### Electronic Submission

Thursday, February 04, 2016 U.S. Department of Transportation, Docket Operations West Building Ground Floor, Room W12-140 1200 New Jersey Avenue, SE Washington, DC 20590

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (herein referred to as FMRA) and 14 CFR Part 11, Airadyme hereby applies for an exemption from the listed Federal Aviation Regulations (FARs) to allow commercial operation of UAS for the acquisition of aerial data, so long as such operations are conducted within and under the conditions outlined herein or as may be established by the FAA.

As detailed in this document and the attached Appendix of UAS, the requested exemption would permit the operation of UAS under controlled conditions in the United States. Approval of this exemption would thereby enhance safety and fulfill the Secretary of Transportation’s responsibilities to “...establish requirements for the safe operation of such aircraft systems in the national airspace system.” Section 333(c) Reform Act.

The name and address of the applicant is: Airadyme Richard Gowen 58C Main Street Plymouth NH 03264



### Regulations from which the exemption is requested:

14 CFR Part 21 14 CFR 45.23(b) 14 CFR 61.113(a) & (b) 14 CFR 91.7(a) 14 CFR 91.9(b)(2)

14 CFR 91.103

14 CFR 91.109

14 CFR 91.119

14 CFR 91.121 14 CFR 91.151(a) 14 CFR 91.203(a) & (b) 14 CFR 91.405(a) 14 CFR 407(a)(1) 14 CFR 409(a)(2) 14 CFR 417(a) & (b)

AUTHORITY FOR EXEMPTIONS

### The Federal Aviation Act expressly grants the FAA authority to issue exemptions. This statutory

authority includes exempting civil aircraft, as the term is defined under §40101 of the Act, including UAS, from the requirement that all civil aircraft must have a current airworthiness certificate.

The Administrator may grant an exemption from a requirement of a regulation prescribed under subsection (a) or (b) of this section or any sections §44702-44716 of this title if the Administrator finds the exemption in the public interest. 49 USC §44701(f). See also 49 USC §44711(a); 49 USC §44704; 14 CFR 91.203(a)(1).

Section 333(b) of the Reform Act assists the Secretary in determining whether UAS may operate in the national airspace system without creating a hazard to the user, the public, or a threat to national security. In making this determination, the Secretary must consider:

• The UAS’ size, weight, speed and operational capability; • Whether the UAS operates within the visual line of sight of the operator; • Whether the UAS operates outside of highly populated areas and away from close proximity to airports.

Reform Act 333(a). If the Secretary determines that a UAS “may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft in the national airspace system.” Id. 333(c).

3 BACKGROUND ON AIRADYME

Airadyme provides turnkey solutions utilizing UAS to deliver specific, low risk, and cost effective actionable data to clients. was founded specifically to help clients avoid the capital expense and operating risks of establishing their own drone programs and to purchase drone support in a way which better fits their operations and cost profiles.

UAS AND OPERATIONAL DESCRIPTION

Airadyme seeks to commercially operate a variety of UAS weighing less than 55 pounds including payload in the United States for the purpose of acquiring aerial data. Appendix 1 attached to this exemption petition lists the aircraft that Airadyme contemplates operating. In addition, Airadyme requests that it be granted permission to operate those aircraft already approved in previous Section 333 exemption petitions.

As the operator of these aircraft, Airadyme is committed to the following conditions and limitations on its operations. Airadyme understands that failure to comply will be grounds for the immediate suspension or rescission any exemption granted.

1. Operations are limited to the UAS listed in the Appendix and those UAS previously approved by the Secretary when weighing less than 55 pounds including payload.

### 2. Operations for the purpose of closed-set motion picture and television filming are not

contemplated.

2. The aircraft will not be operated at a speed exceeding 87 knots (100 miles per hour). In no case will the aircraft be operated at airspeeds greater than the maximum aircraft operating airspeed recommended by the aircraft manufacturer.

