Aviation Administration

800 Independence Avenue, SW Washington, DC 20591 Re: Exemption Request Pursuant to Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation Regulations from: 14 CFR 61.113{a) & (b); 91.7 (a); 91.103; 91.119{c); 91.121; 91.151{a); 91.405{a); 91.407(a)(1); 91.409 (a)(1) and {2}; 91.417{a) & (b). Dear Sir or Madam: Pursuant to Section 333 of the FAA Modernization and Reform Act, I, Marshall T. Frith , operator of an Unmanned Aircraft System (UAS), hereby apply for an exemption from the listed Federal Aviation Regulations (FARs) 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 required by Section 3 33. I formally submit for an exemption from part 21, subpart H; and Sections 45.23(b), 91.7(a), 91.9(b)(2), 91.119, 91.121, 91.151(a), 91.203(a) and (b), 91.405(a), 91.407(a)(1), 91.409(a)(2), and 91.417(a) and (b) of Title 14, Code of Federal Regulations (14 CFR). This proposed exemption would allow the operation of UAS for the purpose of aerial data collection. Applicant: Marshall T. Frith , 3712 Wayland Street , Jacksonville , FL 32277 Marshall.frith@gmail.c om ( 571 ) 431

- 8514 Commercial operation of a UAS as described herein, which is equipped with a camera and sensors, would operate in the following manner: Conduct aerial photography and/or video for public and/or private use in land management, land survey , structural inspection and other related professional activities. As described fully below, the requested exemption would permit the operation of a UAS under controlled conditions in the NAS that would be a) limited, b) controlled, c) predetermined, and d) will provide safety enhancements to the already safe operations in the industry presently using conventional aircraft. As found in Exemption No. 13203 (Gambill), the FAA recently approved similar use of a PHANTOM 3 series UAS , and PHANTOM 4 series UAS

. I will operate a UAS, the DJI Phantom 3 series and Phantom 4 which is comprised of an unmanned aircraft (UAS or Phantom), an attached camera and a transportable ground station. The PHANTOM 3 / PHANTOM 4 is a quad

- copter with a gross weight of 2.8 pounds. It is equipped with four rotors that are driven by electricmotors powered by batteries. Additional UAS details can be found in Appendix

A. UAS Operating Parameters I will abide by the following additional operating conditions under this exemption, whi ch ensures a level of safety at least equal to existing rules: •Operate UAS below 400 feet and within a radius distance of 1000 feet from the controller to aid in direct line of sight visual observation; •Obtain permission from the owner/controller of any vessels, vehicles and structures when operations may be conducted closer than 500 feet to any such vessels, vehicles or structures; I will conduct a safety assessment of the risk of operating closer to those objects and determine that it does not prese nt an undue hazard; •Operate the UAS for 5

- 10 minutes per flight; •Land UAS prior to the manufacturer’s recommended minimum level of battery power; •Operate UAS during daylight hours only within visual line of sight (VLOS); •Use the UAS’ global positioning system (GPS) flight safety feature whereby it hovers and then slowly lands if communication with the remote control pilot is lost; •Conduct all operations under the flight safety protocols (including posting a warning sign reading: “Attention Aerial Photography in Progress

– Remain Back 150 feet”) contained in the operating documents and will actively analyze flight data and other sources of information to constantly update and enhance safety protocols; •Contact respective airports if operatio ns will be within 5 miles to advise them of his estimated flight time, flight duration, elevation of flight and other pertinent information; •Always obtain all necessary permissions prior to operation; have procedures in place to abort flights in the even t of safety breaches or potential danger; •Only operate in safe environments that are strictly controlled, are away from power lines, elevated lights, airports and densely populated areas (defined by areas depicted in “yellow” on VFR charts and through obtaining informationregarding congested areas from the local Flight Standards District Office

(FSDO); •Conduct extensive preflight inspections and protocols, during which safety carries primary importance. Regarding UAS operational training, I have flown numerous practice flights in remote areas as hobbyists simulating flights for future commercial use to gain familiarization with the characteristics of the UAS performance under different temperature and weather conditions.
Any PIC operating our UAS wil l have accumulated and logged, in a manner consistent with 14 CFR 61.51(b), 25 hours of total time as a UAS rotorcraft pilot including at least 10 hours logged as a UAS pilot with a multi

