Prodigy TouchTM System (Garmin G3000)
Integrated Avionics Unit (GIA64E)
Three (3) 14.1” Active Matrix Liquid Crystal Displays (AMLCD)
3 Axis CAT I Automatic Flight Control System (AFCS)
Integrated Electronic Standby Instrument (IESI)
Pitch/Roll/Yaw Servo - Servo Autopilot (GSA 81)
Flight Director (FD)
Two (2) Audio Panels
One (1) Guidance Panel
Two (2) 5.7” Infrared Touch Screen Controllers (Data Input)
Full Authority Digital Engine Control (FADEC)
Air Data Computer (GDC 74B)
VHF Communication (COM)
VOR/ILS Navigation (NAV)
Honeywell DME
ILS/MB/VOR
Dual ADF Automatic Direction Finders
Honeywell Dual Radio Altimeters
Attitude & Heading Reference System (GRS 79)
Garmin Satellite Weather & Radio Receiver
Weather Radar
Garmin Dual Mode S Transponders w/ADS-B In
Package 1 (DME + 2nd Transponder Mode S w/Diversity)
Flight Management System (FMS) w/RNP
Satellite Based Positioning Navigation (GPS-WAAS)
TCAS I – Traffic Alert and Collision Avoidance System I
Terrain Awareness and Warning System Class B (TAWS-B)
Cockpit Voice & Data Recorder (CVDR)
FDR Accelerometer (CAT.IDE.A.191)
Electronic Fuel Conditioning Unit (EFCU)
Brake Control Unit (BCU)
Trim Actuator Controller
Flap System Control Unit
Stall Warning and Protection Computer
KANNAD Martec Serpe ELT