IPH-0061100Airborne Communications Transceiver operated under

December 9, 2001 Federal Communications Commission Equipment Approval Services P.O. Box 35815 Pittsburgh, PA 15251-3315 Applicant:Garmin International, Inc. 1200 east 151 ST Street Olathe, KS 66062 Telephone number (913) 397-8200 FRN 0005-0885-88 Equipment:FCC ID: IPH-0061100 FCC Rules:Part 87 Gentlemen: The Application for Certification of Intentional Radiators operated in the under part 87 (Aviation Services) has been completed. The 731 form and application have been electronically submitted and any attachments will be up loaded to your web site. Please use this information in obtaining a grant of certification for the aviation services transceiver. The receiver will be verified per parts 2 and 15 of the CFR. This transceiver will operate on 25 kHz or 8.33 kHz channel spacing. A request for rule waiver has been filed with the FCC. The FAA has notified of the transceiver design and FCC submittal. Please proceed with the grant of certification upon review of the uploaded information. Should you require any further information, please contact the undersigned. Thank you for your consideration in this matter. Sincerely, Scot Rogers Rogers Labs, Inc. Enclosures ROGERS LABS, INC. 4405 West 259 th Terrace Louisburg, KS 66053 Phone / Fax (913) 837-3214

December 9, 2001 Federal Communications Commission Equipment Approval Services P.O. Box 35815 Pittsburgh, PA 15251-3315 Applicant:Garmin International, Inc. 1200 east 151 ST Street Olathe, KS 66062 Telephone number (913) 397-8200 Re: Confidentiality of schematics Equipment:FCC ID: IPH-0061100 Gentlemen: It is requested that the information contained in the block diagrams, operational description and schematics of the application be held confidential per Section 0.459. Please use this information in obtaining a grant of certification for the aviation transceiver model number GNS430A. In support of this request, we submit the following: 1. Identification of the specific information for which confidential treatment is sought: The materials set fourth in the Operational Description, Block Diagram, and Schematics, are those for which confidentiality is sought. 2. Identification of the Commission proceeding in which the information was submitted or a description of the circumstances giving rise to the submission: The proceeding is that involving the application for equipment authorization (certification) under FCC ID No: IPH-0061100 3. Explanation of the degree to which the information is commercial or financial, or contains a trade secret or is privileged: This material includes a detailed theory of operation and circuit diagrams, (schematics and Block diagrams). As such this material is treated as highly confidential business information and is not subject to public view. Should you require any further information, please contact the undersigned. Thank you for your consideration in this matter. Sincerely, Scot Rogers Rogers Labs, Inc. ROGERS LABS, INC. 4405 West 259 th Terrace Louisburg, KS 66053 Phone / Fax (913) 837-3214

