SS3-RD2484R2111AESA Digital Radar

Agras T40 Quick Start Guide v1.0 2021.11 Aircraft The AGRAS TM T40 has a truss-style body with pitched arms that can be folded to reduce the body size, making it easier to transport. The integrated spraying system can quickly transform into the spreading configuration with a spreading payload up to 50 kg. Thanks to the spatial intelligent sensing system with Binocular Vision and Phased Array Digital Radar combined, the T40 can realize fully autonomous 3D continuous obstacle avoidance to ensure flight safety. The 12MP ultra HD FPV camera with a tiltable gimbal can automatically collect HD field images for local offline reconstruction to assist precise field planning. Using the P4 Multispectral and DJI Agras Cloud, prescription maps can be generated in order to perform variable rate fertilization. The Coaxial Dual Propeller structure brings a strong wind field. Pesticides can penetrate thick canopies to allow thorough spraying. The spraying system is equipped with the brand new Magnetic Drive Impeller Pump, Dual Atomized Centrifugal Sprinklers, and Anti-Drip Centrifugal Valves, using with the weight sensors, to provide real-time liquid level detection and smart supply reminder, improve spraying efficiency, as well as save liquid pesticide. Core modules adopt potting technology and the aircraft has a protection rating of IPX6K (IEC standard 60529) so that it can be washed directly with water. Using the T40 Preparing the Intelligent Flight Battery Only use official DJI flight batteries (model: BAX601-30000mAh-52.22V). Check the battery level before flying and charge according to the corresponding manual document. Preparing the Aircraft Unfold the M3 and M4 arms, and fasten the two arm locks. Avoid pinching fingers. Unfold the M1 and M2 arms, and fasten the two arm locks. Avoid pinching fingers. Unfold the propeller blades. Insert the Intelligent Flight Battery into the aircraft until you hear a click. ●Make sure that the battery is firmly inserted into the aircraft. Only insert or remove the battery when the aircraft is powered off. ●To remove the battery, press and hold the clamp and lift the battery up. ●Fold the M1 and M2 arms followed by the M3 and M4 arms and make sure that the arms are inserted into the storage clamps on both sides of the aircraft. Otherwise, the arms may be damaged. Getting Ready for Takeoff A. Place the aircraft on open, flat ground with the rear of the aircraft facing toward you. B. Make sure that the propellers are securely mounted, there are no foreign objects in or on the motors and propellers, the propeller blades 1. Propellers 2. Motors 3. ESCs 4. Aircraft Front Indicators (on two front arms) 5. Frame Arms 6. Folding Detection Sensors (built-in) 7. Spray Lance 8. Sprinklers 9. Spray Tank 10. Delivery Pumps 11. FPV Camera 12. Binocular Vision System 13. Spotlights 14. Heat Sinks 15. Phased Array Omnidirectional Radar 16. Phased Array Downward Rear Radar 17. Intelligent Flight Battery 18. Landing Gear 19. OCUSYNC TM Image Transmission Antennas 20. Onboard D-RTK TM Antennas 21. Aircraft Status Indicators (on two rear arms) and arms are unfolded, and the arm locks are firmly fastened. C. Make sure that the spray tank and flight battery are firmly in place. D. Pour liquid into the spray tank, and tighten the cover. E. Power on the remote controller, make sure that the DJI Agras app is open, and power on the aircraft. ● When using for the first time, activate the aircraft using the DJI Agras app. A DJI account and internet connection are required. Calibrating the Flow Meter Make sure to calibrate the flow meter before using for the first time. Otherwise, the spraying performance may be adversely affected. ① Fill the spray tank with approximately 10 L of water. ② In the app, go to Operation View. Tap , then , swipe down, and tap Calibration on the right of the flow meter calibration section. ③ Tap Start Calibration and calibration will start automatically. The result of the calibration will be displayed in the app when completed. ●Users can proceed once calibration is completed successfully. ●If calibration fails, tap “?”to view and resolve the problem. Afterwards, recalibrate and wait for successful calibration. Flight In the app, go to Operation View. Make sure that there is a strong GNSS signal and the system status bar indicates Ready (GNSS) or Ready (RTK).* Otherwise, the aircraft cannot take off. * RTK positioning is recommended. In the app, go to Operation View, tap , then RTK to enable Aircraft RTK Positioning, and select a method for receiving RTK signals. Takeoff Perform a Combination Stick Command (CSC) and push the throttle stick up to take off. Landing To land, pull down on the throttle stick to descend until the aircraft touches the ground. There are two methods to stop the motors. Method 1: when the aircraft has landed, push and hold the throttle stick down. The motors will stop after three seconds. Throttle Stick Method 2: When the aircraft has landed, push the throttle stick down, and perform the same CSC that was used to start the motors. Release both sticks once the motors have stopped. Release both sticks once the motors have stopped. ● Spinning propellers can be dangerous. Stay away from spinning propellers and motors. DO NOT start the motors in confined spaces or where there are people nearby. ● Maintain control of the remote controller as long as the motors are running. ● DO NOT stop the motors mid-flight unless in an emergency situation where doing so will reduce the risk of damage or injury. ● It is recommended to use Method 1 to stop the motors. When using Method 2 to stop the motors, the aircraft may roll over OR Throttle Stick (left stick in Mode 2) if it is not completely grounded. Use Method 2 with caution. ●After landing, power off the aircraft before turning off the remote controller. Starting Operations Users can perform aerial surveying for the operation area in the DJI Agras app. Local HD map can be generated using the offline recons…

