Becker AR4201 Technical Instructions
Single block transceiver; single block transceiver
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- Installation and operation manual (50 pages) ,
- Operating instructions manual (22 pages) ,
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Becker Avionics GmbH • Baden-Airpark B108 • 77836 Rheinmünster • Germany
+49 (0) 7229 / 305-0 • Fax +49 (0) 7229 / 305-217
http://www.becker-avionics.com • E-mail: info@becker-avionics.com
Retrofit-Instructions
AR6201
Technical Instruction
Manual
AR6201 Retrofit-Instructions
Issue 01
November 2016
Article-No. 0649.996-071
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Table of Contents
Related Manuals for Becker AR4201
Summary of Contents for Becker AR4201
- Page 1 AR6201 Technical Instruction Manual AR6201 Retrofit-Instructions Issue 01 November 2016 Article-No. 0649.996-071 Becker Avionics GmbH • Baden-Airpark B108 • 77836 Rheinmünster • Germany +49 (0) 7229 / 305-0 • Fax +49 (0) 7229 / 305-217 http://www.becker-avionics.com • E-mail: info@becker-avionics.com...
- Page 2 General Description Preface Dear Customer, Thank you for purchasing Becker Avionics products. We are pleased that you have chosen our product and we are confident that it will meet your expectations. For development of our product, the guidelines for highest quality and reliability have been borne in mind, supplemented by selection of high quality material, responsible production and testing in accordance to the ISO 9001 and DIN EN 9100 standards.
- Page 3 AR6201 Retrofit-Instructions Issue 01 Article Number 0649.996-071 Cover Page 11/2016 Introduction 11/2016 Chapter 1 – 6 11/2016 Section / Issue Page No.: Description Chapter 1...20 First Edition © 2016 by Becker Avionics GmbH / all rights reserved Retrofit-Instructions Issue 01 November 2016 AR6201...
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Page 4: Table Of Contents
3.2.2. Temperature Sensor ......................12 3.2.3. RS232 Interface ........................ 12 3.2.4. AFCU/AGC/AFWB ......................12 3.2.5. CPIN (if Installed) ......................12 3.2.6. +13.75 V Switched (AR4201) - PWR_EVAL (AR6201) ............ 12 3.3. Verification ........................... 13 Post Installation Test ........................14 4.1.1. Mechanical Installation and Wiring Check ................ 14 4.1.2. - Page 5 Technical Instruction General Description List of Abbreviations List of Abbreviations Advisory Circular Aircraft Aircraft Flight Manual AFMS Aircraft Flight Manual Supplement Acceptable Means of Compliance Aircraft Model List Centre of Gravity Circuit Protection Device CSxx Certification Specification xx Electro Magnetic Compliance Electro Magnetic Interference Guidance Material Instructions for Continued Airworthiness...
- Page 6 Technical Instruction General Description General Safety Definitions Indicates a hazardous situation which, if not avoided, will result in death or serious injury. Indicates a hazardous situation which, if not avoided, could result in death or serious injury. Indicates a hazardous situation which, if not avoided, could result in minor or moderate injury.
- Page 7 Additional Conditions of Utilization For more details please refer to I&O manual: → AR620X Family. http://www.becker-avionics.com/downloads/ Non Warranty Clause We checked the contents of this publication for compliance with the associated hard and software. We can, however, not exclude discrepancies and do therefore not accept any liability for the exact compliance.
