QV7-GC88752-71Drone

User Manual Camera with 500 m Image transmission range (Please ensure your mobile phone supports with 5G WiFi ) Accreditation standard: GB/T26701-2011 Palm control Flight plan Waypoint flightGPS tracking One key to retrun Circle flight Human tracking 4K 5G WIFI Camera Optical flow positioning Long battery life Dual-frequency technology 14+ Take-off/landing +1 718-312-0558 (US) +44(0)7723708421 (UK) +49 335-4551-9201 (DE) INSTRUCTIONS FOR USE X500Pro FOLDABLE DRONE  Ś Photo button Record button Left joystick On / Off button One Key Take Off / Landing Calibrating the compass Home button Phone holder Lens up Lens down Right joystick ś Ŝ ŝŞ ţ ş Ţ š Š Remote control Ś Motor ś Propeller blades Ŝ Power switch ŝ Front camera Aircraft components Ş Battery ş Front LED indicator Š Rear LED indicator š Bottom camera Ś ś Ŝ ŝ ş Ş Š š English  ! Assembling the product Installing the propellers Clockwise propellersAnticlockwise propellers Inserting a memory card (optional accessory) Attach the propellers as shown in the diagrams above. Ensure that they are attached in the correct orientation. Ensure that the clockwise and anticlockwise propellers are attached to the correct arms. The aircraft will not fly correctly if the propellers are attached in the wrong position. The propellers are made from a delicate material. Pay attention when attaching them to the aircraft. Only use propellers that are supplied by the manufacturer. The propellers are consumable parts. If necessary, purchase replacements from the manufacturer. This toy is only to be connected to equipment bearing either of the following symbols: 1 2 3 1 2 3 English 5V2A A adapter USB ! * Charge the aircraft with the USB charging cable that came with the product. * The battery will take longer to charge when you use an adapter with a smaller rated current. 123  1 2 Remove the battery Charge the battery Charging the aircraft battery USB charging cableBattery Indicator in slow flashing green: Charging in progress Indicator in constant green: Battery is fully charged Indicator in rapid flashing green: Battery is defective Insert the battery * Ensure that the battery holder clicks into place. * Do not short circuit or compress the battery, as this may cause an explosion. * Do not disassembling the battery or store it in a hot environment. * If you do not plan to use the aircraft for at least 10 days, discharge the battery to 40%-50%. This helps to prolong the lifespan of the battery. * Rechargeable batteries should be removed from the aircraft before charging charged. * Rechargeable batteries should only be charged under the supervision of adults.and keep away from flammable materials. * Exhausted batteries should be removed from the aircraft. * Caution: Risk of explosion if battery is replaced with incorrect ones, please install the batteries according to the instructions. English  5V 1-2A 3 4 1 1 1 11 2 2 22 Open the remote control Close the remote control Flight preparation and turning the aircraft on/off Pairing the remote control with the aircraft Inserting the remote control batteries Attaching the phone holder Indicator stays constant when pairing is complete. When you switch on the remote control, the indicator will flash rapidly for approximately 20 secs to indicate that the remote control is waiting for a signal. The indicator will then flash slowly to indicate that pairing mode has been disabled. ! ! Remote control indicator flashes rapidly Switch on the remote control Indicator flashes rapidly -> slowly Switch off the remote controller during charging Charging : red light is on Finish charging: light is off 2 * When installing the batteries, ensure that you match the + and – ends of the battery with the + and – signs on the controller. * During the battery installation, it must be ensured that the polarities of the batteries are matched with that of the battery box. No battery shall be installed with the opposite polarity. * Please do not use new and old batteries together. * Please do not use different types of batteries together. * The controller Do not use rechargeable batteries. * Exhausted batteries are to be removed from the Remote