Dec. 2, 2015 

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave., 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 of the FAA Modernization 

and Reform Act. 

Dear Sir or Madam: 

Pursuant to Section 333 ofthe FAA Modernization and Reform Act ("FMRA") and 14 C.F.R. Part 11, 

Michael Dauss hereby petitions the Federal Aviation Administration ("FAA") for exemption from 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 other rules the FAA deems necessary, to enable Michael Dauss to operate an unmanned 

aircraft systems ("UAS") for aerial data collection. Specifically, Michael Dauss seeks to operate VAS 

for commercial production, Search and Rescue, housing sales I rentals, agricultural management, 

facilities inspection and support an industrial cleaning I environmental service company using the 

Yuneec Q500 4K and future purchases of the Parrot Bebop, Parrot AR. Drone 2.0, DJI Phantom 3 and 

the Aerosky Delta FPV Wing. See Exhibit A for the product specifications. 

I. PROPOSED OPERATIONS AND PUBLIC INTEREST BENEFITS 

Given the below stated evidence, procedures, and precautions operating VAS commercially for the purposes 

ofbenefitting public 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 of injury or death by locating and isolating unsafe conditions. The final 

video would demonstrate work completion and conditional impact of before, during, and after cleanup 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 community but also the 

consumers. 

4. Aerial search and rescue operations: By the use of drones 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 survivability rate. 

5. Data collection augmented real estate listings: The use of drones 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 of the 

harder to access items of a 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 altemati ve 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 exceed the current level of safety 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 of the UAS to provide low altitude operation will 

provide an alternative to previously used methodology. This will provide a positive, economic and 

environmental potential to the communities and general public. 

II. THE UAS 

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 of all UAS for which exemption is 

requested herein. 

III. REQUEST FOR SUMMARY GRANT 

Because this petition is similar in material respects to previous petitions the FAA has granted, Michael Dauss 

requests that the FAA issue a summary grant of exemption pursuant to the agency's expedited summary grant 

process. Michael Dauss will adhere to a series of operating parameters that will offer the same level of safety 

as the conditions the FAA currently requires in its summary grants. 

IV. APPLICANT INFORMATION 

The name and contact information of the applicant is: 

Michael Dauss 

9113 Timber Lane 

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 operating parameters when operating UAS pursuant to a grant of 

the requested exemption: 

1. Operations will be conducted using the Yuneec Q500 4K, Parrot Bebop, Parrot AR. Drone 2.0, DJI 

Phantom 3 and the Aerosky Delta FPV Wing. 

2. The UAS will not be operated at a speed exceeding 87 knots (100 miles per hour), 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 will be conducted in accordance with a Certificate of Waiver or Authorization ("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 of sight of the PIC or the VO at all times. The PIC will maintain VLOS capability and 

the ability to communicate verbally with the 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 and passing 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 manner consistent with 14 C.F.R. § 61.5l(b). 

7. Michael Dauss operating documents will be accessible during UAS operations and made available to the 

Administrator upon request. 

8. Prior to each flight, the PIC will conduct a pre-flight inspection and determine the UAS is in a condition for 

safe flight. Ifthe inspection reveals a condition that affects the safe operation of the UAS, the UAS will not be 

operated until the necessary maintenance has been performed and the U AS is found to be in a condition for 

safe flight. See Exhibit B for Pre and Post Flight inspections by model design, i.e. Quadcopter and Delta wing. 

9. Any UAS that has undergone maintenance or alterations that affect the UAS operation or flight 

characteristics, e.g., replacement of a flight critical component, will undergo a functional test flight prior to 

conducting further operations under this exemption. 

10. Michael Dauss will follow the UAS manufacturer's maintenance, overhaul, replacement, inspection, and 

life limit requirements, as well as safety bulletins, for the aircraft and aircraft components. 

11. The PIC will abort the flight in the event of unpredicted 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. parts 47 and 45. 

