November 22 , 2015 U.S. Department ofTransportation, Docket Operations West Building Ground Floor, Room w12-140 1200 New Jersey Avenue, SE. Washington , DC 20590 Green Tech Coatings P.O. Box 916 Hopland , CA 95449-0916

VIA FEDERAL DOCUMENT MANAGEMENT SYSTEM Re : Exemption request under Section 333 ofthe FAA Reform Act and Part 11 ofthe Federal Aviation Regulations Dear Sir or Madam , Pursuant to Section 333 ofthe FAA Modernization and Reform Act of 2012 (the "Reform Act") and 14 C.F.

### R. Part 11 , Green Tech Coatings seeks an exemption from Federal Aviation Regulations ("FAR's") detailed below for the following described Unmanned Aerial System , called in this application the UA System, which includes an Unmanned Aircraft (UA) and ground station based equipment and crew: THE UNMANNED AIRCRAFT (UA): • A lightweight (15 lb. gross weight with all on-board equipment) UA, manufactured by Walkera- QR X800 and Yuneec- Typhoon 0500 4K that includes the following equipment in flight. An on-board flight computer with GPS navigation and location ability that receives signals for flight controls from a ground based transmitter/controller. An on-board camera capable of capturing imagery in the form offull color, high definition still photos and video. An on-board telemetry system that delivers flight data from the on-board flight computer to the on-board radio transmitter including: AGL, horizontal and vertical speed , compass direction offlight, and direction back to its launch site. 2.4 GHz and 5.8 GHz on-board radio transmitters that transmit live video from the onboard camera, plus all the flight data from the telemetry system described above . THE GROUND STATION-BASED PART OF THE SYSTEM: A Pilot in Command (PIC) in operational control of a flight operation from beginning to end and who controls the UAwhile in the air. A 2.4 GHz radio transmitter/controller operated by the PIC to control the UA while in flight. A radio receiver receiving live video and flight data from the on-board camera and a computerthat projects it all together onto a screen for the PIC to view during flight. A Visual Observer (VO) is a person who provides a second pair of eyes to visually track the UAwhile in flight.The requested exemption would support an application for a commercial Certificate of Authorization to use the above described UA System to support aerial photography and video primarily of real property, resorts, tourism , boats, agriculture, surveying community events, aerial inspections, aerial surveying , cell tower inspection, and marine property, never operating over persons not directly involved with the UA System . The UA, powered by batteries , is smaller, lighter, and more maneuverable than larger aircraft running on combustible fuel. It operates at lower altitudes with no people on board and will thereby reduce current risk levels and thereby enhance safety and diminish the likelihood of death or serious bodily injury. With a small payload and maximum flight time of only 25 minutes, this offers little or no risk to national security. Low level photos and video from several angles are far more effective than ground-based imagery for displaying the characteristics of large, complex properties with several buildings and large trees. The alternative could be to charter a full-sized helicopter for this purpose, which has proven more costly than many potential clients are able to afford. The benefits of reduced cost and improved quality of presentation from the UAwill be valuable to and benefit many buyers and sellers of real and marine property. Additionally, we request that we be allowed to use our system to benefit first responders nearby who might require assistance, including firefighters, the police, the sheriff, et al. , while remaining subject to all limitations cited in this application as we do so. The UA System will be operated in the field with both PIC and aVO in accordance with FAA Policy N 8900.227 Section 14 "Operational Requirements for UAS" and the following restrictions: 1) No flight will be made with a UA gross weight exceeding 55 pounds. 2) All operations must occur in FAA Class G airspace at no more than 400ft. AGL, at an airspeed of no more than 50 knots, and no furtherthan % NM from the PIC. 3) All operations must utilize a visual observer (VO). The VO and PIC must be able to communicate by voice at all times during a flight operation . 4) Operations will be restricted to flights over property with the permission ofthe property owner. 5) The PIC must have accumulated and logged, in a manner consistent with 14 CFR 

### § 61 .51 (b), a minimum of 100 flight cycles and 25 hours oftotal time as a UA rotorcraft pilot and at least ten hours logged as a UA pilot with a similar UA type. 6) All required permits will be obtained from state and local government prior to operation . 7) The UA System will not be operated over densely populated areas. 8) The UA System will not be operated at air shows . 9) The UA System will not be operated over and open-air assembly of people . 1

