DAVINCI AIRBORNE INFORMATION SYSTEMS 6000 Fairview Rd., Ste. 665, Charlotte, NC 28210

FAA Rulemaking Section 333 Of The FAA Reform Act and Part 11

Prepared by Andrew M. Riolo, Attorney at LawJuly 2, 2015

Attention: United States Secretary of Transportation Mr. Anthony R. Foxx 1200 New lersey Ave. SE Washington, DC 20590 U.S. Department of Transportation, Docket Operations West Building Ground Floor, Room W12-140 1200 New Jersey Avenue, SE Washington, DC 20590 Re: Exemption Request Section 333 of the FAA reform Act and Part 11 of the Federa) Aviation Regulations form 14 CFR 45.23(b); 14 CFR Part 21; 14 CFR61.113 (a) and (b); 91.7 (a); 91.9 (b) (2); 91.103 (b); 91.119; 91.121; 91.151(a); 91.203 (a) and (b); 91.409 (a) (2); 91.417 (a) and (b). And via blanket exemption. Dear Mr. Secretary, Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (The Reform Act) and 14 CFR Part 11, DAVINCI AIRBORNE INFORMATION SYSTEMS (DAVINCI AIS). Is the operator of Small Unmanned Aircraft Systems (SUAS) equipped to conduct aerial photography: motion picture and television filming, aerial, video photography; user measurement air quality measurements; survey and cellular tower and signal analysis inspection; and industrial construction tower, building, smoke stack, power plant and power line; agriculture fields; and data collection, hereby applies for an exemption from the listed Federal Aviation Regulations (FARs) to allow commercial operation of its SUAS so long as such operations are conducted within and under the conditions outlined herein or as may be established by the FAA as required by Section 333. As described in more detail below, the requested exemption would permit the operation of small, unmanned and relatively inexpensive SUAS under controlled conditions in airspace that is 1) limited 2) predetermined 3) would provide safety enhancements to the already safe operations in the industrial, construction, private and survey industries presently using conventional and unmanned aircraft. 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) of the Reform Act.

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### 15 July 2, 2015The name and address of the applicant is:

DAVINCI AIRBORNE INFORMATION SYSTEMS Phone: 704-576-6296 Address: 6000 Fairview Rd., Ste. 665, Charlotte, NC 28210 Regulations from which the exemption is requested:

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 103 14 CFR 91.109
14 CFR 91.119
14 CFR 91.121 14 CFR 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)

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### 15 July 2, 2015This exemption application is expressly submitted to fulfill Congress' goal in passing Section 333 (a)

through (c) of the Reform Act. This directs the Secretary of Transportation to consider whether certain unmanned aircraft systems may operate safely in the National Airspace System (NAS) before compietion of the rulemaking required under Section 332 of the Reform Act. In making this determination, the Secretary is required to determine which types of SUAS do not create a hazard to users of the NAS or the public or pose a threat to national security in light of the following: The SUAS size, weight, speed, and operational capability Operation of the SUAS in close proximity to airports and populated areas Operation of the SUAS within Visual Line of Sight (VLOS) of the pilot and observers Reform Act §333 (a). Lastly, if the Secretary determines that such vehicles "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) The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This statutory authority by its terms includes exempted civil aircraft, as the term is defined under §40101 of the Act, that includes SUAS, 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 U.S.C. §44704; 14 CFR §91.203 (a) (1)

Applicants interpretation of this provision is the duty of said provision is placed on the Administrator to not only process applications for exemptions under section 333, but to also craft conditions herein for the safe operation of the SUAS, if it should be determined that the conditions set forth herein do not fulfill the statutory requirements for approval.

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### 15 July 2, 2015DAVINCI AIS SUAS are DJI, Phantom III, Professional

, weighing 55 or fewer Ibs. including

payload. Operations of rotorcraft do not exceed more than 50 knots and are capable of hover and movement in vertical and horizontal movements simultaneously. Operations of the fixed-wing do not exceed more than 50 knots and have very similar flight characteristics of traditional airplanes. Both types of SUAS will be operated only under visual line of sight (VLOS) and will operate only within the predetermined area and under predetermined conditions and limitations as set forth by U.S. Department of Transportation, Federal Aviation Administration. Adherence to these conditions and limitations will insure that the SUAS will "not create a hazard to the national airspace system or the public." The small size and weight of the SUAS involved and the predetermined area and altitude that operations are conducted will place the applicant within a level of safety congruent with Congress vision that the FAA must, by exemption, allow commercial operations of SUAS to commence immediately. Compliance of the applicants given size and flight parameters of the SUAS will pose no reason that approval of the application presents no national security issue. The clear direction in Section 333 of the Reform Act, the authority contained in the Federal Aviation Act, as amended; the strong equivalent level of safety, surrounding the proposed operations, and significant public benefit, including enhanced safety, reduction environmental impacts, including reduced emissions associated with allowing SUAS for industrial, construction, private, survey and photography operations, the grant of the requested exemptions is in the public's interest. Accordingly, the applicant respectfully requests that the FAA grant the requested exemption without delay.

