Shenandoah Aviation, LLC Attn. Dianna Klein, Founder and President 27514 Chris Ridge Ct. Spring, TX 77386 U.S. Department ofTransportation Docket Management System 1200 New Jersey Ave., SE Washington DC 20590

Re: Exemption Request Pursuantto Section 333 ofthe FAA Reform Act and Part 11 ofthe Federal Aviation Regulations from: 14 CPR 21 subpartH; 14 CPR45.23(b); 14 CPR 61.113(a) and (b); 14 CPR 91.7(a); 14 CPR 91.9(b)(2); 14 CPR91.103; 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 CPR91.409 (a)(l) and (2); 14 CPR 91.417(a) and (b)
Dear Sir orMadam:

Pursuantto Section 333 ofthe FAAModernization and Reform Act of2012 (the "Reform Act") and 14 CPRPart 11, ShenandoahAviation, LLC, LLC operator ofan Unmanned Aircraft System (UAS), hereby applies for an exemption from the listed Federal Aviation Regulations ("PARs") to allow commercial operation ofits UAS, so long as such operations are conducted within and under the conditions outlined herein oras may be established by the FAA.
As detailed in this document and the attached Appendix ofUAS, therequested exemption would permitthe operation ofUAS platforms previously approved by the FAA for commercial operations in the United States. Approval ofthis exemption would thereby enhance safety and fulfill the Secretary of Transportation's responsibilities to "

...establish requirements for the safe operation ofsuch aircraft systems in the national airspace system." Section 333(c)Reform Act.
The name and address ofthe applicant is:
Shenandoah Aviation, LLC Attn: Dianna Klein, President Phone: 540-664-7185 Email: dianna@shenandoahaviation.com Address: 27514 Chris Ridge Ct., Spring, TX 77386
Regulations from which the exemption is requested:
14 CPR Part21 subpartH 14 CPR45.23 (b) 14 CPR 61. 113 (a) & (b) 14 CPR 91.7 (a) 14 CPR91.9 (b) (2) 14 CPR 91.103 14 CPR 91.10914 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 ofthe Act, including UAS, from the requirement that all civil aircraftmusthave a current airworthiness certificate. The Administrator may grant an exemption from a requirement ofa regulation prescribed under subsection (a) or(b) ofthis section or any sections §44702-44716 ofthis title ifthe 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) ofthe Reform Act assists the Secretary in determining whetherUAS 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; • Whether the UAS operates within the visual line ofsight ofthe operator; • Whether the UAS operates outside ofhighly populated areas and away from close proximity to airports. Reform Act 333(a). Ifthe Secretary determines 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." Id. 333 (c).
UASAND OPERATIONAL DESCRIPTION
The operation limitations proposed for an equivalent orhigher level ofsafety because operations will further enhancethe safety ofthe persons and/orproperty 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 thatfailure to comply will be grounds for the immediate suspension orrescission ofany 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 ofclosed-set motion picture and television filming are not contemplated. 3. The aircraft will not be operated at a speed exceeding 87 knots (100 miles perhour). In no case will the aircraftbeoperated atairspeeds greaterthan the maximum aircraft operating airspeed recommended by the aircraft manufacturer.
4. The aircraft will be operated at an altitude ofno more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL.
5. The aircraft will be operated within visual line ofsight (YLOS) ofthe Pilotin Command (PIC) at all times. This requires the PIC to be able to use human vision unaided by any device otherthan 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 ofsight (YLOS) ofthePIC and YO at all times.
7. All operating documents needed to operatetheUAS and will be accessible during 

### VAS operations and made available to the Administrator upon request. The operator will also present updated and revised documents ifitpetitions for extension or amendment.
8. Any UAS that has undergone maintenance oralterations that affectthe UAS operation orflight characteristics, e.g. replacement ofa flight critical component, will undergo a functional testflight priorto conducting further operations.
9. Shenandoah Aviation, LLC is responsible for maintaining and inspectingtheUAS to ensure that it is in a condition for safe operation.
10. Priorto each flight, the PIC will conduct a pre-flight inspection and determinethe 

