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Summary of Contents for Garmin GA 35S
- Page 1 GA 35S Antenna Installation Manual 190-02466-00 July, 2024 Revision 3...
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Page 2: Aviation Limited Warranty
Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to... -
Page 3: Definitions Of Warnings, Cautions, And Notes
California to cause cancer, birth defects, or reproductive harm. This Notice is being provided in accordance with California's Proposition 65. If you have any questions or would like additional information, please refer to our web site at http://www.garmin.com/ prop65. 190-02466-00 GA 35S Installation Manual Rev. 3 Page i... -
Page 4: Software License Agreement
You further acknowledge the structure, organization, and code of the Software are valuable trade secrets of Garmin and/or its third-party providers and the Software in source code form remains a valuable trade secret of Garmin and/or its third-party providers. -
Page 5: Table Of Contents
4.1 Mounting, Wiring, and Power Checks................4-1 4.2 Configuration Setup ......................4-1 4.3 Diagnostic Information ....................4-1 4.4 Ground Checks ........................ 4-1 4.5 Software Loading Procedure ................... 4-1 Section 5 Continued Airworthiness..............5-1 190-02466-00 GA 35S Installation Manual Rev. 3 Page iii... - Page 6 Section 6 Connector Pinout Information............6-1 6.1 Pin Function List......................6-1 Appendix A Outline and Installation Drawings ..........A-1 Appendix B Interconnect Drawings..............B-1 190-02466-00 GA 35S Installation Manual Rev. 3 Page iv...
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Page 7: Section 1 Declaration Of Design And Performance
This manual is intended to provide mechanical and electrical information for use in the planning and design of an installation of the GA 35S into an aircraft. This manual is not a substitute for an approved airframe-specific maintenance manual, installation design drawing, or complete installation data package. -
Page 8: Unit Identification
1.2.1 Unit Identification The GA 35S can be identified by the part numbers listed in Table 1-1. Table 1-1 GA 35S Unit Identification Garmin P/N Garmin P/N Marketing Label (Unit Only) (Shipping Level) GMN-12853 GA 35S 011-05754-00 010-02639-00 1.2.2 Accessories Each of the following accessories are provided separately from the GA 35S. -
Page 9: Certification Statement
1.3.4) that may demonstrate additional airworthiness specification performance standards required by the European Aviation Safety Agency (EASA). The Appliance Project Identifier (API) for the GA 35S is GMN-12853. The API has been used for project identification with the FAA and EASA. - Page 10 Section 4 for instructions on configuration. TSOs listed in this section may require configuration. Coordinate with the applicable Garmin Program Manager to make sure the TSO functionality appropriate to your installation is enabled. Table 1-6 GA 35S (011-05754-00) TSO Compliance...
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Page 11: Interface Summary
1.3.2 TSO/ETSO Deviations Table 1-7 GA 35S (011-05754-00) Standard TSO Deviations Deviation Garmin has been granted a deviation to use RTCA/DO-160F as the standard for TSO-C190 Environmental Qualification and Test Procedures of Airborne Equipment. 1.3.3 Non-TSO Functions The GA 35S has no non-TSO functions. -
Page 12: Performance Technical Specifications
1.5.1 Environmental Qualification Form Reference It is the responsibility of the installing agency to obtain the latest revision of the GA 35S Environmental Qualification Form. This form is available directly from Garmin under the following part number: GA 3XS Environmental Qualification Form, Garmin part number 005-01217-00 To obtain a copy of this form, see the dealer/OEM portion of the Garmin web site (www.garmin.com). -
Page 13: Antenna Specifications
(TSO). Installation of this article requires separate approval . 1.7 Operating Instructions The GA 35S is a remote-mount antenna with no user controls or indicators. All user interface is accomplished through a compatible display and/or interface device. Loss of antenna function is communicated to the pilot by system messages. -
Page 14: Section 2 Installation Overview
The GA 35S has no cooling requirements or considerations. 2.6 Mounting Requirements The GA 35S mounting surface should be capable of providing a sufficient electrical bond to the aircraft to minimize radiated EMI and provide protection from High-Intensity Radiation Fields (HIRF). -
Page 15: Section 3 Installation Procedure
If the unit is damaged, notify the carrier and file a claim. To justify a claim, save the original shipping container and all packing materials. Do not return the unit to Garmin until the carrier has authorized the claim. Retain the original shipping containers for storage. If the original containers are not available, a separate cardboard container should be prepared that is large enough to accommodate sufficient packing material to prevent movement. - Page 16 (ex. GPS and SiriusXM) provided the combination antenna is TSO authorized and has been tested to meet Garmin’s minimum performance standards. b) The GPS antenna should be mounted no closer than two feet from any antennas emitting more than 25 watts of power.
- Page 17 (in a particular azimuth, when one antenna is blocked the other antenna may have a clear view). 190-02466-00 GA 35S Installation Manual Rev. 3 Page 3-3...
- Page 18 Figure 3-1 GPS Antenna Installation Considerations 190-02466-00 GA 35S Installation Manual Rev. 3 Page 3-4...
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Page 19: Antenna Doubler
AC 43.13-2( ) for guidance on manufacturing and installing doublers. Note that design features of the aircraft, such as pressurization, may require FAA approved installation design and substantiating data. Refer to the ‘Dealer Resource Center’ portion of the Garmin website, www.garmin.com, to obtain a copy of STC SA02018SE-D. 3.7 Antenna Grounding Antenna grounding is necessary for optimum antenna performance. -
Page 20: Antenna Installation
Use of these type sealants may void the antenna warranty. 3.9 Installation Approval Installation of any antenna should follow the aircraft TC or STC requirements. 190-02466-00 GA 35S Installation Manual Rev. 3 Page 3-6... -
Page 21: Section 4 Post Installation Configuration & Checkout
After accomplishing a continuity check, perform power and ground checks to verify proper power distribution to the GA 35S. Any faults or discrepancies must be corrected at this time. The GA 35S can be installed after completion of the continuity and power checks. -
Page 22: Section 5 Continued Airworthiness
5 CONTINUED AIRWORTHINESS Maintenance of the GA 35S is “on condition” only. For regulatory periodic functional checks, refer to approved aircraft maintenance manuals or manual supplements for actual aircraft maintenance requirements. 190-02466-00 GA 35S Installation Manual Rev. 3 Page 5-1... -
Page 23: Section 6 Connector Pinout Information
6 CONNECTOR PINOUT INFORMATION 6.1 Pin Function List 6.1.1 TNC Connector Figure 6-1. View of TNC Connector Looking From Front Of Antenna. 190-02466-00 GA 35S Installation Manual Rev. 3 Page 6-1... -
Page 24: Appendix A Outline And Installation Drawings
FABRICATE AND INSTALL A DOUBLER PLATE AS REQUIRED TO COMPLY WITH APPLICABLE AIRWORTHINESS REGULATIONS. MOUNTING HOLES FOR #8 PANHEAD SCREWS (4 PLACES). TOLERANCES FOR MOUNTING CUTOUT: INCH .XX±.02 REFERENCE ONLY .XXX±.010 REFERENCE ONLY Figure A-1 GA 35S Outline and Installation Drawing 190-02466-00 GA 35S Installation Manual Rev 3 Page A-1... -
Page 25: Appendix B Interconnect Drawings
APPENDIX B INTERCONNECT DRAWINGS GA 35S GPS RECEIVER GPS ANTENNA HI GPS ANTENNA LO Figure B-1 GA 35S Example Interconnect 190-02466-00 GA 35S Installation Manual Rev 3 Page B-1...
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