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7

TECHNICAL INFORMATION

Unit size ................................

40 x 35 x 95 millimetres

Fitting area required ..........

110 x 35 x 110 millimetres

Radio Lead length .........................................

2 Metres

Stand-by power consumption ..................

< 100 

µ

Amp

Transmit power consumption ...................

< 30 mAmp

P.T.T. Input .............................

Normally-Open Contact

SPECIFICATION

Technical information is provided in this section which may be useful
during the installation of the interface unit. Additional information can
be obtained directly from Lynx Avionics.

Radio Type

Each interface is configured to work with a specific make and model
of radio transceiver; the individual radio type configuration is marked
on the back of each unit.

P.T.T. Input

Several types of 'Push-To-Transmit' switch are available from Lynx
for direct connection to the interface unit and for use in different

applications. Connectors are also available which allow any 'Normally-
Open Contact' switch to be used to key a radio transmission.

Headset Extension Lead

Headset Extension Leads are available from Lynx for use with Micro
System Headsets. The leads are available in two-metre lengths, and
are fitted with one male connector and one female connector.

Radio Interference

The main cause of radio interference can usually be attributed to the
aircraft engine electrical system. High-tension ignition systems, and
strobe lights, emit strong electromagnetic signals which are received
by the radio antenna and amplified along with the radio reception.
  Micro System communication equipment is virtually immune to
interference from electromagnetic radiation, but can not prevent
interference being introduced into the system by the radio. When
using a radio in an aircraft there are several simple steps that can be
followed to minimise the problem of interference, and considerably
improve the quality of radio reception.
  Mount the radio antenna as far away from the engine as possible
and avoid routing the antenna lead close to the engine. Fit the engine
ignition leads with suppressors or suppressed plug caps as a matter
of course. If necessary screen the ignition leads using a braided
sleeve earthed to the airframe. Finally avoid fitting strobe lights and
their associated power leads near to the antenna and its lead.

©

 Copyright Lynx Avionics       MCMXCVII      All Rights Reserved

Summary of Contents for Micro System

Page 1: ...INSTRUCTIONS RADIO RADIO INTERF INTERFA ACE CE...

Page 2: ...been prepared to provide users of the Lynx Micro Communications System with the necessary information to enable safe and correct use Please read this booklet carefully and take time to familiariseyour...

Page 3: ...CONTENTS SECTION PAGE N 1 INTRODUCTION 1 2 SYSTEM CONFIGURATION 3 3 INSTALLATION 5 4 SPECIFICATION 7...

Page 4: ...proximity to engine ignition systems the interface electronics are designed to be virtually immune to electrical interference All electronic component parts of the unit including the leads and connec...

Page 5: ...ernal switch to be connected During the operation of a P T T switch one of the headset microphones is opened for radio transmission and the microphone of any additional headset is muted In order to pr...

Page 6: ...3 FIG 3 INTERFACE CONFIGURATION RADIO OPTIONAL P T T SWITCH BUILT IN P T T SWITCH INTERFACE UNIT...

Page 7: ...ing operation If necessary the headset leads can be extended by fitting an extension lead to the unit Depending on the application it may be desirable to fit either one or two headset extension leads...

Page 8: ...into the back of the unit for mounting purposes The threads accept M4 x 1 0 metric machine screws and allow the body of the interface to be screwed directly to a panel or bulkhead When mounting the u...

Page 9: ...ut do allow the unit to be easily fitted or removed The clips should be securely attached to the unit using the screws supplied fig 5 Cable Routing All cables connected to the interface should be care...

Page 10: ...available in two metre lengths and are fitted with one male connector and one female connector Radio Interference The main cause of radio interference can usually be attributed to the aircraft engine...

Page 11: ...4 8 FIG 6 MOUNTING HOLE DIMENSIONS 17 5 17 5 18 18 55 M4 x 1 0 THREAD ALL DIMENSIONS IN MILLIMETRES...

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