ESI-500 Electronic Standby Indicator
3Pages

E SI -500 E lect r onic St andby Indi cator Weight (5) ARINC 429 Inputs, (1) ARINC 429 Output, (1) RS-485 Serial Input (interfaces with MAG-500), (1) Analog Input (OAT), (1) Discrete Output, (1) Dimming Bus, (1) I2C interface to the DCM-500 VOR/ILS or GPS Navigation or both EASA accepted in accordance with FAA-EASA Technical Implementation Procedures (TIP) Rev 5 (paragraph 2.5.1 ‘TSO/ETSO Articles Accepted under Reciprocal Acceptance’). No ETSO marking on the Articles are required. DO-178C and DO-254 - Design assurance level C Aviation Products 5353 52nd Street SE Grand Rapids, MI 49512 Tel: 800-253-9525 (toll-free in the U.S.) / 616-949-6600 Fax: 616-285-4224 www.L-3com.com/AviationProducts L-3 Aviation Products is a leading provider of GA, commercial and military avionics, as well as MRO services. We manufacture a diverse line of safety- and efficiency-enhancing products that sets the standard for next-generation cockpit requirements. ©2016 L-3 Aviation Products • Printed in USA This brochure consists of L-3 Avionics Systems general capabilities information that does not contain controlled technical data as defined within the International Traffic in Arms (ITAR) Part 120.10 or Export Administration Regulations (EAR) Part 734.7-11. Aviation Prod

PACK 50 YEARS OF STANDBY EXPERIENCE IN YOUR PANEL Battery Indicator L-3’s NextGen ESI-500 Electronic Standby Instrument is one of the most advanced backup systems designed specifically for piston, turboprop and light helicopter platforms. The compact unit is scalable and comes standard with airspeed, altitude, attitude, slip/skid, vertical speed and back-up battery. Options are available for the display of navigation information and Synthetic Vision (SynVis), including terrain and obstacles. Magnetic heading is an available option when coupled with the low cost and compact MAG-500...

E SI -500 E lect r onic St andby Indi cator Weight (5) ARINC 429 Inputs, (1) ARINC 429 Output, (1) RS-485 Serial Input (interfaces with MAG-500), (1) Analog Input (OAT), (1) Discrete Output, (1) Dimming Bus, (1) I2C interface to the DCM-500 VOR/ILS or GPS Navigation or both EASA accepted in accordance with FAA-EASA Technical Implementation Procedures (TIP) Rev 5 (paragraph 2.5.1 ‘TSO/ETSO Articles Accepted under Reciprocal Acceptance’). No ETSO marking on the Articles are required. DO-178C and DO-254 - Design assurance level C Aviation Products 5353 52nd Street SE Grand Rapids, MI 49512...