-------------------------------- Page3of12 
VI. THE FAA'S AUTHORITY TO GRANT THIS PETITION 

The FAA has authority to grant the exemption requested herein under the FMRA and the Federal Aviation 

Act. Section 333 of the FMRA deals specifically with integrating UAS into the national airspace, and directs 

the Secretary of Transportation to determine which UAS, "as a result of their size, weight, speed, operational 

capability, proximity to airports and populated areas, and operation within visual line of sight do not create a 

hazard to users of the national airspace system or the public or pose a threat to national security." Section 333 

further directs the Secretary to "establish requirements for the safe operation of such aircraft systems in the 

national airspace system." 

The Federal Aviation Act authorizes the Administrator of the FAA to grant exemptions from regulations 

prescribed under certain provisions of the Act where such exemptions are in the public interest. Part 11 of the 

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 in a wide variety of industries. 

VII. SUMMARY TO BE PUBLISHED IN THE FEDERAL REGISTER 

Should the FAA determine that publication in the Federal Register is required, Michael Dauss offers the 

following summary pursuant to section 11.81 of the 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 relief from 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 of the 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 relief is in line with the 

proposed rule for PIC of drone 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 of12 
Exhibit A 

AIRCRAFT SPECIFICATIONS 

Typhoon Q500 4K 

Dimension 

'· 

330mm 

(13.0inl 

···. 

·.·· 

Flight Time up to 25 minutes 

Weight with Battery 

and Payload 60.0 oz ( 1700g) 

Weight without Battery 

and Payload 40.0 oz (1130g) 

Battery 5400mAh 3S 11.1 V LiPo (included) 

420mm 

(16.5in) .. . ~ .. ~ - -- ---.- -- -- -- . . ' 

210mm 

(8.31n) , 

Charger 3S 11.1 V LiPo DC Balancing Smart Charger with AC Adapter (included) 

Transmitter I 0-channel 2.4GHz with 5.8GHz video downlink (included) 

3 Flight Modes 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° 

Operating Temperature 

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 

Weight 6.9oz ( 195g) 

Focusing System Aerial Optimized Fixed Focus 

Field of View 1 15° 

Video Transmission 

Range 

FCC Compliance: Up to 600m (1968.5 ft) 

CE Compliance: Up to 300m (984.252 ft) with ST 1 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 I 0 ~ 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 

Storage Temperature -20°C-60°C 

Angular Vibration 

Range ±0.02° 

Control Range Pitch: between -90° and oa 

Microphone Yes 

Camera Lens 14mm f/2.8 -No distortion 

---- - ----------- Page 5 of 12 
Sensor 1/2.3" CMOS 

Dimensions 

Type STlO+ 

Operating System AndroidTM 

Number of Channels 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 of Sight of Aircraft 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 of Sight of Aircraft 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 

Camera Settings White balance, light exposure, ISO, shutter speed, video resolution, FPS, record video, 

take pictures 

Parrot Bebop Drone 

Specifications : 

Wi-Fi antennas: MIMO dual-band with 2 double-sets of dipole 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. II a/b/g/nlac 

4 Brushless Outrunner motors (fig.3) 

Glass fiber reinforced (15%) ABS structure (fig.4) 

High-resistance EPP outdoor hull: Clip and unclip easily to adapt to indoor and outdoor flight, protects the 

propellers against potential bumps, can be removed to reduce wind factor (fig.9) 

Three-blade auto-block propellers in Polycarbonate with fast disassembly system (fig.5) 

Anti-vibration bumpers (fig.\ 0) 

S LructLm; High-resistance 

Speed 13 m/s 

"Camera with ""Fisheye"" lens 180° 1/2,2"": 6 optical elements and 14 Mega pixels sensor (fig.2) 

Page 6 of12 
Video stabilization: Digital on 3-axes 

Video definition: 1920x 1 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 

Flight time: 22 minutes with 2 batteries included 

Battery Lithium Polymer 

Mother board: (fig. I) 

