October 28, 2015

U.S. Department of Transportation, Docket Operations

West Building Ground Floor, Room W12-140

1200 New Jersey Avenue, SE

Washington, DC 20590

RE: Petition of Douglas Braeckel for Exemption Pursuant to Section 333 of the FAA 

Reform Act.

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 and 14 CFR Part 11, 

Douglas Braeckel (“Petitioner”) respectfully requests an exemption from several provisions of 

Title 14 of the Code of Federal Regulations (C.F.R.) to permit the commercial operation of UAS 

for the purpose of aerial data collection, search and rescue, and training flights, 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:

Douglas Braeckel

13720 Old Saint Augustine Road, Suite 8-187

Jacksonville, FL 32258

Email: doug.braeckel@gmail.com
Regulations from which the exemption is requested:

14 CFR 61.23(a) and (b)

14 CFR 61.101(4) and (5)

14 CFR 61.113(a)

14 CFR 61.315(a)

14 CFR 91.7(a)

14 CFR 91.119(c)

14 CFR 91.121

14 CFR 91.151(a)(1)

14 CFR 91.203(a) and (b)

14 CFR 91.405(a)

14 CFR 407(a)(1)

14 CFR 409(a)(1) and (2)

14 CFR 417(a) and (b)

AUTHORITY FOR EXEMPTIONS

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

authority by its terms includes exempting civil aircraft, as the term is defined under §40101of the

Act, includes 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).
UAS AND OPERATIONAL DESCRIPTION

The 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 aerial data, to assist with 

search and rescue operations as well as for general flight training purposes. The Appendix of 

UAS attached to this exemption petition lists the aircraft that the Petitioner contemplates 

operating. 

The Petitioner, during commercial operations described herein, will hold at minimum a FAA 

Sport Pilot certificate and hold a current and valid U.S. driver’s license as evidence of medical 

eligibility or a third class airmen’s medical certificate. The Petitioner will have a sound 

understanding of FARs, pre-flight inspections, maintenance and repair, operations within 

airspace, as well as being trained to high safety standards.

The Petitioner is committed to the following conditions and limitations on its operations. The 

Petitioner understands that failure to comply will be grounds for the immediate suspension or 

rescission any exemption granted.

 The UAS will weigh less than 55 lbs.

 The UA will not be operated at a speed exceeding 87 knots (100 miles per hour). In no 

case will the UA be operated at airspeeds greater than the maximum UA operating 

airspeed recommended by the aircraft manufacturer.

 The UA will be operated at an altitude of no more than 400 feet above ground level 

(AGL). Altitude will be reported in feet AGL.

 All operations will utilize a visual observer (VO). The UA will be operated within the 

visual line of sight (VLOS) of the PIC and VO at all times. The VO and PIC will be able 

to communicate verbally at all times. The PIC will use human vision unaided by any 

device other than corrective lenses, as specified on the PIC’s FAA-issued airman medical 

certificate or U.S. driver’s license.

 The PIC will be designated before each flight and will not transfer his designation for the 

duration of the flight. The PIC must ensure that the VO can perform the duties required of

the VO.

 All operating documents will be accessible during UAS operations and made available to 

the Administrator upon request. 

 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. Functional test flights will 

only be conducted by a PIC with a VO and will remain at least 500 feet from other 

people. The functional test flight must be conducted in such a manner so as to not pose an

undue hazard to persons and property.
 The Petitioner is responsible for maintaining and inspecting the UAS to ensure that it is 

in a condition for safe operation.

 Prior to each flight, the PIC will conduct a pre-flight inspection and determine the UAS is

in a condition for safe flight.

 The Petitioner will follow the UAS manufacturer’s maintenance, overhaul, replacement, 

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

 Each UAS operated under this exemption must comply with all manufacturer safety 

bulletins.

 The PIC will hold either a private or sport pilot certificate. The PIC will also hold a

current FAA airman medical certificate or a valid U.S. driver’s license. The PIC will also meet 

the flight review requirements specified in 14 CFR § 61.56 for an aircraft in which the PIC is 

rated on his pilot certificate.