0) The UA System will not be operated over heavily trafficked roads. 11) The UA System will not be operated within 5 NM of an airport or heliport. 12) Operations will be restricted to day only and weather conditions equivalent to VFR. 13) The PIC will brief the VO and property owner about the operation and risk before the first flight at each new location. 14) No flight may be made without a pre-flight inspection by the PIC before each operation to ascertain that the UA is in a condition safe for flight (see Appendix A) .The PIC and VO will meet the requirements outlined in FAA Policy N 8900.227 Section 16 Personnel Qualifications. Additionally, the PIC and VO will perform maintenance on the system and will complete a course of maintenance instruction as part oftheir initial training . We submit that the combination ofthe UA's light weightflight performance and ability, fully qualified flight crew, and strict operation under the guidelines established in 8900.227, and under all ofthe restrictions (1) through (14) listed above , the FAA can have full confidence that the operation will have an equivalent or greater level of safety than manned aircraft performing the same mission. The name and contact information ofthe applicant is: Michael Milovina dba Green Tech Coatings (760) 238-6559 gtcoatings@yahoo.com The regulations from which the exemption is requested are listed below. Beside each regulation number is the page ofthe attached Addendum upon which each may be found together with our proposed equivalent level of safety for each regulation :

- 14 CFR Part 21 ..................................................................

- 14 CFR 91 .203...................................................................

- 14 CFR 45.23, 45.29................................ .. .. .......... .. ... .. . ..... .

- 14 CFR 91 .9.................... .. .................................................

- 14 CFR 61 . 113.................................................................... -1 4 CFR 91 . 109, 91 . 119, 91 . 121 ............... .. .................. . ........... -14 CFR 91 . 151 ..................................................................... -14 CFR Subpart E (91.401- 91.417)........... . ............................ -FAA Policy 8900.227 Paragraph 16(c) (4) and Paragraph 16(e) (1)... We are prepared to modify or amend any part ofthis request to satisfy the need for an equivalent level of safety. Please contact us at any time if you require additional information or clarification. We look forward to working with your office . Sincerely,



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**1J Wt~**  Michael Milovina Addendum containing Exemption Requests and Equivalent Level of Safety Appendix A- Flight Manual 's Appendix B - Owner's Manuals for UA's ADDENDUM EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY Green Tech Coatings requests an exemption from the following regulations as well as any additional regulations that may technically apply to the operation ofthe UA System . 14 CFR Part 21 , Subpart H: Airworthiness Certificates.This part establishes the procedures for the issuance of an airworthiness certificate. While the FAA continues to work to develop airworthiness standards for Unmanned Aerial Systems, we request an experimental certificate be issued for the UA System under either or both ofthe following provisions: 21 . 191 Experimental Certificates. Experimental certificates are issued for the following purposes: (1) Research and development. Testing new aircraft design concepts, new aircraft equipment, new aircraft installations, new aircraft operating techniques, or new uses for aircraft. (2) Showing compliance with regulations. Conducting flight tests and other operations to show compliance with the airworthiness regulations including flights to show compliance for issuance of type and supplemental type certificates, flights to substantiate major design changes, and flights to show compliance with the function and reliability requirements of the regulations. Since the experimental certificate can be used for commercial purposes such as market surveys, sales demonstrations, and customer crew training, we would expect that an experimental certificate would permit our commercial purpose as well. The aircraft will not carry persons or property, will not carry fuel , and will only fly under strict operational requirements. Combined with the UA's light weight, being constructed primarily of carbon fiber and plastic, we propose that the UA will be at least as safe , if not safer, than a conventionally certificated aircraft performing the same mission. If an experimental airworthiness certificate is not appropriate for this application, then we request an exemption of 14 CFR Part 21, Subpart H , and the requirement for an airworthiness certificate in general, citing the equivalent level of safety outlined in the previous paragraph . 14 CFR 91 .203(a) & (b) Civil aircraft: Certifications required . The regulation provides that an airworthiness certificate, with the registration number assigned to the aircraft and a registration certificate must be aboard the aircraft. Additionally, subparagraph (b) provides that the airworth iness certificate be "displayed at the cabin or cockpit entrance so that it is legible to passengers or crew." At a maximum gross weight of no more than 15 pounds, the UA is too small to carry documentation, does not have an entrance, and is not capable of carrying passengers or crew. To obtain an equivalent level of safety and meet the intent of 91 .203, we propose that the documents deemed appropriate for this aircraft by the FAA will be co-located with the crew at the ground control station and available for inspection upon request. In order to identify the aircraft, we propose that the information found on airworthiness and registration certificate be permanently affixed to the aircraft via placard containing the following information plus the word "EXPERIMENTAL" to satisfy the requirement of 14 CFR 45.23, which follows immediately after the proposed placard description below: EXPERIMENTAL Manufacturer: Yuneec Electric Aviation 5555 Ontario Mills Parkway Ontario, CA 91764 Model : Typhoon 0500 4K Manufacturer: Walkera 212 S. Mead St. Seattle, WA 98108 Model: QR X800 14 CFR 45.23 Display of marks; general and 45.29 Size of marks. These regulations provide that each aircraft must display "N" and the aircraft's registration number in letters at least 3 inches high . Additionally, the aircraft must display the word "EXPERIMENTAL" in letters at least 2 inches high near the entrance to the cabin , cockpit, or pilot station. The UA does not have an entrance in which the word "EXPERIMENTAL" can be placed , and may not have a registration number assigned to it by the FAA. We propose toachieve an equivalent level of safety by including the word "EXPERIMENTAL" in the placard on the top ofthe aircraft, as shown above, where the PIC, VO, and others in the vicinity ofthe aircraft will be able to see the designation while the aircraft is prepared for launch. Additionally, we feel that the permanent placard discussed in the previous paragraph will provide the aircraft's registration information at the ground station. Finally, we will display at the ground station a high contrast flag or banner that contains the words "Unmanned Aircraft Ground Station" in letters 3 inches high or greater. Since the aircraft will operate within 