control. English  1 Searching for satellites The rear indicator will change from orange to green when the aircraft has locked on to a satellite and recorded the take-off location. The aircraft is now ready to fly. Calibrating the compass Do not calibrate the compass near strong electromagnetic fields or large pieces of metal, e.g. magnetite, car parks or buildings with underground steel reinforcements. When holding the aircraft horizontally, the angle of inclination must not exceed 30 degrees. ! ! It should take approximately one minute for the aircraft to lock on to a satellite. If the aircraft fails to find a satellite, recalibrate the compass. Before take-off, place the aircraft in an open space away from obstacles and ensure that GPS mode is enabled. When the rear green indicator flashes rapidly, this indicates that the GPS signal is weak. If this occurs, land the aircraft manually and restart the satellite search. Turning the aircraft on Push the left and right joysticks downwards in a V shape for 1 second. Move the left joystick upwards or Press to calibrating the compass Hold the aircraft horizontally and rotate 360 degrees for few time. Indicator flashes from slowly to rapidly. Hold the aircraft vertically and rotate 360 degrees for few times. Indicator flashes from rapidly to constant. 2 3 English  ! Turning the aircraft off Method oneMethod twoMethod three The aircraft will switch off automatically if its angle of inclination exceeds 90 degrees. Maximum radio-frequency power transmitted < 10 dBm. Frequency range:2408MHz - 2478MHz Using the remote control Ascend Descend Move forwards Move backwards Rotate left Tilt left Tilt right Rotate right Front 5HDU Front Rear Push the left joystick downwards for 2-3 seconds. Push the left and right joysticks downwards i…

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GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD NO.2 WEST XINGYE ROAD LAIMEI INDUSTRIAL AREA CHENGHAI, Shantou, China Agent Authorization Company: GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD Address: NO.2 WEST XINGYE ROAD LAIMEI INDUSTRIAL AREA CHENGHAI, Shantou, China Product Name: Drone Model Number(s): X500PRO, X20, X300, X400, X500, X650, X600, X600W, X700, X700W, TF1001, TG1001, X21W, X100, X800, X800W, X200, X200W, X110 , X110W, X220, X220W, X330, X330W, X440, X440W, X550, X550W, X660, X660W, X770, X770W, X880, X880W, X990, X990W, X710W, X720W, X730W, X740W, X750W, X760W, X780W, X790W, X810W, X820W, X830W, X840W, X850W, X860W, X870W, X890W, X900W, X910W, X920W, X930W, X940W, X950W, X960W, X970W, X980W, S100, S107H-E, S39, S37, S40, S50H, S51H, S52H, S53H, S54H, S55H, S56H, S57H, S58H, S59H, S60H, S61H, S62H, S63H, S64H, S65H, Q7, Q9, Q10, Q11, Q12, Q13, Q14, Q15, Q16, Q17, Q18, Q19, Q20, Q21, Q22, Q23, Q24, Q25 Product Description: Drone We authorize MiCOM Labs Inc., 575 Boulder Court, Pleasanton, California 94566, USA, to act on our behalf on all matters concerning the certification of above named equipment. We declare that MiCOM Labs Inc. is allowed to forward all information related to the approval and certification of equipment to the regulatory agencies as required and to discuss any issues concerning the approval application. Any and all acts carried out by MiCOM Labs on our behalf shall have the same effect as acts of our own. Signature: Date: Aug. 03, 2022 Name: Ivan Chen Title: General Manager Company: GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD

GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD NO.2 WEST XINGYE ROAD LAIMEI INDUSTRIAL AREA CHENGHAI, Shantou, China Aug. 03, 2022 Office of Engineering Technology Federal Communications Commission 7435 Oakland Mills Road Columbia, MD 21046 USA Subject: Explanation of differences between product types FCC ID: QV7-GC88752-71 Models: X500PRO, X20, X300, X400, X500, X650, X600, X600W, X700, X700W, TF1001, TG1001, X21W, X100, X800, X800W, X200, X200W, X110 , X110W, X220, X220W, X330, X330W, X440, X440W, X550, X550W, X660, X660W, X770, X770W, X880, X880W, X990, X990W, X710W, X720W, X730W, X740W, X750W, X760W, X780W, X790W, X810W, X820W, X830W, X840W, X850W, X860W, X870W, X890W, X900W, X910W, X920W, X930W, X940W, X950W, X960W, X970W, X980W, S100, S107H-E, S39, S37, S40, S50H, S51H, S52H, S53H, S54H, S55H, S56H, S57H, S58H, S59H, S60H, S61H, S62H, S63H, S64H, S65H, Q7, Q9, Q10, Q11, Q12, Q13, Q14, Q15, Q16, Q17, Q18, Q19, Q20, Q21, Q22, Q23, Q24, Q25 