December 04, 2001 Federal Communication Commission c/o Mellon Bank 500 Ross Street Room 670 Pittsburgh, PA 15251-5130 Atten: Mellon Client Service Center - Wireless Bureau Applications P.O. Box 358130 SUBJECT: Request for Rule Waiver of 47 CFR 87.173 to allow Type Acceptance of GARMIN aeronautical VHF Transceiver with 8.33 kHz channel spacing Reference: FCC Type Acceptance application under ID # IPH-0061100 FCC Order DA 98-275 dated February 11, 1998 FCC Order DA 98-1176 dated October 6, 1998 Gentlemen: GARMIN International, Inc. (GARMIN) manufactures aeronautical VHF transceivers which are installed in aircraft worldwide. GARMIN is preparing an application for Certification of an aeronautical VHF transceiver (FCC Identification Number IPH- 0061100). This transceiver has been designed to comply with the new ICAO requirements to transmit and receive on channels that are spaced at 8.33 kHz intervals. The pilot may adjust the channel spacing to either 8.33 kHz or 25 kHz to comply with the local requirements of the area in which he is operating. The FCC Equipment Authorization Division has indicated that a waiver of Section 87.173 of the Commission’s rules and regulations is necessary to allow Certification of aeronautical VHF transceivers that are capable of 8.33 kHz channel spacing. GARMIN respectfully requests a rule waiver to deviate from the 25 kHz channel spacing requirements in 47 CFR 87.173 to allow FCC Certification of our transmitter which utilizes the frequency range as follows: 118.000 MHz - 136.975 MHz in 25 kHz steps or 118.000 MHz - 136.990 MHz in 8.33 kHz steps. Precedence for a rule waiver in this circumstance has been established by other radio manufacturers and GARMIN that have requested and received from the Commission a rule waiver regarding 8.33 kHz channel spacing used in VHF aeronautical transceivers. (reference FCC Order DA 98-275 dated February 11, 1998 and FCC Order DA 98-1176 dated October 6, 1998) The 8.33 kHz channel spacing standard was recommended by the International Civil Aviation Organization (ICAO) in 1995 to address increasing shortages of air traffic control VHF radio frequencies around the world, particularly in western Europe. At least eight western European states are scheduled to implement the 8.33 kHz channel spacing on October 7, 1999. GARMIN believes that Commission approval of a waiver to allow Certification with 8.33 kHz channel spacing is consistent with U.S. international commitments to ensure air safety by providing for efficient VHF communications during flights between the United States and Europe and is therefore in the public interest. It is neither efficient, cost effective, nor necessarily safe to require aircraft operating in both U.S. and European airspace to carry two VHF transceivers; one with Commission certification that can utilize only the frequencies listed in 87.173 and another capable of 8.33 kHz channel spacing but without Commission Certification. U.S. industry and the FAA have recognized that U.S. registered aircraft will need to operate in European airspace and that European registered aircraft will need to operate in U.S. airspace. RTCA, Inc. and ARINC have approved U.S. VHF transceiver standards including the 8.33 kHz channel spacing capability based on the ICAO recommendation. The FAA has recognized these recommendations by approving FAA certification and installation of FCC Type Accepted VHF transceivers with 8.33 kHz channel spacing on Type Certificated aircraft. Time is of the essence. Your early review and approval is appreciated. Sincerely, Van Ruggles Director, Quality Assurance Enclosure: FCC Form 159 (payment by credit card) FCC Form 605, as required by 47 CFR 1.1102 cc: Mr. Steven Dayhoff (by email, [email protected]])

January 22, 2002 Federal Communications Commission Equipment Approval Services P.O. Box 35815 Pittsburgh, PA 15251-3315 Applicant: Garmin International, Inc. 1200 east 151 ST Street Olathe, KS 66062 Telephone number (913) 397-8200 FRN 0005-0885-88 Equipment: Aviation transceiver FCC ID: IPH-0061100 FCC Rules: Part 87 Re: Correspondence reference number: 21808 MR. Stan Lyles: In response to the request for additional information, correspondence reference number 21808, part of which is reproduced here for reference, the following information is submitted. To: Scot Rogers, null From: Stan Lyles [email protected] FCC Application Processing Branch Re: FCC ID IPH-0061100 Applicant: Garmin International Inc Correspondence Reference Number: 21808 731 Confirmation Number: EA733784 1.) What's the difference to make this device narrow band? 2.) Page 10 of test report spurious emmissions at antenna terminals, this test should be modulated Per Section 2.1049. 3.) .) Please note that the attenuation requirement for radiated spurious emissions is referenced to the desired signal yielding dBc. The attenuation specification is not XX uV/M, or derived from absolute value of the field strength. The dBc is determined from the substitution method such as described in the ANSI/TIA/EIA-603-1992 document. What is needed is a determination of the actual power levels necessary to reproduce these field strength levels. Those power levels (from a signal generator source and a dipole antenna replacing the EUT) are then compared to the power output of the transmitter to determine dBc. That is the basis of the "substitution method". ROGERS LABS, INC. 4405 West 259 th Terrace Louisburg, KS 66053 Phone / Fax (913) 837-3214 ? Page 2 January 22, 2002 Please submit data / results obtained in this manner. 4.) Page 15 Step 4 of test report shows input voltage from 5.10 Vdc to 6.90 Vdc. Page 16 of test report shows input voltage 23.80 Vdc, 28.00 Vdc and 32.20 Vdc. Please clarify. 5.) Please submit a reply copy of FAA letter. All filing are electronic. Response: 1.) There is no difference to make this radio a narrow band device. It functions in the same manner as an earlier version of this aviation transceiver (FCC ID number IPH-0021400). 2.) The spurious emissions at the antenna terminal were tested with the unit modulated as required by section 2.1049. 3.) The radiated spurious emissions have been retested and results are included in the revised test report (file name GNS430A.pdf) which has been uploaded to the FCC web site. 4.) The type error on page 15 of the report has been corrected. 5.) The FAA does not return a letter to the manufacturer unless they have a concern about the equipment. The letter informing the FAA about the transceiver (file named gns430a_faa_fcc.pdf) has been uploaded to the FCC web site for your review. Please proceed with the grant of certification procedure. Should you require any further information, please contact the undersigned. Thank you for your consideration in this matter. Sincerely, Scot Rogers Rogers Labs, Inc. Enclosures

