ESI-500 Electronic Standby Instrument

The ESI-500 Electronic Standby Instrument System is one of the most advanced standby instruments designed to mirror primary flight displays (PFDs) for airspeed, altitude, attitude and slip data in piston and turboprop aircraft, as well as light helicopter platforms.

The Acron Aviation ESI-500 Electronic Standby Instrument
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Product overview

The compact unit is scalable and comes standard with altitude, attitude, slip/skid, vertical speed and aircraft track.

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 magnetometer. The ESI-500 is compatible with existing NAV radios and GPS hardware. Upon loss of power an internal lithium-ion battery pack automatically powers the unit and magnetometer without interruption.

Key features

High-resolution, full color display

The scalable ESI-500 has numerous display configurations, including navigation, metric altitude, vertical speed and heading. The navigation function can be configured for VOR/ILS or GPS single-source or both. In the absence of a heading source, the ESI can display aircraft “track” from a GPS source.

Built-in back-up battery

The ESI-500 also features an internal lithium-ion battery, which will automatically power the unit without interruption should the system lose aircraft power. This ensures that pilots will have the critical attitude, altitude and airspeed information they need to fly to a suitable airport.

Optional SynVis display capabilities

The ESI-500 is compatible with a variety of SynVis systems enabling it to display color representations of critical information about terrain and known obstacles along the aircraft’s flight path. SynVis depicts three-dimensional terrain and obstacles to reflect topography and hazards. Terrain and obstacle impact alerts are shaded to increase situational awareness. In addition, the unit can also display magnetic heading when coupled with the optional MAG-500 magnetometer.

Specifications

Weight and power

  • Nominal 2.1 lb. (0.95 kg) – Maximum 2.75 lb. (1.25 kg)
  • 14V or 28 VDC electrical systems (10 to 32 VDC)

Interfaces

  • (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

Navigation

  • VOR/ILS or GPS Navigation or both

TSO

  • C2d, C8e, C10b, C34e, C35d, C36e, C40c, C46a, C106, C113a, C179a, C201

ETSO

  • 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 is required

Aircraft on ground and customer support

We have a global network of support centers to support customers with aircraft on the ground, and other issues.

Skyparts

Skyparts is our spares trading arm, providing immediate, quick-turn access to high-quality, OEM-reliable parts and out-of-production aerospace equipment as used serviceable material.

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