### Dec. 2, 2015

U.S. Department ofTransportation DocketManagement System 1200 NewJerseyAve., SE Washington, D.C. 20590

Re: Petition Michael Dauss for Exemption from Certain Federal Aviation Regulations to Operate Unmanned Aircraft Systems Pursuant to Section 333 ofthe FAA Modernization and Reform Act.

Dear Sir orMadam:

Pursuantto Section 333 ofthe FAA Modernizationand Reform Act ("FMRA") and 14 C.F.R. Part 11, Michael Dauss herebypetitions the Federal Aviation Administration ("FAA") for exemptionfrom 14 C.F.R. §§ 61.3(a), 14 C.F.R. §§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 91.7(a), 91.119(c), 91.121, 91.15l(a)(l), 91.405(a), 91.407(a)(l), 91.409(a)(l) and (2), and 91.417(a) and (b), and any otherrules the FAA deems necessary, to enable Michael Dauss to operate anunmanned aircraft systems ("UAS") for aerial data collection

. Specifically, Michael Dauss seeks to operate VAS for commercialproduction, Search and Rescue, housing sales 

### I rentals, agricultural management, facilities inspection and support an industrial cleaning 

### Ienvironmental service companyusing the Yuneec Q500 4Kand future purchases ofthe ParrotBebop, Parrot AR. Drone 2.0, DJI Phantom 3 and the Aerosky Delta FPV Wing. See Exhibit A for the product specifications.



### I. PROPOSED OPERATIONSAND PUBLIC INTEREST BENEFITS Given the below stated evidence, procedures, and precautions operating VAS commercially for the purposes ofbenefittingpublic interest:

1

. Environmental emergencies: Utilizing the drones during an environmental emergency provides responders with a real time aerial environment for which an assessment can be made to determine the risk associated and reduce the potential ofinjury or death by locating and isolating unsafe conditions. The final video would demonstrate workcompletion and conditional impact ofbefore, during, and aftercleanup efforts. 2

. Mapping: By utilizing drones, new roads as well as construction sites can be analyzed and developmental 

### I environmental impacts can be monitored thus reducing wasted resources. This will also help support the housing market for a realtor to a promote sale from the office prior to using a motor vehicle to drive to the location thus reducing the carbon deposits and making home sales more productive. 3

. Agricultural crop surveillance: The utilization of drones can reduce the amount of lost crops by monitoring large areas that require additional resources such as water/fertilizer which will reduce the time to adjust crop requirements and increase production and reduce cost not only the farming communitybut also the

consumers. 4. Aerial search and rescue operations: By the use ofdrones while operating in conjunction with on the ground search and rescue operations, valuable time can be gained and the ability to locate the target faster can be achieved, leading to a higher survivabilityrate. 5

. Data collection augmented real estate listings: The use ofdrones in this avenue will help and assist potential homeowners in the ability to make decisions in their long term investments. Occasionally houses will sit on the market for some time and by providing real time images, one can determine the condition ofthe harderto access items ofa property, such as roofs.



### Page 1 of12

### 6. Commercial videos: The use of drones will assist in the production of cinematic productions. By offering a low cost altemative to expensive manned systems, production cost are lowered and risk is reduced. Also noise and carbon pollution will be reduced significantly as the drones utilized are quite and carbon deposit free in comparison.

These operations, when executed with prudence, will exceedthe current level ofsafety as the regulations from which the exemption is sought. These UAS operations will allow greater access to commercial aerial services that were not previously economically feasible for many firms and will be associated with less risk of collateral damage to persons and property. The ability ofthe UAS to provide low altitude operation will provide an alternative to previously used methodology. This will provide a positive, economic and environmental potentialto the communities and general public.

II. THEUAS Michael Dauss requests an exemption to operate the Yuneec Q500 4K, Parrot Bebop, Parrot AR. Drone 2.0, DJI Phantom 3 and the Aerosky Delta FPV Wing all of which are well below 55 pounds including payload. Through the section 333 exemption process, the FAA has authorized use ofall UAS for which exemption is requestedherein.

