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VAL AVIONICS LTD

INS 429 INTEGRATED NAVIGATION SYSTEM

INSTALLATION AND OPERATOR’S MANUAL

Original Issue Page 4 of 21

1 SECTION I - GENERAL INFORMATION

1.1 INTRODUCTION

Thank you for purchacing our INS 429 Integrated Navigation System. Here at Val Avionics Ltd., our core

design philosophy is based on the ease of installation and use. The 429 represents 5 years of refinement in

that process, based on the feedback of customers that have used the INS 422. The INS 429 is a totally new

concept, designed with new and exciting features.

That design philosophy translates into the ease of installation and simple operation makes the INS

429 Integrated Navigation System a navigation solution for a wide variety of aircraft panels, from the

Homebuilt through heavy twins. The INS 429 satisfies the need for compact, fully intergraded, quality

navigational aid that can be counted on to provide years of reliable service.

Before installing and /or using your new INS 429 please read this manual completely. This will ensure

proper installation and familiarize you with all of the features your NAV has to offer.

1.2 SCOPE

This manual will provide detailed information about the installation and operation of the INS 429

Integrated Navigation System. It will also provide equipment limitation information and instructions for

continued airworthiness.

1.3 EQUIPMENT DESCRIPTION

The INS 429 has been designed for simplicity. It is straight forward to install and operate. Using state of the

art technology Val Avionics Ltd. has created a navigation instrument that will provide the pilot with simple

easy to interpret navigation information for in-route VOR and ILS Approach. The INS 429 can also be

coupled to an external GPS system and display the GPS course deviation.

The INS 429 also has an enhanced display that features both active and standby frequency displays. A

display that shows the pilot the type of station that is selected as active, be it a VOR or an ILS. Also

continually displayed is the selected radial. Other display features include a three light marker and a back

course indicator. The course deviation indicators are displayed as a dot matrix array that is easily

interpreted by the flight crew. The display incorporates the latest is high intensity LED technology which

provides excellent view ability even in direct sunlight.

The unit’s controls have been designed for simple user interface. The concentric knobs on the left side of

the unit select the standby frequency with a push button flip-flop to load the standby frequency into the

active window. The concentric knobs on the right side of the unit select the desired radial. The push button

on the right side knob set lets the user flip-flop the selected radial 180°. A long push of the right button will

produce the centered radial from the selected station.

The INS 429 has three internal receivers. The VOR/LOC receiver operating from 108.00 MHz to 117.95

MHz, the Glide Slope receiver which operates from 329.15 MHz to 335.0 MHz, and the Marker receiver

operating at 75 MHz. The INS 429 also has an external mode. The external mode is selected as a frequency

as described above. In external mode the INS 429 can be used as a standard NAV Indicator and coupled to

an external NAV or GPS receiver via the rear connector.

August 2008

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VAL Avionics INS 422 Manual del operador Pagina 4