February 22, 2002 Mr. Stan Lyles Federal Communications Commission Equipment Approval Services P.O. Box 35815 Pittsburgh, PA 15251-3315 Applicant: Garmin International, Inc. 1200 east 151 ST Street Olathe, KS 66062 Telephone number (913) 397-8200 FRN 0005-0885-88 Equipment: FCC ID: IPH-0061100 FCC Rules: Part 87 Mr. Lyles: Please find the correspondence I have had with Van Ruggles, of Garmin, about the issues remaining on the GNS430A submittal. It is our understanding that the FAA has no problem with the submittal and if they did, they would have stopped the grant process long ago. I uploaded a PDF file of the rule waiver to the web site, and left it under the cover letters section. Please let me know if you still require information from us. Garmin would very much appreciate getting the grant of certification out of everyone way. Thank you for your help and consideration in resolving this matter. Sincerely, Scot Rogers Rogers Labs, Inc. Enclosures ROGERS LABS, INC. 4405 West 259 th Terrace Louisburg, KS 66053 Phone / Fax (913) 837-3214 ? Page 2 February 22, 2002 No letter back. In the past, the FAA Spectrum folks have 30 days to respond with questions or to stop it at the FCC. To my knowledge, no response is taken as "A-OK" from the Spectrum folks. -----Original Message----- From: Scot Rogers [mailto:[email protected] ] Sent: Friday, February 22, 2002 8:27 AM To: 'Ruggles, Van' Subject: FW: Rule Waiver for FCC submittal IPH-0061100 Hello Van, I took the liberty to send a copy of the waiver to Stan Lyles at the FCC and received this word back from him this morning. Did you ever get a letter from the FAA? I thought they did NOT send a letter unless they thought there was a problem. Anyway, think about this and get back with me. Thanks Scot ________________________________________________ Scot Rogers Rogers Labs, Inc. 4405 West 259th Terrace Louisburg, KS 66053 Telephone/fax number (913) 837-3214 -----Original Message----- From: Stanley Lyles [mailto:[email protected] ] Sent: Friday, February 22, 2002 7:50 AM To: [email protected] Subject: Re: Rule Waiver for FCC submittal IPH-0061100 Hello Scot, I haven't received the Waiver for Garmin. Could you re-send the Waiver for Garmin in EAS. Also, as a reminder we still need a reply letter copy from FAA uploaded in EAS. Stanley Lyles >>> "Scot Rogers" <[email protected]> 02/21/02 04:21PM >>> Hello Stan, I have uploaded the FCC Rule Waiver for the Garmin IPH-0061100 submittal. Please proceed with the grant of certification. Thank you for your help. Scot Rogers ________________________________________________ Scot Rogers Rogers Labs, Inc. 4405 West 259th Terrace Louisburg, KS 66053 Telephone/fax number (913) 837-3214

