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 behalf of AgTech Enterprises, Inc. under Section 

333 of the FAA Modernization and Reform Act of 2012 and 14 C.F.R. Part 11 to allow commercial 

operations of unmanned aircraft for precision aerial survey. 

We here at AgTech request that you consider this request for summary grant based up on the 

companls two (2) existing 333 exemptions (Exemption No. 11573 and 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 of aircraft presently at issue. 

Should you or your staff have any questions, please contact the undersigned. Thank you for your time 

and consideration. 

Jon Tull, CEO 

Enclosures 
September 15,2015 

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington, DC 20590 

Re: Exemption Request Under Section 333 of the FAA Reform Act and Part 11 of the Federal 

Aviation Regulations 

Dear Madam, Sir, 

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the "Reform Act") 

and 14 C.F.R. Part ll, AgTech Enterprises, Inc. ("AgTech") an operator of the Unmanned 

Aircraft Systems (collectively, the "Craft") seeks an exemption from the Federal Aviation 

Regulations ("F ARs") listed below: 

• 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 

• 14CFR91.151(a) 

• 14 CFR 91.203(a) & (b) 14 CFR 91.405(a) 

• 14 CFR 407(a)(l) 14 CFR 409(a)(2) 14 CFR 417(a) & (b) 

The requested exemption would authorize commercial 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 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. 

1. 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 §40 101 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 §4470l(f). See also 49 

USC §44711(a); 49 USC §44704; 14 CFR 91.203(a)(l). 
Section 333(b) of the 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 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 detennines 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." ld. 333(c). 

2. APPLICATIONS AND PUBLIC INTEREST 

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. Ag Tech 

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 under the 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. APPLICABLE LEGAL STANDARD UNDER SECTION 333 

a. Crafi Description 

AgTech seeks to commercially operate a variety ofUAS weighing less than 55 pounds including 

payload in the United States for the purpose of acquiring 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 of Safety 

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 of safety 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 of individuals will have consented to being filmed 

or otherwise they will be made anonymous. 

d. 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. 

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 of any other aircraft 

will require a new petition or a petition to amend this exemption. 

2. Operations for the purpose of closed-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 of no more than 400 feet above ground level 

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

5. The UA must be operated within visual line of sight (VLOS) of the 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 within the 

visual line of sight (VLOS) of the 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 or texting is 

not permitted during flight operations. The PIC must be designated before the flight and 

cannot transfer his or her designation for the duration of the flight. The PIC must ensure 

that the VO can perfom1 the duties required of the 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 between the 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. If the 

operator determines that any update or revision would affect the basis upon which the 

FAA granted this exemption, then the operator must petition for an amendment to its grant 

of exemption. The FAA's UAS Integration Office (AFS-80) may be contacted if questions 

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 of a 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 not pose an undue hazard to persons and property. 

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. If the inspection 

reveals a condition that affects the safe operation of the UAS, the aircraft is prohibited 

from operating until the necessary maintenance 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. Under this grant of exemption, a PIC must hold 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, a territory, a possession, or the 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 on his or her pilot 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 of this 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 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 F AAR 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 must be made available to the Administrator or any law 

enforcement official upon request. 

17. The UA may 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 UA must return to a preR 

detennined location within the private or controlledRaccess property. 

19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies. 

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 

recommended by the manufacturer if greater. 

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 of the 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 operator to ensure the safe operation and flight of the 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 operated by the PIC from any moving device or vehicle. 

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 of an 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 of the 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 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. 

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

persons under this 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 to be conducted. 

28. Any incident, accident, or flight operation that transgresses the lateral or vertical 

boundaries of the 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 of the criteria provided in Section 333 of the Reform Act of 2012 - size, weight, 

speed, operating capabilities, proximity to airports and populated areas, and operation within 

visual line of sight and national security- provide more than adequate justification for the grant of 

the requested exemptions allowing commercial operation of applicant's Craft for the Purposes 

outlined herein and are consistent with exemptions 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 of this exemption would thereby enhance 

safety and fulfill the Secretary of Transportation's (the FAA Administrator's) responsibilities 

under Section 333(c) of the Reform Act to "establish requirement for the safe operation of such 

aircraft systems in the national airspace system." 

Your~~~ 

~<:CV ' 

Jon Tull, CEO 

AgTech Enterprises, Inc. 
APPENDIX A: EXEMPTION REQUEST AND EQUIVALENT LEVEL OF SAFETY 

SHOWINGS UNDER APPLICABLE RULES SUBJECT TO EXEMPTION 

AgTech requests an exemption from the following regulations as well as any additional 

regulations that may technically apply to the operation of the Craft: 

14 CFR Part 21. Subpart H: Airwurthiness certificates 

Subpart H, establishes the procedural requirements for the issuance of ainvorthiness certificates as 

required by FAR §91.203(a)(l). Given the size and limited operating area associated with the 

aircraft to be utilized by AgTech, 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 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. 

