**Electronic Submission**

March 9, 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, Sky High Imaging, LLC (herein referred to as SHI) hereb y 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. Commercial operation of an UAS, as described herein, which are equipped with camera(s) and s ensors, would provide professional services in the following areas:
1. Aerial photograph y and/or video for public and/or private use including real estate, architecture, land survey

ing, engineering and other related professional activities.
2. Aerial video and /or photography for public and/or private use including television, public events, cinematograph y and newsgathering.
3. Aerial inspection/photograph y of residential/commercial structures under contract with owners or local government authority

. 4. Aerial inspection/photography of residential/commercial utility infrastructure including but not limited to electrical power lines, wind turbines and cell towers.
5. Aerial video/photography or providing live video feed to assist with search and rescue operations i n cases of an emergency or natural disaster onl y when the local authorities or government has requested it by contract or donation.
6. Training to persons individually or belonging to both private and/or public organizations to increase awareness and improve safet y for current and future UAS operations within the NAS. 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 exemp tion would thereby enhance safety and fulfill the Secretary of Transportation’sresponsibilities to “...establish requirements for the safe operation of such aircraft s ys tems in the

national airspace s ys tem.” Section 333(c) Reform Act.
The name and addres s of the applicant is: Robert Moore d/b/a Sky

High Imaging, LLC Robert Moore Owner/Operator 9668 L ower Valley

Pike Medway , OH 45341 Tel: 937

- 543

- 8374 Email: Sky

HighImagingLLC@gmail.com 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 airc raft 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 an y sections §44702

- 44716 of this title if the Administrator finds th e 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 sy stem without crea ting a hazard to the user, the public, or a threat to national securit y. 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 op erator;Whether the UAS operates outside of highl y populated areas and away from close proximity to airports. Reform Act 333(a). If the Secretary determines that a UAS “may operate safel y in the national airspace sy stem, the Secretary shall establish requ irements for the safe operation of such aircraft in the national airspace sy stem.” Id. 333(c).
**BACKGROUND ON SHI**  The applicant, Robert Moore , holds a private pilot license with an instrument rating and is currentl y completing his commercial requirements. He has over 150 hours of fixed wing time. Mr. Moore has owned and operated sUAS platforms for the past three ye ars and has operated them for hobb y without incident during this period. Robert has an in

- depth understanding of the capabilities and safet y con cerns involved in using this technology as an asset to the community

. Satisfaction of criteria provided in Section 333 of the Reform Act of 2012 provide more than adequate justification for the grant of the requested exemptions allowing the commercial ope ration of the applicant’s UAS.
**UAS AND OPERATIONAL DESCRIPTION** 
SHI seeks to commercially operate a variet y of UAS weighing less than 55 pounds including pay load in the United States for the purpose of acquiring aerial data. The Appendix attached to this exemption petition lists the aircraft that SHI contemplates operatin g. As the operator of these aircraft, SHI is committed to the following conditions and limitations on its operations. SHI 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 b y 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.
3. The ai rcraft 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.
4. The aircraft will be opera ted at an altitude of no more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL.
5. The aircraft will be operated within visual line of sight (VLOS) of the Pilot in Command (PI C) at all times. This requires the PI C to be able to u se human vision unaided by any device other than corrective lenses, as specified on the PIC’s U.S. driver’s license.6. All operations will utilize a visual observer (VO). The aircraft will be operated within the

visual line of sight (VLOS) of the PI C and VO at all times.
7. 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.
8. 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.
9. SH I is responsible for maintaining and inspecting the UAS to ensure that it is in a condition for safe operation.
10. Prior to each flight, the PIC will conduct a pre

- flight inspection and determine the UAS is in a condition for safe flight.
11. SHI 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 PI C w ill hold a Private Pilot L icense, UAS flight training certificate, in some cases training directl y from the aircraft manufacturer, and a valid U.S. driver’s license issued b y a state, the District of Columbia, Puerto Rico, a territory , a possession, or the Federal government.
14. SHI will not permit any PI C to operate unless the PI C demonstrates the ability to safel y 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. PI C qualification flight hours and currency will be logged in a manner consistent with 14 CFR § 61.51(b). SHI will operate flights for the purposes of training SHI PI Cs and V Os (training, proficiency , and experience

