Jon Tull, CEO AgTech Enterprises, Inc. 4580 E

. Thousand Oaks Blvd

. Suite 300 Westlake Village, CA 91362

September 15, 2015

Unmanned Aircraft Systems Integration Office AFS-80 800 Independence Ave., S.W

. Washington, D.C. 20591

To Whom It May Concern:

Enclosed please find an exemption application filed on behalfofAgTech Enterprises, Inc. underSection 333 ofthe FAA Modernization and Reform Act of2012 and 14C.F.R. Part 11to allow commercial operationsof unmanned aircraft for precision aerial survey.

We here atAgTech requestthatyou considerthis request for summarygrant based up on the companlstwo (2) existing 333 exemptions (Exemption No. 11573and Exemption No. 12802)for use of

a similar aircraft, and also based upon the exemptions that have already been granted regarding the make and model ofaircraft presently at issue

.
Should you oryour staffhave any questions, please contactthe undersigned

. Thankyou foryourtime and consideration.

Jon Tull, CEO

EnclosuresSeptember 15,2015

U.S. Department ofTransportat ion DocketManagement System 1200 NewJerseyAve.
, SE Washington,DC 20590

Re: Exemption Request Under Section 333 ofthe FAA Reform Act and Part 11 ofthe Federal AviationRegulations

DearMadam, Sir,

Pursuant to Section 333 ofthe FAA Modernization and Reform Act of2012 (the "Reform Act") and 14 C.F.R. Part ll
, AgTech Enterprises, Inc. ("AgTech") an operator of the Unmanned Aircra ft Systems (collectively, the "Craft") seeks an exem ption from the Federal Aviation Regulations ("F ARs") listed below:

• 14 CFRPart21
• 14 CFR45.23(b)
• 14 CFR61.113(a) & (b) 14 CFR91.7(a)
• 14 CFR91.9(b)(2)
• 14 CFR9 1.103

• 14 CFR91.109
• 14 CFR 91.119
• 14 CFR 91.121
• 14CFR91.1 51(a)
• 14 CFR91.203(a) & (b) 14 CFR91.405(a)
• 14 CFR407(a)(l) 14 CFR409(a)(2) 14 CFR 417(a)& (b)

The requested exempt ion would authorize commer cial operations for use of the Craft in agriculture, mining, precision aerial surveys, patrols, as well as other mapping and survey applications. These operations will be subject to strict operating requirements and conditions to ensure at least an equiva lent level of safety to currently authorized opera tions using manned aircraft andunderconditions asmaybemodified by the FAA as required by Section333.

1. AUTHORITY FOREXEMPTIONS

TheFederal Aviation Act expressly grants the FAA authority to issue exempt ions. 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 ofa regulation prescribed under subsection (a) or (b) ofthis sect ion orany sections §44702-44716 ofthis title ifthe Administratorfinds theexemption inthepublic interest. 49 USC §4470l(f). See also 49 USC §44711(a); 49 USC §44704; 14 CFR91.203(a)(l).

### Section 333(b) ofthe Reform Act assists the Secretary in detennining 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 makingthis determination, the Secretary must consider

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

Reform Act 333(a). Ifthe Secretary detennines that a UAS "may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation ofsuch aircraft in the national airspace system." ld. 333(c).

2. APPLICATIONSAND PUBLICINTEREST
AgTech intends to use the Craft (listed in "Appendix B") to assist customers with crop yield optimization, resource allocation and management, pest control, and risk management. AgTech proposes to use these small, lightweight Craft and proprietary cloud-based software to collect, process, and analyze aerial data. In doing so, AgTech would occupy a brand new space in a transformative industry by providing high quality and actionable information to users. AgTech's
use of the Craft would contribute to various social goods, fTom environmental protection to improved crop yields. In 

### providing this service, AgTech would empower businesses, researchers, farmers, and other land owners to make better management decisions through software that identifies disease and insects, nutrient deficiencies, and materials for increasing yields with fewer
resources.
Operations underthe exemption will be subject to strict operating requirements and conditions to
ensure at least an equivalent level of safety to currently authorized operations using manned aircraft and under conditions as may be modified by the FAA as required by Section 333.