- rotor UAS. The PIC will also have accumulated and logged a minimum o f 5 hours as a UAS pilot operating the same make and model of UAS to be used for operations. In addition to the hour requirements, the PIC will accomplish 3 take

- offs and landings in the preceding 90 days (for currency purposes) prior to any flight. Speci fic Exemptions Requested Given the size, weight, speed, and limited operating area associated with the UAS , I feel an exemption from 14 CFR part 21, Subpart H (Airworthiness Certificates) and §91.203(a) and (b) (Certifications required), subject to certain conditions and limitations, is warranted and meets the requirements for an equivalent level of safety under 14 CFR part 11 and Section 333 of P.L. 112

- 95 (Section 333). I request an exemption from § 45.23 Marking of the aircraft because the UAS will not have a cabin, cockpit or pilot station on which to mark certain words or phrases. Further, the two

- inch lettering is difficult to place on such a small aircraft with dimensions smaller than the minimal lettering requirement. Regardless of this, I can mark the UAS in the largest possible lettering by placing the word “Experimental” on its fuselage as required by § 45.29(f) so that anyone will see the markings. I request an exemption from § 91.7(a) which prohibits the operation of an aircraft without an airw orthiness certificate, since there is currently no certificate applicable to our operation, this regulation is inapplicable. I request an exemption from §§ 91.405(a), 91.407(a)(1), 91.409(a)(2) and 91.417(a) and (b) Maintenance inspections since they only apply to aircraft with an airworthiness certificate. However, as a safety precaution I will perform a preflight inspection of the UAS before each flight as outlined in the attached operating documents.I request an exemption from § 91.9(b)(2) which requires an aircraft flight

manual in the aircraft, however since there are no pilots or passengers on board the aircraft and given its size, this regulation is inapplicable. I believe an equivalent level of safety will be achieved by maintaining a safety/flight manual with the UAS ground station. I request an exemption from § 91.119 which prescribes safe altitudes for the operation of civil aircraft, but it allows helicopters to be operated at lower altitudes in certain conditions. I will not operate our UAS above the altitude of 400 feet above ground level (AGL) and will also only operate in safe areas away from the public and traffic, thus “providing a level of safety at least equivalent to or below those in relation to minimum safe altitudes.” Given the size, weight, maneuverability, and speed of the UAS, an equivalent or higher level of safety will be achieved. I request an exemption from § 91.121 Altimeter settings as it is inapplicable since the UAS utilizes electronic GPS with a barometric sensor. I request an exemption from § 91.151(a) Fuel requirements for flight in VFR conditions. The UAS is 100% electric and two low battery alerts are issued

- per the operating documents, the UAS will be landed at the first alert. Also, our flights will last onl y 5

- 10 minutes each, and the UAS has an automated function, which results in immediate landing when a low battery is detected. The PIC will not begin a flight unless (considering wind and forecast weather conditions) there is enough power to fly to the first point of intended landing and, assuming normal cruising speed, land the UAS with 30% battery power remaining. Public Interest Aerial photography and videography are proven strategies to enhance marketing efforts and increase business success. The industry is not new. However, until recently it was conducted through the use of costly manned aircraft, a prohibitive business activity for small companies. By granting this exemption I would be able to provide affordable services. Further, the small UAS will pose no threat to the public given its small size and lack of combustible fuel when compared to larger manned aircraft. Additionally, the operation of our UAS will minimize harm to the environment economic growth by providing information to companies an d the public looking to relocate or build in the metro areas I service. Public and private events serviced by our business enhance vibrancy and add culture to the community and its citizens.Summary

I will comply with all of the following conditions and li mitations should this exemption be provided: 1) Operations will be limited to the following aircraft described in the operating documents, which is a quad