- building) and determining the PI C’s ability to safel y 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 s ym bol 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 PI C.18. If the UAS loses communications or loses its GPS signal, the aircraft will return to a pre

determined location.
19. The PI C will abort the flight in the event of unpredicted obstacles or emergencies.
20. The PI C 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 fiv e minutes or with the reserve power or fuel recommended b y 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 identif ied b y 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 b y SHI 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 PI C 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 oper ations 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 person s, 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 an y vessels, vehicles or structures has granted permission for operating closer to those objects and the PI C 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 PI C, 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 propert y owner/controller or authorized representative. Permission from propert y owner/controller or authorized representative will be obtained for each flight to be conducted. 29. Any incident, accident, or flig ht operation that transgresses the lateral or verticalboundaries of the operational area as defined b y t he applicable COA will be

reported to the FAA's UAS I ntegration Office (AFS −80) within 24 hours. Accidents must be reported to the National Transpor tation Safet y 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 b y FAR §91.203(a)(1). Given the size and limited operating area associated with the aircraft to be utilized by SHI , an exemption from Part 21 Subpart H meets the requirements of an equivalent level of saf

et y 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 si ze, weight, speed, operational capability and proximity

to airports and populated areas of the particular UAS. In all cases, an anal ys is of these criteria demonstrates that the UAS operated without an airworthiness certificate, in the restricted environmen t 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 r equires that certain experimental, provisionally certified aircraft, or light

- sport 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. SHI 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 safet y of current operations by requiring the pilot operating the aircraft to have completed a UAS flight

- training course. Unlike a convention al 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 diminis hed 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 safet y achieved b y 14 CFR 61.113(a) and (b). 14 CFR 91.7(a): Civil aircraf t airworthinessThe 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 SHI 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 provi ded. 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 becau se there is no room or capacity to carry such an item on the aircraft. The equivalent level of safet y will be maintained by keeping the Operating Manuals at the ground control point where the pilot fl yi ng the UAS will have immediate access to it.
14 CFR 9 1.103: Preflight action This regulation requires each pilot in command take certain actions before flight to ensure the safet y of flight. An exemption is needed from this requirement, as the pilot will take separate preflight actions, including checking f or weather conditions, checking flight battery or fuel requirements, checking takeoff and landing distances, and all other actions in the Operating Manual and safet y checklists. These actions will provide an equivalent level of safet y. 14 CFR 91.109: Flig ht 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 full y functioning dual controls. By

design, UAS do not have fully function al 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 safet y is provided b y the fact that neither a pilot nor passengers will be carried in th e aircraft, the ability to control the UAS via radio signals from the controller and b y 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 neve r operate at altitude higher than 400 AGL and all operations will occur during day light hours under Visual Meteorological Conditions (VMC) only

. The equivalent level of safet y 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 permission of the property owner. Because advance notice to the propert y owner and an y 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 (PI C) or visual observer (VO)), vessels, vehicles and structures, unless operations do not p resent an undue hazard. The UAS will remain within visual line of sight of the PI C 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 airpor t 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 here in, an y risk associated with our operations is far less than those presentl y 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 t hese 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 b y 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 safet y will be achieved b y 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 beginni ng a flight in VFR conditions. Relief from Section 91.151(a)(1) is requested to the extent required to allow flights of a variet y of UAS during day light hours in visual flight rules (VFR) conditions to continue until 90 percent of remaining battery

power o r fuel reserves remain. SHI 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 severel y constrain the practicality of any aerial acquisition of data that SHI proposes to conduct pursuant to this Petition. The technical specifications of the proposed UAS, their Operations Manuals, and SHI ’s proposed operating limitations, ensure that SHI will safel y operate the selected aircraft during day light hours in VFR conditions until 90 percent of remaining battery power or fuel reserves remain. 14 CFR 91.203(a) & (b): Carry ing civil aircraft certification and registration The UAS has no cabin, cockpit or pilot station and is operated without an onboard pilot. There fore, there is no ability or place to carry