3. The aircraft will be operated at an altitude of no more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL.

4. The aircraft will be operated within visual line of sight (VLOS) of the Pilot in Command (PIC) at all times. This requires the PIC to be able to use human vision unaided by any device other than corrective lenses, as specified on the PIC’s U.S. driver’s license.

5. All operations will utilize a visual observer (VO). The aircraft will be operated within the visual line of sight (VLOS) of the PIC and VO at all times.

6. All operating documents needed to operate the UAS and will be accessible during UAS operations and made available to the Administrator upon request. The operator will also present updated and revised documents if it petitions for extension or amendment.

7. 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.

8. Airadyme is responsible for maintaining and inspecting the UAS to ensure that it is in a condition for safe operation.

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

10. Airadyme will follow the UAS manufacturer’s maintenance, overhaul, replacement, inspection, and life limit requirements for the aircraft and aircraft components.

12. Each UAS operated under this exemption will comply with all manufacturer safety bulletins.

13. The PIC will hold a UAS flight training certificate, in some cases training directly from the aircraft manufacturer, and a valid U.S. driver’s license issued by a state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal government.

### 14. Airadyme will not permit any PIC to operate unless the PIC demonstrates the ability to safely

operate the UAS in a manner consistent with how the UAS will be operated to acquire aerial data, 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 5 consistent with 14 CFR § 61.51(b). Airadyme will operate flights for the purposes of training Airadyme PICs and VOs (training, proficiency, and experiencebuilding) and determining the PIC’s ability to safely operate the UAS.

15. UAS operations will not be conducted during night, as defined in 14 CFR § 1.1. All operations will be conducted under visual meteorological conditions (VMC).

16. The aircraft will not operate within 5 nautical miles of an airport reference point (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) or for airports not denoted with an ARP, the center of the airport symbol as denoted on the current FAA-published aeronautical chart, unless a letter of agreement with that airport’s management is obtained or otherwise permitted by a COA.

17. The aircraft will not be operated less than 500 feet below or less than 2,000 feet horizontally from a cloud or when visibility is less than 3 statute miles from the PIC.

18. If the UAS loses communications or loses its GPS signal, the aircraft will return to a predetermined location.

19. The PIC will abort the flight in the event of unpredicted obstacles or emergencies.

20. The PIC will be prohibited from beginning a flight unless (considering wind and forecast weather conditions) there is enough available power or fuel for the aircraft to conduct the intended operation and to operate after that for at least five minutes or with the reserve power or fuel recommended by the manufacturer if greater.

21. All operations shall be conducted in accordance with an ATO-issued COA if the blanket COA does not cover the intended operation.

22. All aircraft operated will be identified by serial number, registered in accordance with 14 CFR part 47, and have identification (N−Number) markings in accordance with 14 CFR part 45, Subpart C. Markings will be as large as practicable.

23. Documents used by Airadyme to ensure the safe operation and flight of the UAS and any documents required under 14 CFR §§ 91.9 and 91.203 will be available to the PIC at the Ground Control Station of the UAS any time the aircraft is operating.

24. The aircraft will remain clear and give way to all manned aviation operations and activities at all times.

### 25. The UAS may be operated by the PIC from a moving device or vehicle; however, specific

requests will be made via subsequent COA.

26. All flight operations will be conducted at least 500 feet from all nonparticipating persons, vessels, vehicles, and structures unless: a. Barriers or structures are present that sufficiently protect nonparticipating persons from the aircraft or debris in the event of an accident; or b. The owner/controller/operator of any vessels, vehicles or structures has granted permission for operating closer to those objects and the PIC has made an assessment of the risk of operating closer to those objects and determined that it does not present an undue hazard.

27. The PIC, VO, operator trainees or essential persons will not be considered nonparticipating persons under this exemption.

28. All operations conducted over private or controlled-access property will be conducted with the permission from the property owner/controller or authorized representative. Permission from property owner/controller or authorized representative will be obtained for each flight to

be conducted.

29. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of the operational area as defined by the applicable COA will be reported to the FAA's UAS Integration Office (AFS −80) within 24 hours. Accidents must be reported to the Na Ɵ onal Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

.

DESCRIPTION OF SPECIFIC REGULATIONS

14 CFR Part 21, Subpart H: Airworthiness certificates

Subpart H, establishes the procedural requirements for the issuance of airworthiness certificates as required by FAR §91.203(a)(1). Given the size and limited operating area associated with the aircraft to be utilized by Airadyme, an exemption from Part 21 Subpart H meets the requirements of an equivalent level of safety under Part 11 and Section 333 of the Reform Act. The Federal Aviation Act (49 USC §44701(f)) and Section 333 of the Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration of the size, weight, speed, operational capability and proximity to airports and populated areas of the particular UAS. In all cases, an analysis of these criteria demonstrates that the UAS operated without an airworthiness certificate, in the restricted environment and under the conditions proposed, will be at least as safe, or safer, than a conventional aircraft operating with an airworthiness certificate without the restrictions and conditions proposed.

### 14 CFR 45.23(b): Marking of the aircraft

This regulation requires that certain experimental, provisionally certified aircraft, or lightsport category aircraft to be marked with letters between 2 inches and 6 inches high “limited”, “restricted,” “light-sport,” “experimental,” or “provisional,” near each entrance to a cabin, cockpit or pilot station. Even though the UAS will have no airworthiness certificate, an exemption may be needed as the UAS will have no entrance to the cabin, cockpit or pilot station on which the word “Experimental” can be placed. Given the size of the UAS, 2 inch lettering may be impossible. Airadyme will mark the UAS as practicable.

14 CFR 61.113(a) & (b): Private pilot privileges and limitations: Pilot in command

Sections 61.113(a) and (b) limit private pilots to non-commercial operations. Because the UAS will not carry a pilot or passengers, the proposed operations can achieve the equivalent level of safety of current operations by requiring the pilot operating the aircraft to have completed a UAS flight-training course. Unlike a conventional aircraft that carries the pilot and passengers, the UAS is remotely controlled. The area of operation is controlled and restricted, and all flights are planned and coordinated in advance. The risks associated with the operation of the UAS are so diminished from the level of risk associated with commercial operations contemplated by Part 61 when drafted, that allowing operations of the UAS as requested exceeds the present level of safety achieved by 14 CFR 61.113(a) and (b).

14 CFR 91.7(a): Civil aircraft airworthiness

The regulation requires that no person may operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for the aircraft Airadyme contemplates operating, should this exemption be granted, no FAA regulatory standard will exist for determining airworthiness. Given the size of the aircraft and the operational restrictions put on the aircraft, an equivalent level of safety will be provided.

14 CFR 91.9(b)(2): Civil aircraft flight manual, marking and placard requirements

The UAS, given its size and configuration has no ability or place to carry such a flight manual on the aircraft, not only because there is no pilot on board, but because there is no room or capacity to carry such an item on the aircraft. The equivalent level of safety will be maintained by keeping the Operating Manuals at the ground control point where the pilot flying the UAS will have immediate access to it.

14 CFR 91.103: Preflight action

This regulation requires each pilot in command take certain actions before flight to ensure the safety of flight. An exemption is needed from this requirement, as the pilot will take separate preflight actions, including checking for weather conditions, checking flight battery or fuel

### requirements, checking takeoff and landing distances, and all other actions in the Operating

Manual and safety checklists. These actions will provide an equivalent level of safety.

14 CFR 91.109: Flight instruction

Section 91.103 provides that no person may operate a civil aircraft (except a manned free balloon) that is being used for flight instruction unless that aircraft has fully functioning dual controls. By design, UAS do not have fully functional dual controls. Flight control is accomplished through the use of a control box that communicates with the aircraft via radio communications. The equivalent level of safety is provided by the fact that neither a pilot nor passengers will be carried in the aircraft, the ability to control the UAS via radio signals from the controller and by the size and speed of the aircraft.