- rotor aircraft weighing 2.8 pounds: Phantom 3 / Phantom 4 Unmanned Aircraft System. 2) The UAS will not be flown at an indicated airspeed exceeding 50 knots. 3) The UAS will be operated at an altitude of no more than 400 feet above ground level (AGL), All altitudes reported to ATC must be in feet AGL. 4) The UAS will be operated within visual line of sight (VLOS) of the Pilot In Command (PIC) at all times. 5) All operations will utilize a visual observer (VO). The UAS will be operated within the visual line of sight (VLOS) of the VO at all times. The VO and PIC will be able to communicate verbally at all times. The PIC will be designated before the flight and will not transfer his or her designation for the duration of the flight. The PIC will ensure that the VO can perform the functions prescribed in the operating documents. 6) The operating documents will be accessible during UAS operations and made available to the Administrator upon request. Any revisions to the operating documents will be presented to the Administrator upon request. 7) Prior to each flight, the PIC will inspect the UAS to ensure it is in a condition for safe flight. If the inspection reveals a condition that affects the safe operation of the UAS, the UAS will not be operated until the necessary maintenance has been performed and the UAS is found to be in a condition for safe fligh t. The Ground Control Station will be included in the preflight inspection. All maintenance and alterations will be properly documented in the aircraft records. 8) Any UAS 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. The PIC who conducts the functional test flight will make an entry in the aircraft records. 9) The pre

-flight inspection section in the operating documents will accou nt for all discrepancies, i.e. inoperable components, items, or equipment, not already covered in the relevant sections of the operating documents.10) I will follow the UAS manufacturer’s aircraft/component, maintenance,

overhaul, replacement, inspection , and life limit requirements. 11) I will carry out maintenance, inspections, and record keeping requirements, in accordance with the operating documents. Maintenance, inspection, and alterations will be noted in the aircraft records, including total flig ht hours, description of work accomplished, and the signature of the authorized person returning the UAS to service. 12) Each UAS operated will comply with all manufacturer Safety Bulletins. 13) An authorized person will make an entry in the aircraft rec ord of the corrective action taken against discrepancies discovered between inspections. 14) UAS operations will be conducted by a PIC possessing at least a private pilot certificate and at least a current third

- class medical certificate. The PIC will als o meet the flight review requirements specified in 14 CFR 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate. 15) Prior to operations conducted for the purpose of aerial videography/photography and for real estate listing video s and public and private events and similar operations, the PIC will have accumulated and logged, in a manner consistent with 14 CFR 61.51(b), a minimum of 25 hours of total time as a UAS rotorcraft pilot including at least 10 hours logged as a UAS pilot w ith a multi

- rotor UAS. 16) Prior to operations conducted for the purpose of aerial videography/photography and for real estate listing videos and public and private events and similar operations, the PIC will have accumulated and logged, in a manner consi stent with 14 CFR 61.51(b), a minimum of 5 hours as UAS pilot operating the make and model of the UAS to be used in operations. The PIC will accomplish 3 take

- offs and landings in the preceding 90 days. 17) The PIC will not operate the UAS for the purpose of aerial videography/photography and for real estate listing videos and public and private events and similar operations, unless the PIC has demonstrated and logged in a manner consistent with 14 CFR 61.51(b), the ability to safely operate the UAS in a m anner consistent with the operating documents, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicles and structures.18) UAS operations will not be conducted during night, as defined in 14 CFR

1.1. All operations will be conducted under visual meteorological conditions (VMC). 19) The UAS will not operate within 5 nautical miles of an airport reference point as denoted on a current FAA

- published aeronautical chart. 20) The UAS 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. 21) If a UAS loses communications or loses its GPS signal, it will return to a predetermined loc ation within the planned operating area and land or be recovered in accordance with the operating documents. 22) The PIC will abort a flight in the event of unpredicted obstacles or emergencies in accordance with the operating documents. 23) The PIC will not begin a flight unless (considering wind and forecast weather conditions) there is enough power to fly at normal cruising speed to the intended landing point and land the UAS with 30% battery power remaining. 24) I will obtain an Air Traffic Organizat ion (ATO) issued Certificate of Waiver or Authorization (COA) prior to conducting operations outside approved conditions, and also request a Notice to Air

- man (NOTAM) not more than 72 hours in advance, but not less than 48 hours prior to the operation. 25 ) Before conducting operations, the radio frequency spectrum used for operation and control of the UAS will comply with the Federal Communications Commission (FCC) or other appropriate government oversight agency requirements. 26) The documents required u nder 14 CFR 91.9 and 91.203 will be available to the PIC at the Ground Control Station of the UAS any time the UAS is operating. These documents will be made available to the Administrator or any law enforcement official upon request. 27) The UAS will rem ain clear and yield the right of way to all manned aviation operations and activities at all times. 28) The UAS will not be operated by the PIC from any moving device or vehicle.29) The UAS will not be operated over congested or densely populated areas.