 The Petitioner will not operate unless he demonstrates the ability to safely operate the 

UAS in a manner consistent with how the UAS is intended to be operated, including 

evasive and emergency maneuvers and maintaining appropriate distances from persons, 

vessels, vehicles and structures. PIC qualification flight hours and currency will be 

logged in a manner consistent with 14 CFR § 61.51(b). During training, proficiency, and 

experience-building flights, all persons not essential for flight operations will be 

considered nonparticipants, and the PIC will operate the UA with appropriate distance 

from nonparticipants in accordance with 14 CFR § 91.119.

 All UAS operations will be conducted under visual meteorological conditions (VMC) 

during the daytime.

 The UAS 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 issued to the exemption holder. The letter of agreement 

with the airport management will be made available to the Administrator or any law 

enforcement official upon request.

 The UAS 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.

 If the UAS loses communications or loses its GPS signal, the UAS will return to a predetermined location within the private or controlled-access property.

 The PIC will abort the flight in the event of unpredicted obstacles or emergencies.
 The PIC will not begin a flight unless (considering wind and forecast weather conditions)

there is enough available power for the UA to conduct the intended operation and to 

operate after that for at least five minutes or with the reserve power recommended by the 

manufacturer if greater.

 All aircraft 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.

 Documents used by the operator 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. These 

documents will be made available to the Administrator or any law enforcement official 

upon request.

 The UAS will remain clear of and give way to all manned aviation operations and 

activities at all times.

 The UAS wil not be operated from any moving device or vehicle.

 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 UA and/or debris in the event of an accident. The operator will 

ensure that nonparticipating persons remain under such protection. If a situation 

arises where nonparticipating persons leave such protection and are within 500 

feet of the UA, flight operations will cease immediately in a manner ensuring the 

safety of nonparticipating persons; and

b. The owner/controller of any vessels, vehicles or structures has granted 

permission for operating closer to those objects and the PIC has made a safety 

assessment of the risk of operating closer to those objects and determined that it 

does not present an undue hazard.

 Any operations conducted over private property will be with permission from the 

property owner/controller or authorized representative.

 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 will be reported 

to the National Transportation Safety Board (NTSB) per instructions contained on the 

NTSB Web site: www.ntsb.gov.
DESCRIPTION OF SPECIFIC REGULATIONS

14 C.F.R.61.23(a) and (c), 14 C.F.R. 61.101(e)(4) and (5), 14 C.F.R. 61.113(a), 14 C.F.R. 

61.315(a)

The FAA has previously determined that individuals holding a sport, recreational or private pilot 

certificate possess the requisite knowledge of the national airspace system to safely operate a 

UAS. The FAA has also recognized that, absent an exemption, all pilots other than commercial 

pilots could not receive compensation for their work as PIC. Accordingly, the FAA has granted 

well over one hundred exemptions that permit an individual possessing at least a sport pilot 

certificate to act as a PIC and be compensated. Granting the Petitioner's request would be 

consistent FAA precedent in this regard.

14 CFR 91.7(a)

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 the 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.

14 CFR 91.119(c)

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 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

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)

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. The 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 reduced and severely constrain the practicality of any aerial acquisition of data 

that the Petitioner proposes to conduct pursuant to this Petition. The technical specifications of 

the proposed UAS, their Operations Manuals, and the Petitioner’s proposed operating 

limitations, ensure that the 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 91.203(a) & (b)

The UAS has no cabin, cockpit or pilot station and is operated without an on board 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)(1) & (2), 417(a) & (b)

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 the Petitioner. 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

The 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 they 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 issue. With small payloads and maximum 

flight times well below 60 minutes, this offers little or no risk to national security. 

The Petitioner respectfully requests an exemption under Section 333 to enable the operation of 

efficient, limited, low-risk commercial UAS for the activities stated, and respecting at all times 

the space and privacy of citizens and property while keeping our skies safe. 

