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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.

Содержание Motorola Series

Страница 1: ...ss and is being addressed on an as needed basis All references to AEM and NAT product part numbers and associated images are equivalent to Cobham product part numbers Contact info Cobham Aerospace Com...

Страница 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...

Страница 3: ...elephone 250 763 1088 Facsimile 250 763 1089 Website www aem corp com 2012 Anodyne Electronics Manufacturing Corp AEM All Rights Reserved SM71 NTA01 001 Motorola Series Radio Adapter These commodities...

Страница 4: ...ublication 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 phot...

Страница 5: ...led by revision shown in the footer of each page All revisions affecting sections of this manual have been incorporated AEM MANUAL REVISIONS Section Revision Number Revision Description Date All Rev 5...

Страница 6: ...troduction 2 1 2 2 Unpacking and Inspection 2 1 2 2 1 Warranty 2 1 2 3 Installation Procedures 2 1 2 3 1 Warnings 2 1 2 3 2 Cautions 2 1 2 3 3 Cabling and Wiring 2 2 2 3 4 Installation of Radio into N...

Страница 7: ...ce functions to integrate a car motorcycle radio into an aircraft environment such as power conversion mic excitation sidetone generation impedance matching and level conversion 1 3 Features The NTA01...

Страница 8: ...With radio 500 mA typical 28 Vdc Standby 2 75 A typical 28 Vdc transmitting at 10 W Power Output to radio 13 Vdc 10 5 A max 20 duty cycle Internal Fuse 7 A Breaker Current Rating 5 A Input Signals Mic...

Страница 9: ...ted output Receive Audio Output Regulation 10 variation when the load is changed to 75 and 400 of the rated load Relay Contacts 1 A 30 Vdc max Closed when keyline active Bi directional Signals RF Inpu...

Страница 10: ...it AEM part NTA IKC 1 4 3 Environmental Specifications Operating Temperature Low 30 C High 60 C Short time High 60 C Ground Survival Temperature Low 40 C High 85 C Altitude 15 000 ft 4 572 m Shock Ope...

Страница 11: ...Procedures 2 3 1 Warnings Do not bundle any lines from this unit with transmitter coax lines Do not bundle any logic audio or DC power lines from this unit with 400 Hz synchro wiring or AC power line...

Страница 12: ...unit in anti static bags Attached to the inside of the unit closest to the external connectors is the RF coaxial cable connector the power supply connector and a 15 pin ribbon cable J102 and at the o...

Страница 13: ...rnal adjustments that can be varied can be found on the top of the rear subassembly after removing the cover of the unit and are mic level sidetone and RX level as shown above These levels can be adju...

Страница 14: ...Interconnect NTA01 001 403 3 1 00 Astro Radio Adapter Interconnect NTA01 001 403 4 1 00 Astro Radio Adapter Interconnect NTA01 001 405 0 1 10 Astro Radio Adapter Connector Map NTA01 001 922 0 1 00 As...

Страница 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...

Страница 16: ...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...

Страница 17: ...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...

Страница 18: ...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...

Страница 19: ...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...

Страница 20: ...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...

Страница 21: ...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...

Страница 22: ...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...

Страница 23: ...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...

Страница 24: ...craft environment It provides all required interface functions to integrate a car motorcycle radio into an aircraft environment such as power conversion mic excitation sidetone generation impedance ma...

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