III.REQUEST FORSUMMARYGRANT Because this petition is similarin material respects to previous petitions the FAA has granted, Michael Dauss requests that the FAA issue a summary grant ofexemption pursuant to the agency's expedited summary grant process. Michael Dauss will adhere to a series ofoperatingparameters that will offerthe same level ofsafety

as the conditions the FAA currentlyrequires in its summarygrants.

IV. APPLICANTINFORMATION The name and contact information ofthe applicantis: Michael Dauss 9113 TimberLane Navarre FL, 92566
Regulations from which exemption is requested:

14 C.F.R. §§ 61.3(a): 14 C.F.R. §§ 61.23(a) and (c); 14 C.F.R. §§ 61.101(e)(4) and (5); 14C.F.R. § 61.113(a); 14 C.F.R. § 61.315(a); 14 C.F.R. 

### § 91.7(a); 14 C.F.R. 

### § 91.119(c); 14 C.F.R. 

### § 91.121; 14 C.F.R. § 91.151(a)(l); 14 C.F.R. § 91.405(a); 14 C.F.R. § 91.407(a)(l); 14 C.F.R. §§ 91.409(a)(l) and (2); 14 C.F.R. §§ 91.417(a) and (b).

-------------------------------- Page2of12

### V. OPERATING PARAMETERS 

### Michael Dauss will adhere to the following operatingparameters when operating UAS pursuantto a grant of the requested exemption:

1. Operations will be conductedusingthe Yuneec Q500 4K, Parrot Bebop, Parrot AR. Drone 2.0, DJI Phantom 3 andthe Aerosky Delta FPV Wing.

2

.The UAS will notbe operated at a speed exceeding 87 knots (100 miles perhour), at an altitude greater than 400 feet above ground level, or, when visibility is less than 3 statute miles, less than 500 feet below or 2,000 feet horizontally from a cloud. All operations will be conducted during the day under visual meteorological conditions

.
3

.All operations willbeconducted in accordance with a Certificate ofWaiver orAuthorization ("CO A").

4

. All operations will use a pilot-in-command ("PIC") and a visual observer ("VO"), and the UAS will remain within the visual line ofsight ofthe PIC or the VO at all times. The PIC will maintain VLOS capability and the abilityto communicate verballywiththe VO at all times.

5. The PIC will hold an airline transport, commercial, private, recreational I 

### sport pilot certificate or as a minimum the requirements of 14 C.F

.R. §§ 61.35 Knowledge test: prerequisites andpassing grades, as well as an FAA airman medical certificate or a valid U.S. driver's license. The PIC will meet the flight review requirements specified in 14 C.F.R. § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

6

. Michael Dauss will ensure prior to operation that the PIC has demonstrated the ability to safely operate the UAS in a manner consistent with how the UAS will be operated under this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from persons, vessels, vehicles and structures. PIC qualification flight hours and currency will be logged in a mannerconsistent with 14 C.F.R. § 

### 61.5l(b).

7

.Michael Dauss operating documents will be accessible during UAS operations and made availableto the Administratoruponrequest.

8. Priorto each flight, the PIC will conduct apre-flight inspection and determine the UAS is in a condition for safe flight. Ifthe inspection reveals a condition that affects the safe operation ofthe UAS, the UAS will notbe operated until the necessary maintenance has been performed and the U AS is found to be in a condition for safe flight. See ExhibitB for Pre andPost Flight inspections bymodel design, i.e. Quadcopterand Delta wing.

9

. Any UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics, e.g., replacement ofa flight critical component, will undergo a functional test flight prior to conducting further operations underthis exemption.

10

. Michael Dauss will follow the UAS manufacturer's maintenance, overhaul, replacement, inspection, and life limitrequirements, as well as safetybulletins, for the aircraft and aircraft components.

11. The PIC will abort the flight in the event ofunpredicted obstacles or emergencies, and will yield to all manned aviation activities.

12. Michael Dauss will register and mark its UAS in accordance with 14 C.P.R. parts47 and45

.