- Parrot P7 dual-core CPU Cortex 9 

- Quad core GPU 

- 8Gb flash memory 

All fixed on a magnesium shelf that acts as electromagnetic shielding and as a radiator 

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 compared to the previous one to determine the speed of the Bebop Drone) 

Ultrasound sensor (Analyzes the flight altitude up to 8 meters) 

Pressure sensor 

GNSS (GPS + GLONASS) (fig.6) 

Geo-location GNSS 

28x32x3.6cm without the hull 

33x38x3.6cm with the hull 

Dimensions 28x32x3.6cm 

With battery, 400g without the hull and 420g with the hull 

Weight 400g 

Compatibility !OS, Android, Windows Phone Smartphones/tablets 

HD video recording 

Parrot A.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 or tablet as you are flying. See a clean, sharp image just as if you were in 

the pilot seat. 

•HD Camera. 720p 30FPS 

Page 7 of12 
•Wide angle lens: 92° diagonal 

•H264 encoding base profile 

• Low latency streaming 

•Video storage on the fly with the remote device 

•JPEG photo 

•Video storage on the fly with Wi-Fi directly on your remote device or on a USB key 

Robust structure 

Trying your most daring tricks won't even challenge this cutting edge design which is made to last. 

•Carbon fiber tubes : Total weight 380g with outdoor hull, 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-Coating on ultrasound sensors 

•Fully reparable: All parts and instructions for repairing available on the internet 

Electronic assistance 

AR.Drone 2.0 on-board technology gives you extreme precision control and automatic stabilization features. 

•I GHz 32 bit ARM Cortex A8 processor with 800MHz video DSP TMS320DMC64x 

•Linux 2.6.32 

•I GB DDR2 RAM at 200M Hz 

•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+/- I 0 Pa precision 

•Ultrasound sensors for ground altitude measurement 

•60 FPS vertical QVGA camera for ground speed measurement 

Motors 

Fly high. 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 propeller reductor 

•I Tempered steel propeller shaft 

•I Self-lubrificating bronze bearing 

•I Specific high propelled drag for great maneuverability 

•I 8 MIPS A VR CPU per motor controller 

•Emergency stop controlled by software 

•Fully reprogrammable motor controller 

•Water resistant motor's electronic controller 

PHANTOM 3 PROFESSIONAL 

- ra-. ii "'"' (( .,_...,.. ... "" , .. · ~- ~ , __ ,, ~ 

AIRCRAFT 

Page 8 of12 
Weight (including battery and propellers) 1280 g 

Diagonal size (including propellers) 590 mm 

Max Ascent Speed 5 mls 

Max Descent Speed 3 m/s 

Hover Accuracy Vertical:+/- 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 Sea Level 6000 m (Software altitude limit: 120m above takeoff point) 

Operating Temperature 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 or 3.1 miles (unobstructed, free of interference) when FCC compliant 

Up to 3.5 km or 2.1 miles (unobstructed, free of interference) whenCE compliant 

Video Output Port USB 

Operating Temperature 0°C- 40°C 

Battery 6000 mAh LiPo 2S 

Mobile Device Holder For tablet or phone 

Receiver Sensitivity (I %PER) -1 0 I dBm ±2 dBm 

Transmitter Power (EIRP) FCC: 20 dBm 

CE: 16 dBm 

Working Voltage 1.2 A @7.4 V 

INTELLIGENT FLIGHT BATTERY 

Capacity 4480 mAh 

Voltage 15.2 V 

Battery Type LiPo 4S 

Energy 68 Wh 

Net Weight 365 g 

Max Flight Time Approximately 23 minutes 

Operating Temperature -I 0°C to 40°C 

Max Charging Power I 00 W 

CAMERA 

Sensor Sony EXMOR 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 I 00-3200 (video) I 00-1600 (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: 1920x I 080p 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: 1920xl080p 24/25/30/48/50/60 