To Whom It May Concern: We, The GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD hereby declare that the model : X500PRO is identical with the model : X20, X300, X400, X500, X650, X600, X600W, X700, X700W, TF1001, TG1001, X21W, X100, X800, X800W, X200, X200W, X110 , X110W, X220, X220W, X330, X330W, X440, X440W, X550, X550W, X660, X660W, X770, X770W, X880, X880W, X990, X990W, X710W, X720W, X730W, X740W, X750W, X760W, X780W, X790W, X810W, X820W, X830W, X840W, X850W, X860W, X870W, X890W, X900W, X910W, X920W, X930W, X940W, X950W, X960W, X970W, GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD NO.2 WEST XINGYE ROAD LAIMEI INDUSTRIAL AREA CHENGHAI, Shantou, China X980W, S100, S107H-E, S39, S37, S40, S50H, S51H, S52H, S53H, S54H, S55H, S56H, S57H, S58H, S59H, S60H, S61H, S62H, S63H, S64H, S65H, Q7, Q9, Q10, Q11, Q12, Q13, Q14, Q15, Q16, Q17, Q18, Q19, Q20, Q21, Q22, Q23, Q24, Q25, Only the color of appearance is different, and others are consistent. Except for the different above, no other modification is performed. Sincerely, GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD Signature: [Ivan Chen, General Manager]

GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD NO.2 WEST XINGYE ROAD LAIMEI INDUSTRIAL AREA CHENGHAI, Shantou, China FCC Software Configuration Control Declaration Rev1.1 FCC Software Configuration Control Declaration Date: Aug. 03, 2022 Federal Communications Commission 7435 Oakland Mills Road Columbia, MD 21046 USA Attn: OET Dept. Product/ Model Number: X500PRO, X20, X300, X400, X500, X650, X600, X600W, X700, X700W, TF1001, TG1001, X21W, X100, X800, X800W, X200, X200W, X110 , X110W, X220, X220W, X330, X330W, X440, X440W, X550, X550W, X660, X660W, X770, X770W, X880, X880W, X990, X990W, X710W, X720W, X730W, X740W, X750W, X760W, X780W, X790W, X810W, X820W, X830W, X840W, X850W, X860W, X870W, X890W, X900W, X910W, X920W, X930W, X940W, X950W, X960W, X970W, X980W, S100, S107H-E, S39, S37, S40, S50H, S51H, S52H, S53H, S54H, S55H, S56H, S57H, S58H, S59H, S60H, S61H, S62H, S63H, S64H, S65H, Q7, Q9, Q10, Q11, Q12, Q13, Q14, Q15, Q16, Q17, Q18, Q19, Q20, Q21, Q22, Q23, Q24, Q25 Regarding FCC Country Code Selection guidelines identified in KDB 594280 D01 v02r01. “All applications for equipment authorization for transmitters that can have radio parameters, or other technical parameters, reported to the Commission set by software must have an attestation indicating that no third party will have software, or configuration control, to program the device out of compliance of the technical rules under which it has been certified.” We declare that no third party will have software, or configuration control, to program the device out of compliance of the technical rules under which it has been certified. Name: Ivan Chen Title: General Manager Signature of applicant

Report No.: AGC12319220501AP02 Page 1 of 3 EXTERNAL PHOTOS TOP VIEW OF EUT BOTTOM VIEW OF EUT Report No.: AGC12319220501AP02 Page 2 of 3 FRONT VIEW OF EUT BACK VIEW OF EUT Report No.: AGC12319220501AP02 Page 3 of 3 LEFT VIEW OF EUT RIGHT VIEW OF EUT ****************************************End of Report****************************************

FCC ID Label Location 10mm*10mm FCC ID: QV7-GC88752-71

Report No.: AGC12319220501AP02 Page 1 of 7 INTERNAL PHOTOS OPEN VIEW OF EUT (FIGURE 1) OPEN VIEW OF EUT (FIGURE 2) Report No.: AGC12319220501AP02 Page 2 of 7 OPEN VIEW OF EUT (FIGURE 3) VIEW OF BATTERY Report No.: AGC12319220501AP02 Page 3 of 7 INTERNAL VIEW OF EUT (FIGURE 1) INTERNAL VIEW OF EUT (FIGURE 2) 5G WIFI Antenna 1 5G WIFI Antenna 2 Report No.: AGC12319220501AP02 Page 4 of 7 INTERNAL VIEW OF EUT (FIGURE 3) INTERNAL VIEW OF EUT (FIGURE 4) Report No.: AGC12319220501AP02 Page 5 of 7 INTERNAL VIEW OF EUT (FIGURE 5) INTERNAL VIEW OF EUT (FIGURE 6) Report No.: AGC12319220501AP02 Page 6 of 7 INTERNAL VIEW OF EUT (FIGURE 7) INTERNAL VIEW OF EUT (FIGURE 8) 2.4G RX Antenna Report No.: AGC12319220501AP02 Page 7 of 7 INTERNAL VIEW OF EUT (FIGURE 9) ****************************************End of Report****************************************