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TCB Authority to Act as Agent Number: MS-0045317 Revision: 0 Effective date: Oct 8, 2021 Page 1 of 1 SZ DJI TECHNOLOGY CO.,LTD. Authority to Act as Agent Date: 2022-02-16 TUV Rheinland of North America, Inc. 1279 Quarry Lane., Suite. A Pleasanton, CA 94566 To Whom It May Concern: I appoint TUV Rheinland (Shenzhen) Co., Ltd. and TUV Engineer to act as our agent in the preparation of this application for equipment certification. I certify that submitted documents properly describe the device or system for which equipment certification is sought. I also certify that each unit manufactured, imported or marketed, as defined in the FCC or Industry Canada’s regulations will have affixed to it a label identical to that submitted for approval with this application. For instances where our authorized agent signs the application for certification on our behalf, I acknowledge that all responsibility for complying with the terms and conditions for Certification, as specified by TUV Rheinland Group, still resides with SZ DJI TECHNOLOGY CO.,LTD. 14th floor, West Wing, Skyworth Semiconductor Design Building NO.18 Gaoxin South 4th Ave, Nanshan, Shenzhen, Guangdong, China For TCB applications, We certify that we are not subject to denial of federal benefits, that includes FCC benefits, pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 U.S.C. 862. Further, no party, as defined in 47 CFR 1.2002 (b), to the application is subject to denial of federal benefits, that includes FCC benefits. Thank you, Agency Agreement Date: ___2022-02-16________________ Agreement is valid for 12 months from the above date. By: __________________________ ____Fajia Wang__ (Signature) (Print name) _Certification Manager +86 755 26656677 (Title) (Telephone) On behalf of: SZ DJI TECHNOLOGY CO.,LTD. (Company Name)

Standard Form Sample Request for Confidentiality Letter MS-0044715 Page 1 of 1 Revision 0 SZ DJI TECHNOLOGY CO.,LTD. Date: 2022-02-16 ________ Subject: Confidentiality Request for FCC ID: SS3-RD2484R21111 and IC: 11805A-RD2484R2111 Pursuant to FCC 47 CRF 0.457(d) and 0.459 and IC RSP-100, Section 10, the applicant requests that a part of the subject FCC/IC application be held confidential. Type of Confidentiality Requested Exhibit Short Term Permanent Block Diagrams Short Term Permanent Internal Photos *** Short Term Permanent Operation Description/Theory of Operation Short Term Permanent Tune-Up Procedure Short Term Permanent Schematics Short Term Permanent User’s Manual*** Short Term n/a Test Setup Short Term n/a External Photos SZ DJI TECHNOLOGY CO.,LTD.has spent substantial effort in developing this product and it is one of the first of its kind in industry. Having the subject information easily available to "competition" would negate the advantage they have achieved by developing this product. Not protecting the details of the design will result in financial hardship. Permanent Confidentiality: The applicant requests the exhibits listed above as permanently confidential be permanently withheld from public review due to materials that contain trade secrets and proprietary information not customarily released to the public. (*** PAG only) Short-Term Confidentiality: The applicant requests the exhibits selected above as short term confidential be withheld from public view for a period of 180 days from the date of the Grant of Equipment Authorization and prior to marketing. This is to avoid premature release of sensitive information prior to marketing or release of the product to the public. Applicant is also aware that they are responsible to notify TUV Rheinland in the event information regarding the product or the product is made available to the public. TUV Rheinland will then release the documents listed above for public disclosure pursuant to FCC Public Notice DA 04-1705. Sincerely, By: _________________________________ ________Fajia Wang________________ (Signature/Title) (Print name)

Appendix EPPhotographs of EUT Page 1 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Appendix EPPhotographs of EUT Page 2 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Appendix EPPhotographs of EUT Page 3 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R

Importer for EU: EU contact address: DJI GmbH, Industriestrasse 12, 97618, Niederlauer, Germany Importer for UK: Not decided yet, but it will be determined before it placed on UK market.

