Alacrity Productions, Inc

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4152 Arbor Lane Eagan, MN 55122

U.S. Department of Transportation Federal Aviation Administration October 21st, 2015

Re: Exemption request pursuant to Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation Regulations from: 14 CFR 21 subpart H ; 14 CFR 45.23(b) ; 14 CFR 61.113(a) and (b) ; 14 CFR 91.7(a); 14 CFR 91.9(b)(2); 14 CFR 91.109 ; 14 CFR 91.119(C); 14 CFR 91.121 ; 14 CFR 91.151(a); 14 CFR 91.203(a) and (b) ; 14 CFR 91.405(a); 14 CFR 91.407(a)(1); 14 CFR 9 1.409(a)(1) and (2) ; 14 CFR 91.417(a) and (b)

Dear Sir or Madam, Pursuant to Section 333 of the Federal Aviation Administration (FAA) Modernization and Reform Act of 2012 (the “Reform Act”) and 14 CFR Part 11, Alacrity Productions, Inc which owns and ope rates an Unmanned Aircraft System (UAS), hereby applies 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 333. Commercial operation of an UAS, as described herein, which are equipped with camera(s) and sensors, would operate in the following manner:

Aerial photography and/or video for public and/or private use including real estate, architecture, surveying, engineering and other related professional activities. Ae rial video and/or photography for public and/or private use including television, public events, private events, cinematography and news gath ering. Aerial inspection/photography of residential/commercial structures under contract with the owners or local government authority.

Alacrity Productions, Inc operates o ne Inspire1 (4 ) blade quadcopter W eighing 6.47 pounds. The UAS has a maximum airspeed of 49.21 miles per hour and uses a remote controller on an operating on fre quency of 5.725~5.825 GHz / 2.400~2.483 GHz and range of up to 5 km or 3.1 miles (unobstructed, free of interference) when FCC compliant. Up to 3.5 km or 2.1 miles (unobstructed, free of interference) when CE compliant. The Inspire1 is equipped with built in ground support technology that allows it to fly utilizing global positioning system (GPS) for stability, tracking, safe flight mode, and a return to home feature in the event of loss of remote control signal or critical low battery.All flights start with a preflight safety check and all flight data are recorded. The

Inspire1 is equipped with a gimbal

- mounted camera that sends a live video si gnal to the controller allowing the person in control (PIC) to monitor real

-time video. Flight data, speed height, distance, battery level and general aircraft conditions are also displayed during operation. The Inspire1 battery has a flight time of approx 18 minutes and is, therefore, always returned to original takeoff point and always flown utilizing visual line of sight (VLOS). The Inspire 1 maximum range is 4 00ft vertical. Our request for exemption would allow us to offer unique aerial photography and videography services to our clientele.

**UA S Safety Operating Parameters**  Wewill abide by the following additional operating conditions under this exemption, which ensures a level of safety during UAS flight including operating the UAS below 400 feet and within a radiu s of 1,000 feet from PIC always maintaining VLOS and obtaining 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. We will conduct a safety assessment of the risk of operating closer to those objects and determine that it does not present an undue hazard. Other safety operating parameters include:

Operate the UAS for 1520 minutes per flight. Land UAS prior to the manufacturer's recommended minimum level of battery power.

Operate the UAS during daylight hours only within VLOS. Utilize the UAS’ GPS flight safety feature whereby it hovers and then slowly lands if communication with the PIC is lost or battery becomes critically low. Always obtain all necessary permissions prior to operation.

Have procedures in place to abort flights in the event of safety breaches or potential danger. Review weather reports prior to flight and never operate UAS in unsafe conditions, high wind, low clouds or conditions that hinder visibility.

Only operate in safe environments that are strictly controlled, are away from power lines, elevated lights, airports and densely populated areas.

Also conduct extensive preflight inspections a nd protocols during which safety carries primary importance.

The PIC will also have a minimum of five hours logged on this craft and 10 hours minimum flying UAS quad copters under varying conditions and environm ents and will follow all safety protocol of Alacrity Productions, Inc as well as guidelines of 14 CFR §61.51(b) having the ability to safely operate the UAS in a manner consistent with the operating documents, including evasive and emergency maneuvers and maintaining appropriate distances from peopl e.**Specific Exemptions Requested**

Given the size, weight, speed and limited operating area associated with the UAS, an exemption from 14 CFR Part 21, Subpart H (Airworthiness Certificates) and 14 CFR 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. 11295 (Section 333). Werequest an exemption from 14 CFR 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 l ettering is difficult to place on such a small aircraft with dimensions smaller than the minimal lettering requirement. Regardless of this

, we can mark the UAS in the largest possible lettering by placing the word “Experimental” on its fuselage as required by 14 CFR 45.29(f) so that anyone will see the markings.