Federal Communications Commission DA 02-379 Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of GARMIN INTERNATIONAL, INC. Request for Waiver of Section 87.173(b) of the Commission's Rules Governing Assignable Carrier Frequencies in the Aviation Services ) ) ) ) ) ) ) ) ORDER Adopted: February 19, 2002 Released: February 20, 2002 By the Acting Chief, Public Safety and Private Wireless Division, Wireless Telecommunications Bureau: I. INTRODUCTION 1. Under consideration is a request for waiver filed by GARMIN International, Inc. (Garmin) on December 4, 2001. 1 Garmin seeks waiver of Section 87.173(b) of the Commission's Rules 2 to permit type certification of VHF aircraft transceiver capable of transmitting on both the 25 kHz spaced channels currently authorized pursuant to Section 87.173(b) of the Commission's Rules and on the 8.33 kHz spaced channels that are used in certain countries in Europe and in the United Kingdom. Such transceivers are known as dual spacing transceivers. For the reasons discussed herein, we grant the requested waiver regarding operation of the Rockwell Collins transceivers with 25 kHz and 8.33 kHz channel spacing, subject to the Commission’s decision regarding a pending Notice of Proposed Rule Making that proposes to amend our rules to permit the type certification of dual spacing transceivers. We note, however, that this Order does not authorize aircraft to transmit on 8.33 kHz spaced channels within airspace of the United States, its territories or the Commonwealth of Puerto Rico, but is limited to permitting type certification of specified transceivers capable of transmitting on both 25 kHz spaced channels in the United States and on the 8.33 kHz spaced Aeronautical Mobile Service (AMS) channels used in certain other countries. II. BACKGROUND 2. In March of 1997, the International Civil Aviation Organization (ICAO), an international body operating under the auspices of the United Nations, amended its International Standards and Recommended Practices to incorporate a channel plan specifying 8.33 kHz channel spacings in the AMS. 3 The 8.33 kHz 1 Letter to Federal Communications Commission, from Van Ruggles, Director, Quality Assurance, GARMIN International, Inc., dated December 4, 2001. (Garmin Letter). 2 47 C.F.R. § 87.173(b). 3 See International Standards and Recommended Practices, Aeronautical Telecommunications, Annex 10 to the Convention on Civil Aviation, Vol. V, Aeronautical Radio Frequency Spectrum Utilization, Amendment No. 72, International Civil Aviation Organization, Montreal, 1997 (ISRP). When the ICAO adopts an International Standard and Recommended Practice, it is binding on the contracting countries. See Amendment of Part 87 of the Commission's Rules to Establish Technical Standards and Licensing Procedures for Aircraft Earth Stations, Report (continued....) Federal Communications Commission DA 02-379 2 channel plan was adopted to alleviate the shortage of VHF Air Traffic Control (ATC) channels experienced in western Europe and in the United Kingdom. 4 Seven western European countries and the United Kingdom implemented the 8.33 kHz channel plan in 1999. 5 Accordingly, aircraft operating in the airspace of these countries must have the capability of transmitting and receiving on the 8.33 kHz spaced channels. 3. Section 87.39 of the Commission's Rules requires that (1) U.S.-registered aircraft employ type certified radios; and (2) aircraft radios must meet the technical requirements of Subpart D of Part 87 of the Commission's Rules in order to be type certified under the Commission’s Rules. 6 Subpart D of Part 87 contains a list of "assignable carrier frequencies or frequency bands" and includes carrier frequencies in the VHF aircraft band used for ATC communications (namely, 117.975 MHz to 136.975 MHz). 7 The listed frequencies are based on 25 kHz spacing. There is no provision in the Commission's Rules for operating on 8.33 kHz spaced channels as envisioned by the ICAO channel plan. Accordingly, type certification of dual spacing transceivers may not be obtained absent a waiver of Section 87.173(b) of the Commission’s Rules. However, the Commission has released a Notice of Proposed Rule Making to review the Aviation Radio Service rules and seeks comment on whether to permit the certification of dual spacing transceivers for aircraft also operating in countries which employ 8.33 kHz channel spacing. 8 III. DISCUSSION 4. Section 1.925 of the Commission's Rules provides that we may grant a waiver if it is shown that (a) the underlying purpose of the rule(s) would not be served or would be frustrated by application to the instant case, and grant of the requested waiver would be in the public interest; or (b) in light of unique or unusual circumstances, application of the rule(s) would be inequitable, unduly burdensome, or contrary to the public interest, or the applicant has no reasonable alternative. 9 We find that the waiver requested by Garmin is warranted under the circumstances presented. Specifically, we conclude that the underlying purpose of the subject rules would not be served by application to the instant case and grant of the requested waiver would be in the public interest. We note, as an initial matter, that we have granted similar waivers regarding dual spacing transceivers. 10 As we have noted previously, two industry standard setting (Continued from previous page) and Order, PR Docket No. 90-315, 7 FCC Rcd 5895, 5896 n.12 (1992). However, contracting countries are not required to implement 8.33 kHz spacing if their current channel spacing standards provide an adequate number of frequencies. ISRP at 6, para. 4.1.2.1 (note). 4 See Plan for the 8.33 kHz Channel Spacing Implementation in Europe (8.33 kHz Spacing Plan), Edition 2.0, European Civil Aviation Conference, Dec. 2, 1996 at 2. 5 The implementing countries are Austria, Belgium, France, Germany, Luxembourg, Netherlands, Switzerland and the United Ki…