AgTech 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 AgTech 

contemplates operating, should this exemption be granted, no FAA regulatory standard will exist 

for detennining 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 91.1 03: 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 91.1 09: 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 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 of the UAS as 

well as the location where it is operated. No flight will be taken without the pennission 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 

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 

with helicopters and other conventional aircraft operating at or below 500 feet AGL. In addition, 

the low-altitude operations of the VAS will ensure separation between these VAS 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 crmsmg 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)(!) 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. 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 conduct pursuant to this 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 CFR 91.203(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 at the grmmd 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)(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 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 AgTech. 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. 
APPENDIX B: LIST OF CRAFT INCLUDED WITHIN PETITION 

l. AgEagle 

2. 3D Robotics Aero-M 

3. 3D Robotics Iris 

4. 3D Robotics Iris+ 

5. 3D Robotics X8 

6. 3D Robotics Fixed Wing 

7. 3DRobotics Multirotor 

8. 3DRobotics Quadrotor 

9. 3DR Solo 

10. 3DR Spektre 

11. 3DRobotics Spektre Industrial Multi-Rotor Aerial Vehicle 

12. 3D Robotics Solo 

13. 3DRobotics X8+ 

14. 3D Robotics X8-M 

15. 3D Robotics Y6 

16. Aerial Mob Heavy Lifter 

17. Aerial Mob Light Lifter 

18. Aerial Remote Mineral Detection System (ARMDS) 

19. Aerialtronics Zenith with intergrated Airware system 

20. Aerialtronics Altura Zenith ATX8 

21. Aerigon 

22. Aerobo 

23. AeroCine Kopterworx Hammer X12 

24. Aeromao AeroMapper 300 

25. Aeromao Talon 

26. Aerornao Aeromapper 300 

27. Aeromao Aeromapper EV -2 

28. AeroVironment Shrike 

29. AeroVironment Puma 

30. Aeronavics X4 Titanium 

31. Aeryon Sky Ranger 

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

33. Aero-M 

34. Aeryon Scout 

35. Aeryon SkyRanger 

36. AgEagle 

37. AgEagle Robotic 

38. AgScout 

39. AgScout Mini 

40. Agribotix Hornet Drone 

41. Agribotix Enduro Quad 

42. AgriView VK Ranger EX 

43. Aibot 

44. Aibotix X-6 

45. Air Rover AR-3000 

46. AirCover QR-425s 
47. AirRobotAR 180 

48. Air Robot AR 100 

49. Air Robot AR200 

50. Air-X 

51. Align M690 

52. Altavian Nova 

53. Altavian Nova F6500 

54. Altavian Nova R8400 

55. Altus X-4 

56. Altus X-8 

57. American Drones, LLC Eagle 

58. Apprentice 

59. Arch Aerial OCTO multi-rotor UAS 

60. Arris hexacoper 

61. AR-960 Hex Rotor 

62. AR-540 Quad Rotor 

63. ARF-MikroKopter OktoXL 

64. ARF-MikroKopter OktoXL + 

65. ArrowLite 

66. AscTec Falcon 

67. AscTec Falcon 8 

68. Astraeus Aerial Cinema System V.3CS 

69. Atlantic RC Aircraft LC04 

70. Auburn Trimble UX5 

71. Auburn War Eagle 

72. Auburn EasyStar 

73. Auburn 

74. AV44 

75. Bixler 3DR Plane 

76. Blade 350QX 

77. Bixler 2 

78. Boomerang Carbon Fiber Frame (The Identified System) 

79. Bormatec Maja UAV 

80. BOSH Technologies Super Swiper 

81. Bumblebee-S 

82. C-Astral Bramor gEO 

83. CarbonCore Octocopter 1000 

84. Carbon Core Cortex Quadcopter 

85. ceo w/Wkrn M 

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 Multirotor V A02-V2 
95. CopelandRED LLC Delta Wing Aircraft 