### -------------------------------- Page3of12

### VI. THE FAA'SAUTHORITYTO GRANT THIS PETITION The FAA has authority to grant the exemption requested herein under the FMRA and the Federal Aviation Act. Section 333 ofthe FMRA deals specifically with integrating UAS into the national airspace, and directs the Secretary ofTransportation to determine which UAS, "as a result oftheir size, weight, speed, operational capability, proximity to airports and populated areas, and operation within visual line ofsight do not create a hazard to users ofthe national airspace system orthe public orpose a threat to national security." Section 333 further directs the Secretary to "establish requirements for the safe operation ofsuch aircraft systems in the national airspace system." The Federal Aviation Act authorizes the Administrator of the FAA to grant exemptions from regulations prescribedundercertainprovisions ofthe Act where such exemptions are inthe public interest. Part 11 ofthe Federal Aviation Regulations governs the FAA's exemption process and requirements. The FAA has granted

more than 1,100 exemptions to date pursuant to its Section 333 and exemption authority, enabling commercial UAS operations ina wide variety ofindustries.



### VII. SUMMARYTO BE PUBLISHEDINTHEFEDERAL REGISTER Shouldthe FAA determine thatpublication in the Federal Register is required, Michael Dauss offers the following summarypursuant to section 11.81 ofthe FAA's rules:



### Petitioner: Michael Dauss 

### Sections of 14 C. 

### FR. Affected: 14 C.F.R. §§ 61.3(a), 14 C.F.R. §§ 61.23(a) and (c); 14 C.F.R. §§ 61.101(e)(4) and (5); 14 C.F.R. § 61.113(a); 14 C.F.R. § 61.315(a); 14 C.F.R. § 

### 91.7(a); 14 C.F.R. 

### § 91.119(c); 14 C.F.R. § 91.121; 14 C.F.R. 

### § 91.151(a)(l); 14 C.F.R. 

### § 91.405(a); 14 C.F.R. 

### § 91.407(a)(l); 14 C.F.R. §§ 

### 91.409(a)(l) and (2); 14 C.F.R. §§ 91.417(a) and (b). 

### Description of Relief Sought: Petitioner seeks relieffrom the requirements of 14 C.F.R. §§ 61.3(a), 14 C.F.R. §§ 61.23(a) and (c); 14 C.F.R. §§ 61.101(e)(4) and (5); 14 C.F.R. § 61.113(a); 14 C.F.R. § 61.315(a); 14 C.F.R. § 

### 91.7(a); 14C.F.R. § 

### 91.119(c); 14 C.F.R. § 91.121; 14 C.F.R. § 91.151(a)(l); 14 C.F.R. § 91.405(a); 14 C.F.R. § 91.407(a)(l); 14 C.F.R. §§ 91.409(a)(l) and (2); 14 C.F.R. §§ 91.417(a) and (b) to operate unmanned aerial systems for commercial production, search and rescue, housing sales I 

### rentals, agricultural management, facilities inspection and support an industrial cleaning I

### environmental service company.

NOTE: The relief sought from 14 C.F.R. §§ 

### 61.3(a) is only for the requirement ofthe practical tests and Pilots Certificate. The PIC will still be required to meet the minimum requirements of 14 C.F.R. 

### §§ 61.35 Knowledge test: prerequisites and passing grades and the must be renewed every two years. This reliefis in line with the proposedrule for PIC ofdrone aircraft.



### VIII. CONCLUSION As demonstrated above, the UAS operations Raycom has proposed in this petition for exemption will gamer significant public benefits while presenting minimal safety risks. Michael Dauss's petition satisfies the criteria of Section 333 of the FMRA and is substantially similar to previous petitions the FAA has granted, meriting a summary grant of exemption. Michael Dauss respectfully requests that the FAA grant this petition to enhance Michael Dauss's ability to provide a service to the commercial production, search and rescue, housing sales I 

### rentals, agricultural management, facilities inspection and support an industrial cleaning I 

### environmental service company.

Please do not hesitate to contact Michael Dauss at (704)654-2193 with any questions about this filing.