3. APPLICABLELEGAL STANDARD UNDER SECTION333

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

b. Equivalent Level ofSafety 

### AgTech 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 ofsafety to operations 1U1der the current and proposed regulatory structure.

c. Privacy

All flights will occur over private or controlled access property with the property owner's prior

### consent and knowledge. Images or video taken ofindividuals will have consented to being filmed
or otherwise they will be made anonymous.
d. National Security

Given the small size ofthe UAS involved and the restricted environment within which they will operate, ourpetitionpresents no national security issue.

e. Operating requirements

Grant of the exemption to AgTech for the Craft will be subject to the following operating conditions:

1. 

### Operations authorized by this grant of exemption are limited to the Craft when weighing less than 55 pounds including payload. Proposed operations ofany other aircraft will require a newpetition or apetitionto amend this exemption.

2. Operations for the purpose ofclosed-set motion picture and television filming are not permitted.

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The exemption holder may use either groundspeed or calibrated airspeed to determine compliance with the 87 knot speed restriction. In 

### no case will the UA be operated at airspeeds greater than the maximum UA operating airspeed recommended by the aircraft manufacturer.

4. The UA must be operated at an altitude ofno more than 

### 400 feet above ground level 

### (AGL). Altitudemust be reported in feet AGL.

5. The UA must be operated within visual line of sight (VLOS) ofthe 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 FAA-issued ainnan medical certificate or U.S. driver's license.

6. All operations must utilize a visual observer (VO). The UA must be operated withinthe 

### visual line ofsight (VLOS) ofthe PIC and VO at all times. The VO may be used to satisfy the VLOS requirement as long as the PIC always maintains VLOS capability. The VO and PIC must be able to communicate verbally at all times; electronic messaging ortexting is not permitted during flight operations. The PIC must be designated before the flight and cannot transfer his or her designation for the duration ofthe flight. The PIC must ensure thatthe VO canperfom1 the duties required ofthe VO.

7. This exemption and all docmnents needed to operate the UAS and conduct its operations in accordance with the conditions and limitations stated in this grant of exemption, are hereinafter referred to as the operating documents. The operating docmnents must be accessible during UAS operations and made available to the Administrator upon request. If

### a discrepancy exists betweenthe conditions and limitations in this exemption and the procedures outlined in the operating docmnents, the conditions and limitations herein take precedence and must be followed. Otherwise, the operator must follow the procedures as outlined in its operating documents. The operator may update or revise its operating doctunents. It is the operator's responsibility to track such revisions and present updated and revised documents to the Administrator or any law

### enforcement official upon request. The operator must also present updated and revised documents if it petitions for extension or amendment to this grant of exemption. Ifthe operator determines that any update or revision would affect the basis upon which the FAA granted this exemption, then the operatormustpetition for an amendment to its grant ofexemption. The FAA's UAS Integration Office (AFS-80) may be contacted ifquestions arise regarding updates or revisions to the operating documents.

8. Any UAS that has undergone maintenance or alterations that affect the UAS operation
or flight characteristics, e.g. replacement ofa flight critical component, must undergo a functional test flight prior to conducting further operations under this exemption. Functional test flights may only be conducted by a PIC with a VO and must remain at least 500 feet from other people. The functional test flight must be conducted in such a manner so as to notpose an undue hazardto persons andproperty.

9. The operator 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 must conduct a pre-flight inspection and determine the UAS is in a condition for safe flight. The pre-flight inspection must account for all potential discrepancies, e.g. inoperable components, items, or equipment. Ifthe inspection reveals a condition that affects the safe operation ofthe UAS, the aircraft is prohibited from operating until the necessarymaintenance has been performed and the UAS is found to be in a condition for safe flight.

11. The operator must follow the VAS manufacturer's maintenance, overhaul, replacement, inspection, and life limit requirements for the aircraft and aircraft components.

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

13. Underthis grant ofexemption, a PIC musthold either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC must also hold a current FAA airman medical certificate or a valid U.S. driver's license issued by a state, the District of Colombia, Puerto Rico, aterritory, a possession, orthe Federal govenunent. The PIC must also meet the flight review requirements specified in 14 CFR § 61.56 in an aircraft in which the PIC is rated onhis orherpilot certificate.