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### 15 July 2, 2015AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY

DAVINCI AIS Requests exemptions to operate multi-engine quads. The applicant proposes that the exemption requested herein apply to civil aircraft that have the characteristics and that operate with the limitations listed below. These limitations provide for at least an equivalent or even higher level of safety to operations under the current FAR's.
Current SUAS

1. DJI, Phantom III, Professional

Description 2.8 pounds, 23.2 inches diagonal, quad-copter

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### 15 July 2, 2015ALL SUAS operations conducted by DAVINCI AIS will:

A: Be conducted in accordance with conditions and limitations of the Department of Transportation, Federal Aviation Administration. SUAS will weigh less than 55 Ibs. including the payload SUAS and attachments, i.e., camera and components. C: Preflight operations include PIC attaining FAA approved weather briefing, review of current sectional chart for the area of operation to preclude operation within 5 miles of an airport with surface class E or greater airspace. D: Monitor Common traffic Advisory Frequency (CTAF) or Air Traffic Control (ATC) with the ability to communicate with local traffic or ATC with intentions and current locations via handheld aviation broadband radio. Be conducted and operated by a FAA certificated airman holding no less than Private Pilot certificate and no less than a 3` d class medical. Operate only in visual line of sight (VLOS) of the PIC. G: Operate at an altitude of no more than 400 feet above ground level (AGL). H: Operate at speeds of no more than 50 knots. Be operated at a lateral distance of no less than 100 feet from any inhabited structures, buildings, vehicles, vessels, or people not associated with the operation or who have not signed a waiver in advance of the operation. Limit each flight mission to 30 minutes or less. Flights will be terminated at 25% battery power reserve or 30 minutes which ever should occur first. K: Have the capability to return to the point of departure or a pre-determined location if the SUAS loses RC communications or GPS signal. L: Be monitored by the ground station, receiving real time SUAS info (i.e., battery, attitude, altitude, coarse heading, GPS location and flight time). M: Minimum 2 man crew for each SUAS operation will consist of the PIC and Observer. In most cases a third Observer will observe or monitor imaging equipment.

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### July 2, 201514 CFR Part 21, subpart H: Airworthiness Certificates 14 CFR §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 DAVINCI AIS, 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 form the requirement capability, and proximity to airports and populated areas of the particular (UAS). In all cases, an analysis of these criteria demonstrates that the SUAS 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. The SUAS to be operated hereunder is less than 55 Ibs. fully loaded, carries neither a pilot not passenger, carries no explosive materials or flammable liquid fuels, and operates exclusively within a secured area as set out in the manual. Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by both the PIC and Observers. These safety enhancements, which already apply to civil aircraft operated in the industrial, construction, private, survey and photography, 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 SUAS 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.

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### 15 July 2, 201514 CFR §45.23 (b): Marking of the Aircraft

The regulation requires marks include only the Roman capital letter N and the registration number is displayed on limited, restricted or light-sport category aircraft or experimental or provisionally certificated aircraft, the operator must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches not more than 6 inches high, the words "limited, restricted, light-sport, experimental, or provisional", as applicable. The SUAS will have no airworthiness certificate, and exemption may be needed as the SUAS will have no entrance to the cabin, cockpit or pilot station on which the word "Experimental" can be placed. Given the size of the SUAS, two-inch lettering will be impossible. The word "Experimental" will be placed on the fuselage in compliance with §45.29 (f). The equivalent level of safety will be provided by having the SUAS marked on its fuselage as required by §45.29 (f) where the pilot, Spotter (Observer) and others working with the SUAS will see the identification of the SUAS as "Experimental". The FAA has issued the following exemptions to this regulation to Exemptions Nos. 10700, 8738, 10167 and 10167A.

14 CFR §61.113 (a) &(b): Private Pilot Privileges and Limitations — PIC Sections 61.113 (a) &(b) limit private pilots to non-commercial operations. Given the SUAS will not carry a pilot or passenger, the proposed operations can achieve the equivalent level of safety of current operations by requiring the PIC operating the aircraft to have a private pilot's license rather than a commercial pilot's license to operate this SUAS. Unlike a conventional aircraft that carries the pilot and passengers, the SUAS is remotely controlled with no living thing on board. The area of operation is controlled and all flights are planned and coordinated in advance as set forth by the conditions and limitations of the Department of Transportation, Federal Aviation Administration. The level of safety provided by the requirements included in the conditions and limitations of the Department of Transportation, Federal Aviation Administration, exceeds that of a single individual holding a commercial pilot's certificate operating a conventional aircraft. The risks associated with commercial operations contemplated by Part 61 when drafted, that allowing operations of the SUAS as requested with a private pilot as the PIC exceeds the present level of safety achieved by 14 CFR §61.113 (a) &(b).