RF EXPOSURE EVALUATION 1. PRODUCT INFORMATION Product Description Drone Test Model X500PRO Series Model X20, X300, X400, X500, X650, X600, X600W, X700, X700W, TF1001, TG1001, X21W, X100, X800, X800W, X200, X200W, X110 , X110W, X220, X220W, X330, X330W, X440, X440W, X550, X550W, X660, X660W, X770, X770W, X880, X880W, X990, X990W, X710W, X720W, X730W, X740W, X750W, X760W, X780W, X790W, X810W, X820W, X830W, X840W, X850W, X860W, X870W, X890W, X900W, X910W, X920W, X930W, X940W, X950W, X960W, X970W, X980W, S100, S107H-E, S39, S37, S40, S50H, S51H, S52H, S53H, S54H, S55H, S56H, S57H, S58H, S59H, S60H, S61H, S62H, S63H, S64H, S65H, Q7, Q9, Q10, Q11, Q12, Q13, Q14, Q15, Q16, Q17, Q18, Q19, Q20, Q21, Q22, Q23, Q24, Q25 FCC ID QV7-GC88752-71 2. EVALUATION METHOD AND LIMIT Human exposure to RF emissions from mobile devices (47 CFR §2.1091) may be evaluated based on the MPE limits adopted by the FCC for electric and magnetic field strength and/or power density, as appropriate, since exposures are assumed to occur at distances of 20 cm or more from persons. LIMITS FOR GENERAL POPULATION / UNCONTROLLED EXPOSURE Frequency Range (MHz) E-field Strength (E) (V/m) Magnetic Field Strength (H) (A/m) Power Density (S) (mW/cm 2 ) Averaging Time |E| 2 , |H| 2 or S (Minutes) 0.3 -- 1.34 614 1.63 (100)* 30 1.34 -- 30 824/f 2.19/f (180/f 2 )* 30 30 -- 300 27.5 0.073 0.2 30 300 -- 1500 -- -- f/1500 30 1500 -- 100,000 -- -- 1.0 30 *Note: 1. f= Frequency in MHz * Plane-wave Equivalent Power Density 2. The averaging time for General Population/Uncontrolled exposure to fixed transmitters is not applicable for mobile and portable transmitters. See 47 CFR §§2.1091 and 2.1093 on source-based time-averaging requirement for mobile and portable transmitters. S=PG/4πR² Where: S=power density P=power input to antenna G=power gain of the antenna in the direction of interest relative to an isotropic radiator R=distance to the center of radiation of the antenna CALCULATION A minimum test separation distance ≥ 20 cm is required between the antenna and radiating structures of the device and nearby persons to apply mobile device exposure limits. The distance must be at least 20 cm and fully supported by the operating and installation configurations of the transmitter and its antenna(s), according to the source-based time-averaged maximum power requirements of § 2.1091(d)(2). In cases where cable losses or other attenuations are applied to determine compliance, the most conservative operating configurations and exposure conditions must be evaluated. Antenna Gain=2dBi (Numeric 1.58), π=3.14 Note: 1. Only the worst case recorded. Frequency Output Power Output Power Power Density Power Density Limit MHz dBm mW mW/cm 2 mW/cm 2 5500 (antenna 1) 12.06 16.07 0.0051 1 5500 (antenna 1) 12.39 17.34 0.0055 1 5500 (antenna 1+2) 13.82 24.10 0.0076 1

Page 1 of 76 Report No.: AGC12319220501FE06 FCC ID : QV7-GC88752-71 APPLICATION PURPOSE : Original Equipment PRODUCT DESIGNATION : Drone BRAND NAME : N/A MODEL NAME : Please see the page 6. APPLICANT : GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD DATE OF ISSUE : Aug. 01, 2022 STANDARD(S) TEST PROCEDURE(S) : FCC Part 15.407 KDB 789033 D02 v02r01 REPORT VERSION : V1.0 Attestation of Global Compliance (Shenzhen) Co., Ltd FCC Test Report Report No.: AGC12319220501FE06 Page 2 of 76 REPORT REVISE RECORD Report Version Revise Time Issued Date Valid Version Notes V1.0 / Aug. 01, 2022 Valid Initial Release Report No.: AGC12319220501FE06 Page 3 of 76 TABLE OF CONTENTS 1. VERIFICATION OF CONFORMITY .................................................................................................................. 5 2. GENERAL INFORMATION .............................................................................................................................. 6 2.1. PRODUCT DESCRIPTION ........................................................................................................................ 6 2.2. TABLE OF CARRIER FREQUENCYS ....................................................................................................... 