Shenandoah Aviation, LLC 

Attn. Dianna Klein, Founder and President 

27514 Chris Ridge Ct. 

Spring, TX 77386 

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington DC 20590 

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

Aviation Regulations from: 14 CPR 21 subpart H; 14 CPR 45.23(b); 14 CPR 61.113(a) and (b); 14 CPR 

91.7(a); 14 CPR 91.9(b)(2); 14 CPR 91.103; 14 CPR 91.109; 14 CPR 91.119(c); 14 CPR 91.121; 14 CPR 

91.151(a); 14 CPR 91.203 (a) and (b); 14 CPR 91.405 (a); 14 CPR 91.407 (a) (1) 14 CPR 91.409 (a)(l) 

and (2); 14 CPR 91.417(a) and (b) 

Dear Sir or Madam: 

Pursuant to Section 333 of the FAA Modernization and Reform Act of2012 (the "Reform Act") and 14 

CPR Part 11, Shenandoah Aviation, LLC, LLC operator of an Unmanned Aircraft System (U AS), hereby 

applies for an exemption from the listed Federal Aviation Regulations ("PARs") to allow commercial 

operation of its UAS, 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 ofUAS, the requested exemption 

would permit the operation of U AS platforms previously approved by the FAA for commercial operations 

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: 

Shenandoah Aviation, LLC 

Attn: Dianna Klein, President 

Phone: 540-664-7185 

Email: dianna@shenandoahaviati on.com 

Address: 27514 Chris Ridge Ct., Spring, TX 77386 

Regulations from which the exemption is requested: 

14 CPR Part 21 subpart H 

14 CPR 45.23 (b) 

14 CPR 6 1. 113 (a) & (b) 

14 CPR 91.7 (a) 

14 CPR 91.9 (b) (2) 

14 CPR 91.103 

14 CPR 91.109 
14 CFR 91.119 (c) 

14 CFR 91.121 

14 CFR 91.151 (a) 

14 CFR 91.203 (a) & (b) 

14 CFR 91.405 (a) 

14 CFR 91.407 (a) (1) 

14 CFR 91.409 (a) (2) 

14 CFR 91.417 (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)(l). 

Section 333(b) of the Reform Act assists the Secretary in determining whether UAS may 

operate in the national airspace system without creating a hazard to the user, the public, 

or a threat to national security. In making this determination, the Secretary must consider: 

• The UAS' size, weight, speed and operational capability; 

• Whether the UAS operates within the visual line of sight of the operator; 

• Whether the UAS operates outside of highly populated areas and away from close 

proximity to airports. 

Reform Act 333(a). If the Secretary determines that a UAS "may operate safely in the 

national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft 

in the national airspace system." Id. 333 (c). 

UAS AND OPERATIONAL DESCRIPTION 

The operation limitations proposed for an equivalent or higher level of safety because operations will 

further enhance the safety of the persons and/or property using conventional aircraft. 

As the operator ofthese aircraft, Shenandoah Aviation, LLC is committed to the following conditions and 

limitations on its operations. Shenandoah Aviation, LLC understands that failure to comply will be 

grounds for the immediate suspension or rescission of any exemption granted. 

1. Operations are limited to the UAS listed in the Appendix when weighing less than 

55 pounds including payload. 

2. Operations for the purpose of closed-set motion picture and television filming are 

not contemplated. 

3. 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. 

4. 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. 

5. The aircraft will be operated within visual line of sight (YLOS) 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. 

6. All operations will utilize a visual observer (YO). The aircraft will be operated 

within the visual line of sight (YLOS) of the PIC and YO at all times. 

7. All operating documents needed to operate the UAS and will be accessible during 

VAS 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. 

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, 

will undergo a functional test flight prior to conducting further operations. 

9. Shenandoah Aviation, LLC 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 will conduct a pre-flight inspection and determine the 

VAS is in a condition for safe flight. 

11. Shenandoah Aviation, LLC 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. Shenandoah Aviation, LLC 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 consistent with 14 CFR § 61.5l(b). Shenandoah Aviation, 

LLC will operate flights for the purposes of training Shenandoah Aviation, LLC's PICs and YOs 

(training, proficiency, and experience building) and determining the PIC's ability to safely 

operate the UAS. 