### 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. EachUAS operated underthis 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 ofColumbia, PuertoRico, a territory, a possession, orthe Federal government. 14. Shenandoah Aviation, LLC will notpermit any PICto operate unless the PIC demonstrates the ability to safely operatethe UAS in a mannerconsistent with how the UAS will be operated to acquire aerial data, includingevasive 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 consistentwith 14 CFR § 61.5l(b). Shenandoah Aviation, LLC will operate flights for the purposes oftraining Shenandoah Aviation, LLC's PICs and YOs (training, proficiency, and experience building) and determiningthe PIC's ability to safely operate the UAS. 15. UAS operations will notbe 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 ofan airportreference point (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) orfor airports not denoted with an ARP, the center ofthe airport symbol as denoted on the currentFAA-published aeronautical chart, unless a letter ofagreement with that airport's management is obtained or otherwise permitted by a COA. 17. The aircraftwill not be operated less than 500 feet below orless than 2,000 feet horizontally from a cloud orwhen visibility is less than 3 statute miles from the PIC. 18. Ifthe UAS loses communications orloses its GPS signal, the aircraft will return to apre-determined location. 19. The PIC will abortthe flight in the event ofunpredicted obstacles oremergencies. 20. The PIC will be prohibited from beginning a flight unless (considering wind and forecast weather conditions) there is enough availablepowerorfuel for the aircraft to conductthe intended operation and to operate after that for at least five minutes orwiththe reserve poweror fuel recommended by the manufacturer if greater. 21. All operations shall be conducted in accordance with an ATO-issued COA ifthe blanket COA does not coverthe intended operation. 22. All aircraft operated will be identified by serial number, registered in accordance with 14 CFRpart47, 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, LLCto ensure the safe operation and flight ofthe UAS and any documents required under 14 CFR §§ 91.9 and 91.203 will be available to thePIC atthe Ground Control Station ofthe UAS any time the aircraft is operating. 24. The aircraftwill 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 orvehicle; however, specificrequests 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 presentthat sufficiently protectnonparticipating persons from the aircraft or debris in the event ofan accident; or b. The owner/controller/operatorofany vessels, vehicles or structures has granted permission for operating closerto those objects and the PIC has made an assessment ofthe risk ofoperating closerto those objects and determined that it does not present an undue hazard. 27. The PIC, VO, operatortrainees or essential persons will not be considerednonparticipating persons underthis exemption. 28. All operations conducted overprivate or controlled-access property will be conducted with the permission from the property owner/controllerorauthorized representative. Permission from property owner/controller orauthorized representative will be obtained for each flight to be conducted. 29. Any incident, accident, orflight operationthat transgresses the lateral orvertical boundaries ofthe 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) perinstructions contained on the NTSB Web site: www.ntsb.gov.
DESCRIPTION OF SPECIFIC REGULATIONS
C.P.R. Part 21, SubpartH: Airworthiness Certificates 14 C.P.R. §91.203 (a) (1) SubpartH, entitled Airworthiness Certificates, establishes the procedural requirements forthe 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 SubpartH meets the requirements ofan equivalent level ofsafety under Part 11 and Section 333 ofthe Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333 ofthe Reform Actboth authorize the FAA to exempt aircraft from the requirementfor an airworthiness certificate, upon consideration ofthe size, weight, speed, operational capability, and proximity to airports and populated areas ofthe particularUAS. In all cases, an analysis ofthese criteriademonstrates that the UAS operated without an airworthiness certificate, in the restricted environment and underthe conditions proposed will be at least as safe, or safer, than a conventional aircraft (fixed wing orrotorcraft) 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 orflammable liquid fuels, and operates exclusively within a secured and designated area. Unlike other civil aircraft, operations underthis 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 ofsafetytothe public and property owners than conventional operations conducted with airworthiness certificates issued under 14 C.F.R. Part 21, SubpartH. Lastly, application ofthese same criteria demonstrates that there is no crediblethreatto national security posed by the UAS, due to its size, speed ofoperation, location ofoperation, lack ofexplosive materials or flammable liquid fuels, and inability to carry a substantial external load.
14 C.P.R. §45.23 (b). Marking ofthe aircraft
This regulation requires that certain limited, restricted or light-sport category aircraft orexperimental or provisionally certificated aircraft must be marked with letters not less than 2 inches normore 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 orpilot station on which the word "Experimental" can be placed. Given the size ofthe UAS, two-inch lettering will be impossible. Shenandoah Aviation, LLC will mark the UAS as practical.
14 CFR 61.113 (a) & (b): Private pilotprivileges and limitations: Pilotin commandSections 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 achievethe equivalent level ofsafety ofcurrentoperations by requiringthe pilot operatingthe aircraftto 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 ofthe UAS are so diminished from the level ofrisk associated with commercial operations contemplated by Part 61 when drafted, that allowing operations oftheUAS as requested exceeds the present level ofsafety 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 ofthe aircraft for maintenance and use ofsafety checklists priorto each flight an equivalent level ofsafety 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) Forwhich an Airplane orRotorcraft Flight Manual is notrequired by §21.5 ofthis chapter, unless there is available in the aircraft a current approved airplane orRotorcraft FlightManual, approved manual material, markings, and placards, orany combination thereof. The UAS, given its size and configurationhas no ability or place to carry such aflight manual on the aircraft, not only because there is no pilot on board, but because there is no room orcapacity to carry such an item on the aircraft. The equivalent level ofsafety will be maintained by keeping the flight manual at the ground control point wherethe pilot flying the UAS will have immediate access to it.
14 C.F.R. 