14 CFR 91.119: Minimum safe altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. The UAS will never operate at altitude higher than 400 AGL and all operations will occur during daylight hours under Visual Meteorological Conditions (VMC) only. The equivalent level of safety will be achieved given the size, weight and speed of the UAS as well as the location where it is operated. No flight will be taken without the 9 permission of the property owner. Because advance notice to the property owner and any onsite personnel, as well as the precautions outlined below, all affected individuals will be aware of the planned flight operations. Flight operations will be conducted at least 500 feet from all non-participating persons (persons other than the pilot in command (PIC) or visual observer (VO)), vessels, vehicles and structures, unless operations do not present an undue hazard. The UAS will remain within visual line of sight of the PIC or VO. Flight operations will be conducted at least 5 miles from an airport. The PIC or VO will provide notification to the local Flight Standards District Office and airport controller of all operations within 5 miles of an airport. The FAA will have advance notice of all operations through the filing of notices-to-airmen. Compared to flight operations with aircraft or rotorcraft weighing far more than the UAS proposed herein, any risk associated with our operations is far less than those presently presented with helicopters and other conventional aircraft operating at or below 500 feet AGL. In addition, the low-altitude operations of the UAS will ensure separation between these UAS operations and the operations of conventional aircraft that must comply with Section 91.119.

14 CFR 91.121: Altimeter Settings

This regulation requires each person operating the aircraft to maintain cruising altitude by reference to an altimeter that is set “...to the elevation of the departure airport or an appropriate altimeter setting available before departure.” As the UAS may not have a barometric altimeter, but instead a GPS altitude read out, an exemption may be needed. An equivalent level of safety will be achieved by the PIC confirming the altitude of the launch site shown on the GPS altitude indicator before flight.

### 14 CFR 91.151(a): Fuel requirements for flight in VFR conditions

Section 91.151(a) outlines fuel requirements for beginning a flight in VFR conditions. Relief from Section 91.151(a)(1) is requested to the extent required to allow flights of a variety of UAS during daylight hours in visual flight rules (VFR) conditions to continue until 90 percent of remaining battery power or fuel reserves remain. Airadyme seeks the requested relief because without an exemption from Section 91.151(a)(1), the flight time duration of the selected aircraft will be reduced and severely constrain the practicality of any aerial acquisition of data that Airadyme proposes to conduct pursuant to this Petition. The technical specifications of the proposed UAS, their Operations Manuals, and Airadyme’s proposed operating limitations, ensure that Airadyme will safely operate the 10 selected aircraft during daylight hours in VFR conditions until 90 percent of remaining battery power or fuel reserves remain.

14 CFR 91.203(a) & (b): Carrying civil aircraft certification and registration

The UAS has no cabin, cockpit or pilot station and is operated without an onboard pilot. Therefore, there is no ability or place to carry certification and registration documents or to display them on the UAS. An equivalent level of safety will be achieved by keeping these documents at the ground control point where the pilot flying the UAS will have immediate access to them, to the extent they are applicable to the UAS.

14 CFR 91.405(a); 407(a)(1); 409(a)(2); 417(a) & (b): Maintenance inspections

These regulations require that an aircraft operator or owner “shall have that aircraft inspected as prescribed in subpart E of this part and shall between required inspections, except as provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and others shall inspect or maintain the aircraft in compliance with Part 43. Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to Airadyme. Maintenance will be accomplished pursuant to the User Guide or Operating Manual. An equivalent level of safety will be achieved because these UASs are limited in size and will carry a small payload and operate only in restricted areas for limited periods of time. If mechanical issues arise, the UAS can land immediately and will be operating from no higher than 400 feet AGL. The PIC will ensure that the UAS is in working order prior to initiating flight, perform required maintenance and keep a log of any maintenance performed. Moreover, the PIC is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivalent level of safety.

