Electronic Submission

October 26, 2015

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 (“FMRA”) 

and 14 CFR Part 11, Shaud G. Tavakoli (“Petitioner”) hereby applies for an exemption 

from the listed Federal Aviation Regulations (“FARs”) to allow commercial operation of

small unmanned aircraft systems (“UAS”) for the acquisition of aerial data and closed set 

motion picture and filming within and under the conditions outlined herein or as may be 

established by the Federal Aviation Administration (“FAA”).

As detailed in this petition and the attached Appendix, the requested exemption would 

permit the operation of UAS platforms previously approved by the FAA for commercial 

operation in the United States. Approval of this exemption would 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.” FMRA 

§ 333(c).

The name and address of the applicant is: 

Shaud G. Tavakoli

29255 Nottingham Ct.

Westlake, Ohio 44145

Email: shaud.tavakoli@gmail.com
Petition of Shaud G. Tavakoli | 2

Regulations from which the exemption is requested:

14 CFR Part 21

14 CFR 45.23(b)

14 CFR 61.23(a) & (c)

14 CFR 61.101(e)(4) & (5)

14 CFR 61.113(a) & (b) 

14 CFR 61.315(a)

14 CFR 91.7(a)

14 CFR 91.9(b)(2)

14 CFR 91.103(b)(2)

14 CFR 91.109

14 CFR 91.119

14 CFR 91.121

14 CFR 91.151(a)

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 exempt civil aircraft, as

the term is defined under §40101 of the Act, including UAS, from the requirement that all 

civil aircraft 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. See 49 USC §44701(f); see 

also 49 USC §§ 44711(a), 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 may 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.

FMRA 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.” FMRA 333(c).
Petition of Shaud G. Tavakoli | 3

BACKGROUND ON PETITONER

Shaud G. Tavakoli is an individual with experience flying UAS in a variety of 

environments in the United States and abroad.

UAS AND OPERATIONAL DESCRIPTION

Petitioner seeks to commercially operate a variety of UAS weighing less than 55 pounds 

including payload in the United States for the purpose of acquiring and closed set motion 

picture and filming. The Appendix attached to this exemption petition lists the aircraft that 

Petitioner contemplates operating. In prior, similar exemptions the Secretary has approved 

every UAS platform included in the Appendix. See, e.g., Exemption No. 12646.

As the operator of these aircraft, Petitioner is committed to the following conditions and

limitations on its operations.

1. Operations are limited to the UAS listed in the Appendix and those UAS previously 

approved by the Secretary that weigh less than 55 pounds including payload.

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”). 

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 VLOS of the PIC and VO at all times.

6. All operating documents needed to operate the UAS 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. Petitioner 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.
Petition of Shaud G. Tavakoli | 4

10. Petitioner will follow the UAS manufacturer’s maintenance, overhaul, replacement, 

inspection, and life limit requirements for the aircraft and aircraft components.

11. Each UAS operated under this exemption will comply with all manufacturer 

safety bulletins.

12. 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.

13. Petitioner 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.

14. 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”).

15. 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 Certificate of Waiver 

or Authorization (“COA”).

16. To the extent possible and observable to the PIC, 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.

17. If the UAS loses communications or loses its GPS signal, the aircraft will return 

to a pre-determined location.

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

19. 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.

20. All operations shall be conducted in accordance with an Air Traffic Organization 

(“ATO”) issued COA if the blanket COA does not cover the intended operation.

21. 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.

22. Documents used by Petitioner 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.

23. The aircraft will remain clear and give way to all manned aviation operations and 
Petition of Shaud G. Tavakoli | 5

activities at all times.

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

specific requests will be made via subsequent COA.

25. 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; and

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.

The PIC, VO, operator trainees or essential persons will not be considered 

nonparticipating persons under this exemption.

26. 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.

27. 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 National Transportation Safety Board (“NTSB”)

per instructions contained on the NTSB Web site: www.ntsb.gov.
Petition of Shaud G. Tavakoli | 6

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 Petitioner, an exemption from Part 21 Subpart 

H meets the requirements of an equivalent level of safety under Part 11 and Section 333 

of the FMRA. The Federal Aviation Act (49 USC §44701(f)) and Section 333 of the 

FMRA 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. Petitioner 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 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 provides 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 Petitioner

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.
Petition of Shaud G. Tavakoli | 7

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 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(b)(2): Preflight action

This regulation requires each PIC take certain actions before flight to ensure the

safety of flight that are not applicable to UAS. The PIC will take preflight actions

tailored to UAS flight, 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. 

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 because neither a pilot 

nor passengers will be carried in the aircraft, the PIC is able to control the UAS via radio 

signals from the controller and the size and speed of the aircraft are comparably lower

compared to those employed by flight instruction contemplated by this regulation.

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 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 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, 

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 
Petition of Shaud G. Tavakoli | 8

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 digital altitude read out, an exemption is necessary. 