# s~ Michael Dauss

Page 4 of12ExhibitA 

### AIRCRAFT SPECIFICATIONS

Typhoon Q5004K Dimension

'·

330mm (13.0inl 

### ···.

·.·· Flight Time up to 25 minutes Weight with Battery and Payload 60.0 oz (1700g) Weightwithout Battery and Payload40.0 oz (1130g) Battery5400mAh 3S 11.1V LiPo (included) 420mm (16.5in)

.. .**~** ..**~** ------.--- ----

## .
. '

210mm (8.31n)
,

Charger 3S 11.1V LiPo DC Balancing Smart Charger with AC Adapter (included) Transmitter I0-channel 2.4GHz with 5.8GHz video downlink (included) 3 FlightModes Smart (Follow Me and Watch Me), Angle and Home Maximum Flying Height Default 122m (400ft) above Ground Level (Adjustable via the Typhoon GUI) Maximum Rotation Rate 65°/s Maximum Roll Angle 35° OperatingTemperature Range -sac to 80°C Radio Control Frequency Band 2.4GHz Max. Descent Speed 2m/s Max. Flight Speed 17mph I 27 kph (Angle Mode), 22mph I 35 kph (Follow Me/Watch Me)
Type CG03 Weight6.9oz (195g) Focusing System Aerial Optimized Fixed Focus Field ofView 115° Video Transmission Range FCC Compliance: Up to 600m (1968.5 ft) CE Compliance: Up to 300m (984.252 ft) with ST1 0 Video Resolution UHD: 4K at 30FPS, 2.7K at 30FPS, 2.5K at 30FPS- FULL HD: 1080p at 24/25/30/48/50/60/120FPS Photo Resolution 12 Megapixels Storage (memory) microSD Class I0**~** 4 to 128 GB Control Angle Accuracy ±0.02° White Balance Automatic or manual settings Transmission Band 5.8GHz. Input/Operating Voltage 12V Working Temperature -10°C-soac StorageTemperature-20°C-60°C Angular Vibration Range ±0.02° Control Range Pitch: between -90° and oa Microphone Yes Camera Lens 14mm f/2.8 -Nodistortion

---- - ----------- Page 5 of12Sensor 1/2.3" CMOS

Dimensions Type STlO+ Operating System AndroidTM Number ofChannels 10 Control Transmission Range (Optimum Conditions) FCC Compliance: Up to 800m (2624.67 ft) CE Compliance: Up to 400m (1312.34 ft) Warning: You Must Follow Local Laws and Maintain Visual Line ofSightofAircraft at All Times Robust Radio Control Modulation Yuneec Protocol Video Link Frequency Band 5.8GHz Video Transmission Range (Optimum Conditions) FCC Compliance: Up to 600m (1968.5 ft) CE Compliance: Up to 300m (984.252 ft) Warning: You Must Follow Local Laws and Maintain Visual Line ofSight ofAircraft at All Times Flight Systems Telemetry Data On Screen Display Yes LED Backlit LCD Screen Capacitive Multi-touch 5.5" Tactile (Vibrating) and Audible Feedback Yes Built-in LiPo Battery Voltage I Capacity 3.6V/5200mAh 18.72Wh Screen Resolution 854 x 480px CameraSettings White balance, light exposure, ISO, shutter speed, video resolution, FPS, record video, take pictures

ParrotBebop Drone

Specifications : Wi-Fi antennas: MIMO dual-band with 2 double-sets ofdipole antennas for 2.4 and 5 GHz (fig.7) Sending power: Up to 2 I dBm Signal range: Up to 250 meters Connectivity Wi-Fi 802. IIa/b/g/nlac 4 Brushless Outrunnermotors (fig.3) Glass fiber reinforced (15%) ABS structure (fig.4) High-resistance EPP outdoorhull: Clip and unclip easily to adapt to indoor and outdoor flight, protects the propellers againstpotential bumps, can be removed to reduce wind factor (fig.9) Three-blade auto-block propellers in Polycarbonate with fast disassembly system (fig.5) Anti-vibrationbumpers (fig.\0) SLructLm; High-resistance Speed 13 m/s "Camerawith ""Fisheye"" lens 180° 1/2,2"": 6 optical elements and 14 Mega pixels sensor (fig.2)



### Page 6 of12Video stabilization: Digital on 3-axes Video definition: 1920x1 080p (30fps) Photo definition: 4096x3072 px Video encoding: H264 Photo file format: JPEG, RAW, DNG Internal memory: Flash 8 GB Camera CMOS 14Mpx, 1/2.3" Lithium Polymer 1200 mAh Flighttime: 22 minutes with 2batteries included Battery Lithium Polymer Motherboard: (fig.I)