Sincerely,

Douglas Braeckel

13720 Old Saint Augustine Road, Suite 8-187

Jacksonville, FL 32258

Email: doug.braeckel@gmail.com
Appendix of UAS

1. 3D Robotics Aero

2. 3D Robotics Aero-M

3. 3D Robotics DIY Quad Kit

4. 3D Robotics Iris

5. 3D Robotics Iris+

6. 3D Robotics Solo

7. 3D Robotics Spektre

8. 3D Robotics X8

9. 3D Robotics X8-M

10. 3D Robotics X8+

11. 3D Robotics Y6

12. Advanced Robotics AR-540

13. Advanced Robotics AR-960

14. Aerialtronics Altura Zenith ATX8

15. AeroLogix GeoStar

16. Aeromao AeroMapper 300

17. Aeromao Aeromapper EV-2

18. Aeromao Talon

19. Aeronavics X4 Titanium

20. AeroVironment Puma

21. AeroVironment Shrike

22. Aervonics Skyjib 8

23. Aeryon Scout

24. Aeryon SkyRanger

25. AgEagle AgEagle

26. Agribotix Enduro Quad

27. Agribotix Hornet Drone

28. Aibotix Aibot X6

29. AirCover QR-425

30. AirCover QR-425s

31. AirRobot AR100

32. AirRobot AR180

33. AirRobot AR200

34. Align M424

35. Align M470

36. Align M480L

37. Align M690L

38. Align TREX 100

39. Align TREX 150

40. Align TREX 250

41. Align TREX 450

42. Align TREX 500

43. Align TREX 500E

44. Align TREX 550

45. Align TREX 600E

46. Align TREX 700E

47. Align TREX 800E

48. Altavian Nova F6500

49. Altavian Nova R8400

50. Altus Delta X-8

51. AscTec Falcon 8

52. Birdseyeview FireFly 6

53. Blade 120 SR

54. Blade 180 CFX

55. Blade 180 QX

56. Blade 200 QX

57. Blade 200 SR X

58. Blade 230 S

59. Blade 270 CFX

60. Blade 300 CFX

61. Blade 350 QX3

62. Blade 360 CFX

63. Blade 450 X

64. Blade Chroma

65. Blade FPV Nano QX

66. Blade Glimpse

67. Blade Inductrix Quadcopter

68. Blade Mach 25 FPV Racer

69. Blade mCP X BL

70. Blade mCX2

71. Blade mCX2

72. Blade NANO CP S

73. Blade Nano CP X

74. Blade Nano QX

75. Blade Nano QX 3D

76. Blade Pico QX

77. Blade Scout CX

78. CarbonCore Cortex

79. CarbonCore Octocopter 1000

80. Cheerson 6050

81. Cheerson 6051

82. Cheerson 6457

83. Cheerson 6048F

84. Cheerson CX-10/CX-10A/CX-10C

85. Cheerson CX-11

86. Cheerson CX-12

87. Cheerson CX-20

88. Cheerson CX-22

89. Cheerson CX-30/CX-30C/CX-30S/CX-30W

90. Cheerson CX-31

91. Cheerson CX-32/CX-32C/CX-32-S/CX-32W

92. Cheerson CX-33/CX-33S/CX-33W-TX

93. Cheerson CX-90

94. Cheerson CX-STARS
95. CineStar 8 HL

96. CineStar 8 Okto XL

97. Diatone Blade series 150mm

98. Diatone Blade series 180mm

99. Diatone Color series 250mm

100. Diatone ET series 150mm

101. Diatone ET series 180mm

102. Diatone ET series 200mm

103. DJI Flame Wheel F330 and clones

104. DJI Flame Wheel F450 and clones

105. DJI Flame Wheel F550 and clones

106. DJI Inspire 1

107. DJI M P330z

108. DJI Phantom

109. DJI Phantom 1

110. DJI Phantom 2

111. DJI Phantom 2 Vision

112. DJI Phantom 2 Vision+

113. DJI Phantom 2+

114. DJI Phantom 3

115. DJI Phantom 3 Advanced

116. DJI Phantom 3 Professional

117. DJI Phantom FC40

118. DJI Phantom Vision+

119. DJI S800

120. DJI S800 EVO

121. DJI Spreading Wings S1000

122. DJI Spreading Wings S1000+

123. DJI Spreading Wings S900

124. DJI T600

125. Draganflyer Guardian