An equivalent level of safety will be achieved by the PIC confirming the altitude of the 

launch site shown on the digital 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. Petitioner seeks the 

requested relief because without an exemption from Section 91.151(a)(1), the flight time 

duration of the selected aircraft will be dramatically reduced (in some cases to zero), 

which will render any flights contemplated by this Petition impossible or impractical.

The technical specifications of the proposed UAS, their Operations Manuals, and

Petitioner’s proposed operating limitations, ensure that Petitioner will safely operate 

the selected aircraft during daylight hours in VFR conditions until 90 percent of

remaining battery power or fuel reserves remain.

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 Petitioner. Maintenance will be accomplished 

pursuant to the User Guide or Operating Manual. An equivalent level of safety will be 

achieved because these UAS 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.
Petition of Shaud G. Tavakoli | 9

PUBLIC INTEREST

Approval of exemptions allowing commercial operations of UAS for aerial acquisition 

of data enhances safety while reducing risk. Manned aircraft create a greater risk than 

UAS because manned 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 persons to the risks associated with manned aircraft flights. 

EQUIVALENT LEVEL OF SAFETY

Petitioner 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 will be made anonymous.

NATIONAL SECURITY

Given the small size of the UAS involved and the restricted environment within which 

they will operate, this petition presents no national security concern.

FEDERAL REGISTER SUMMARY

Docket No.: No. FAA-2015-

Petitioner: Shaud G. Tavakoli

Description of Relief Sought: Petitioner is seeking an exemption to conduct

commercial acquisition of aerial data and raining operations using unmanned aircraft 

systems.

Regulations from which Exemption Requested: Part 21 and §§ 45.23(b), 61.23(a) and 

(c), 61.101(e)(4) and (5), 61.113(a) and (b), 61.315(a), 91.7(a), 91.9(b)(2), 91.103,

91.109, 91.119, 91.121, 91.151(a), 91.405(a), 407(a)(1), 409(a)(2), 417(a) and (b) of

Title 14, Code of the Federal Regulations (14 CFR).

Based upon the foregoing, Petitioner requests that the FAA grant him the necessary 

exemptions under Section 333 of the FAA FMRA as requested herein to allow for 

commercial operations of UAS within the United States.