14. The operator may not pennit 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 under this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from persons, vessels, vehicles and structures. PIC qualification flight hours and currency must be logged in a manner consistent with 14 

### CFR § 

### 61.5l(b). Flights for the purposes of training the operator's P!Cs and VOs (training, proficiency, and experience-building) and detennining the PIC's ability to safely operate the UAS in a mrumer consistent with how the UAS will be operated under this exemption are permitted under the tenns ofthis exemption. However, training operations may only be conducted during dedicated training sessions. During training, proficiency, and experience-building flights, all persons not essential for flight operations are considered nonparticipants, and the PIC must operate the UA with appropriate distance from nonparticipants in accordance with 14 CFR 

### §91.119.15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All operations must be conducted under visual meteorological conditions (VMC). Flights m1der special visual flight rules (SVFR) are not authorized.

16. The UA may not operate within 5nautical miles ofan airport reference point (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) or for airports not denoted with an ARP, the center ofthe airport symbol as denoted on the current FAAR published aeronautical chart, unless a letter ofagreement with that airport's management is obtained
or otherwise permitted by a COA issued to the exemption holder. The letter ofagreement with the airport management must be made available to the Administrator or any law enforcementofficial uponrequest.

17. The UA may not be operated less than 500 feet below or less than 2,000 feet horizontally from a cloud orwhenvisibilityis less than 3 statute miles fromthe PIC.

18. Ifthe UAS loses communications or loses its GPS signal, the UA must return to a preR detennined locationwithin the private orcontrolledRaccess property.

19. The PIC must abortthe flight in the eventofunpredicted obstacles oremergencies.

20. The PIC is prohibited from beginning 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 recommendedby the manufacturerifgreater.

21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All operations shall be conducted in accordance with an ATORissued COA. The exemption holder may apply for a new or amended COA if it intends to conduct operations that cannot be conducted under the terms ofthe attached CO A.

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

23. Documents used by the operatorto ensure the safe operation and flight ofthe UAS and any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the PIC at the Ground Control Station of the UAS any time the aircraft is operating. These documents must be made available to the Administrator or any law enforcement official upon request.

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

25. The UAS may not be operatedby the PIC from any moving device orvehicle.

26. All Flight operations must 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 ofan accident. The operator must ensure that nonparticipating persons remain under such protection. If a situation arises where nonparticipating persons leave such protection and are within 500 feet ofthe UA, flight

### operations must 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 closerto those objects and the PIC has made a safety assessment ofthe risk ofoperat ing closer to those objects and determined that it does not present an unduehazard.

The PIC
, VO
, operator trainees or essential persons are not considered nonparticipating persons underthis exemption.

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

28. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries ofthe operational area as defined by the applicable COA must 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

. 3. CONCLUSION



### Satisfaction ofthe criteria provided in Section 333 ofthe Reform Act of 2012

- size, weight
, speed, operating capabilities, proximity to airports and popula ted areas, and operation within visual line ofsight and national security- providemorethan adequatejustificationfor the grantof the requested exemptions allowing commercial operation of applicant's Craft for the Purposes outlinedhereinandareconsistent withexemptions already granted. AgTech respectfully submits that because these small
, unmanned aerial vehicles will be 

### used in lieu of comparatively hazardous operations now conducted with fixed wing and rotary conventional aircraft
, the FAA can have confidence that the operations will achieve at least an equivalent level or greater level of safety. Approval ofthis exemption would thereby enhance safety and fulfill the Secretary of Transportation's (t he FAA Administrator's) responsibilities under Section 333(c) ofthe Reform Act to "establish requirement for the safe opera tion ofsuch aircraft systems in the national airspace system."