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Page 8: General Description
The retrofit work depends on the type of aircraft and its equipment. Therefore, this instructions only provides general information. 1.2. Device Assignment This manual is valid for the following devices: • Retrofitting AR4201 → AR6201 AR6201 Retrofit-Instructions Issue 01 November 2016... -
Page 9: Preparation - Transceiver Replacement
Technical Instruction Preparation - Transceiver Replacement Preparation - Transceiver Replacement 2.1. Visual Inspection • Inspect the structure of the VHF-COM installation area to be free from any mechanical defect like cracks or deformation. In case of any findings involve qualified and authorized personnel for trouble shooting and repair before performing retrofit-instructions. -
Page 10: Replacement Of The Transceiver
AR4201 → AR6201 3.1. In most cases, a retrofit of the AR4201 with an AR6201 will not cause any problems. In a few cases differences may occur due to pin incompatibility. The AR4201 normally is mounted from the rear side of the instrument panel. -
Page 11: Pin Compatibility Ar4201 - Ar6201
Technical Instruction Replacement of the Transceiver 3.2. Pin Compatibility AR4201 - AR6201 AR4201 - P1 AR6201 - P1 Pin Name AR4201 Function Pin Name AR6201 Function P1-1 AF-ASYM Speaker output, unbalanced SPK_HI Speaker output, unbalanced P1-2 AF-HI Headphone output, balanced HDPH1_A... -
Page 12: Dynamic Microphone Input
Technical Instruction Replacement of the Transceiver 3.2.1. Dynamic Microphone Input Retrofitting an AR4201 with the AR6201 in a typical glider installation with a dynamic microphone is shown below: Figure 3-1: AR6201 with Wiring Interface for AR4201 Connect the cable shielding to pin P1-6, which is the low side input for dynamic microphone. Because in AR6201 this input is balanced, the cable shield is no longer connected to ground (unlike it was with the AR4201). -
Page 13: Verification
Technical Instruction Replacement of the Transceiver 3.3. Verification • Check that the AR6201 is fixed correctly. • Check that the AR6201 wirings are completed. • Check the power supply lines and confirm correct polarity. • Check the power supply protection (fuse or circuit breaker). For the AR6201 a 7.5 A external circuit breaker or fuse shall be installed. -
Page 14: Post Installation Test
For details about "Installation Setup” please refer to I&O manual: → AR620X Family http://www.becker-avionics.com/downloads/ Note: It is assumed that the "Configuration Setup" has been done before the Post Installation Tests will be carried out. Once the 620X is installed, complete a test procedure to verify system functionality. Ensure compliance with authority required procedures. -
Page 15: Interference Check
Technical Instruction Post Installation Test 4.1.5. Interference Check • Check the 620X while engine is running and all other avionics/ electrical systems on the aircraft are powered, to verify that no significant interference exists. • Check also that the 620X does not cause significant interference with other systems. The installer´s standard test procedure may be used for the interference check and the table can be taken as a reference. -
Page 16: Flight Test Check
Technical Instruction Post Installation Test Channel Frequency (MHz) 121.140 121.1416 121.150 121.1500 121.155 121.1500 121.160 121.1583 121.165 121.1666 121.175 121.1750 121.180 121.1750 121.185 121.1833 121.190 121.1916 121.200 121.2000 121.205 121.2000 121.210 121.2083 131.240 131.2416 131.250 131.2500 131.255 131.2500 131.260 131.2583 131.265 131.2666 131.275... -
Page 17: Magnetic Compass Interference Test
Technical Instruction Post Installation Test 4.2. Magnetic Compass Interference Test • Check the interference of the magnetic compass in 30° steps over a full 360° turn. • Record the found deviation from the aircraft compass deviation table after the AR6201 installation. -
Page 18: Technical Data
In the airplane flight manual (AFM), weight, balance and electrical load records shall be updated after successful completion of this retrofit work. For current detailed data please refer to I&O manual: → AR620X Family http://www.becker-avionics.com/downloads/ AR6201 Retrofit-Instructions Issue 01 November 2016... - Page 19 Technical Instruction Technical Data Blank Retrofit-Instructions Issue 01 November 2016 AR6201...
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Page 20: Index
Warranty Conditions ..........7 We reserve the right to make technical changes. The data correspond to the current status at the time of printing. © 2016 by Becker Avionics GmbH / all rights reserved *** End of the Document *** AR6201...
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