COBHAM AEM AA35-001 Quick Start Manual Download Page 2

 

Proprietary Information: Use or disclosure of this data is subject to the restrictions specified in the introductory 

section of this document 

 

Page 1 

REVISION 1.00.150430

 

 

PROPRIETARY NOTICE 

PROPRIETARY STATEMENT 

This document contains confidential and proprietary information and is the property of Chelton Avionics, Inc., a subsidiary of 
Cobham plc.  It is to be provided in confidence on the condition that by receipt it is not reproduced or copied in whole or in part, or 

used to furnish such information to others, or to make use of it for purposes other than specified by the Usage Statement.  The 
previous statement shall not apply to the extent that such statement violates any federal or state laws requiring such information to 

be made available to the public.  Non-current versions of this document must be returned to Chelton Avionics, Inc. or destroyed or 
shredded in a manner that renders the document completely and totally unusable and illegible. 

EXPORT CONTROLS  STATEMENT 

The technical data within this document is controlled for export under the export administration regulations (EAR), 15 CFR PARTS 

730-774,  violations of these laws may be subject to fines and penalties under the export administration act.  

 

FCC STATEMENT 

This device complies with part 15 of the FCC Rules. Operation is subject to the following two 

conditions: (1) This device may not cause harmful interference, and (2) this device must accept any interference received, including 
interference that may cause undesired operation. Before operating the products covered by this document, read the operating 

instructions for safe usage.  Regarding Part 15.21, changes or modifications not expressly approved by the party responsible for 
compliance could void the user’s authority to operate the equipment. 

USAGE STATEMENT 

The data in this document was developed only to maintain systems and/or parts manufactured by, manufactured for, or approved 

by Cobham. The data may not be applicable to any other systems and/or parts, regardless of their apparent similarity to systems 
and/or parts manufactured by, manufactured for, or approved by Cobham.  Do not rely, in any way, on data in this document to 

maintain or otherwise support systems and/or parts that were not manufactured by, manufactured for, or approved by Cobham, 
without evidence that the Federal Aviation Administration or other regulatory agency has determined that the data in this document 

is valid for such use. This document shall not be used for the development, manufacture, service, support, modify, overhaul or 
obtain FAA or any other regulatory approval of any other products than are specified within.   

Cobham assumes no liability whatsoever, whether contractual, warranty, tort or otherwise, for unauthorized work not performed in 
accordance with Chelton Avionics, Inc. approved procedures. 

DOCUMENT COPYRIGHTS 

Recipients agree to hold the contents of this document in confidence and agree to use only for the recipients internal purposes to 
maintain the referenced equipment.  This document and its contents shall not be used, reproduced, transmitted, or distributed for 

any other purpose.  The recipient also agrees to not disclose, share, or copy for distribution any of the contents of this document to 
any third party except as provided by written permission from Chelton Avionics, Inc.  Copy or disclosure of the contents of this 

document by anyone without the written approval of Chelton Avionics, Inc. may result in criminal or civil liability.  

DISCLAIMER 

The content of this document has been reviewed for accuracy and is believed to be reliable, however no responsibility is assumed 
for typographical errors and inaccuracies.  Chelton Avionics, Inc. reserves the rights to revise the contents within to improve 

accuracy and apply updated information related to design and serviceability without prior notice to users.  The latest published 
revision is the only version authorized for use. 

PROPERTY AND COPYRIGHT STATEMENT 

The copyright and ownership of all manuals, drawings, specifications and data as may be provided by Chelton Avionics, Inc. within 

this document shall remain the property of Chelton Avionics, Inc.   
 

All other brand and product names are trademarks or registered trademarks of their respective holders. 

Copyright

©

 Chelton Avionics, Inc.

 

All Rights Reserved 

Cobham Aerospace 

Communications 

6400 Wilkinson Drive 

Prescott, AZ USA 86301 

T: (928) 708-1550 

F: (928) 541-7627

 

 

 

These commodities, technology or software are controlled in accordance with the United States Export Administration Regulations, Export Classification
Control Number(ECCN) EAR99. When exporting, diversion contrary to U.S. law is prohibited.