certification and registration documents or to display them on the UAS. An equivalent level of safet y will be achieved b y keeping these documents at the ground control point where the pilot fly ing the UAS will ha ve 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 p rescribed 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 appl y only to aircraft with an airworthiness certificate, these sections will not apply to SHI . Maintenance will be accomplished pursuant to the User Guide or Operating Manual. An equivalent l evel of safet y will be achieved because these UASs are limited in size and will carry a small pay load and operate onl y in restricted areas for limited periods of time. If mechanical issues arise, the UAS can land immediately and will be operating from no h igher 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 an y maintenance performed. Moreover, the PI C is the person most familiar with the aircraft and best sui ted to maintain the aircraft in an airworth y condition to provide the equivalent level of safet y. **PUBLIC INTEREST** Approval of exemptions allowing commercial operations of UASs for aerial acquisition of data enhances safet y 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. I n 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 safet y and cost

- effectiveness of their operations. **EQUIVALENT LEVEL OF SAFETY**
SHI 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 equiva lent 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 anony

mous. **NATIONAL SECURITY** Given the small size of the UAS involved and the restricted environment within which they will operate, our petition presents no national secur ity issue.**FEDERAL REGISTER SUMMARY**

Docket No.: No. FAA

- 2015

- Petitioner: SHI 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: SHI is seeking an exemption to conduct commercial acquisition of aerial data using unmanned aircraft s ys tems. Based upon the foregoing, SHI 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.
Sincerel y,

Robert Moore Owner

- Operator Sky High Imaging, LLC 9668 L ower Valley

Pike Medway , OH 45341 **Appendix 1**
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. Aerial Mob Heav y Li fter 17. Aerial Mob Light Li fter 18. Aerial Remote Mineral Detection Sy stem (ARMDS) 19. Aerialtronics Zenith with intergrated Airware sy stem20. Aerialtronics Altura Zenith ATX8

21. Aerigon 22. Aerobo 23. AeroCine Kopterworx Hammer X12 24. Aeromao AeroMapper 300 25. Aeromao Talon 26. Aeromao Aeromapper 300 27. Aeromao Aeromapper EV

- 2 28. AeroVironment Shrike 29. AeroVironment Puma 30. Aeronavics X4 Titanium 31. Aery on Sky Ranger 32. Aervonics Sk y J ib frame with a DJ I A2 flight sy stem 33. Aero

- M 34. Aery on Scout 35. Aery on Sky Ranger 36. AgEagle 37. AgEagle Robotic 38. AgScout 39. AgScout Mini 40. Agribotix Hornet Drone 41. Agribotix Enduro Quad 42. AgriView VK Ranger EX Aibot 43. Aibotix X

- 6 44. Air Rover AR

- 3000 45. AirCover QR

- 425s 46. AirRobot AR 180 47. AirRobot AR 100 48. AirRobot AR200 49. Air

- X 50. Align M690 51. Altavian Nova 52. Altavian Nova F6500 53. Altavian Nova R8400 54. Altus X

- 4 55. Altus X

- 8 56. American Drones, LLC Eagle 57. Apprentice 58. Arch Aerial OCTO multi

- rotor UAS 59. Arris hexacoper 60. AR

- 960 Hex Rotor 61. AR

- 540 Quad Rotor 62. ARF

- MikroKopter OktoXL 63. ARF

- MikroKopter OktoXL + 64. ArrowLite 65. AscTec Falcon66. AscTec Falcon 8

67. Astraeus Aerial Cinema Sy stem V.3CS 68. Atlantic RC Aircraft LC04 69. Auburn Trimble UX5 70. Auburn War Eagle 71. Auburn Easy Star 72. Auburn 73. AV44 74. Bixler 3DR Plane 75. Blade 350QX 76. Bixler 2 77. Boomerang Carbon Fiber Frame (The Identified Sy stem) 78. Bormatec Maja UAV 79. BOSH Technologies Super Swiper 80. Bumblebee

- S 81. C

- Astral Bramor gEO 82. CarbonCore Octocopter 1000 83. Carbon Core Cortex Quadcopter 84. CCO w/Wkm M 85. Chameleon Pro 86. CinesStar 87. Cinestar 6 88. Cinestar X8 89. Cinestar 8 90. Cinestar 8 HL 91. Cinestar 8 Okto XL 92. Coaxial Quad Multirotor VAO1