96. CyberQuad Maxi 

97. DJl Flame Wheel F450 

98. DJI Flame Wheel F550 

99. DAx8 

100. DJllnspire 

I 01. DJ!lnspire I 

I 02. DJI Inspire 2 

103. DJI M P330z 

I 04. DJI Phantom 

105. DJI Phantom I 

I 06. 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 S 1 000+ 

116. DJI S800 

117. DJI S800 EVO 

118. DJI T600 

119. Draganflyer Guardian 

120. Draganflyer X4ES 

121. Draganflyer X4P 

122. Draganflyer X6 

123. DT-18 

124. DYS D800-X8 

125. Eagle VTOL 

126. Eagle V2 

127. E-Flite Apprentice 

128. Event 38 E384 

129. F-450 

130. Falcon VTOL 

131. Fire Fly 6 

132. First Aerial Responder UA V 

133. Flame Wheel G4 7.8 Skycrane 

134. Flying-Cam 3.0 SARAH 

135. Foxtech Kraken 130 V2 

136. FreeF!y Systems ALTA RTF 

137. FreeFly Systems Octocopter Airframe (Legacy) 

138. G4 

139. G4 models 

140. GeoStar 

141. GerMAP G220 

142. GerMAP G180 
143. goFarm GF-1 

144. Gryphon Dynamics X8 

145. GT80X 

146. Harris 18 HL 

147. HEFF 

148. Helicopters West DJI Inspire 

149. Helicopters West SkyJib 8 

150. Helios 960 

151. Hawkeye Mk-lll 

152. HexaCrafter HC-1100 85. 

153. HexaCrafter H0-1250 

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.ldentified System 

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. KongCopter X8 

170. Kopterworx Hammer Xl2 

171. Latitude HQ-4 Hybrid Multirotor 

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. Mikrokopter 2.5 

184. MLB Company Super Bat 

185. MU-IH 

186. Multi rotor G4 7. 8 Skycrane 

187. Nighthawk 

188. Nighthawk VTOL 

189. OktoXL 6Sl2 

190.PAGX4 
191. Parksone Radian RTF 

192. Panot Bebop drone 

193. Parrot PF 725100 Bebop Drone 14MP 

194. Parrot Skycontroller 

195. Patriot X4 

196. Patriot X8 

197. Finwing Penguin V2 

198. Birdseyeview FireFly 6 

199. Phoenix 

200. Phoenix VTOL 

201. Phoenix 60 

202. Phoenix 60LE 

203. Pixhawk 

204. Precision Drone Pacesetter 

205. PrecisionHawk 

206. PrecisionHawk Hawkeye Mk-III 

207. PrecisionHawk Lancaster 

208. Precision Lancaster MK3 

209. Prioria Hex 

210. Prioria's Maveric 

211. Pulse Aerospace, P A 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. Quiet UA 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. RV Jet 
238. Scout X4 

239. SD02 

240. Seahawk 1.2 

241. SelectTech Geospacial's EH-4 

242. SenseFly eBee 

243. SenseFly eBee RTK 

244. SenseFly eXom 

245. Sensurion Magpie MP-1 

246. Service-Drone Recon One 

24 7. Service-Drone Blackbird 

248. SH 900 

249. ShadowHawk 

250. Shrike 

251. Sirius 

252. SkyCatch 

253. SkyJib 8 v.2 Heavy Lifter 

254. SkyPhilly MI 

255. Skywalker Aero 

256. Skywalker Flying Wing X8 

257. SnapRoll Media SUAS 

258. Solutions Phoenix 30 

259. SteadiDrone 

260. Steadidrone Quad 

261. Steadydrone QU4D 

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. Tarot T690 

277. Tarot T810 

278. Tarot T960 

279. Tarsier Systems MoAC 

280. Tayzu Robotics Titan X8 

281. TBS Discovery Pro 

282. Team Black Sheep Discovery Pro Tarot Tl5 

283. T-Rex 700E F3C 

284. TREX 800E DFC PRO 

285. Trimble UX5 
286. 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 Patriot X4/X8 Multirotor 

306. Viking UAS X6 Model 800 

307. Viking UAS Viking ONE 

308. VK-450 

309. Viking Unmanned Aerial Systems, LLC AgriView VK Ranger EX 

310. Viking VK-FF-X4 

311. VK- Ranger EX- SAR Fixed Wing UAS 

312. Volantex Raptor Tarot T-18 

313. Volt Aerial Robotics Octane 

314. Vulcan frame controlled by a DJl A2 flight controller 

315. Vulcan Mantis 

316. Vulcan Octocopter 

317. Vulcan Raven 

318. Vulcan UAV 

319. WalkeraTALIH500 

320. Walkera Scout X4 

321. Wookong DJ15800 

322. xCe1 Drones XD550CDR 

323. XFold Rig with four configurations: Quadcopter, Hexcopter, Octocopter and xl2 Copter 

324. X8-M