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### 15 July 2, 201514 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, should this exemption be granted, no FAA FAR will exist for determining airworthiness. Given the size of the aircraft and the requirements contained in the Manual for maintenance and the use of safety check lists prior to each flight, and equivalent level of safety will be provided.

14 CFR §91.9 (b) (2): Civil Aircraft Flight Manual in the Aircraft Section 91.9 (b) (2): 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.
Given the size and configuration of the SUAS they are incapable of carrying a flight manual, there is no room, capacity or pilot on board the aircraft. The equivalent level of safety will be maintained by keeping the conditions and limitations of the Department of Transportation, Federal Aviation Administration at the ground station for the PIC or the Observer to access immediately. The FAA has issued the following exemptions to this regulation: Exemption Nos. 8607, 8737, 8738, 9299, 9299A, 9565, 95656, 10167A, 10602, 32827, and 10700.

14 CFR §91.103: Preflight Action This regulation required each pilot in command to take certain actions before flight to insure that safety of flight. As FAA approved rotorcraft flight manuals will not be provided for the aircraft and exemption will be needed. An equivalent level of safety will be provided as required by the conditions and limitations of the Department of Transportation, Federal Aviation Administration. The PIC will take all actions including reviewing weather, battery requirements, landing and takeoff performance before initiating flight missions.

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### 15 July 2, 201514 CFR §91.109: Flight Instruction

Section 91.103 states that no person may operate a civil aircraft (except a manned free balloon) that is used for flight instruction unless that aircraft has fully functioning dual controls. SUAS is flown through the use of a control box that communicates with the aircraft via RC, by design these aircraft do not have fully functional dual controls. The FAA has approved exemptions for flight training for aircraft without fully functional dual controls, (experimental) such as Nos. 5778K and 9862A. Furthermore, DAVINCI AIS has a training program set out by the conditions and limitations of the Department of Transportation, Federal Aviation Administration. This will provide at minimum the equivalent level of safety.

14 CFR §91.119: Minimum Safe Altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. Section (b) "... Except when necessary for takeoff or landing, no person may operate an aircraft below the following altitudes: ... (b) Over other than congested areas. An altitude of 500 feet above the surface, except over open water or sparsely populated areas. In those cases, the aircraft may not be operated closer than 500 feet to any person, vessel, vehicle, or structure." (d) Allows helicopters to be operated at less than the minimums prescribed, provided the person operating the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. Due to the Applicants request to operate at altitudes up to, but not exceeding 400 AGL, an exemption is needed. Furthermore, the conditions and limitations of the Department of Transportation, Federal Aviation Administration address that the SUAS will never operate higher than 400 feet AGL. It will however be operated in areas where buildings and people will be exposed to operations only after consent is signed and owners permissions are obtained. The equivalent level of safety will be achieved given the size, weight, speed of the SUAS as well as location. No flight will be taken without the permission of the property owner or local officials. Compared to conventional aircraft weight, flammable fuel load, and speed, the SUAS prove to be as safe or safer. In addition, the low-altitude operations of the SUAS will ensure separation between these operations and those of conventional aircraft that must comply with Section 91.119.

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### 15 July 2, 201514 CFR §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 SUAS may not have a barometric altimeter, it utilizes GPS altitude readout, an exemption may be needed. An equivalent level of safety will be achieved by the PIC as the conditions and limitations of the Department of Transportation, Federal Aviation Administration states. Confirming the altitude of the launch site shown on the GPS altitude indicator before each flight will be an essential part of every mission.

14 CFR §91.151 (a): Fuel Requirements for Flight in VFR Conditions Section 91.151 (a) prohibits an individual from beginning "a flight in an airplane under VFR conditions unless (considering wind and forecast weather conditions) there is enough fuel to fly to the first point of intended landing, and, assuming normal cruising speed —(1) During the day, to fly after that for at least 30 minutes; or (2) At night, to fly after that for at least 45 minutes. The battery powering the SUAS provide approximately 30-40 minutes of flight. To meet the 30 minute reserve requirement in 14 CFR §91.151, SUAS flights would be limited to, at most, 10 minutes. Given the limitations on the SUAS proposed flight area and the Iocation of its proposed operations within a predetermined area, a longer time frame for flight in daylight or night VFR conditions is reasonable. DAVINCI AIS. believes that an exemption from 14 CFR §91.151 (a) falls within the scope of prior exemptions. Exemption 10673 allowing Lockheed Martin Corporation to operate without compliance with FAR 91.151(a). Operating the SUAS in a small controlled area where only people and property owners or official representatives who have signed waivers will be allowed, with 30 minute or less flight reserve, does not engender the type of risks that section 91.151(a) was intended to alleviate given the size and speed of the SUAS. Furthermore, limiting flights to 10 minutes would greatly reduce the utility for which the exemption will be granted. The Applicant believes that an equivalent level of safety can be achieved by limiting flights to 30 minutes or 25% battery power, whichever happens first. This restriction would be more than adequate for return of the SUAS to its predetermined landing zone. Similar exemptions have been granted to other operations, including Exemptions 2689F, 5745, 10673, and 10808.