15. U AS operations will not be conducted during night, as defined in 14 CFR § 1.1. 

All operations will be conducted under visual meteorological conditions (YMC). 
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 U AS loses communications or loses its GPS signal, the aircraft will return 

to a pre-determined 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 A TO-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 Shenandoah Aviation, LLC 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 National Transportation Safety Board (NTSB) per instructions 

contained on the NTSB Web site: www.ntsb.gov. 

DESCRIPTION OF SPECIFIC REGULATIONS 

C.P.R. Part 21, Subpart H: Airworthiness Certificates 14 C.P.R. §91.203 (a) (1) 

Subpart H, entitled Airworthiness Certificates, 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 the Applicant, 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 U.S.C.§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 (fixed wing or rotorcraft) operating with an airworthiness certificate 

without the restrictions and conditions proposed. The UAS to be operated here under is less than 55 lbs. 

fully loaded, carries neither a pilot nor passenger, carries no explosive materials or flammable liquid 

fuels, and operates exclusively within a secured and designated area. Unlike other civil aircraft, 

operations under this exemption will be tightly controlled and monitored by both the operator and under 

the requirements and in compliance with local public safety requirements. These safety enhancements 

provide a greater degree of safety to the public and property owners than conventional operations 

conducted with airworthiness certificates issued under 14 C.F .R. Part 21, Subpart H. 

Lastly, application of these same criteria demonstrates that there is no credible threat to national security 

posed by the UAS, due to its size, speed of operation, location of operation, lack of explosive materials or 

flammable liquid fuels, and inability to carry a substantial external load. 

14 C.P.R. § 45.23 (b). Marking of the aircraft 

This regulation requires that certain limited, restricted or light-sport category aircraft or experimental or 

provisionally certificated aircraft must be marked with letters not less than 2 inches nor more than 6 

inches high, the words "limited," "restricted," "light-sport," "experimental," or "provisional," as 

applicable. 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, two-inch lettering will be impossible. Shenandoah Aviation, 

LLC will mark the UAS as practical. 

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 ofthe UAS as requested exceeds the present level of safety achieved by 

14 CFR 61.113(a) and (b). 

14 C.F.R. §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, should this exemption be granted, no FAA 

regulatory standard will exist for determining airworthiness. Given the size of the aircraft for maintenance 

and use of safety checklists prior to each flight an equivalent level of safety will be provided. 

14 C.F.R. § 91.9 (b) (2): Civil aircraft flight manual in the aircraft 

Section 91.9 (b) (2) provides: No person may operate a U.S.-registered civil aircraft ... (2) For which an 

Airplane or Rotorcraft Flight Manual is not required by §21.5 of this chapter, unless there is available in 

the aircraft a current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, 

and placards, or any combination thereof. 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 flight manual at the ground control point where the pilot flying the UAS will 

have immediate access to it. 

14 C.F.R. § 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 C.F.R. §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. UAS and remotely 

piloted aircraft, by their design 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 FAA 

has approved exemptions for flight training without fully functional dual controls for a number of aircraft 

and for flight instruction in experimental aircraft. The equivalent level of safety provided by the fact that 

neither a pilot nor passengers will be carried in the aircraft and by the size and speed of the aircraft. 

14 C.F .R. §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 ofthe UAS as well as the 

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

permission of the property owner. Because advance notice to the property owner and any 

onsite personnel, as well as the precautions outlined below, all affected individuals will 

be aware 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 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 C.F.R. §91.121 Altimeter settings 

This regulation requires each person operating an 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 operator, pursuant to 

the safety check list and live flight data monitoring, confirming the altitude of the launch site shown on 

the GPS altitude indicator before flight. 

14 C.F.R. § 91.15l(a): Fuel requirements for flight in VFR conditions 

Section 91.15l(a) outlines fuel requirements for beginning a flight in VFR conditions. 

Relief from Section 91.15l(a)(l) is requested to the extent required to allow flights of a 

variety ofUAS during daylight hours in visual flight rules (VFR) conditions to continue 

until 90 percent of remaining battery power or fuel reserves remain. Shenandoah Aviation, LLC seeks the 

requested relief because without an exemption from Section 91.15l(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 Shenandoah Aviation, LLC proposes to conduct pursuant to this 

Petition. 

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

Shenandoah Aviation, LLC's proposed operating limitations, ensure that Shenandoah Aviation, LLC will 

safely operate the selected aircraft during daylight hours in VFR conditions until 90 percent of remaining 
battery power or fuel reserves remain. 

14 C.F.R. §91.203 (a) and (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 C.F.R. §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 4 3 of this chapter ... ," and 

others shall inspect or maintain the aircraft in compliance with Part 43. 