Appendix EPPhotographs of EUT Page 4 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Antenna_1T1R Appendix EPPhotographs of EUT Page 5 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Appendix EPPhotographs of EUT Page 6 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Antenna_8T4R Appendix EPPhotographs of EUT Page 7 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Appendix EPPhotographs of EUT Page 8 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Appendix EPPhotographs of EUT Page 9 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R Appendix EPPhotographs of EUT Page 10 of 10 CN22PQM6 (P15C-24GHz) 001 CN22PQM6 (FCC-MPE) 001 CN22VWHW (RSS210-24GHz) 001 CN22VWHW (ISED-MPE) 001 CN22QUKQ (EN300440-24GHz) 001 CN22QUKQ (EN62311) 001 Product: AESA Digital Radar Type Identification: RD2484R

Prü fbericht - Produkte Test Report - Products Prü fbericht-Nr.: Test report no.: CN22PQM6 (FCC-MPE) 001 Auftrags-Nr.: Order no.: 238523230 Seite 1 von 9 Page 1 of 9 Kunden-Referenz-Nr.: Client reference no.: N/A Auftragsdatum: Order date: 2021-12-03 Auftraggeber: Client: SZ DJI TECHNOLOGY CO.,LTD. 14th floor, West Wing, Skyworth Semiconductor Design Building NO.18 Gaoxin South 4th Ave, Nanshan, Shenzhen, Guangdong, China Prü fgegenstand: Test item: AESA Digital Radar Bezeichnung / Typ-Nr.: Identification / Type no.: RD2484R Auftrags-Inhalt: Order content: FCC Certification Prü fgrundlage: Test specification: 47 CFR §2.1091 47 CFR §1.1310 Wareneingangsdatum: Date of sample receipt: 2021-11-26 Prü fmuster-Nr.: Test sample no: A003190968-001 Prü fzeitraum: Testing period: 2021-12-23 - 2022-01-21 Ort der Prü fung: Place of testing: EMC/RF Taipei Testing Site Prü flaboratorium: Testing laboratory: Taipei Testing Laboratories Prü fergebnis*: Test result*: Pass ü berprü ft von: compiled by: Jack Wang genehmigt von: authorized by: Brenda Chen Datum: Date: 2022-01-22 Ausstellungsdatum: Issue date: 2022-01-22 Stellung / Position: Senior Project Engineer Stellung / Position: Senior Project Manager Sonstiges / Other: Zustand des Prü fgegenstandes bei Anlieferung: Condition of the test item at delivery: Prüfmuster vollständig und unbeschädigt Test item complete and undamaged * Legende: 1 = sehr gut 2 = gut 3 = befriedigend 4 = ausreichend 5 = mangelhaft P(ass) = entspricht o.g. Prüfgrundlage(n) F(ail) = entspricht nicht o.g. Prüfgrundlage(n) N/A = nicht anwendbar N/T = nicht getestet * Legend: 1 = very good 2 = good 3 = satisfactory 4 = sufficient 5 = poor P(ass) = passed a.m. test specification(s) F(ail) = failed a.m. test specification(s) N/A = not applicable N/T = not tested Dieser Prü fbericht bezieht sich nur auf das o.g. Prü fmuster und darf ohne Genehmigung der Prü fstelle nicht auszugsweise vervielfältigt werden. Dieser Bericht berechtigt nicht zur Verwendung eines Prü fzeichens. This test report only relates to the a. m. test sample. Without permission of the test center this test report is not permitted to be duplicated in extracts. This test report does not entitle to carry any test mark. TUV Rheinland Taiwan Ltd. 11F., No. 758, Sec. 4, Bade Rd., Taipei 105, Taiwan, R.O.C. Mail: [email protected] ∙ Web: www.tuv.com Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (FCC-MPE) 001 Seite 2 von 9 Page 2 of 9 Contents HISTORY OF THIS TEST REPORT .............................................................................. 3 1 GENERAL REMARKS ............................................................................................. 4 1.1 COMPLEMENTARY MATERIALS ............................................................................... 4 1.2 DECISION RULE OF CONFORMITY ........................................................................... 4 2 TEST SITES .......................................................................................................... 5 2.1 TEST FACILITIES ................................................................................................... 5 2.2 TEST FACILITY ...................................................................................................... 5 3 GENERAL PRODUCT INFORMATION ......................................................................... 6 3.1 PRODUCT FUNCTION AND INTENDED USE ............................................................... 6 3.2 RATINGS AND SYSTEM DETAILS ............................................................................. 6 4 MAXIMUM PERMISSIBLE EXPOSURE EVALUATION .................................................... 7 4.1 INTRODUCTION ..................................................................................................... 7 4.2 REFERENCE LEVELS ............................................................................................. 7 4.3 CLASSIFICATION OF THE ASSESSMENT METHODS.................................................... 8 5 TEST RESULTS ..................................................................................................... 9 5.1 MAXIMUM POWER DENSITY ................................................................................... 9 APPENDIX EP - PHOTOGRAPHS OF EUT Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (FCC-MPE) 001 Seite 3 von 9 Page 3 of 9 HISTORY OF THIS TEST REPORT Report No. Description Date Issued CN22PQM6 (FCC-MPE) 001 Original Release 2022-01-22 Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (FCC-MPE) 001 Seite 4 von 9 Page 4 of 9 1 General Remarks 1.1 Complementary Materials All attachments are integral parts of this test report. This applies especially to the following appendix: Appendix EP - Photographs of EUT 1.2 Decision Rule of Conformity The decision rule of conformity of this test report is following the requirements of the requested standard in the quotation, and agreed among testing laboratory and manufacturer (applicant) to exclude the consideration of Measurement Uncertainty, unless it is required by the specific standard. Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (FCC-MPE) 001 Seite 5 von 9 Page 5 of 9 2 Test Sites 2.1 Test Facilities Taipei Testing Laboratories 11F. No.758, Sec. 4, Bade Rd., Songshan Dist. Taipei City 105 Taiwan (R.O.C.) 2.2 Test Facility Taipei Testing Laboratories No.458-18, Sec. 2, Fenliao Rd., Linkou Dist., New Taipei City 244 Taiwan (R.O.C.) Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (FCC-MPE) 001 Seite 6 von 9 Page 6 of 9 3 General Product Information 3.1 Product Function and Intended Use The EUT is AESA Digital Radar. It contains a 24GHz compatible module enabling the user to detect the object from the blindside through a radar detector. For details refer to the User…