126. Draganflyer X4ES

127. Draganflyer X4P

128. Draganflyer X6

129. DYS 250

130. DYS 320

131. DYS D800 V-6

132. DYS D800 V-8

133. DYS D800 X4

134. DYS D800 X8

135. Estes Proto-X

136. Estes Proto-X FPV

137. Estes Proto-X Six

138. Estes Proto-X SLT

139. Estes Proto-Z

140. FliteTest ElectroHub Dragonfly

141. FliteTest ElectroHub Quadcopter

142. FliteTest ElectroHub Tricopter

143. FliteTest ElectroHub Y6

144. FliteTest VersaCopter 280

145. Foxtech Kraken

146. Foxtech Kraken 130 V2

147. FreeFly Systems Alta

148. FreeFly Systems Cinestar 6

149. FreeFly Systems Cinestar 8

150. FreeFly Systems Cinestar X8

151. GerMap G180

152. Gryphon Dynamics X8

153. Hitec Q-Cop 450

154. HMF Totem Q330

155. HMF Totem Q380

156. HMF Totem Q450

157. Hobbyking Alien 560

158. Hobbyking Bix3 Trainer

159. Hobbyking Bixler

160. Hobbyking Bixler 2

161. Hobbyking Darkwing

162. Hobbyking FPV / UAV V2

163. Hobbyking Go Discover

164. Hobbyking H500

165. Hobbyking Hawkeye 1700

166. Hobbyking Phantom Flying Wing

167. Hobbyking Quanum Observer

168. Hobbyking RoboCat

169. Hobbyking Sky Eye

170. Hobbyking SkyRay

171. Hobbyking SkyRay

172. Hobbyking UFO 280

173. Hobbyking Zeta Sky Observer

174. HobbyZone Champ

175. HobbyZone Duet

176. HobbyZone Sport Cub S

177. Horizon Hobby Blade 350 QX2

178. Horizon Hobby Blade 350 QX3

179. Horizon Hobby Blade 350 QX3 AP

180. Hubsan H109S

181. Hubsan X4 Micro Drone

182. Ideafly Hero 550

183. InstantEye Mk-2

184. InstantEye Mk-2 Gen2

185. InstantEye Mk-2 Gen3

186. Intuitive Aerial Aerigon

187. Lockheed Martin Desert Hawk III

188. Lockheed Martin Indago

189. Lumenier Danaus

190. Lumenier QAV180

191. Lumenier QAV210

192. Lumenier QAV220 V2

193. Lumenier QAV250

194. Lumenier QAV250 V2

195. Lumenier QAV280 V2

196. Lumenier QAV310 V2
197. Lumenier QAV330 V2

198. Lumenier QAV350 V2

199. Lumenier QAV400

200. Lumenier QAV500 V2

201. Lumenier QAV540G

202. Microdrones MD4-1000

203. Microdrones MD4-200

204. Microdrones MD4-3000

205. Mikrokopter Hex XL

206. Mikrokopter OktoXL

207. Mugin 3m H tail Platform

208. Mugin 3m UAV V-Tail Platform

209. Mugin 4500mm Super Huge UAV

210. Mugin Mini Mugin 2.6m UAV

211. Mugin Plus 4500mm FPV Plane

212. Nine Eagles Bravo III

213. Nine Eagles Bravo SX

214. Nine Eagles Draco

215. Nine Eagles Solo Pro

216. Nine Eagles Solo Pro 125

217. Nine Eagles Solo Pro 130

218. Nine Eagles Solo Pro 180

219. Nine Eagles Solo Pro 228P

220. Nine Eagles Solo Pro 270

221. Nine Eagles Solo Pro 287

222. Nine Eagles Solo Pro 319

223. Nine Eagles Solo Pro 328

224. Nine Eagles Solo Pro V-260A

225. Parrot Airborne Cargo Drone

226. Parrot AR Drone

227. Parrot AR Drone 2.0

228. Parrot Bebop Drone

229. Parrot Rolling Spider

230. Patriot X4

231. Patriot X8

232. Phoenix 30

233. Phoenix 60

234. Phoenix 60LE

235. PrecisionHawk Hawkeye

236. PrecisionHawk Hawkeye MK-III

237. PrecisionHawk Lancaster

238. PrecisionHawk Lancaster MK-III

239. Prioria Maveric

240. Pulse Aerospace PA 01 Vapor

241. Pulse Aerospace Vapor 35