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ROGERS LABS, INC.Garmin International, Inc. 4405 W. 259th TerraceMODEL: GNS430A Louisburg, KS 66053Test #: 011119 Phone/Fax: (913) 837-3214Test to: FCC Parts 2 and 87Page 1 of 2 GNS430AExtPho.doc 11/29/2001 External Photgraphs for GNS430A ROGERS LABS, INC.Garmin International, Inc. 4405 W. 259th TerraceMODEL: GNS430A Louisburg, KS 66053Test #: 011119 Phone/Fax: (913) 837-3214Test to: FCC Parts 2 and 87Page 2 of 2 GNS430AExtPho.doc 11/29/2001

ROGERS LABS, INC.Garmin International, Inc. 4405 W. 259th TerraceMODEL: GNS430A Louisburg, KS 66053Test #: 011119 Phone/Fax: (913) 837-3214Test to: FCC Parts 2 and 87Page 1 of 1 GNS430ALabel.doc 11/29/2001 FCC ID Label placement and Label for GNS430A

ROGERS LABS, INC.Garmin International, Inc. 4405 W. 259th TerraceMODEL: GNS430A Louisburg, KS 66053Test #: 011119 Phone/Fax: (913) 837-3214Test to: FCC Parts 2 and 87Page 1 of 1 GNS430AIntPho.doc 11/29/2001 Internal Photgraphs of Printed Circuit Board for GNS430A Note: There are no components located on bottom side of printed circuit board.