7 2.3. RELATED SUBMITTAL(S) / GRANT (S) .................................................................................................... 8 2.4. TEST METHODOLOGY ............................................................................................................................. 8 2.5. SPECIAL ACCESSORIES ......................................................................................................................... 8 2.6. EQUIPMENT MODIFICATIONS ................................................................................................................. 8 2.7. ANTENNA REQUIREMENT....................................................................................................................... 8 3. MEASUREMENT UNCERTAINTY ................................................................................................................. 10 4. DESCRIPTION OF TEST MODES ................................................................................................................. 11 5. SYSTEM TEST CONFIGURATION ................................................................................................................ 12 5.1. CONFIGURATION OF EUT SYSTEM ...................................................................................................... 12 5.2. EQUIPMENT USED IN EUT SYSTEM ..................................................................................................... 12 5.3. SUMMARY OF TEST RESULTS .............................................................................................................. 12 6. TEST FACILITY .............................................................................................................................................. 13 7. MAXIMUM CONDUCTED OUTPUT POWER ................................................................................................ 14 7.1. MEASUREMENT PROCEDURE ............................................................................................................. 14 7.2. TEST SET-UP........................................................................................................................................... 14 7.3. LIMITS AND MEASUREMENT RESULT .................................................................................................. 15 8. BANDWIDTH .................................................................................................................................................. 17 8.1. MEASUREMENT PROCEDURE ............................................................................................................. 17 8.2. TEST SET-UP (BLOCK DIAGRAM OF CONFIGURATION) .................................................................... 17 8.3. LIMITS AND MEASUREMENT RESULTS ............................................................................................... 18 9. MAXIMUM CONDUCTED OUTPUT AVERAGE POWER SPECTRAL DENSITY ........................................ 32 9.1. MEASUREMENT PROCEDURE ............................................................................................................. 32 9.2. TEST SET-UP (BLOCK DIAGRAM OF CONFIGURATION) .................................................................... 32 9.3. MEASUREMENT EQUIPMENT USED .................................................................................................... 32 9.4. LIMITS AND MEASUREMENT RESULT .................................................................................................. 32 10. CONDUCTED SPURIOUS EMISSION ........................................................................................................ 46 Report No.: AGC12319220501FE06 Page 4 of 76 10.1. MEASUREMENT PROCEDURE ........................................................................................................... 46 10.2. TEST SET-UP (BLOCK DIAGRAM OF CONFIGURATION) .................................................................. 46 10.3. MEASUREMENT EQUIPMENT USED .................................................................................................. 46 10.4. LIMITS AND MEASUREMENT RESULT ............................................................................................... 46 11. RADIATED EMISSION ................................................................................................................................. 58 11.1. MEASUREMENT PROCEDURE............................................................................................................ 58 11.2. TEST SETUP .......................................................................................................................................... 59 11.3. LIMITS AND MEASUREMENT RESULT .....................…