### Your **~~ ~** 



# ~<:CV

' 

### JonTull, CEO AgTech Enterprises, Inc.APPENDIXA: EXEMPTIONREQUEST AND EQUIVALENTLEVEL OF SAFETY SHOWINGS UNDERAPPLICABLERULES SUBJECTTOEXEMPTION


### AgTech requests an exemption from the following regulations as well as any additional regulations thatmaytechnically applyto the operation ofthe Craft:

14 CFRPart 21. SubpartH: Airwurthiness certificates
Subpart H, establishes the procedural requirements for the issuance ofainvorthiness certificates as 

### required by 

### FAR §91.203(a)(l). Given the size and limited operating area associated with the aircraft to be utilizedbyAgTech, 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(1)) and Section 333 ofthe Reform Act both authorize the FAAto exempt aircraft from the requirement for an airworthiness certificate, upon consideration ofthe size, weight, speed, operational capability and proximity to airports and populated areas ofthe particular UAS. In all cases, an analysis ofthese 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 withoutthe restrictions and conditions proposed.

14 CFR45.23(b): Marking ofthe 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
orpilot station. Eventhough the UAS will have no airworthiness certificate, an exemption may be needed as the UAS will have no entrance to the cabin, cockpit orpilot station on which the word "Experimental" can be placed. Given the size ofthe UAS, 2 inch lettering may be impossible. AgTech will marktheUAS 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 tonon-commercial operations. Becausethe UAS will not carry a pilot or passengers, the proposed operations can achieve the equivalent level of safety ofcurrent operations by requiring the pilot operating the aircraft to have completed a UAS flight-training course. Unlike a conventional aircraftthat carries the pilot and passengers, the UAS is remotely controlled. The area ofoperation is controlled and restricted, and all flights are planned and coordinated in advance. The risks associated with the operation ofthe UAS are so diminished from the level ofrisk associated with commercial operations contemplated by Part 61 when drafted, that allowing operations ofthe UAS as requested exceeds thepresentlevel ofsafety 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 AgTech contemplates operating, should this exemption be granted, no FAA regulatory standard will exist for detennining airworthiness. Giventhe size ofthe aircraft andthe operational restrictions put on the aircraft, anequivalent level ofsafetywill be provided.

14 CFR91.9(b)(2): Civil aircraft flight manual, marking and placard requirementsThe UAS, given its size and configuration has no ability orplace 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 onthe aircraft. The equivalent level ofsafety will bemaintained by keeping the Operating Manuals at the ground control point where the pilot flying the UAS will have immediate accessto it.

14 CFR91.103: 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 equivalentlevel ofsafety.

14 CFR91.109: Flight instruction

Section 91.103 provides thatno 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 nothave fully functional dual controls. Flight control is accomplished through the
use ofa control box thatcommunicates withthe aircraftviaradio 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 ofthe aircraft.

14 CFR 91.119: Minimum safe altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. The VAS 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 ofthe UAS as well as the location where it is operated. No flight will be taken without the pennission ofthe 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 ofthe 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 notpresent anundue 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

**a~rport.** The FAA will have advance notice of all operations through the filing of notices-toairmen.
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 withhelicopters and other conventional aircraft operating at or below 500 feet AGL. In addition, the low-altitude operations ofthe VAS will ensure separation between these VAS operations andthe operations ofconventional aircraftthat must comply with Section 91.119.

14 CFR91.121: Altimeter Settings

This regulation requires each person operating the aircraft to maintain crmsmg altitude by reference to an altimeter that is set "

...to the elevation ofthe 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 ofthe launch site shown on the GPS altitude indicatorbefore flight.

14 CFR91.151(a): Fuel requirements for flight inVFR conditions

Section 91.151(a) outlines fuel requirements for beginning a flight in VFRconditions. Relieffrom Section 91.151(a)(!) is requested tothe extentrequired to allowflights ofa variety ofUAS during daylight hours in visual flight rules (VFR) conditions to continue until 90 percent ofremaining battery power or fuel reserves remain. AgTech seeks the requested relief because without an exemption from Section 91.151(a)(l), the flight time duration of the selected aircraft will be reduced and severely constrain the practicality of any aerial acquisition of data that AgTech proposes to conductpursuanttothis Petition.

The technical specifications of the proposed UAS, their Operations Manuals, and AgTech's proposed operating limitations, ensure that AgTech will safely operate these elected aircraft during daylight hours in VFR conditions until 90 percent of remaining battery power or fuel
reserves remain.

14 CFR91.203(a) & (b): Carrving 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 atthe grmmd control point where the pilot flying the UAS will have immediate access to them, to the extentthey are applicable to the UAS.