- V1 93. Coaxial Quad Multirotor VAO2

- V2 94. CopelandRED LLC Delta Wing Aircraft 95. Cy berQuad Maxi 96. DJI Flame Wheel F450 97. DJI Flame Wheel F550 98. DAx8 99. DJI Inspire 100. DJI I nspire 1 101. DJI I nspire 2 102. DJI M P330z 103. DJI Phantom 104. DJI Phantom 1 105. DJI Phantom 2 106. DJI Phantom 2+ 107. DJI Phantom 2 Vision 108. DJI Phantom 2 Vision+ 109. DJI Phantom Vision + 110. DJI Phantom 3 111.5 DJI Phantom 4111. DJI Phantom FC40

112. DJI Spreading Wings S900 113. DJI Spreading Wings S1000 114. DJI Spreading Wings S1000+ 115. DJI S800 116. DJI S800 EVO 117. DJI T600 118. Draganfly er Guardian 119. Draganfly er X4ES 120. Draganfly er X4P 121. Draganfly er X6 123. DT

- 18 124. DYS D800

- X8 125. Eagle VTOL 126. Eagle V2 127. E

- Flite Apprentice 128. Event 38 E384 129. F

- 450 130. Falcon VTOL 131. Fire Fl y 6 132. First Aerial Responder UAV 133. Flame Wheel G4 7.8 Sky crane 134. Fly ing

- Cam 3.0 SARAH 135. Foxtech Kraken 130 V2 136. FreeFl y S ys tems ALTA RTF 137. FreeFl y S ys tems Octocopter Airframe (Legacy ) 138. G4 139. G4 models 140. GeoStar 141. GerMAP G220 142. GerMAP G180 143. goFarm GF

- 1 144. Gry phon Dy namics X8 145. GT80X 146. Harris 18 HL 147. HEFF 148. Helicopters West DJI Inspire 149. Helicopters West Sky Jib 8 150. Helios 960 151. Hawkey e Mk

- III 152. HexaCrafter HC

- 1100 85. 153. HexaCrafter HO

- 1250 154. HH Blade 350QX2 AP 155. Hobby

king “Bixler” Fixed Wing Trainer 156. Honey Comb AgDrone 157. Horizon Hobby

Blade 350 Qx2 quadcopter158. Hoverfl y LiveSk y, BigSk y 60 and H

- Frame

159. Hubsan X4 micro drone 160. HVP 14301 Multi Rotor 161. I dentified Sy stem 162. I MT Global xFold Cinema 163. I ndago 164. I novalDrone: Inova One 165. I nstantEy e Mk

- 2 166. I nstantEy e Mk

- 2 Gen2 167. I ntuitive Aerial Aeragon 168. K130 Octocopter 169. KongCopter X8 170. Kopterworx Hammer X12 171. L atitude HQ

- 4 Hy

brid Multirotor 172. LB700 173. Le ading Edge Precision Vision 10 174. L eptron Avenger 175. L ewis Realty

Associates Hexacopter 650 176. L iberty 1 177. L ockheed Martin Desert Hawk III 178. L ockheed Martin Indago 179. Matrix quad copter 180. MaxFlight 181. MD4

- 200 182. MD4

- 1000 183. Mikrokopter 2.5 184. MLB Compan y Super Bat 185. MU

- 1H 186. Multirotor G4 7.8 Sky crane 187. Nighthawk 188. Nighthawk VTOL 189. OktoXL 6S12 190. PAG X4 191. Parksone Radian RTF 192. Parrot Bebop drone 193. Parrot PF 725100 Bebop Drone 14MP 194. Parrot Sky controller 195. Patriot X4 196. Patriot X8 197. Finwing Penguin V2 198. Birdsey eview FireFly 6 199. Phoenix 200. Phoenix VTOL 201. Phoenix 60 202. Phoenix 60L E 203. Pixhawk204. Precision Drone Pacesetter