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Prü fbericht - Produkte Test Report - Products Prü fbericht-Nr.: Test report no.: CN22PQM6 (P15C-24GHz) 001 Auftrags-Nr.: Order no.: 238523230 Seite 1 von 22 Page 1 of 22 Kunden-Referenz-Nr.: Client reference no.: N/A Auftragsdatum: Order date: 2021-12-03 Auftraggeber: Client: SZ DJI TECHNOLOGY CO.,LTD. 14th floor, West Wing, Skyworth Semiconductor Design Building NO.18 Gaoxin South 4th Ave, Nanshan, Shenzhen, Guangdong, China Prü fgegenstand: Test item: AESA Digital Radar Bezeichnung / Typ-Nr.: Identification / Type no.: RD2484R Auftrags-Inhalt: Order content: FCC Part 15C Test report Prü fgrundlage: Test specification: FCC 47CFR Part 15: Subpart C Section 15.249 Wareneingangsdatum: Date of sample receipt: 2021-11-26 Prü fmuster-Nr.: Test sample no: A003172229 Prü fzeitraum: Testing period: 2021-12-23 - 2022-01-21 Ort der Prü fung: Place of testing: EMC/RF Taipei Testing Site Prü flaboratorium: Testing laboratory: Taipei Testing Laboratories Prü fergebnis*: Test result*: Pass überprü ft von: compiled by: Jack Wang genehmigt von: authorized by: Brenda Chen Datum: Date: 2022-01-22 Ausstellungsdatum: Issue date: 2022-01-22 Stellung / Position: Senior Project Engineer Stellung / Position: Senior Project Manager Sonstiges / Other: Zustand des Prü fgegenstandes bei Anlieferung: Condition of the test item at delivery: Prüfmuster vollständig und unbeschädigt Test item complete and undamaged * Legende: 1 = sehr gut 2 = gut 3 = befriedigend 4 = ausreichend 5 = mangelhaft P(ass) = entspricht o.g. Prüfgrundlage(n) F(ail) = entspricht nicht o.g. Prüfgrundlage(n) N/A = nicht anwendbar N/T = nicht getestet * Legend: 1 = very good 2 = good 3 = satisfactory 4 = sufficient 5 = poor P(ass) = passed a.m. test specification(s) F(ail) = failed a.m. test specification(s) N/A = not applicable N/T = not tested Dieser Prü fbericht bezieht sich nur auf das o.g. Prü fmuster und darf ohne Genehmigung der Prü fstelle nicht auszugsweise vervielfältigt werden. Dieser Bericht berechtigt nicht zur Verwendung eines Prü fzeichens. This test report only relates to the a. m. test sample. Without permission of the test center this test report is not permitted to be duplicated in extracts. This test report does not entitle to carry any test mark. TUV Rheinland Taiwan Ltd. 11F., No. 758, Sec. 4, Bade Rd., Taipei 105, Taiwan, R.O.C. Mail: [email protected] ∙ Web: www.tuv.com Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (P15C-24GHz) 001 Seite 2 von 22 Page 2 of 22 TEST SUMMARY Report Section FCC Clause Test Item Result 5.1.1 15.203 Antenna Requirement Pass 5.1.2 15.215 20 dB Bandwidth Pass 5.1.2 2.1049 99% Occupied Bandwidth Pass 5.1.3 15.249 (a) Field Strength of Fundamental Emissions Pass 5.1.4 15.249 (d) Radiated Spurious Emissions Pass - 15.207 Mains Conducted Emission Not Applicable Note: Determining compliance based on the results of the compliance measurement, not taking into account measurement instrumentation uncertainty. Prü fbericht - Produkte Test Report - Products Prü fbericht - Nr.: Test Report No. CN22PQM6 (P15C-24GHz) 001 Seite 3 von 22 Page 3 of 22 Contents HISTORY OF THIS TEST REPORT .............................................................................. 4 1. GENERAL REMARKS ............................................................................................. 5 1.1 COMPLEMENTARY MATERIALS ............................................................................... 5 1.2 DECISION RULE OF CONFORMITY ........................................................................... 5 2. TEST SITES .......................................................................................................... 6 2.1 TEST LABORATORY .............................................................................................. 6 2.2 TEST FACILITY ...................................................................................................... 6 2.3 TRACEABILITY ...................................................................................................... 7 2.4 CALIBRATION ....................................................................................................... 7 2.5 MEASUREMENT UNCERTAINTY ............................................................................... 7 3. GENERAL PRODUCT INFORMATION ......................................................................... 8 3.1 PRODUCT FUNCTION AND INTENDED USE ............................................................... 8 3.2 SYSTEM DETAILS AND RATINGS ............................................................................. 8 3.3 NOISE GENERATING AND NOISE SUPPRESSING PARTS ............................................ 9 3.4 SUBMITTED DOCUMENTS ....................................................................................... 9 4. TEST SET-UP AND OPERATION MODES ................................................................. 10 4.1 PRINCIPLE OF CONFIGURATION SELECTION .......................................................... 10 4.2 TEST OPERATION AND TEST SOFTWARE ............................................................... 10 4.3 SPECIAL ACCESSORIES AND AUXILIARY EQUIPMENT ............................................. 11 4.4 TEST SETUP DIAGRAM ........................................................................................ 11 5. TEST RESULTS ................................................................................................... 12 5.1 TRANSMITTER REQUIREMENT & TEST SUITES ....................................................... 12 5.1.1 Antenna Requirement .............................................................................................................12 5.1.2 20 dB Bandwidth and 99% Occupied Bandwidth ....................................................................13 5.1.3 Field Strength of Fundamental Emissions ..............................................................................16 5.1.4 Radiated Spurious Emissions ........…