Given that these section and Part 43 apply only to aircraft with an airworthiness certificate, these sections 

will not apply to the applicant. 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 ofUASs 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 

Shenandoah Aviation, LLC 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 ofthe UAS involved and the restricted environment within which they will operate, 

our petition presents no national security issue. 

ADDITIONAL INFORMATION 

Dianna Klein has been involved in numerous facets of aviation including Part 91 and 141 flight 

instruction, Part 135 charter operations, Part 121 airline operations at the regional and major 

level, and as an officer and pilot in the United States Air Force. She is currently a B-787 pilot for 

a major U.S. airline and holds type ratings in the BE-400 and the B-737. 

Dianna holds a Master of Science in Aeronautical Science degree with a dual specialization in 

Aviation Safety and Human Factors from Embry-Riddle Aeronautical University-Daytona 

Beach. Additionally, she is a graduate of the MITRE Corporation's Aviation Safety Management 

Systems Principals course. 

Dianna has held several Flight Operations positions at her airline, including B-73 7 

Instructor/Evaluator, Project Manager, and Flight Manager. Prior to flying for a major U.S. 

airline, Dianna flew the EMB-145 for a large U.S. regional airline, and was also a Captain on a 

King Air C90 for a Part 135 operator. Also, she flew the C-5 Galaxy in support of combat 

operations during Operations Iraqi and Enduring Freedom for both the USAFR and Air National 

Guard. 

FEDERAL REGISTER SUMMARY 

Docket No.: No. FAA-2015-

Petitioner: Shenandoah Aviation, LLC, LLC 

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)(l), 409(a)(2), 417(a) and (b) of 

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

Description of Relief Sought: Shenandoah Aviation, LLC is seeking an exemption to conduct commercial 

acquisition of aerial data using unmanned aircraft systems. 

Sincerely, _) =::~- {-1. ({e._. 

Dianna Klein 

Founder and President 

Shenandoah Aviation, LLC 

27514 Chris Ridge Ct. 

Spring, TX 77386 
Appendix 

1. 2AgEagle 

2. 3D Robotics Aero-M 

3. 3D Robotics Iris 

4. 3D Robotics Iris+ 

5. 3D Robotics X8 

6. 3DRobotics Fixed Wing 

7. 3DRobotics Multirotor 

8. 3DRobotics Quadrotor 

9. 3DR Solo 

10. 3DR Spektre 

11. 3DRobotics Spektre Industrial Multi-Rotor Aerial Vehicle 

12. 3D Robotics Solo 

13. 3DRobotics X8+ 

14. 3D Robotics X8-M 

15. 3D Robotics Y6 

16. Aerial Mob Heavy Lifter 

17. Aerial Mob Light Lifter 

18. Aerial Remote Mineral Detection System (ARMDS) 

19. Aerialtronics Zenith with intergrated Airware system 

20. Aerialtronics Altura Zenith ATX8 

21. Aerigon 

22. Aerobo 

23. AeroCine Kopterworx Hammer X 12 

24. Aeromao AeroMapper 300 

25. Aeromao Talon 

26. Aeromao Aeromapper 300 

27. Aeromao Aeromapper EV -2 

28. Aero Vironment Shrike 

29. Aero Vironment 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. AirRobot AR 180 

48. AirRobot AR 1 00 

49. AirRobot AR200 

50. Air-X 

51. Align M690 

52. Altavian Nova 

53. Altavian Nova F6500 

54. Altavian Nova R8400 

55. Altus X-4 

56. Altus X-8 

57. American Drones, LLC Eagle 

58. Apprentice 

59. Arch Aerial OCTO multi-rotor UAS 

60. Arris hexacoper 

61. AR-960 Hex Rotor 

62. AR-540 Quad Rotor 

63. ARF-MikroKopter OktoXL 

64. ARF-MikroKopter OktoXL + 

65. ArrowLite 

66. AscTec Falcon 

67. AscTec Falcon 8 

68. Astraeus Aerial Cinema System V.3CS 

69. Atlantic RC Aircraft LC04 

70. Auburn Trimble UX5 

71. Auburn War Eagle 

72. Auburn EasyStar 

73. Auburn 

74. AV44 

75. Bixler 3DR Plane 

76. Blade 350QX 

77. Bixler 2 

78. Boomerang Carbon Fiber Frame (The Identified System) 

79. Bormatec Maja UA V 

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