GNC 400 COMM TRANSCEIVER ALIGNMENT PROCEDURE P/N 005-00051-55 REV. T Page 1 GNC400 COMM TRANSCEIVER ALIGNMENT PROCEDURE GARMIN Corporation 1200 E. 151st Street Olathe, KS 66062 005-00051-55 Rev. T ApprovalsDate Revisions Rev.DateDescription of ChangeApprvd. G10/26/98Change tuning order of IF transformers, change RF AGC setting. 9901 H10/30/98Increase TX MOSFET bias to 100mA9929 J11/20/98Add 25 KHz noise squelch adjustment, change SI program reference to test page display. 10058 K8/11/99Add instructions for tuning –03 board TCXO.11584 L5/5/00Change voltage range on VCO alignment. Add troubleshooting note to TX MOSFET bias setting 13278 M5/23/00Add Q-Dope to L30213396 N6/7/00Q504 Fix13512 P5/10/01Eliminate TCXO and RX IF Alignment15734 Q08/15/01Add Digital adjustments for PA and Driver bias, and MIC gain 16341 R08/20/01Change AF IN LO from 600 TO HI to GND16379 S09/25/01Change TX MOD adjustment on-05 comm to 80%16582 T11/14/01Update procedures for 16Watt TX16894 Drawn: BAS6/4/98 Checked: MDD6/5/98 Approved: MLR6/5/98 Project Mgr.: TLJ6/5/98 CONFIDENTIAL This drawing and these specifications contained herein are the property of GARMIN Corporation and may not be reproduced or used in whole or in part as the basis for manufacture or sale of products without the written permission of GARMIN Corporation. GNC 400 COMM TRANSCEIVER ALIGNMENT PROCEDURE P/N 005-00051-55 REV. T Page 2 TABLE OF CONTENTS 1.GENERAL......................................................................................................3 2.REFERENCE DOCUMENTS.........................................................................3 2.1Test Equipment.............................................................................................................................3 2.2Setup Procedure............................................................................................................................4 3.COMM TRANSCEIVER ASSEMBLY ALIGNMENT.......................................5 3.1Initial Control Settings.................................................................................................................5 3.1.1Discrete Adjustment................................................................................................................5 3.1.2Digital Pots.............................................................................................................................6 3.1.3Covers.....................................................................................................................................6 3.2Synthesizer Alignment..................................................................................................................6 3.2.1VCO Alignment......................................................................................................................6 3.2.2TCXO Alignment....................................................................................................................7 3.3Transmitter Power MOSFET Bias Setting.................................................................................7 3.3.1Bias Settings for –04 and Lower 10 Watt Comm Boards.......................................................7 3.3.2Bias Settings for –05 and Higher 10 Watt, and 16 Watt Comm Boards.................................7 3.4Receiver IF Alignment..................................................................................................................8 3.4.1IF Alignment – 8.33 KHz Mode.............................................................................................8 3.4.2IF Alignment - 25 KHz Mode.................................................................................................8 3.5Receiver / Transmitter Digital Pot Adjustments........................................................................9 3.5.1Comm Automated Alignment Instructions..............................................................................9 3.5.2Receiver Preselector Alignment..............................................................................................9 3.5.3Receiver Noise Squelch Calibration - 25 KHz Mode.............................................................9 3.5.4Receiver Carrier Squelch Calibration - 25 KHz Mode.........................................................10 3.5.5Receiver Carrier Squelch Calibration - 8.33 kHz Mode.......................................................11 3.5.6Transmitter Output Power Calibration..................................................................................11 3.5.7Transmitter Modulator Adjust..............................................................................................11 3.5.7.1Modulator Adjustment for 10 Watt comm boards............................................................11 3.5.7.2Modulator Adjustment for 16 Watt comm boards............................................................12 3.5.8Transmitter Sidetone Adjust.................................................................................................12 GNC 400 COMM TRANSCEIVER ALIGNMENT PROCEDURE P/N 005-00051-55 REV. T Page 3 1. GENERAL The alignment procedures are intended to be performed after board assembly . The alignment procedures are also used after replacing a component or module causing misalignment. The alignment procedures should be followed in the sequence presented. Certain sections of the radio must be aligned using subsections of the alignment procedure before the whole board can be aligned. This alignment procedure is written for a complete realignment. If only a subsection is required, use only the initial settings required as outlined in the procedure for the subsection. The comm board must be placed into a main chassis before alignment. Unless otherwise specified, alignment should be performed with the input power supply set to 27.5 ± 0.2 VDC. 2. REFERENCE DOCUMENTS 004-00044-03 Min Prfm Spec, GNC 400 Comm 016-00214-XX Assy Dwg, GNC400 Comm PCB 016-00611-XX Assy Dw…

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ROGERS LABS, INC.Garmin International, Inc. 4405 W. 259th TerraceMODEL: GNS430A Louisburg, KS 66053Test #: 011119 Phone/Fax: (913) 837-3214Test to: FCC Parts 2 and 87Page 1 of 1 GNS430ARFExp.doc 11/30/2001 General The GNS430A is considered to be a “mobile” device operating in the Aviation Services authorized under part 87 of CFR 47. Per 2.1093 (c) of CFR 47, the equipment is categorically excluded from routine environmental evaluation for RF exposure prior to equipment authorization or use. The radiating structure for the device is mounted more than 20 centimeters away and located outside the aircraft. Due to the location of the antenna and normal operating conditions and use the unit will satisfy the requirements for RF Exposure per FCC rule 1.1311.