PUBLIC INTEREST

Approval of exemptions allowing commercial operations of UASs for aerial acquisition of data enhances safety while reducing risk. Manned aircraft in certain application such as pipeline monitoring create a greater risk because the aircraft are much larger and carry an onboard human pilot. In contrast, a UAS weighing 55 pounds or less will carry no passengers or crew and, therefore, will not expose them to the risks associated with manned aircraft flights. In addition,

### additional streams of aerial data will allow large commercial entities to make decisions about

how to best deploy ground resources and ensure the safety and cost-effectiveness of their operations.

EQUIVALENT LEVEL OF SAFETY

Airadyme proposes that the exemption requested herein apply to civil aircraft that have the characteristics and that operate within the limitations listed herein. These limitations provide for at least an equivalent or even higher level of safety to operations under the current and proposed regulatory structure.

PRIVACY

All flights will occur over private or controlled access property with the property owner’s prior consent and knowledge. Images or video taken of individuals will have consented to being filmed or otherwise they will be made anonymous.

NATIONAL SECURITY

Given the small size of the UAS involved and the restricted environment within which they will operate, our petition presents no national security issue.

FEDERAL REGISTER SUMMARY

Petitioner: Airadyme, Part 21 and §§ 45.23(b), 61.113(a) and (b), 91.7(a), 91.9(b)(2), 91.103, 91.109, 91.119, 91.121, 91.151(a), 91.203(a) and (b), 91.405(a), 407(a)(1), 409(a)(2), 417(a) and (b) of Title 14, Code of the Federal Regulations (14 CFR).

Description of Relief Sought: Airadyme is seeking an exemption to conduct commercial acquisition of aerial data using unmanned aircraft systems.

Based upon the foregoing, Airadyme requests that the FAA grant it the necessary exemptions under Section 333 of the FAA Reform Act as requested herein to allow for commercial operations of UAS within the United States.

Sincerely,

Richard Gowen UAV Administrator Airadyme

# Appendix 1 List of UAV’s to be flown:

1 2AgEagle 2 3D Robotics Aero -M 3 3D Robotics Iris 4 3D Robotics Iris+ 5 3D Robotics X8 6 3DRobotics Fixed Wing 7 3DRobotics Multirotor 8 3DRobotics Quadrotor 9 3DR Solo 10 3DR Spektre 11 3DRobotics Spektre Industrial Multi -Rotor Aerial Vehicle 12 3D Robotics Solo 13 3DRobotics X8+ 14 3D Robotics X8 - M 15 3D Robotics Y6 16 16 Aerial Mob Heavy Lifter 17 17 Aerial Mob Light Lifter 18 18 Aerial Remote Mineral Detection System (ARMDS) 19 19 Aerialtronics Zenith with intergrated Airware system 20 20 Aerialtronics Altura Zenith ATX8 21 21 Aerigon 22 22 Aerobo 23 23 AeroCine Kopterworx Hammer X12 24 24 Aeromao AeroMapper 300 25 25 Aeromao Talon 26 26 Aeromao Aeromapper 300 27 27 Aeromao Aeromapper EV - 2 28 28 AeroVironment Shrike 29 29 AeroVironment Puma 30 30 Aeronavics X4 Titanium 31 31 Aeryon Sky Ranger 32 32 Aervonics Sky Jib frame with a DJI A2 flight system 33 33 Aero - M 34 34 Aeryon Scout 35 35 Aeryon SkyRanger 36 36 AgEagle 37 37 AgEagle Robotic 38 38 AgScout 39 39 AgScout Mini 40 40 Agribotix Hornet Drone 41 41 Agribotix Enduro Quad 42 42 AgriView VK Ranger EX 11 43 43 Aibot 44 44 Aibotix X -6 45 45 Air Rover AR -3000 46 46 AirCover QR -425s 47 47 AirRobot AR 180 4848 AirRobot AR 100 49