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Report No.: AGC12319220501FE06 Page 60 of 76 11.3. LIMITS AND MEASUREMENT RESULT 15.209(a) Limit in the below table has to be followed Frequencies (MHz) Field Strength (microvolts/meter) Measurement Distance (meters) 0.009~0.490 2400/F(kHz) 300 0.490~1.705 24000/F(kHz) 30 1.705~30.0 30 30 30~88 100 3 88~216 150 3 216~960 200 3 Above 960 500 3 Note: All modes were tested for restricted band radiated emission, the test records reported below are the worst result compared to other modes. 11.4. TEST RESULT Radiated emission below 30MHz The amplitude of spurious emissions from 9kHz to 30MHz which are attenuated more than 20 dB below the permissible value need not be reported. Report No.: AGC12319220501FE06 Page 61 of 76 Radiated emission from 30MHz to 1000MHz EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5500MHz Antenna Horizontal RESULT: PASS Report No.: AGC12319220501FE06 Page 62 of 76 EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5500MHz Antenna Vertical RESULT: PASS Note: All test channels had been tested. The 802.11a20 of antenna 2 at 5500MHz is the worst case and recorded in the test report. Factor = Antenna Factor + Cable loss - Amplifier gain, Margin= Limit-Level. The “Factor” value can be calculated automatically by software of measurement system. Report No.: AGC12319220501FE06 Page 63 of 76 Radiated emission above 1GHz EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5260MHz Antenna Horizontal/Vertical RADIATED EMISSION ABOVE 1GHZ–Horizontal FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 10520.04447.539.2956.8268.20-11.38 peak 15780.06642.1910.4252.6174.00-21.39 peak 15780.06632.5710.4242.9954.00-11.01 AVG Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type RADIATED EMISSION ABOVE 1GHZ–Vertical FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 10520.04447.529.2956.8168.20-11.39 peak 15780.06642.5910.4253.0174.00-20.99 peak 15780.06631.5710.4241.9954.00-12.01 AVG Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type Report No.: AGC12319220501FE06 Page 64 of 76 EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5300MHz Antenna Horizontal/Vertical RADIATED EMISSION ABOVE 1GHZ–Horizontal FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 10600.04448.529.3157.8374.00-16.17 peak 10600.04437.549.3146.8554.00-7.15 AVG 15900.06642.1610.4452.6074.00-21.40 peak 15900.06631.4910.4441.9354.00-12.07 AVG Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type RADIATED EMISSION ABOVE 1GHZ–Vertical FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 10600.04449.639.3158.9474.00-15.06 peak 10600.04438.549.3147.8554.00-6.15 AVG 15780.06641.1510.4451.5974.00-22.41 peak 15780.06632.5710.4443.0154.00-10.99 AVG Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type Report No.: AGC12319220501FE06 Page 65 of 76 EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5320MHz Antenna Horizontal/Vertical RADIATED EMISSION ABOVE 1GHZ–Horizontal FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 10640.04448.139.3557.4874.00-16.52 peak 10640.04437.549.3546.8954.00-7.11 AVG 15960.06641.0510.4651.5174.00-22.49 peak 15960.06632.4610.4642.9254.00-11.08 AVG Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type RADIATED EMISSION ABOVE 1GHZ–Vertical FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 10640.04447.529.3556.8774.00-17.13 peak 10640.04436.489.3545.8354.00-8.17 AVG 15960.06642.1610.4652.6274.00-21.38 peak 15960.06632.5810.4643.0454.00-10.96 AVG Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type Report No.: AGC12319220501FE06 