The MD41 Helicopter TAWS Annunciation Control Unit is a three-button horizontal 28 volt TAWS for Garmin 430W/530W. Designed to place annunciation and mode selection for the Terrain Awareness Warning System (TAWS)...
Course Deviation Indicator2"", 5V lighting.
The MD222-406 course deviation indicator (CDI) is designed to work with VHF and GPS navigational equipment to provide OMNI (VOR), GPS, localizer (LOC), and glideslope information. The MD222 is designed...
The MD200 Series Course Deviation Indicator is designed to work with VHF and GPS navigational equipment to provide OMNI (VOR), GPS, localizer (LOC), and glideslope information. The MD200 is designed...
The rechargeable lithium ion battery is designed for the EKP V Portable Glass Cockpit System allowing portable use.
The power adapter accessory is used in combination with the PC interface cable to provide power to the EKP V from an AC power source.
The plastic knee pad support accessory is designed for the EKP V Portable Glass Cockpit System. The knee pad allows for hands-free use of the EKP V when panel installation...
The joystick kit for the EKP V Portable Glass Cockpit System contains joysticks with various textures and a replacement wheel selector.
This knee strap (EDMO# K10LCE007A) is for use with the knee pad bracket for the EKP V.
This protective cover (EDMO# HPC50AX) is for the EKP V Portable Glass Cockpit System.
The DWA2000 is a self-contained WAAS GPS annunciator panel for 14 and 28 volt aircrafts. The unit displays annunciation status from GPS receivers that output discrete signals for remote annunciation...
This PC interface cable (EDMO# CBYUMG0400) provides a USB connection from a computer to the EKP V unit.