49 AirRobot AR200 50 50 Air - X 51 51 Align M690 52 52 Altavian Nova 53 53 Altavian Nova F6500 54 54 Altavian Nova R8400 55 55 Altus X - 4 56 56 Altus X - 8 57 57 American Drones, LLC Eagle 58 58 Apprentice 59 59 Arch Aerial OCTO multi -rotor UAS 60 60 Arris hexacoper 61 61 AR -960 Hex Rotor 62 62 AR -540 Quad Rotor 63 63 ARF -MikroKopter OktoXL 64 64 ARF -MikroKopter OktoXL + 65 65 ArrowLite 66 66 AscTec Falcon 67 67 AscTec Falcon 8 68 68 Astraeus Aerial Cinema System V 69 3CS 69 70 Atlantic RC Aircraft LC04 70 71 Auburn Trimble UX5 71 72 Auburn War Eagle 72 73 Auburn EasyStar 73 74 Auburn 74 75 AV44 75 76 Bixler 3DR Plane 76 77 Blade 350QX 77 78 Bixler 2 78 79 Boomerang Carbon Fiber Frame (The Identified System) 79 80 Bormatec Maja UAV 80 81 BOSH Technologies Super Swiper 81 82 Bumblebee - S 82 83 C -Astral Bramor gEO 83 84 CarbonCore Octocopter 1000 84 85 Carbon Core Cortex Quadcopter 85 86 CCO w/Wkm M 86 87 Chameleon Pro 12 87 88 CinesStar 88 89 Cinestar 6 89 90 Cinestar X8 90 91 Cinestar 8 91 92 Cinestar 8 HL 92 93 Cinestar 8 Okto XL 93 94 Coaxial Quad Multirotor VAO1 -V1 94 95 Coaxial Quad Multirotor VAO2 -V2 95 96 CopelandRED LLC Delta Wing Aircraft 96 97 CyberQuad Maxi 9798 DJI Flame Wheel F450 98

99 DJI Flame Wheel F550 99 100 DAx8 100 101 DJI Inspire 101 102 DJI Inspire 1 102 103 DJI Inspire 2 103 104 DJI M P330z 104 105 DJI Phantom 105 106 DJI Phantom 1 106 107 DJI Phantom 2 107 108 DJI Phantom 2+ 108 109 DJI Phantom 2 Vision 109 110 DJI Phantom 2 Vision+ 110 111 DJI Phantom Vision + 111 112 DJI Phantom 3 112 113 DJI Phantom FC40 113 114 DJI Spreading Wings S900 114 115 DJI Spreading Wings S1000 115 116 DJI Spreading Wings S1000+ 116 117 DJI S800 117 118 DJI S800 EVO 118 119 DJI T600 119 120 Draganflyer Guardian 120 121 Draganflyer X4ES 121 122 Draganflyer X4P 122 123 Draganflyer X6 123 124 DT -18 124 125 DYS D800 -X8 125 126 Eagle VTOL 126 127 Eagle V2 127 128 E -Flite Apprentice 128 129 Event 38 E384 129 130 F -450 130 131 Falcon VTOL 13 131 132 Fire Fly 6 132 133 First Aerial Responder UAV 133 134 Flame Wheel G4 7 135 8 Skycrane 134 136 Flying -Cam 3 137 0 SARAH 135 138 Foxtech Kraken 130 V2 136 139 FreeFly Systems ALTA RTF 137 140 FreeFly Systems Octocopter Airframe (Legacy) 138 141 G4 139 142 G4 models 140 143 GeoStar 141 144 GerMAP G220 142 145 GerMAP G180 143 146 goFarm GF -1 144 147 Gryphon Dynamics X8 145148 GT80X 146