Page 66 of 76 EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5500MHz Antenna Horizontal/Vertical RADIATED EMISSION ABOVE 1GHZ–Horizontal FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 11000.04446.399.3755.7674.00-18.24 peak 11000.04437.549.3746.9154.00-7.09 AVG 16500.06641.0510.4851.5368.20-16.67 peak Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type RADIATED EMISSION ABOVE 1GHZ–Vertical FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 11000.04447.529.3756.8974.00-17.11 peak 11000.04436.599.3745.9654.00-8.04 AVG 16500.06641.0510.4851.5368.20-16.67 peak Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type Report No.: AGC12319220501FE06 Page 67 of 76 EUT Drone Model Name X500PRO Temperature 25°C Relative Humidity 60% Pressure 960hPa Test Voltage Normal Voltage Test Mode 802.11a20 5600MHz Antenna Horizontal/Vertical RADIATED EMISSION ABOVE 1GHZ–Horizontal FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 11200.04448.459.3857.8374.00-16.17 peak 11200.04437.569.3846.9454.00-7.06 AVG 16800.06641.0910.4951.5868.20-16.62 peak Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type RADIATED EMISSION ABOVE 1GHZ–Vertical FrequencyMeter ReadingFactorEmission LevelLimitsMargin (MHz)(dBμV)(dB)(dBμV/m)(dBμV/m)(dB) 11200.04448.629.3858.0074.00-16.00 peak 11200.04437.549.3846.9254.00-7.08 AVG 16800.06641.0510.4951.5468.20-16.66 peak Remark: Factor = Antenna Factor + Cable Loss – Pre-amplifier. Value Type Report No.: AGC12319220501FE06 Page 68 of 76 EUT Drone Model Name X500PRO Temp…

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Page 1 of 15 Report No.: AGC12319220501FE07 FCC ID : QV7-GC88752-71 APPLICATION PURPOSE : Original Equipment PRODUCT DESIGNATION : Drone BRAND NAME : N/A MODEL NAME : Please see the page 5. APPLICANT : GUANGDONG SYMA MODEL AIRCRAFT INDUSTRIAL CO., LTD DATE OF ISSUE : Jul. 08, 2022 STANDARD(S) TEST PROCEDURE(S) : FCC Part 15.407 KDB 905462 D02 REPORT VERSION : V1.0 Attestation of Global Compliance (Shenzhen) Co., Ltd FCC Test Report Report No.: AGC12319220501FE07 Page 2 of 15 Report Revise Record Report Version Revise Time Issued Date Valid Version Notes V1.0 / Jul. 08, 2022 Valid Initial Release Report No.: AGC12319220501FE07 Page 3 of 15 TABLE OF CONTENTS 1. VERIFICATION OF CONFORMITY .............................................................................................................. 4 2. GENERAL INFORMATION ........................................................................................................................... 5 3. DESCRIPTION OF TEST MODES ................................................................................................................ 7 4. SUMMARY OF TEST RESULTS .................................................................................................................. 7 5. TEST FACILITY............................................................................................................................................. 7 6. DYNAMIC FREQUENCY SELECTION (DFS) .............................................................................................. 8 6.1. APPLICABILITY OF DFS REQUIREMENTS ........................................................................................ 8 6.2. TEST SET-UP ........................................................................................................................................ 9 6.3. LIMITS .................................................................................................................................................... 9 6.4. RADAR TEST WAVEFORMS .............................................................................................................. 11 6.5. TEST PROCEDURE ............................................................................................................................ 11 6.6. TEST RESULT ..................................................................................................................................... 12 APPENDIX A: PHOTOGRAPHS OF TEST SETUP ..................................................................................…

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