- Parrot P7 dual-core CPU Cortex 9

- Quad core GPU

- 8Gb flash memory All fixed on a magnesium shelfthat acts as electromagnetic shielding and as aradiator Operating system: Linux Developping: Open-source SDK Processor CPU: Dual-Core 3-axes magnetometer 3-axes gyroscope 3-axes accelerometer (fig.6) Optical-flow sensor (fig.8): Vertical stabilization camera (Every 16 milliseconds, an image ofthe ground is taken Sensors 3-axes and comparedto the previous one to determine the speed ofthe Bebop Drone) Ultrasound sensor (Analyzes the flight altitude up to 8 meters) Pressure sensor GNSS (GPS +GLONASS) (fig.6) Geo-location GNSS 28x32x3.6cmwithout the hull 33x38x3.6cm with the hull Dimensions 28x32x3.6cm With battery, 400g withoutthe hull and 420g with the hull Weight 400g Compatibility !OS, Android, Windows Phone Smartphones/tablets

HD video recording ParrotA.R. 2.0

Z 451mm- 

# ----

.......

• lndQor Hull: 14.82oz/42Qg • Outdoor Hull : 1"

3,40oz/380g 

# I
f i 

# 1

Get high definition live video streaming to your smartphone ortablet as you are flying. See aclean, sharp imagejust as ifyou were in the pilot seat. •HD Camera. 720p 30FPS



### Page 7 of12•Wide angle lens: 92° diagonal •H264 encodingbase profile

•Low latency streaming •Video storage on the fly with the remote device •JPEG photo •Video storage onthe fly with Wi-Fi directlyon your remote device oron a USB key

Robust structure Trying yourmost daring tricks won'teven challenge this cutting edge design which is made to last. •Carbon fiber tubes :Total weight 380gwith outdoorhull, 420g with indoor hull •High grade 30% fiber charged nylon plastic parts •Foam to isolate the inertial center from the engines' vibration •EPP hull injected by a sintered metal mold •Liquid Repellent Nano-Coatingon ultrasound sensors •Fully reparable: All parts and instructions for repairing available on the internet

Electronic assistance AR.Drone 2.0 on-board technologygives you extremeprecision control and automatic stabilization features. •IGHz 32 bit ARM Cortex A8 processor with 800MHz video DSP TMS320DMC64x •Linux 2.6.32 •IGB DDR2 RAM at 200MHz •USB 2.0 high speed for extensions •Wi-Fi b g n •3 axis gyroscope 2000°/second precision •3 axis accelerometer+-50mg precision •3 axis magnetometer 6° precision •Pressure sensor+/- I0 Pa precision •Ultrasound sensors for ground altitude measurement •60 FPS vertical QVGAcamerafor ground speed measurement

Motors Flyhigh. Fly fast. Far away from the ground. •4 brushless inrunner motors. 14.5W 28,500 RPM •I Micro ball bearing •I Low noise Nylatron gears for 1/8.75 propellerreductor •I Tempered steel propeller shaft •I Self-lubrificating bronze bearing •I Specific high propelled drag for great maneuverability •I 8 MIPS AVR CPU permotor controller •Emergency stop controlledby software •Fullyreprogrammable motor controller •Waterresistant motor's electronic controller
PHANTOM 3 PROFESSIONAL