149 Harris 18 HL 147 150 HEFF 148 151 Helicopters West DJI Inspire 149 152 Helicopters West SkyJib 8 150 153 Helios 960 151 154 Hawkeye Mk -III 152 155 HexaCrafter HC -1100 85 156 157 HexaCrafter HO -1250 154 158 HH Blade 350QX2 AP 155 159 Hobbyking “Bixler” Fixed Wing Trainer 156 160 HoneyComb AgDrone 157 161 Horizon Hobby Blade 350 Qx2 quadcopter 158 162 Hoverfly LiveSky, BigSky 60 and H -Frame 159 163 Hubsan X4 micro drone 160 164 HVP 14301 Multi Rotor 161 165 Identified System 162 166 IMT Global xFold Cinema 163 167 Indago 164 168 InovalDrone:Inova One 165 169 InstantEye Mk - 2 166 170 InstantEye Mk -2 Gen2 167 171 Intuitive Aerial Aeragon 168 172 K130 Octocopter 169 173 KongCopter X8 170 174 Kopterworx Hammer X12 171 175 Latitude HQ -4 Hybrid Multirotor 172 176 LB700 173 177 Leading Edge Precision Vision 10 174 178 Leptron Avenger 14 175 179 Lewis Realty Associates Hexacopter 650 176 180 Liberty 1 177 181 Lockheed Martin Desert Hawk III 178 182 Lockheed Martin Indago 179 183 Matrix quad copter 180 184 MaxFligh t 181 185 MD4 -200 182 186 MD4 -1000 183 187 Mikrokopter 2 188 5 184 189 MLB Company Super Bat 185 190 MU -1H 186 191 Multirotor G4 7 192 8 Skycrane 187 193 Nighthawk 188 194 Nighthawk VTOL 189 195 OktoXL 6S12 190 196 PAG X4 191 197 Parksone Radian RTF 192198 Parrot Bebop drone 193

199 Parrot PF 725100 Bebop Drone 14MP 194 200 Parrot Skycontroller 195 201 Patriot X4 196 202 Patriot X8 197 203 Finwing Penguin V2 198 204 Birdseyeview FireFly 6 199 205 Phoenix 200 206 Phoenix VTOL 201 207 Phoenix 60 202 208 Phoenix 60LE 203 209 Pixhawk 204 210 Precision Drone Pacesetter 205 211 PrecisionHawk 206 212 PrecisionHawk Hawkeye Mk -III 207 213 PrecisionHawk Lancaster 208 214 Precision Lancaster MK3 209 215 Prioria Hex 210 216 Prioria’s Maveric 211 217 Pulse Aerospace, PA 01 Vapor 212 218 Pulse Aerospace Pulse Vapor 35 213 219 Pulse Vapor 214 220 Puma AE DDL 215 221 PV 14817 Multi Rotor 216 222 PV HL1 217 223 PV HL2 218 224 Q1 15 219 225 Quadcopter LLC MikroKopter 220 226 Quiet UAV 221 227 Qube 222 228 R/C Rotors and Aerial Media: Matrix Prof 229 Multi Rotor Frame & Octo Heavy Lift Prof 230 Multi Rotor 223 231 Frame Ronin Edition Microdrones:MD4-1000 224 232 RCTimer Hexacopter 225 233 RDASS 226 234 REHawk 500 227 235 REHawk 680 228 236 RF-70 229 237 Riegl RiCopter 230 238 RITEWING Z3 Spade 47” 231 239 Ritewing Drake 60” 232 240 RITEWING Z3 Spade 70” 233 241 RITEWING Z4 Spade 52” 234 242 RMAX 235 243 Roboflight 236 244 Rotomotion SR-15 237 245 RV Jet 238 246 Scout X4 239 247 SD02 240248 Seahawk 1