HD: 1280x720p 24/25/30/48/50/60 

Supported SO Card Types Micro SO 

Max capacity: 64 GB. Class 1 0 or UHS-1 rating required 

Max Bitrate of Video Storage Phantom 3 Professional 

60 Mbps 

Phantom 3 Advanced 

40 Mbps 

Supported File Formats F AT32/exF AT 

Photo: JPEG, DNG 

Video: MP4, MOV (MPEG-4 A VC/H.264) 

Operating Temperature 0°C to 40°C 

VISION POSITIONING 

Max Velocity Less than 8 m/s (when 2m above ground) 

--------------------------------- Page9of12 
Altitude Range 50 cm-300 em 

Operating Range 50 cm-300 em 

Operating Environment Surface with clear pattern and adequate lighting (Lux> 15) 

BATTERY CHARGER 

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) 

Latency 220ms (depending on conditions and mobile device) 

Required Operating Systems iOS 8.0 or later 

Android 4.1.2 or later 

Recommended Devices iOS: iPhone 5s, iPhone 6, iPhone 6 Plus, iPad Air, iPad Air Wi-Fi +Cellular, iPad 

mini 2, iPad mini 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, 

Samsung NOTE3, Google Nexus 9, Google Nexus 7 II, Ascend Mate7, Nubia Z7 

FPV Wing Specifications: 

FPV Wing Features: 

Autopilot system +on screen display 2in 1 

Current and voltage sensors 

uBlx 6m GPS External Antenna 

5.8G I OOOmw FPV Video transmitter (5km) 

5.8G FPV Video Receiver 

5.8G circular polarized antenna 

Mushroom Antenna 

Sony CCD 600 TVL Camera 

7-inch Monitor 

CNC screen mounting bracket 

2.4G 6ch transmitter 

Motor 3536 880kv motor 

40A ESC 

9x6 propeller 

9g servos x2 

FPV Wing Specifications: 

mini, SONY Z3 EXPERIA, MI 3, MI PAD 

Page 10 of12 
Laser (U A V FPV system) 

Wing span: 1550mm(61 in) 

Length: 683 mm(26.88in) 

Flying weight: 900g(31. 74 oz) 

Transmitter: 6CH 

Servo: 2*9g 

Motor: 3536-KV1200 Powerful Out runner Brush less Motor 

ESC: 40A Brushless ESC 

Prop Size: 9 inches propeller 

Battery: 11.1 v(3s) 3000-6000mAh battery 

Average flight time: 25 min-40min 

Payload capacity: 1.3kg 

Maximum speed: 90 kmh 

Minimum speed: 15 kmh 

FPV Electronics Specifications: 

5.8Ghz Transmitter Specifications: 

Transmission frequency: 5725-5865MHz; Eight channels 

Transmission power: 23dBm/200mW 

Transmission distance: >2000m 

Frequency control: Built-in frequency PLL 

A V 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 

Frequency control: Built-in frequency PLL 

Dual A V output: Direct output video signals 

The antenna interface: SMA(The needle) 

Power supply voltage: 6.5-ISV 

Power supply current: !SOmA 

Outsize: 61 *52*13mm, Aluminum alloy shell 

Monitor: 

Mount: CNC machined mount will attach monitor to JR/Spektrum and Futaba TX 

Rate: 800*480 

The screen size: 154mm (width) *87mm (height) 

Aspect ratio: 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: P AL:762(H) X 504(V) 

Formats: PAL 

Work voltage: DC8.5V-DC18V 

Work current: DC12V SOmA 

Work temperature: -I 0 - +60 C 

Page 11 of12 
Exhibit B 

PRE I POST FLIGHT lNSPECTlONS 

Operator:------------- Date: ______________ ___ PAGE: ___ _ 

Arrival Checklist: 

1. If day and operating out of back of vehicle, 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 of field if closer than 5 NM 

5. Inform tower I CTAF of UAS ops, location, and max height of flight. 

PREFLIGHT: cw After Takeoff Checklist! 

1. Remove transmitter. 1. Hover approximately ten 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 of Oos 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 

cw 

cw 

cw 

cw