### :X NM ofthe ground station, the banner should be visible to anyone that observes the aircraft and chooses to investigate its point of origin. 14 CFR 91 .9 Civil aircraft flight manual, marking, and placard requirements. This regulation provides that no person may operate an aircraft unless a current, approved flight manual is in the aircraft. We assume that the intent ofthis requirement is to ensure that flight manual information is available to the aircrew while operating the aircraft. We request an exemption to this requirement since the aircraft is not only too small to carry documentation , but the documentation would not be available to the crew during flight operations. To obtain an equivalent level of safety and meet the intent of 91 .9, we propose that a current, approved UA Flight Manual (Appendix A) must be available to the crew at the ground station anytime the aircraft is in , or preparing for, flight. 14 CFR 61 . 113 Private pilot privileges and limitations: Pilot in Command. The regulation provides that no person that holds a private pilot certificate may act as pilot in command of an aircraft for compensation or hire. Subparagraph (b) allows a private pilot to act as pilot in command of an aircraft in connection with any business or employment if: (1) The flight is only incidental to that business or employment; and (2) The aircraft does not carry passengers or property for compensation or hire. Our proposed operations require that the PIC must either: 1. Hold a Private Pilot Certificate issued by the FAA, and have logged 25 hours offlight experience in this type of UA, or 2. Meet the requirements of 8900.227 paragraph 16(c)(2)(c) "Operations without a pilot certificate" in which the PIC is required to complete "FAA private pilot ground instruction" and pass "the FAA Private Pilot written examination ." Since the aircraft cannot carry passengers or property, we feel we meet the intent of 61 . 113 Subparagraph (b) even though the intent ofthis application is to conduct a business. 14 CFR 91 . 109 Flight instruction: Simulated instrument flight and certain flight tests. The regulation states that "No person may operate a civil aircraft that is being used for flight instruction unless that aircraft has fully functioning dual controls. " The UA System groundbased control station consists of a small hand-held radio transmitter and while it does not offer a second set of "controls", both the student and instructor can, and will , operate the single set of controls simultaneously. With both student and instructor having "hands-on" the controls during the flight, we feel that this technique meets the intent of 91 . 109 and provides an equivalent level of safety. 14 CFR 91 . 119 Minimum safe altitudes: General. The regulation states that over sparsely populated areas the aircraft cannot be operated closer than 500 feet to any person, vessel, vehicle, or structure. Since the aircraft will be operating at a maximum altitude of400 feet AGL, we cannot comply with this requirement. In order to provide an equivalent level of safety, we will only fly over private property with the permission of the owner ofthe property flown over. The aircraft will not be operated over congested areas orover any open air assembly of persons. The property ownerwill be briefed on the expected route offlight and the associated risks to persons and property on the ground . The aircraft will be operated at a low altitude allowing , if a power unit fails, an emergency landing without undue hazard to persons or property on the surface. Therefore, we maintain that due to the small size ofthe UA, the hazards to persons, vehicles, and structures is minimal compared to manned aircraft,which should be considered in granting the exemption . 14 CFR 91 .121 Altimeter settings. The regulation requires that aircraft shall maintain cruising altitudes be reference to an altimeter setting available within 100 NM ifthe aircraft. The UA will always fly below 400 feet AGL and will not need to maintain cruising altitudes in order to prevent conflict with other aircraft. An Above Ground Level altimeter measurement above the takeoff point is transmitted via radio from the UA on-board computer to the display screen held by the PIC, providing a constantly updated AGL readout. 14 CFR 91.151 Fuel requirements for flight in VFR conditions. The regulation provides that no person may begin a flight in an airplane under day-VFR conditions unless there is enough fuel to fly to the first point of intended landing and to fly after that for at least 30 minutes. We feel the intention ofthis paragraph is to provide an energy reserve as a safety buffer for delays to landing . The UA is battery operated and the maximum duration ofthe flight from a single battery charge is 22 minutes with a 20% reserve . Since the aircraft will never fly more