249 2 241 250 SelectTech Geospacial’s EH-4 242 251 SenseFly eBee 243 252 SenseFly eBee RTK 244 253 SenseFly eXom 245 254 Sensurion Magpie MP-1 246 255 Service-Drone Recon One 247 256 Service-Drone Blackbird 248 257 SH 900 249 258 ShadowHawk 250 259 Shrike 251 260 Sirius 252 261 SkyCatch 253 262 SkyJib 8 v 263 2 Heavy Lifter 254 264 SkyPhilly MI 255 265 Skywalker Aero 256 266 Skywalker Flying Wing X8 257 267 SnapRoll Media SUAS 258 268 Solutions Phoenix 30 259 269 SteadiDrone 260 270 Steadidrone Quad 261 271 Steadydrone QU4D 16 262 272 Steadidrone Mavik 263 273 SuperX/P2 Multirotor 264 274 Swift Radioplanes Lynx 265 275 Tali 500 266 276 Talon 120LE 267 277 Tarot FY690S Hexacopter 268 278 Tarot quadcopter 269 279 Tarot 680pro 270 280 Tarot 690 271 281 Tarot 900 272 282 Tarot 960 273 283 Tarot T -15 274 284 Tarot T15 C/F Folding Octocopter 275 285 Tarot T18 UAV 276 286 Tarot T690 277 287 Tarot T810 278 288 Tarot T960 279 289 Tarsier Systems MoAC 280 290 Tayzu Robotics Titan X8 281 291 TBS Discovery Pro 282 292 Team Black Sheep Discovery Pro Tarot T15 283 293 T -Rex 700E F3C 284 294 TREX 800E DFC PRO 285 295 Trimble UX5 286 296 Trimble UX5 hp 287 297 Trimble ZX5 288298 Turningy Talon 500 289

299 TUP X8 -800 290 300 Turbo Ace CINEWING 6 291 301 TurboAce Matrix -G quadcopter 292 302 Turbo Ace matrix - E 293 303 Turbo Ace MATRIX - 1 294 304 UAV Solutions Phoenix 60 295 305 Universeye Penguin 296 306 Unmanned Flying Rolling Orb “UFRO” 297 307 US2 GreenHawk 298 308 UtiliCopter ITX8 299 309 VA03 -v1 300 310 VA04 -v1 301 311 VA07 -v1 302 312 Viking UAS Multicopter (VTOL) 303 313 Viking UAS FF -X4/X8 304 314 VK -Patriot X4/X8 305 315 Viking UAS Patriot X4/X8 Multirotor 17 306 316 Viking UAS X6 Model 800 307 317 Viking UAS Viking ONE 308 318 VK-450 309 319 Viking Unmanned Aerial Systems, LLC AgriView VK Ranger EX 310 320 Viking VK-FF-X4 311 321 VK- Ranger EX- SAR Fixed Wing UAS 312 322 Volantex Raptor Tarot T-18 313 323 Volt Aerial Robotics Octane 314 324 Vulcan frame controlled by a DJI A2 flight controller 315 325 Vulcan Mantis 316 326 Vulcan Octocopter 317 327 Vulcan Raven 318 328 Vulcan UAV 319 329 Walkera TALI H500 320 330 Walkera Scout X4 321 331 Wookong DJI 5800 322 332 xCel Drones XD550CDR 323 333 XFold Rig with four configurations: Quadcopter, Hexcopter, Octocopter and x12 Copter 324 334 X8-M 335 AlignM490 336 ExponentGS1200 337 H20Hex 338 FOXTECHD130 339 FOXTECHK130 340 TarotT910 341 TarotTX4 342 YuneecTornado H920 343 YuneecTyphoon Q500 344 YuneecTyphoon G 345 Gryphon DynamicsDodeca 346 Gryphon DynamicsOcto 347 Gryphon DynamicsHex348 Gryphon DynamicsQuad

349 Y6Y6 350 X8X8 351 Spider 6Spider 6 352 Skywaker1680 353 Skywaker1880 354 Skywaker1900 355 SkywakerCF 356 SkywakerX7 357 X-UAVThe One 358 X-UAVMFD 359 X-UAVMini Talon 360 X-UAVLarge Talon 361 X-UAVSkyhunter 362 RV JETRV ONE