer, displays maintenance information on MFD and downloads through the DBU-5000 to memory stick.
Terrain Awareness and Warning System (TAWS) - ACSS TAWS+ system provides a Class A terrain awareness and warning system display on the MFD in normal mode or PFD in reversionary mode.

TCAS 1 - traffic alert and collision avoidance system (level 1) using L3 Communications Skywatch HP displayed on MFD in normal mode, PFD in reversionary mode.
Checklist display capability - normal and emergency checklists displayed on the MFD.
Cabin paging - cockpit to cabin paging with four cabin speakers.
Ground comm switch tied to comm 1 and pilot's and copilot's audio.
Dual hand held microphones.
Microphone key button on pilot's and copilot's control wheels.
Static wicks.
Emergency Locator Transmitter Artex ELT C406-2 with cockpit switch.
White lighting.
Avionics master switch.
Lighted panels.