**than~** NM from the point of intended landing , a full battery charge at launch will ensure that we meet the reserve energy requirement ofthis paragraph. We request an exemption to the word "fuel" and ask for an equivalent interpretation with the word "energy". 14 CFR Subpart E (91.401 - 91.417) - Maintenance, Preventative Maintenance, and Alterations. The regulation provides that the operator is primarily responsible for maintaining the aircraft in airworthy condition, including compliance with part 39 and 43. Paragraphs 91.407 and 91.409 require that the aircraft be "approved for return to service by a person authorized under 43. 7'' after maintenance and inspection . It is our intention that the PIC perform maintenance and inspection ofthe aircraft and "be authorized to approve the aircraft for return to service." As provided in the Pre-Flight Checklist in Appendix A, the PIC will ensure that the aircraft is in an airworthy condition priorto every flight and in addition conduct detailed inspections after every two hours offlight. Maintenance performed by the PIC is limited to repairing small cracks, replacing a propeller, checking electrical connections, and updating software and firmware for the on-board computer. All other maintenance will be performed by the manufacturer or their designated repair facility. The PIC will document work performed in accordance with 91.417. We feel that due to the size, construction , and simplicity of our aircraft, the PIC can ensure an equivalent level of safety. 8900.227 Paragraph 16(c) (4) PIC Medical and Paragraph 16(e) (1) Observer Medical. This policy states that both the PIC and VO must have a valid FAA second-class medical certificate issued under Part 67 in order to perform as a pilot or observer. The UA maximum gross weight is no more than 15 pounds, it is constructed of carbon fiber and plastic, and the PIC is not on board . Both the PIC and the VO are required to be in VLOS. Given the unlikely event that both the PIC and VO become medically incapacitated while the aircraft is in flight, the UA will return autonomously to the site of launching and land without crew intervention. Therefore, requiring the PIC and VO to meet the same medical requirements as a commercial pilot who carries passengers in a large aircraft is an unnecessary burden. We propose that the minimum medical requirements for the PIC and VO be vision corrected to 20/20 and a valid ,state issued driver's license. The 20/20 vision requirement will ensure that the PIC and VO can see and avoid air traffic; a licensed driver is medically qualified to operate a much larger vehicle. APPENDIX A- FLIGHT MANUALS FLIGHT RESTRICTIONS 1. No flight will be made with a UA gross weight exceeding 55 pounds. 2. All operations must occur in FAA Class G airspace at no more than 400 feet AGL, at an airspeed of no more than 50 knots and no further than % NM form the PIC . 3. All operations must utilize a visual observer (VO). The VO and PIC must be able to communicate verbally at all times during a flight operation. 4. Operations will be restricted to flights over property with the permission ofthe property owner. 5. The PIC must have accumulated and logged , in a manner consistent with 14 CFR 

### § 61 .51 (b), a minimum of 100 flight cycles and 25 hours of total time as a UA rotorcraft pilot and at least 10 hours logged as a UA pilot with a similar UAtype. 6. All required permits will be obtained from state and local government prior to operation . 7. The UA System will not be operated over densely populated areas. 8. The US System will not be operated at air shows. 9. The UA System will not be operated over any open air assembly of people. 10. The UA System will not be operated over heavily trafficked roads. 11. The UA System will not be operated within 5 NM of an airport or heliport. 12. Operations will be restricted to day only and weather conditions equivalent to VFR. 13. The PIC will briefthe VO and property owner about the operation and risk before the first flight at each new location. 14. No new flight may be made without a successful Pre-Flight Inspection by the PIC before each operation to ascertain that the UA is in a condition for safe flight. PREFLIGHT CHECKLIST 1 . Remote controller, aircraft battery, and mobile device fully charged. 2. Propellers are mounted correctly and firmly. 3. Micro-SO card has been inserted if necessary. 4. Gimbal is functioning as normal. 5. Motors can start and are functioning as normal. TO REGAIN CONTROL AFTER LOST RADIO CONTACT If radio contact is lost and not restored within 3 seconds, an automatic Return to Home feature is activated and will bring the UAV back to the PIC. APPENDIX 8 - Owner's Manuals