Sincerely,

/s/ Shaud G. Tavakoli

Shaud G. Tavakoli
Petition of Shaud G. Tavakoli

APPENDIX

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 Heavy Lifter

17. Aerial Mob Light Lifter

18. Aerial Remote Mineral Detection System (ARMDS)

19. Aerialtronics Zenith with intergrated Airware system

20. 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. Aeryon Sky Ranger

32. Aervonics Sky Jib frame with a DJI A2 flight system

33. Aero-M

34. Aeryon Scout

35. Aeryon SkyRanger

36. AgEagle

37. AgEagle Robotic

38. AgScout

39. AgScout Mini

40. Agribotix Hornet Drone

41. Agribotix Enduro Quad

42. AgriView VK Ranger EX
Petition of Shaud G. Tavakoli

43. Aibot

44. Aibotix X-6

45. Air Rover AR-3000

46. AirCover QR-425s

47. AirRobot AR 180

48. AirRobot AR 100

49. AirRobot AR200

50. Air-X

51. Align M690

52. Altavian Nova

53. Altavian Nova F6500

54. Altavian Nova R8400

55. Altus X-4

56. Altus X-8

57. American Drones, LLC Eagle

58. Apprentice

59. Arch Aerial OCTO multi-rotor UAS

60. Arris hexacoper

61. AR-960 Hex Rotor

62. AR-540 Quad Rotor

63. ARF-MikroKopter OktoXL

64. ARF-MikroKopter OktoXL +

65. ArrowLite

66. AscTec Falcon

67. AscTec Falcon 8

68. Astraeus Aerial Cinema System V.3CS

69. Atlantic RC Aircraft LC04

70. Auburn Trimble UX5

71. Auburn War Eagle

72. Auburn EasyStar

73. Auburn

74. AV44

75. Bixler 3DR Plane

76. Blade 350QX

77. Bixler 2

78. Boomerang Carbon Fiber Frame (The Identified System)

79. Bormatec Maja UAV

80. BOSH Technologies Super Swiper

81. Bumblebee-S

82. C-Astral Bramor gEO

83. CarbonCore Octocopter 1000

84. Carbon Core Cortex Quadcopter

85. CCO w/Wkm M

86. Chameleon Pro
Petition of Shaud G. Tavakoli

87. CinesStar

88. Cinestar 6

89. Cinestar X8

90. Cinestar 8

91. Cinestar 8 HL

92. Cinestar 8 Okto XL

93. Coaxial Quad Multirotor VAO1-V1

94. Coaxial Quad Multirotor VAO2-V2

95. CopelandRED LLC Delta Wing Aircraft

96. CyberQuad Maxi

97. DJI Flame Wheel F450

98. DJI Flame Wheel F550

99. DAx8

100. DJI Inspire

101. DJI Inspire 1

102. DJI Inspire 2

103. DJI M P330z

104. DJI Phantom

105. DJI Phantom 1

106. DJI Phantom 2

107. DJI Phantom 2+

108. DJI Phantom 2 Vision

109. DJI Phantom 2 Vision+

110. DJI Phantom Vision +

111. DJI Phantom 3

112. DJI Phantom FC40

113. DJI Spreading Wings S900

114. DJI Spreading Wings S1000

115. DJI Spreading Wings S1000+

116. DJI S800

117. DJI S800 EVO

118. DJI T600

119. Draganflyer Guardian

120. Draganflyer X4ES

121. Draganflyer X4P

122. Draganflyer 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
Petition of Shaud G. Tavakoli

131. Fire Fly 6

132. First Aerial Responder UAV

133. Flame Wheel G4 7.8 Skycrane

134. Flying-Cam 3.0 SARAH

135. Foxtech Kraken 130 V2

136. FreeFly Systems ALTA RTF

137. FreeFly Systems Octocopter Airframe (Legacy)

138. G4

139. G4 models

140. GeoStar

141. GerMAP G220

142. GerMAP G180

143. goFarm GF-1

144. Gryphon Dynamics X8

145. GT80X

146. Harris 18 HL

147. HEFF

148. Helicopters West DJI Inspire

149. Helicopters West SkyJib 8

150. Helios 960

151. Hawkeye Mk-III

152. HexaCrafter HC-1100 85.

153. HexaCrafter HO-1250

154. HH Blade 350QX2 AP

155. Hobbyking “Bixler” Fixed Wing Trainer

156. HoneyComb AgDrone

157. Horizon Hobby Blade 350 Qx2 quadcopter

158. Hoverfly LiveSky, BigSky 60 and H-Frame

159. Hubsan X4 micro drone

160. HVP 14301 Multi Rotor

161. Identified System

162. IMT Global xFold Cinema

163. Indago

164. InovalDrone:Inova One

165. InstantEye Mk-2

166. InstantEye Mk-2 Gen2

167. Intuitive Aerial Aeragon

168. K130 Octocopter

169. KongCopter X8

170. Kopterworx Hammer X12

171. Latitude HQ-4 Hybrid Multirotor

172. LB700

173. Leading Edge Precision Vision 10

174. Leptron Avenger
Petition of Shaud G. Tavakoli

175. Lewis Realty Associates Hexacopter 650

176. Liberty 1

177. Lockheed Martin Desert Hawk III

178. Lockheed Martin Indago

179. Matrix quad copter

180. MaxFlight

181. MD4-200

182. MD4-1000

183. Mikrokopter 2.5

184. MLB Company Super Bat

185. MU-1H

186. Multirotor G4 7.8 Skycrane

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 Skycontroller

195. Patriot X4

196. Patriot X8

197. Finwing Penguin V2

198. Birdseyeview FireFly 6

199. Phoenix

200. Phoenix VTOL

201. Phoenix 60

202. Phoenix 60LE

203. Pixhawk

204. Precision Drone Pacesetter

205. PrecisionHawk

206. PrecisionHawk Hawkeye 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 HL1

217. PV HL2

218. Q1
Petition of Shaud G. Tavakoli

219. Quadcopter LLC MikroKopter

220. Quiet UAV

221. Qube

222. R/C Rotors and Aerial Media: Matrix Prof. Multi Rotor Frame & Octo Heavy

Lift Prof. Multi Rotor

223. Frame Ronin Edition Microdrones:MD4-1000

224. RCTimer Hexacopter

225. RDASS

226. REHawk 500

227. REHawk 680

228. RF-70

229. Riegl RiCopter

230. RITEWING Z3 Spade 47”

231. Ritewing Drake 60”

232. RITEWING Z3 Spade 70”

233. RITEWING 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. SenseFly eBee

243. SenseFly eBee RTK

244. SenseFly eXom

245. Sensurion Magpie MP-1

246. Service-Drone Recon One

247. Service-Drone Blackbird

248. SH 900

249. ShadowHawk

250. Shrike

251. Sirius

252. SkyCatch

253. SkyJib 8 v.2 Heavy Lifter

254. SkyPhilly MI

255. Skywalker Aero

256. Skywalker Flying Wing X8

257. SnapRoll Media SUAS

258. Solutions Phoenix 30

259. SteadiDrone

260. Steadidrone Quad

261. Steadydrone QU4D
Petition of Shaud G. Tavakoli

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 Systems MoAC

280. Tayzu 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. TUP X8-800

290. Turbo Ace CINEWING 6

291. TurboAce Matrix-G quadcopter

292. Turbo Ace matrix-E

293. Turbo Ace MATRIX-1

294. UAV Solutions Phoenix 60

295. Universeye Penguin

296. Unmanned Flying Rolling Orb “UFRO”

297. US2 GreenHawk

298. UtiliCopter ITX8

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
Petition of Shaud G. Tavakoli

306. Viking UAS X6 Model 800

307. Viking UAS Viking ONE

308. VK-450

309. Viking Unmanned Aerial Systems, 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 DJI 5800

322. xCel Drones XD550CDR

323. XFold Rig with four configurations: Quadcopter, Hexcopter, Octocopter and x12

Copter

324. X8-M