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Appendix SP Photographs of Test Setup Page 1 of 4 CN22PQM6 (P15C-24GHz) 001 CN22VWHW (RSS210-24GHz) 001 Product: AESA Digital Radar Type Identification: RD2484R Photograph 1: Test Setup for Spurious Emissions (Front View 1) Photograph 2: Test Setup for Spurious Emissions (Front View 2) Appendix SP Photographs of Test Setup Page 2 of 4 CN22PQM6 (P15C-24GHz) 001 CN22VWHW (RSS210-24GHz) 001 Product: AESA Digital Radar Type Identification: RD2484R Photograph 3: Test Setup for Spurious Emissions (Back View 1) Photograph 4: Test Setup for Spurious Emissions (Back View 2) Appendix SP Photographs of Test Setup Page 3 of 4 CN22PQM6 (P15C-24GHz) 001 CN22VWHW (RSS210-24GHz) 001 Product: AESA Digital Radar Type Identification: RD2484R Photograph 5: Test Setup for Spurious Emissions (Back View 3) Photograph 6: Test Setup for Spurious Emissions (Back View 4) Appendix SP Photographs of Test Setup Page 4 of 4 CN22PQM6 (P15C-24GHz) 001 CN22VWHW (RSS210-24GHz) 001 Product: AESA Digital Radar Type Identification: RD2484R Photograph 7: Test Setup for Spurious Emissions (Back View 5) Photograph 8: Test Setup for Spurious Emissions (Back View 6)