30) 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 UAS and/or debris in the event of an accident. I will ensure that nonparticipating persons remain under such protection. If a situation arises where nonparticipating persons leave such protection and are within 500 feet of the UAS , flight operations must ceas e immediately and/or; b. The aircraft is operated near vessels, vehicles or structures where the owner/controller of such vessels, vehicles or structures has granted permission and the PIC has made a safety assessment of the risk of operating closer to th ose objects and determined that it does not present an undue hazard, and; c. Operations nearer to the PIC, VO, operator trainees or essential persons do not present an undue hazard to those persons per § 91.119(a). 31) All operations will be conducted ov er private or controlled

- access property with permission from the land owner/controller or authorized representative. Permission from land owner/controller or authorized representative will be obtained for each flight to be conducted. 32) 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 will be r eported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

. If you have questions or need additional information, please contact me at marshall.frith@gmail.com or ( 571) 431 8514

. Thank you, Marshall Frith APPENDIX

– A DJI PHANTOM 3 TECHNICAL SPECIFICATIONS Marshall Frith only utilizes safe and reliable UASs. DJI is an industry leader in small UAS production. DJI UASs are loaded with ground breaking software enabling the user to set parameters which will not allow flight into controlledairspace. Parameters can also be set to limit flight to no higher than a

predetermined and set altitude as well as limit flig ht to a predetermined and set distance. In addition, DJI software provides real

-time altitude and location information to the PIC via the linked monitor (smart phone/tablet devices) DJI Phantom 3 1. Aircraft a. Supported Battery

– DJI 4480 mAH LiPo Batte ry b. Weight (Battery & Propellers Included)

– 2lbs 11.810oz (1242g) c. Hover Accuracy (Ready to Fly)

– Vertical: .8m; Horizontal: 2.5m d. Max Yaw Angular Velocity

- 200/s e. Max Tilt Angel

- 35 1.1.1.6 Max Ascent Speed

– 6m/s f. Max Descent Speed

– 2m/s g . Max Flight Speed

– 15m/s (NOT RECOMMENDED) 2. Gimbal a.Working Current

– Static: 750mA; Dynamic: 900mA b. Control Accuracy

- ±0.03 c. Controllable Range

– Pitch:

- 90

- 0 d. Maximum Angular Speed

– Pitch: 90/s 3. Camera a.Operating Temperature Range

- 32F

- 104F (0C

- 40C) b. Sensor Size

– 1/2.3” c. Effective Pixels

– 14M d. Resolution

– 4384x3288 e. HD Video Recording

– 1080p30 & 720p f. Recording Field of View

- 110/85 DJI Phantom 4 1. Aircraft a. Weight (including battery) 1380g b. Max Ascent speed

– 6 m/s c. Max Descent speed

– 4 m/s d. Max Speed

– 20 m/s e. Max Service Ceiling above sea level

– 19685 feet (6000m) f. Max flight time

– Approximately 28 mins g. Operating Temperature range 32F to 104F h. Satellite systems (GPS/GLONASS)

– 32 satellite constel lation i. Accuracy

- +

- 0.1m Vertical, +

- 0.3m Horizontal 2. Obstacle Sensing System a. Sensory range: 0.7m to 15mb. Operating Environment: Surface with clear pattern and adequate lighting (lux >15) 3. Camera a. Sensor 1/2.3” Effective pixels (12MP) b. Lens: (FOV 94 degrees 20mm) c. Video recording (4096 x 2160) 4K to 1280 x 720P at various frame rates from 24 to 120 fps 4. Remote controller a. Operating frequency: 2.400 to 2.483 GHz