TEST REPORT For APPLICATION of CERTIFICATION For GARMIN INTERNATIONAL, INC. 1200 East 151 st Street OLATHE, KS 66062 Phone: (913) 397-8200 Van Ruggles Director of Quality Assurance VHF AVIATION TRANSCEIVER Model: GNS430A Part Number: 010-00286-() which includes the 011-00836-() Frequency: 118 – 136.992 MHz FCC ID: IPH-0061100 Test Date: November 19, 2001 Certifying Engineer: Scot D. Rogers ROGERS LABS, INC. 4405 West 259th Terrace Louisburg, KS 66053 Phone: (913) 837-3214 FAX: (913) 837-3214 This report shall not be reproduced except in full, without the written approval of the laboratory. This report must not be used by the client to claim product endorsement by NVLAP or any agency of the U.S. Government. ROGERS LABS, INC. 4405 West 259 th Terrace Louisburg, KS 66053 Phone / Fax (913) 837-3214 NVLAP Accredited LaboratoryNVLAP Lab Code: 200087-0 ROGERS LABS, INC.GARMIN INTERNATIONAL, INC.MODEL: GNS430HPSN:ENG-001 4405 West 259 th TerracePN: 010-00286-() which includes the 011-00836-() Louisburg, KS 66053Test #: 011119FCC ID#: IPH-0061100 Phone/Fax: (913) 837-3214Test to: FCC Parts 2, 15 and 87Page 2 of 26 CERTIFICATION\GARMINGNS430A 11/27/01 TABLE OF CONTENTS FORWARD:3 LIST OF TEST EQUIPMENT3 2.1033(C)APPLICATION FOR CERTIFICATION4 2.1046RF POWER OUTPUT5 Measurements Required:5 Test Arrangement:5 Results:5 2.1047MODULATION CHARACTERISTICS6 Measurements Required:6 Test Arrangement:6 Results:7 2.1049OCCUPIED BANDWIDTH8 Measurements Required:8 Test Arrangement:9 Results:9 2.1051 SPURIOUS EMISSIONS AT ANTENNA TERMINALS10 Measurements Required:10 Test Arrangement:10 Results:11 2.1053FIELD STRENGTH OF SPURIOUS RADIATION12 Measurements Required:12 Test Arrangement:12 Results:13 2.1055FREQUENCY STABILITY14 Measurements Required:14 Test Arrangement:15 Results:16 APPENDIX17 NVLAP Accredited LaboratoryNVLAP Lab Code: 200087-0 ROGERS LABS, INC.GARMIN INTERNATIONAL, INC.MODEL: GNS430HPSN:ENG-001 4405 West 259 th TerracePN: 010-00286-() which includes the 011-00836-() Louisburg, KS 66053Test #: 011119FCC ID#: IPH-0061100 Phone/Fax: (913) 837-3214Test to: FCC Parts 2, 15 and 87Page 3 of 26 CERTIFICATION\GARMINGNS430A 11/27/01 FORWARD: In accordance with the Federal Communications Code of Federal Regulations, dated October 1, 2000, Part 2 Subpart J, Paragraphs 2.907, 2.911, 2.913, 2.915, 2.925, 2.926, 2.1031 through 2.1057, and Part 87, Subchapter D, Paragraphs 87.131 through 87.147, and applicable paragraphs of Part 15, the following is submitted: List of Test Equipment A Hewlett Packard 8591EM and or 8562A Spectrum Analyzer was used as the measuring device for the emissions testing. The analyzer settings used are described in the following table. Refer to the Appendix for a complete list of Test Equipment. HP 8591EM SPECTRUM ANALYZER SETTINGS CONDUCTED EMISSIONS: RBWAVG. BW DETECTOR FUNCTION 9 kHz30 kHzPeak/Quasi Peak RADIATED EMISSIONS (30 – 1000 MHz): RBWAVG. BW DETECTOR FUNCTION 120 kHz300 kHzPeak/Quasi Peak HP 8562A SPECTRUM ANALYZER SETTINGS RADIATED EMISSIONS (1 – 40 GHz): RBWAVG. BW DETECTOR FUNCTION 1 MHz1 MHzPeak/Average ANTENNA CONDUCTED EMISSIONS: RBWAVG. BW DETECTOR FUNCTION 100 kHz100 kHzPeak NVLAP Accredited LaboratoryNVLAP Lab Code: 200087-0 ROGERS LABS, INC.GARMIN INTERNATIONAL, INC.MODEL: GNS430HPSN:ENG-001 4405 West 259 th TerracePN: 010-00286-() which includes the 011-00836-() Louisburg, KS 66053Test #: 011119FCC ID#: IPH-0061100 Phone/Fax: (913) 837-3214Test to: FCC Parts 2, 15 and 87Page 4 of 26 CERTIFICATION\GARMINGNS430A 11/27/01 2.1033(c)Application for Certification (1) Manufacturer:GARMIN INTERNATIONAL, INC. 1200 East 151 st Street OLATHE, KS 66062 Marketer/Vendor:GARMIN INT…

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