205. PrecisionHawk 206. PrecisionHawk Hawkey e Mk

- III 207. PrecisionHawk Lancaster 208. Precision Lancaster MK3 209. Prioria Hex 210. Prioria’s Maveric 211. Pulse Aerospace, PA 01 Vapor 212. Pulse Aerospace Pulse Vapor 35 213. Pulse Vapor 214. Puma AE DDL 215. PV 14817 Multi Rotor 216. PV HL 1 217. PV HL 2 218. Q1 219. Quadcopter LL C MikroKopter 220. Quiet UAV 221. Qube 222. R/C Rotors and Aerial Media: Matrix Prof. Multi Rotor Frame & Octo Heav y Lift Prof. Multi Rotor 223. Frame Ronin Edition Microdrones:MD4

- 1000 224. RCTimer Hexacopter 225. RDASS 226. REHawk 500 227. REHawk 680 228. RF

- 7 0 229. Riegl RiCopter 230. RI TEWING Z3 Spade 47” 231. Ritewing Drake 60” 232. RI TEWING Z3 Spade 70” 233. RI TEWING Z4 Spade 52” 234. RMAX 235. Roboflight 236. Rotomotion SR

- 15 237. RV Jet 238. Scout X4 239. SD02 240. Seahawk 1.2 241. SelectTech Geospacial’s EH

- 4 242. SenseFl y eBee 243. SenseFl y eBee RTK 244. SenseFl y eXom 245. Sensurion Magpie MP

- 1 246. Service

- Drone Recon One 247. Service

- Drone Blackbird 248. SH900249. ShadowHawk

250. Shrike 251. Sirius 252. Sky Catch 253. Sky Jib 8 v.2 Heavy Li fter 254. Sky Phill y MI 255. Sky walker Aero 256. Sky walker Fl yi ng Wing X8 257. SnapRoll Media SUAS 258. Solutions Phoenix 30 259. SteadiDrone 260. Steadidrone Quad 261. Steady drone QU4D 262. Steadidrone Mavik 263. SuperX/P2 Multirotor 264. Swift Radioplanes Lynx 265. Tali 500 266. Talon 120LE 267. Tarot FY690S Hexacopter 268. Tarot quadcopter 269. Tarot 680pro 270. Tarot 690 271. Tarot 900 272. Tarot 960 273. Tarot T

- 15 274. Tarot T15 C/F Folding Octocopter 275. Tarot T18 UAV 276. Tarot T690 277. Tarot T810 278. Tarot T960 279. Tarsier S ys tems MoAC 280. Tay zu Robotics Titan X8 281. TBS Discovery Pro 282. Team Black Sheep Discovery Pro Tarot T15 283. T

- Rex 700E F3C 284. TREX 800E DFC PRO 285. Trimble UX5 286. Trimble UX5 hp 287. Trimble ZX5 288. Turningy

Talon 500 289. TUPX8

- 800 290. Turbo Ace CINE WI NG 6 291. TurboAce Matrix

- G quadcopter 292. Turbo Ace matrix

- E 293. Turbo Ace MATRIX

- 1 294. UAV Solutions Phoenix 60295. Universey e Penguin

296. Unmanned Fl yi ng Rolling Orb “UFRO” 297. US2 GreenHawk 298. UtiliCopter IT X8 299. VA03

- V1 300. VA04

- v1 301. VA07

- v1 302. Viking UAS Multicopter (VTOL) 303. Viking UAS FF

- X4/X8 304. VK

- Patriot X4/X8 305. Viking UAS Patriot X4/X8 Multirotor 306. Viking UAS X6 Model 800 307. Viking UAS Viking ONE 308. VK

- 450 309. Viking Unmanned Aerial S ys tems, LLC AgriView VK Ranger EX 310. Viking VK

- FF

- X4 311. VK

- Ranger EX

- SAR Fixed Wing UAS 312. Volantex Raptor Tarot T

- 18 313. Volt Aerial Robotics Octane 314. Vulcan frame controlled by a DJI A2 flight controller 315. Vulcan Mantis 316. Vulcan Octocopter 317. Vulcan Raven 318. Vulcan UAV 319. Walkera TALI H500 320. Walkera Scout X4 321. Wookong DJ I 5800 322. xCel Drones XD550CDR 323. XFold Rig with four configurations: Quadcopt er, Hexcopter, Octocopter and x12 Copter 324. X8

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