14 CFR91.405(a); 407(a)(l); 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 ofthis 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 inspectormaintainthe aircraft 

### incompliance with Part43.

Given thatthese sections and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to AgTech. Maintenance will be accomplished pursuantto 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 oftime. Ifmechanical issues arise, the UAS can land immediately and will be operating from no higherthan 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 ofsafety.APPENDIXB: LIST OFCRAFTINCLUDEDWITHINPETITION

l. AgEagle 2. 3DRobotics Aero-M 3. 3DRobotics Iris 4. 3DRobotics Iris+ 5. 3DRobotics X8 6. 3D Robotics FixedWing 7. 3DRoboticsMultirotor 8. 3DRobotics Quadrotor 9. 3DR Solo 10. 3DRSpektre 11. 3DRobotics Spektre Industrial Multi-RotorAerial Vehicle 12. 3DRobotics Solo 13. 3DRoboticsX8+ 14. 3DRobotics X8-M 15. 3DRobotics Y6 16. Aerial Mob HeavyLifter 17. Aerial Mob Light Lifter 18. Aerial Remote Mineral Detection System (ARMDS) 19. Aerialtronics Zenithwith intergratedAirware system 20. AerialtronicsAlturaZenith ATX8 21. Aerigon 22. Aerobo 23. AeroCine Kopterworx HammerX12 

### 24. Aeromao AeroMapper 300 25. Aeromao Talon 26. Aerornao Aeromapper 300 

### 27. Aeromao Aeromapper EV-2 28. AeroVironment Shrike 29. AeroVironment Puma 30. AeronavicsX4 Titanium 31. Aeryon SkyRanger 32. Aervonics SkyJib 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. AgriViewVKRangerEX 43. Aibot 44. Aibotix X-6 45. Air RoverAR-3000 46. AirCover QR-425s47. AirRobotAR 180 48. AirRobotAR 100 49. AirRobotAR200 50. Air-X 51. Align M690 

### 52. Altavian Nova 53. AltavianNova F6500 54. AltavianNovaR8400 55. Altus X-4 56. Altus X-8 

### 57. American

### Drones, LLC Eagle 58. Apprentice 59. Arch Aerial OCTOmulti-rotorUAS 

### 60. Arris hexacoper 61. AR-960 Hex Rotor 62. AR-540 QuadRotor 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 AircraftLC04 70. Auburn Trimble UX5 71. Auburn WarEagle 

### 72. Auburn EasyStar 73. Auburn 74. AV44 75. Bixler3DR 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. 

# ceo w/WkrnM 

### 86. Chameleon Pro 87. CinesStar 

### 88. Cinestar 6 89. Cinestar X8 90. Cinestar 8 91. Cinestar 8 HL 92. Cinestar 8 Okto XL 93. Coaxial Quad Multirotor VAOl-Vl 94. Coaxial Quad MultirotorVA02-V295. CopelandRED LLC Delta Wing Aircraft 96. CyberQuad Maxi 97. DJl Flame Wheel F450 98. DJI Flame Wheel F550 99. DAx8 100. DJllnspire I01. DJ!lnspire I I02. DJI Inspire 2 103. DJI M P330z I04. DJI Phantom 105. DJI Phantom I I06. DJI Phantom 2 107. DJI Phantom 2+ 

### 108. DJI Phantom 2 Vision 109. DJI Phantom 2 Vision+ 110. DJI Phantom Vision+ Ill. DJI Phantom 3 112. DJI Phantom FC40 113. DJI Spreading Wings S900 114. DJI Spreading Wings SlOOO 115. DJl Spreading Wings S1 000+ 116. DJI S800 117. DJI S800 EVO 118. DJI T600 

### 119. Draganflyer Guardian 120. Draganflyer X4ES 121. Draganflyer X4P 122. DraganflyerX6 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 Fly 6 

### 132. FirstAerial Responder UAV 133. Flame Wheel G4 7.8 Skycrane 134. Flying-Cam 3.0 SARAH 135. FoxtechKraken 130 V2 136. FreeF!y Systems ALTA RTF 