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### ,,**~**

AIRCRAFT



### Page 8 of12Weight (includingbattery and propellers) 1280g Diagonal size (including propellers) 590 mm Max Ascent Speed 5mls Max Descent Speed 3 m/s HoverAccuracyVertical:+/- 0.1 m (when Vision Positioning is active) or+/- 0.5 m Horizontal:+/- 1.5 m Max Speed 16 m/s (ATTI mode, no wind) Max Service Ceiling Above SeaLevel 6000m (Software altitude limit: 120m above takeoffpoint) OperatingTemperature 0°C to 40°C GPS Mode GPS/GLONASS GIMBAL Controllable Range Pitch -90° to +30° Stabilization 3-axis (pitch, roll, yaw) REMOTE CONTROLLER Operating Frequency 2.400 GHz-2.483 GHz Max Distance Up to 5 km or3.1 miles (unobstructed, free ofinterference) when FCC compliant Up to 3.5 km or2.1 miles (unobstructed, free ofinterference) whenCE compliant Video Output Port USB OperatingTemperature 0°C- 40°C Battery 6000mAh LiPo 2S Mobile Device Holder Fortabletor phone Receiver Sensitivity (I%PER) -10I dBm±2 dBm TransmitterPower (EIRP) FCC: 20 dBm CE: 16 dBm Working Voltage 1.2 A @7.4 V INTELLIGENT FLIGHT BATTERY Capacity4480mAh Voltage 15.2 V Battery Type LiPo 4S Energy 68 Wh Net Weight 365 g Max FlightTime Approximately 23 minutes OperatingTemperature -I0°C to 40°C Max Charging Power I00 W CAMERA Sensor SonyEXMOR 112.3" Effective pixels: 12.4 M(total pixels: 12.76 M) Lens FOV 94° 20 mm (35 mm format equivalent) f/2.8, focus at oo ISO Range I00-3200 (video) I00-1600 (photo) Shutter Speed 8s -l/8000s Image Max Size 4000 x 3000 Still Photography Modes Single Shot Burst Shooting: 3/5/7 shots Auto Exposure Bracketing (AEB): 3/5 Bracketed Frames at 0.7EV Bias Time-lapse Video Recording Modes Phantom 3 Professional UHD: 4096x2160p 24/25, 3840x2160p 24/25/30 FHD: 1920xI080p 24/25/30/48/50/60 HD: 1280x720p 24/25/30/48/50/60 Phantom 3 Advanced 2.7K: 2704 xl520p 24/25/30 (29.97) FHD: 1920xl080p24/25/30/48/50/60 HD: 1280x720p 24/25/30/48/50/60 Supported SO CardTypes Micro SO Max capacity: 64 GB. Class 1 0 or UHS-1 rating required Max Bitrate ofVideo Storage Phantom 3 Professional 60 Mbps Phantom 3 Advanced 40 Mbps Supported File Formats FAT32/exFAT Photo: JPEG, DNG Video: MP4, MOV (MPEG-4 AVC/H.264) OperatingTemperature 0°C to 40°C VISION POSITIONING Max Velocity Less than 8m/s (when 2m above ground)



### --------------------------------- Page9of12Altitude Range 50 cm-300 em Operating Range 50 cm-300 em OperatingEnvironment Surface with clearpattern and adequate lighting (Lux> 15) BATTERYCHARGER Voltage 17.4 V Rated Power Phantom 3 Professional lOOW Phantom 3 Advanced 57W APP I LIVE VIEW Mobile App DJI GO EIRP IOOmW Power Spectral Density 6.9mW/MHz Live View Working Frequency 2.4GHz ISM Live View Quality 720P@ 30fps (depending on conditions and mobile device) Latency220ms (depending on conditions and mobiledevice) Required Operating Systems iOS 8.0 orlater Android4.1.2 orlater Recommended Devices iOS: iPhone 5s, iPhone 6, iPhone 6 Plus, iPad Air, iPadAir Wi-Fi +Cellular, iPad mini 2, iPadmini 2 Wi-Fi +Cellular, iPad Air 2, iPad Air 2 Wi-Fi +Cellular, iPad mini 3, and iPad mini 3 Wi-Fi +Cellular. This app is optimized for iPhone 5s, iPhone 6, and iPhone 6 Plus Android: Samsung tabs 705c, Samsung S6, Samsung S5, Samsung NOTE4, SamsungNOTE3, GoogleNexus 9, Google Nexus 7 II, Ascend Mate7, NubiaZ7

FPV Wing Specifications:

FPV Wing Features: Autopilot system +on screen display 2in1 Current andvoltage sensors uBlx 6m GPS External Antenna 5.8G IOOOmw FPV Video transmitter (5km) 5.8G FPV Video Receiver 5.8G circularpolarized antenna Mushroom Antenna SonyCCD 600 TVL Camera 7-inch Monitor CNC screen mounting bracket 2.4G 6ch transmitter Motor3536 880kvmotor 40A ESC 9x6 propeller 9g servos x2