### § 91.103: Preflight action
This regulation requires eachpilot in command take certain actions before flight to ensure the safety offlight. 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, checkingtakeoffand 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 nothave fully functional dual controls. Flightcontrol is accomplished through the use ofa control box that communicates with the aircraftviaradio communications. The FAA has approved exemptions for flight training withoutfully functional dual controls for a numberofaircraft and for flight instruction in experimental aircraft. The equivalent level ofsafety provided by the fact that neither apilot norpassengers will be carried in the aircraft and by the size and speed ofthe aircraft.
14 C.F.R. §91.119: Minimum safe altitudesSection 91.119 establishes safe altitudes for operation ofcivil 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 ofsafety 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 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-participatingpersons (persons otherthan the pilot in command (PIC) or visual observer (VO)), vessels, vehicles and structures, unless operations do notpresent an undue hazard.
The UAS will remain within visual line ofsight ofthe PIC orVO. 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 ofall operations within 5 miles ofan airport. The FAA will have advance notice ofall operations through the filing ofnotices-to-airmen. Compared to flight operations with aircraft or rotorcraft weighing far more than the UAS proposed herein, any risk associated with ouroperations is far less thanthose presently presented with helicopters and other conventional aircraft operating at orbelow 500 feet AGL. In addition, the low-altitude operations ofthe UAS will ensure separation between these UAS operations and the operations ofconventional 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 altimeterthat is set "

...to the elevation ofthe departure airport or an appropriate altimeter setting available before departure." As the UAS may nothave a barometric altimeter, but instead a GPS altitude read out, an exemption may be needed. Anequivalent level ofsafety will be achieved by the operator, pursuantto the safety check list and live flight datamonitoring, confirmingthe altitude ofthe 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. Relieffrom Section 91.15l(a)(l) is requested to the extent required to allow flights ofa variety ofUAS during daylight hours in visual flight rules (VFR) conditions to continue until 90 percent ofremaining battery power or fuel reserves remain. Shenandoah Aviation, LLC seeks the requested reliefbecause without an exemption from Section 91.15l(a)(l), the flight time duration ofthe selected aircraft will be reduced and severely constrain the practicality of any aerial acquisition ofdata that ShenandoahAviation, LLC proposes to conduct pursuantto this Petition. Thetechnical specifications ofthe proposed UAS, their Operations Manuals, and Shenandoah Aviation, LLC's proposed operating limitations, ensurethat Shenandoah Aviation, LLC will safely operate the selected aircraft during daylight hours in VFR conditions until 90 percent ofremainingbattery power orfuel reserves remain.
14 C.F.R. §91.203 (a) and (b): Carryingcivil aircraft certification and registration
The UAS has no cabin, cockpit orpilot station and is operated without an onboard pilot. Therefore, there is no ability orplace to carry certification and registration documents or to display them on the UAS. An equivalent level ofsafety will be achieved by keeping these documents at the ground control point where the pilot flyingthe UAS will have immediate access to them, to the extentthey are applicable tothe 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 orowner "shall have that aircraft inspected as prescribed in subpartE ofthis part and shall between required inspections, except as provided in paragraph (c) ofthis section, have discrepancies repaired as prescribed in part 4 3 ofthis chapter

...," and others shall inspect ormaintain the aircraft in compliance with Part43.
Giventhatthese section and Part43 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 orOperatingManual. An equivalent level ofsafety will be achieved becausethese UASs are limited in size and will carry a small payload and operate only in restricted areas for limitedperiods oftime. Ifmechanical issues arise, the UAS can land immediately and will be operating from no higherthan 400 feet AGL. The PIC will ensure thatthe UAS is in working orderpriorto initiating flight, perform required maintenance and keep a log ofany maintenance performed. Moreover, the PIC is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy conditionto provide the equivalent level ofsafety. 