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### 15 July 2, 201514 CFR §91.203 (a) &(b): Carrying Civil Aircraft Certification and Registration

The regulation provides in pertinent part: (a) Except as provided in §91.715, no person may operate a civil aircraft unless it has within it the following: (1) An appropriate and current airworthiness certificate...
(b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (b) of this section or a special flight authorization issued under §91.715 is displayed at the cabin or cockpit entrance so that it is legible to passengers or crew. The SUAS fully loaded weighs no more than 55 Ibs. and is operated without an onboard Pilot. There is no ability or place to carry certification of registration documents or to display then on the SUAS. An equivalent level of safety will be achieved by keeping these documents at the ground control station where the PIC will have immediate access to them, to the extent they are applicable to the SUAS. The FAA has issued numerous exemptions to this regulation including Nos. 9565, 9665, 9789, 9789A, 9797, 9797A, 9816A and 10700.

14 CFR §91.405 (a); 407 (a) &(b): Maintenance Inspections 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 section and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to the Applicant. Maintenance will be accomplished by the operator pursuant to the conditions and limitations of the Department of Transportation, Federal Aviation Administration. An equivalent level of safety will be achieved because these SUAS are limited in size and will carry a small payload and operate only in predetermined areas for not more than 30 minutes. If inechanical issues arise, the SUAS can land immediately. SUAS will be operated from no higher than 400 feet AGL. The PIC will conduct visual and control checks in the preflight operations to ensure the SUAS is in working order prior to all missions to confirm whether any maintenance is needed and, furthermore, will document and log any and all maintenance done as well as all flight hours. In addition the (PIC) is the most familiar person with the aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivalent level of safety.

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### 15 July 2, 2015Pursuant to 14 CFR Part 11, the following summary is provided to publication in the Federal Register,

should it be determined that publication is needed: Applicant seeks an exemption from the following rules: 14 CFR §21, subpart H; 14 CFR §45.23 (b); 14 CFR §61.113 (a) &(b); 91.7 (a); 91.9 (b) (2); 91.103 (b); 91.109; 91.119; 91.121; 91.151 (a); 91.203 (a) & (b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2) and 91.417 (a) &(b) to operate commercially a small unmanned vehicle (55 Ibs. or less) in industrial, construction, private, survey and photography operation.

Privacy AII flights will occur over private or controlled areas with the property owner's prior consent and knowledge. Image capture of people will rarely take place; in the event they are, they will have consented prior to being filmed or otherwise have agreed to be in the area where data collection will take place. DAVINCI AIS primary focus is to utilize SUAS in assisting the survey community for the purpose of conduct aerial photography: motion picture and television filming, aerial, video photography; user measurement air quality measurements; survey and cellular tower and signal analysis inspection; and industrial construction tower, building, smoke stack, power plant and power line; agriculture fields; and data collection. Given the high cost, environmental impact, close proximity to people, structures, and vessels, the weight (average 4000 Ibs.) of conventional aircraft that are currently safely performing these same types of missions, the Applicant believes with the grant of requested exemptions letpool can offer a more cost efFective (to the consumer), more environmentally friendly (with no combustible fuel), controlled predetermined area, and weighing 55 Ibs. or less (compared to several thousand Ibs.) an equally and likely a safer option that is in the public's best interests and benefits.

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### 15 July 2, 2015Summary:

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 DAVINCI AIS in the industrial, construction, private, survey and photography industry's pursuant to the conditions and limitations set by the Department of Transportation, Federal Aviation Administration. DAVINCI AIS is eagerly standing by to support the FAA and SUAS community in its quest to establish proper regulations and protocols for the safe introduction of unmanned aircraft into the national airspace. If you have any questions or concerns, please contact at 704-576-6296 or amriolo@riolo.com

.

Sincerel ,i

~ Andrew M. Riolo Attorney At Law ATP, CFI-MEI Owner DAVINCI AIS 

# ~ Eric Legvoid 

### ATP Jetpool, LLC. 135 Operator 

### CEO Owner DAVINCI AIS

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