FPV Wing Specifications: mini, SONYZ3 EXPERIA, MI 3, MI PAD



### Page 10of12Laser (UA V FPV system) Wing span: 1550mm(61in) Length: 683 mm(26.88in) Flying weight: 900g(31.74 oz) Transmitter: 6CH Servo: 2*9g Motor: 3536-KV1200Powerful Out runner Brushless Motor ESC: 40A Brushless ESC Prop Size: 9 inches propeller Battery: 11.1v(3s) 3000-6000mAh battery

Average flight time: 25 min-40min Payload capacity: 1.3kg Maximum speed: 90 kmh Minimum speed: 15 kmh

FPVElectronics Specifications:

5.8Ghz Transmitter Specifications: Transmission frequency: 5725-5865MHz; Eight channels Transmission power: 23dBm/200mW Transmission distance: >2000m Frequencycontrol: Built-in frequency PLL AV Input: Direct input video signals Power supply voltage: 6.5-ISV Power supply current: 200mA Outsize: 55*26*17mm 5.8Ghz Receiver Specifications: Receive frequency: 5725-5865MHz; Eight Channels Receiving sensitivity: -90dBm Frequencycontrol: Built-in frequency PLL Dual A V output: Direct outputvideo signals The antenna interface: SMA(The needle) Power supply voltage: 6.5-ISV Power supplycurrent: !SOmA Outsize: 61 *52*13mm, Aluminum alloy shell Monitor: Mount: CNC machined mount will attach monitorto JR/Spektrum and FutabaTX Rate: 800*480 The screen size: 154mm (width) *87mm (height) Aspectratio: 4:3 I 16:9 (can choose switch by yourself) Contrast: 350:I Power: 12V General consumption power: Around 6W Size: 174mm (length) *114mm (width) *23mm (height) Camera: DSP: Next chip 2040 Resolution: 600TVL High Resolution CCD:Sony Image Sensor D-WDR: Digital Wide Dynamic Range Pixel: PAL:762(H) X 504(V) Formats: PAL Work voltage: DC8.5V-DC18V Work current: DC12V SOmA Work temperature: -I0

- +60 C



### Page 11of12

### ExhibitB PRE 

### IPOST FLIGHTlNSPECTlONS

Operator:-

------------ Date:

______________ ___ PAGE:

___ _
Arrival Checklist: 1. Ifday and operating out of back ofvehicle, point vehicle into sun. 2. Remove case and place on level surface. 3. Check distance to nearest airport and/or controlled airspace using smartphone or tablet app. 4. If required, use VHF aviation transceiver, to contact tower offield if closerthan 5 NM 5. Inform tower 

### I CTAF of UAS ops, location, and max height offlight.

PREFLIGHT: 

## cw AfterTakeoffChecklist! 1. Remove transmitter

. 1. Hover approximatelyten feet above the 2. Router- On ground to confirm UAS is under control. 3. Transmitter- On 2. All sticks operate correctly while in hover. 4. Toggle Switches- Full Up Pre-Landing_ Checklist 5. Video Monitor- On 1. Camera

- Full Up 6. Remove UAS from case

. 2. Video Recorder

- Stop 7. Gimbal Lock & Lens Cap- Removed 3. Landing Zone

- Clear I Safe 8. Micro-SD card- Inserted

. 9. UAS Battery- Inserted Post-Landina Checklist

- Returnina to 10. Place UAS in clear and safe launch Fliaht Immediate/vi and recovery position if it returns to home. 1 . Battery

- Remove &Replace
11. UAS Battery

- On 2. Wifi Connection to Monitor- Verified 12. Wifi Connection to Monitor- Verified 3. Application- Connect to Camera 13. Application

- Load 4. Takeoff 14. Application- Connect to Camera End ofOos Checklist! 15. SD Card

- Format 1 . Battery

- Off 16. Camera- Full Up 2. Transmitter- Off 17. Satellite Connections- Verified 3. Router- Off 18. Charge Levels

- Safe for Flight 4. Notify Tower/CTAF- End of Ops 19. Video Recording

- Start 20. Takeoff



### ------------------- Page12of12 

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