Summary of Contents for AEM AA35-001

Page 1: ...nces to AEM and NAT product part numbers and associated images are equivalent to Cobham product part numbers Contact info Cobham Aerospace Communication 6400 Wilkinson Drive Prescott Arizona 86301 Tel...

Page 2: ...t were not manufactured by manufactured for or approved by Cobham without evidence that the Federal Aviation Administration or other regulatory agency has determined that the data in this document is...

Page 3: ...4N7 Telephone 250 763 1088 Facsimile 250 763 1089 Website www aem corp com 2012 Anodyne Electronics Manufacturing Corp AEM All Rights Reserved SM25 AA35 001 Audio Mixer Panel These commodities technol...

Page 4: ...ion is the property of AEM and is protected by Canadian copyright laws No part of this document may be reproduced or transmitted in any form or by any means including electronic mechanical photocopyin...

Page 5: ...ISSUE REVISION RECORD Manual Issue Number Section Revision Number Revision Description Issue Date 4 01 Section 1 Rev 1 00 Section 2 Rev 1 00 Section 3 Rev 1 00 Rewritten in latest format Oct 10 2008...

Page 6: ...2 1 Warranty 2 1 2 3 Continued Airworthiness 2 1 2 4 Installation Procedures 2 1 2 4 1 Warnings 2 1 2 4 2 Cautions 2 2 2 4 3 Cabling and Wiring 2 2 2 4 4 Post Installation Checks 2 2 2 5 Adjustments a...

Page 7: ...also available in remote mount configurations see Section 1 5 1 3 Design Features The AA35 001 Audio Mixer Panel provides six independent channels with differential inputs and balanced outputs for hi...

Page 8: ...cuitry Type Balanced output for high common mode noise rejection Coupling 50 dB input to output Crosstalk Audio Noise Level 60 dB down from rated output level Without Signal Output Regulation at 400 1...

Page 9: ...up to six in six out or six in one composite out 2 5 Vrms or 7 Vrms input level Output 7 7 Vrms or 100 mW 600 Ohm max Panel Lighting 28 Vdc normal AA35 100 Remote mount audio mixer summing amplifier P...

Page 10: ...Certificate of Conformity Verify that all items are present before proceeding and report any shortage immediately to your supplier 2 2 1 Warranty All Anodyne Electronics Manufacturing Corp AEM produc...

Page 11: ...termination details Note that the hood is a clamshell hood and is installed after the wiring is complete Aircraft harnessing shall permit the unit to be removed from the panel for easy access to all s...

Page 12: ...ven 8 600 adjustment jumpers JP1 thru JP7 Each jumper controls one of the six independent channels or the Composite Output refer to table 1 When the jumper is connected across pins A and B the channel...

Page 13: ...to complete the installation The kit consists of the following D37SV IKC Quantity Description AEM Part 1 D min 37 Socket Housing 20 21 037 37 MS Crimp Socket 20 26 901 1 37 Pin JVL Hood Locklever 20...

Page 14: ...technology or software are controlled in accordance with the United States Export Administration Regulations Export Classification Control Number ECCN EAR99 When exporting diversion contrary to U S l...

Page 15: ...technology or software are controlled in accordance with the United States Export Administration Regulations Export Classification Control Number ECCN EAR99 When exporting diversion contrary to U S l...

Page 16: ...00 905 0 AUDIO MIXER PANEL 1 1 1 of 3 2 00 RAS 8 CHANGED TO AEM LOGO UPDATED HOLE SCHEDULE OCT 25 11 RDB 27 Oct 11 Oct 25 11 These commodities technology or software are controlled in accordance with...

Page 17: ...D AEM LOGO ADDED Reviewed Approved RAS 8 Tony Pearson Designer Oct 27 2011 These commodities technology or software are controlled in accordance with the United States Export Administration Regulation...

Page 18: ...o 2 5 or 7 Vrms Output impedance of each channel is individually selectable via internal jumpers to allow the connection of an 8 or 600 load 3 3 Controls and Indicators 3 3 1 Channel Controls The AA35...

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