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 NaƟonal 

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 48 
48 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 97 
98 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 145 
148 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 192 
198 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 240 
248 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 288 
298 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 DynamicsHex 
348 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