### PUBLIC INTEREST Approval ofexemptions allowing commercial operations ofUASs for aerial acquisition ofdata enhances safety while reducing risk. Manned aircraft in certain application such as pipeline monitoring create a greaterrisk 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 exposethem to the risks associated with manned aircraft flights. In addition, additional streams ofaerial data will allow large commercial entities to make decisions abouthow to best deploy ground resources and ensurethe safety and cost-effectiveness oftheiroperations. 

### EQUIVALENT LEVEL OF SAFETY Shenandoah Aviation, LLC proposes thatthe exemption requested herein apply to civil aircraft thathave the characteristics and that operate within the limitations listed herein. These limitations provide for at least an equivalent oreven higher level ofsafety to operations under the current and proposed regulatory structure. 

### PRIVACY All flights will occur overprivate orcontrolled access property with the property owner's prior consent and knowledge. Images or video taken ofindividuals will have consented to being filmed orotherwisethey will be made anonymous. NATIONAL SECURITY Given the small size oftheUAS involved and the restricted environment within whichthey will operate, ourpetition presents no national security issue.
ADDITIONALINFORMATION 

### Dianna Klein has been involved in numerous facets ofaviation including Part 91 and 141 flight instruction, Part 135 charter operations, Part 121 airline operations atthe 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. Diannaholds a Master ofScience inAeronautical Science degree with a dual specialization in Aviation Safety and Human Factors from Embry-Riddle Aeronautical University-Daytona Beach. Additionally, she is a graduate ofthe MITRE Corporation's Aviation Safety Management Systems Principals course. Diannahas held several FlightOperations positions ather airline, including B-737 Instructor/Evaluator, Project Manager, and FlightManager. Priorto 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 ofcombat operations during Operations Iraqi and Enduring Freedom for boththe USAFRand AirNational Guard.

FEDERALREGISTER SUMMARY DocketNo.: 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 ofthe Federal Regulations (14 CFR). Description ofReliefSought: Shenandoah Aviation, LLC is seeking an exemption to conduct commercial acquisition ofaerial 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 LightLifter 18. Aerial Remote Mineral Detection System (ARMDS) 19. Aerialtronics Zenith with intergrated Airware system 20. Aerialtronics Altura ZenithATX8 21. Aerigon 22. Aerobo 23. AeroCine Kopterworx HammerX12 24. Aeromao AeroMapper 300 25. Aeromao Talon 26. Aeromao Aeromapper 300 27. Aeromao AeromapperEV-2 28. AeroVironment Shrike 29. AeroVironmentPuma 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. AgScoutMini 40. Agribotix HornetDrone 41. Agribotix Enduro Quad 42. AgriView VK Ranger EX

### 43. Aibot 44. Aibotix X-6 45. Air RoverAR-3000 46. AirCover QR-425s 47. AirRobotAR 180 48. AirRobot AR 1 00 49. AirRobot AR200 50. Air-X 51. Align M690 52. AltavianNova 53. Altavian NovaF6500 54. Altavian Nova R8400 55. Altus X-4 56. Altus X-8 57. American Drones, LLC Eagle 58. Apprentice 59. Arch Aerial OCTO multi-rotorUAS 60. Arrishexacoper 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 SystemV.3CS 69. Atlantic RC AircraftLC04 70. AuburnTrimbleUX5 71. Auburn WarEagle 72. AuburnEasyStar 73. Auburn 74. AV44 75. Bixler 3DRPlane 76. Blade 350QX 77. Bixler2 78. Boomerang CarbonFiberFrame (The Identified System) 79. Bormatec MajaUAV 80. BOSH Technologies Super Swiper 81. Bumblebee-S 82. C-Astral BramorgEO 83. CarbonCore Octocopter 1000 84. Carbon Core Cortex Quadcopter 85. 

# ceo w/Wkrn 

### M 86. Chameleon Pro