242. Pulse Aerospace Vapor 55

243. Range Video RV Jet

244. Ready Made RC Mini Skyhunter

245. Ready Made RC Skyhunter

246. ReadyToFlyQuads Opera

247. Riegl RiCopter

248. Ritewing Z3 Spade 47"

249. Ritewing Z3 Spade 70"

250. Ritewing Z4 Spade 52"

251. RJX CAOS 330

252. SenseFly eBee

253. SenseFly eBee RTK

254. SenseFly eXom

255. Service-Drone Blackbird

256. Service-Drone Recon One

257. SkyCatch SkyCatch

258. Skywalker 1680

259. Skywalker 1800

260. Skywalker 1830

261. Skywalker 1880

262. Skywalker 1900

263. Skywalker Aero

264. Skywalker Mini Skywalker

265. Skywalker Naja

266. Skywalker Revolution

267. Skywalker X1

268. Skywalker X5

269. Skywalker X6

270. Skywalker X7

271. Skywalker X8

272. SteadiDrone Mavrik

273. SteadiDrone QU4D

274. SweepWings Behemoth 60”

275. SweepWings Flinch 37”

276. SweepWings Juggernaut 48”

277. Swift Radioplanes Lynx

278. Syma X11/X11C

279. Syma X12/X12S

280. Syma X13 Storm

281. Syma X3 Pioneer

282. Syma X4/X4S

283. Syma X5/X5C/X5S/X5SW

284. Syma X6 Super Ship

285. Syma X8C/X8G

286. Tarot 690

287. Tarot 960

288. Tarot 680PRO

289. Tarot FY650

290. Tarot FY680

291. Tarot FY690S

292. Tarot T-15

293. Tarot T-18

294. Tarot T1000

295. Tarot T690

296. Tarot T810

297. Tarot T960

298. Tarsier Systems MoAC
299. Tayzu Robotics Titan X8

300. Team Black Sheep Caipirinha

301. Team Black Sheep Discovery

302. Team Black Sheep Discovery Pro

303. Topcon Sirius Basic

304. Topcon Sirius Pro

305. Trimble UX5

306. Trimble UX5 hp

307. Trimble ZX5

308. Turbo Ace Cinewing 6HL

309. Turbo Ace Matrix

310. Turbo Ace Matrix-E

311. Turbo Ace Matrix-S

312. Turnigy Talon 500

313. Turnigy Talon Hexcopter

314. Turnigy Talon Tricopter

315. UDI Nano 3D

316. UDI U818A

317. UDI U818A-HD

318. UDI U830A

319. UDI U839

320. Viking Patriot X4/X8

321. Viking Patriot X4/X8

322. Viking Viking ONE

323. Viking X6 Model 800

324. Volantex Firstar 1600 Composite

325. Volantex Firstar 200

326. Volantex Firstar 2000 V2

327. Volantex Firstar V767-1

328. Volantex FPVraptor

329. Volantex FPVraptor EX

330. Volantex FPVraptor V2

331. Volantex Ranger EX

332. Vulcan BW950

333. Vulcan Octo

334. Vulcan Raven

335. Vulcan SkyHook Mantis

336. Walkera Scout X4

337. Walkera TALI H500

338. WL Toys Q212

339. WL Toys V262

340. WL Toys V303

341. WL Toys V333

342. WL Toys V666

343. WL Toys V686/V686G/V686K

344. WL Toys V911/V911 Pro

345. WL Toys V912

346. WL Toys V913/V913A

347. WL Toys V929

348. WL Toys V930

349. WL Toys V931

350. WL Toys V933

351. WL Toys V939

352. WL Toys V944

353. WL Toys V949

354. WL Toys V955

355. WL Toys V966

356. WL Toys V977

357. WL Toys V988

358. WL Toys V989

359. X-CAM KongCopter AQ450

360. X-CAM KongCopter AQ550

361. X-CAM KongCopter FH800

362. X-CAM KongCopter FQ700

363. X-CAM KongCopter Y600

364. X-UAV Skua

365. X-UAV Talon

366. Yuneec Typhoon G

367. Yuneec Typhoon Q500

368. Yuneec Typhoon Q500 4K

369. Yuneec Typhoon Q500+

370. Zeta Science FX-61 Phantom

371. Zeta Science FX-79 Buffalo

372. Zeta Science Wing Wing Z-84