Honeywell KMA28 Section I General Information, Introduction, Scope, Equipment Description

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Bendix/King

KMA28

Audio Amplifier/Intercom/Marker Beacon Receiver

Section I GENERAL INFORMATION

1.1INTRODUCTION

The KMA 28 represents the next step in cockpit audio control and intercommunications. Using proprietary IntelliVox® design, this unit eliminates the requirements for intercom squelch adjustments. The unit is designed for outstanding ergonomics and visually de- fined mode annunciation and selection.

Before installing and/or using this product, please read this manual completely. This will ensure that you will take full advantage of all the advanced features in the KMA 28.

1.2SCOPE

This manual provides detailed installation and operation instructions for the Honeywell, Inc. KMA 28 Audio Selector Panel/Intercom System

Model

Description

Part Number

KMA 28

Stereo Audio Panel with Marker

066-01176-0101

1.3EQUIPMENT DESCRIPTION

The KMA 28 is a state of the art audio isolation amplifier and audio selector that contains an automatic voice activated (VOX) intercom system. It can switch up to three transceiv- ers (Com 1, Com 2 and Com 3) and six receivers (Nav 1, Nav 2, ADF, DME, MKR and AUX).

The TEL mode allows the KMA 28 to act as an audio interface between aircraft head- phone and microphones and specific aircraft approved (FAA/FCC) cellular telephone equipment.

Warning: Use of non-aviation approved cellular telephone equipment may be prohibited by regulation. Honeywell, Inc. is not responsible for unauthorized airborne use of cellular telephones.

There are two unswitched inputs, for autopilot disconnect, and/or radar altimeter warning. Push buttons select the receiver audio source provided to the headphones. A SPR button allows the user to listen to the receiver(s) selected on the cabin speaker. Except for the unswitched inputs, all speaker audio is muted during transmit.

A rotary switch selects one of the three communication transceivers for the pilot and co- pilot position, and allows radio transmission. In "Split Mode" the KMA 28 has the ability to allow the pilot and copilot to operate different transceivers independently. The TEL mode allows the pilot to use the cellular telephone interface. External switches permit telephone operation for the copilot and passengers.

An emergency mode connects the pilot headphone and microphone to COM 1 if power is removed for any reason, or if the power switch is placed in the Off (emergency ) position.

IntelliVox® is a trademark of PS Engineering, Incorporated, and used with their permission

006-10565-0000

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Rev. 0, Sept. 2000

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Contents BENDIX/KING Table of Contents Cellular Interface Checkout Section I General Information IntroductionScope Equipment DescriptionApproval Basis TSO ApprovalSpecifications TSO ComplianceIntercom Specifications Equipment SuppliedEquipment Required but not Supplied License RequirementsSection II Installation Equipment Installation ProceduresGeneral Information Unpacking and Preliminary InspectionMounting Rack Installation Connector AssemblyCable Harness Wiring NoiseExisting KMA-24 Installation Existing PS Engineering PMA6000 installationsPower Communications Push-to-TalkSwap Mode Unswitched inputsIntercom wiring BacklightingCom 3 Audio Public Address functionMarker Installation Communications Antenna Installation Notes AdjustmentsWireless telecommunications interface Hook Switches KMA 28 Pin Assignments Unit Installation Post Installation CheckoutOperational Checkout Marker Checkout Receiver SensitivityCellular Interface Checkout Final InspectionSection III KMA28 Operation Audio SelectorKey click Speaker AmplifierPublic Address PA Function Power Switch /Emergency EMG OperationMicrophone Selector Swap Mode Switch from Com 1 to Com 2 remotely Split ModeSplit Mode ICS Telephone ModeIntercom System IntelliVox VOX-SquelchMono headsets in Stereo Installation Volume ControlIntercom Modes Soft Mute and Soft Mute inhibit Marker Beacon Operation Telephone Operation if equipped with approved systemWill lose intercom capability when it is in use Connector viewed from the rear Appendix a Installation DrawingsTray Dimensions in inches Top View Tray Assembly Drawing Appendix B Bottom Connector Interconnect Bottom Connector, J1Appendix C Top Connector Interconnect J2 TOP ConnectorInstructions for Continuing Airworthiness Instructions for FAA FormConditions Section Conducted Tests