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Becker RT6201 - Installation and Configuration; General Requirements; Customized Applications; Antenna Installation

Becker RT6201
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Installation
Becker Avionics
Installation and Configuration
66 Transceivers 6200 Series DV14307.03 Issue 06 February 2021
2.6 Installation and Configuration
The minimum installation for the 62XX series transceivers is:
Power supply.
Antenna.
Microphone (direct or with external audio panel).
Headphone or speaker (direct or with external audio panel).
Push-To-Talk (PTT) switch.
General Requirements
For general instruction e.g. installation distance, cable types etc. please see "Installation
Requirements" page 47.
Type-specific cable harnesses are also available for the aircraft wiring (see "Accessories",
page 41).
No RF antenna cables or HF cables should be included in the cable harnesses of the
system.
Prevent routing of the cable harness along with other wiring, which carry audio power or
pulses.
Examine the wiring carefully before power up the device(s) and examine
particularly correct connection of the power supply lines.
Customized Applications
Customized applications and wiring and configuration adjustments.
Applications
Reference
Single Seat Glider
page 88
Twin Seat Motor Glider
page 94
General Aviation (GA) Aircraft
page 96
Individual Dual Headset Installation (two IC Circuits)
page 98
Twin Seat with AR62XX (Tandem-Installation)
page 100
Four Seat Installation (no Tandem)
page 102
Installation with RT62X1 and RCU62X1Fehler! Verweisquelle konnte
nicht gefunden werden.
page Fehler! Textmarke
nicht definiert.
Installation in Aircraft with Intercom System
page 104
Twin Seat with RT62X1 (Tandem-Installation)Fehler! Verweisquelle
konnte nicht gefunden werden.
page Fehler! Textmarke
nicht definiert.
Antenna Installation
A distance of 50 cm from the COM antenna to any installed GPS antenna is necessary
and a distance as far away from any ELT antenna.
Refer always to the manufacturer's instructions for antenna installation.
Make the antenna installation in accordance with AC 43.13-2B Chapter 3.
For penetration of the pressurized cabin on a pressurized aircraft are additional
data necessary which are not contained in this installation manual.

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