### 137. FreeFly Systems OctocopterAirframe (Legacy) 138. G4 139. G4 models 

### 140. GeoStar 141. GerMAP G220 142. GerMAP G180143. 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-lll 152. HexaCrafter HC-1100 85. 153. HexaCrafterH0-1250 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 16l.ldentifiedSystem 162. lMT Global xFold Cinema 163. Indago 

### 164. InovalDrone:Inova One 165. lnstantEye Mk-2 166.lnstantEye Mk-2 Gen2 

### 167. Intuitive Aerial Aeragon 168. Kl30 Octocopter 169. KongCopterX8 

### 170. Kopterworx Hammer Xl2 171. Latitude HQ-4 HybridMultirotor 172. LB700 

### 173. Leading Edge Precision Vision 10 

### 174. Leptron Avenger 175. Lewis Realty Associates Hexacopter 650 176. Liberty I 177. Lockheed Martin Desert Hawk 

### lli 178. Lockheed Martin Indago 

### 179. Matrix quad copter 180. MaxFlight 181. MD4-200 182. MD4-1000 183. Mikrokopter2.5 184. MLB Company Super Bat 185. MU-IH 186. Multirotor G4 7.8 Skycrane 187. Nighthawk 188. NighthawkVTOL 189. OktoXL 6Sl2 190.PAGX4191. Parksone RadianRTF 

### 192. Panot Bebop drone 193. Parrot PF 725100 Bebop Drone 14MP 194. Parrot Skycontroller 195. PatriotX4 196. PatriotX8 

### 197. Finwing Penguin V2 

### 198. BirdseyeviewFireFly 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 3 5 213. Pulse Vapor 214. Puma AE DDL 215. PV 14817 Multi Rotor 216. PV HLl 217. PV HL2 218. Ql 219. Quadcopter LLC MikroKopter 220. QuietUA V 221. Qube 

### 222. RIC

### 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. RJTEWING Z3 Spade 47" 231. Ritewing Drake 60" 232. RJTEWING Z3 Spade 70" 233. RJTEWING Z4 Spade 52" 234.RMAX 235. Roboflight 

### 236. Rotomotion SR-15 237. RVJet238. ScoutX4 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 8v.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 

### 262. Steadidrone Mavik 263. SuperXIP2 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 Tl5 C/F Folding Octocopter 275. Tarot Tl8 UAV 276. TarotT690 277. TarotT810 278. Tarot T960 

### 279. Tarsier Systems MoAC 280. Tayzu Robotics Titan X8 281. TBS Discovery Pro 282. TeamBlack Sheep Discovery Pro Tarot Tl5 283. T-Rex 700E F3C 284. TREX 800E DFC PRO 285. Trimble UX5286. Trimble UX5 hp 287. Trimble ZX5 288. Tumingy Talon 500 289. TUP XS-800 290. Turbo Ace CINEWING 6 

### 291. TurboAce Matrix·G quadcopter 292. Turbo Ace matrix-E 293. Turbo Ace MATRJX-1 294. UAV Solutions Phoenix 60 

### 295. Universeye Penguin 296. Unmanned Flying Rolling Orb "UFRO" 297. US2 GreenHawk 298. UtiliCopter 1TX8 299. VA03-vl 300. VA04-vl 301. VA07-v1 302. Viking UAS Multicopter (VTOL) 303. Viking UAS FF-X4/X8 304. VK-Patriot X4/X8 305. Viking UAS PatriotX4/X8 Multirotor 306. Viking UAS X6 Model 800 307. Viking UAS Viking ONE 308. VK-450 309. Viking Unmanned Aerial Systems, LLC AgriView VKRanger EX 310. Viking VK-FF-X4 311. VK- Ranger EX- SARFixed Wing UAS 

### 312. Volantex Raptor Tarot T-18 313. Volt Aerial Robotics Octane 314. Vulcan frame controlledby a DJl A2 flight controller 315. VulcanMantis 

### 316. Vulcan Octocopter 317. Vulcan Raven 318. Vulcan UAV 319. WalkeraTALIH500 320. Walkera ScoutX4 321. Wookong DJ15800 322. xCe1 Drones XD550CDR 323. XFold Rig 

### with four configurations: Quadcopter, Hexcopter, Octocopter and xl2 Copter 324. X8-M