Werequest an exemption from 14 CFR 61.113(a) and (b) Private Pilot Privileges and Limitations: Pilot in Command. The applicant’s UAS do not carry any pilots or passengers nor property. The Risks attendant to the operation of the UAS is far less than the risk levels inherent in the commercial activities outlined in 14 CFR §61. The op eration and limitations in the flight operation manual (FOM) will equate to the safe operations of the UAS.

Werequest an exemption from 14 CFR 91.7(a) which prohibits the operation of an aircraft without an airworthiness certificate, since there is curre ntly no certificate applicable to our operation, this regulation is inapplicable. W e request an exemption from 14 CFR 91.405(a), 14 CFR 91.407(a)(1), 14 CFR 91.409(a)2) and 14 CFR 91.417(a) and (b) Maintenance inspections since they only apply to aircraft with an airworthiness certificate. However, as a safety precaution, we will perform a preflight inspection of the UAS before each flight as outlined in the attached operating documents.

Werequest an exemption from 14 CFR 91.9(b)(2) which requires an airc raft FOM in the aircraft, however, since there are no pilots or passengers on board the aircraft, and given its size, this regulation is inapplicable. Webelieve an equivalent level of safety will be achieved by maintaining a safety/flight manual with the UAS ground station.

Werequest an exemption from 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 th at aircraft has fully functioning dual controls. Although the Hexo+ is capable of dual/linked controls, we will be operating with a single remote controller.

Werequest an exemption from 14 CFR 91.119(c) which prescribes safe altitudes for the operation of civil aircraft, but allows helicopters to be operated at loweraltitudes in certain conditions. Wewill 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 and maneuverability and speed of the UAS, an equivalent or higher level of safety will be achieved.

Werequest an exemption from 14 CFR 91.121 Altimeter Settings, as it is inapplicable since the UAS utilizes electronic GPS with a barometric sensor. We request an exemption from 14 CFR 91.151(a) Fuel Requirements for Flight in visual flight rules (VFR) conditions. The U AS is 100 percent 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 only 15 minutes each and the UAS has an automated function, which results in immediate la nding 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 percent battery power remaining.

**Summary** Wewill comply with all of the following conditions and limitations should this grant of exemption be provided:

1. Operations will be limited to the following aircraft described in the operating documents which is a quadcopter weighin g less than seven pounds:

2. The UAS will not be flown at an indicated airspeed exceeding 4 5 mph.

3. The UAS will be operated at an altitude of no more than 400 feet AGL, as indicated by the procedures specified in the operating documents.

4. The UAS will be operated within VLOS of the PIC at all times.

5. All operations may utilize a visual observer (VO. The UAS will be operated within the VLOS of the VO at all times. The VO and PIC will be able to communicate verbally at all t imes. 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 wil l be accessible during the 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 i t 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 flight . The Ground Control Station will be included in the preflight inspection. All maintenance and alterations will be properly documents 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 into the aircraft records.

9. The preflight inspection section in the operating documents will accoun t for all discrepancies, i.e. inoperable components, items or equipment not already covered in the relevant sections of the operating documents.

10. Wewill follow the UAS manufacturer’s aircraft/component, maintenance, overhaul, replacement, inspection and life limit requirements.

11. Wewill carry out maintenance, inspections and recordkeeping requirements, in accordance with the op erating documents. Maintenance, inspection and alterations will be noted in the aircraft records, including total flight h ours, 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's Safety Bulletins.

13. An authorized person will make an entry in the aircraft record of the corrective action taken against discrepancies discovered between inspections.

14. The PIC will also meet the flight review requirements specified in 14 CFR 61.56 in an aircraft in which the PIC is rated on.

15. Prior to operations conducted for the purpose of aerial videography/cinematography and augmenting real estate listing videos (or similar operations), the PIC will have accumulated and logged, in a manner consistent with 14 CFR 61.51(b), a minimum of five hours as an UAS pilot operating the make and model of the UAS to be used in operations.

16. The PIC will not operate the UAS for the purpose of aerial videography/cinematography and augmenting real estate listing videos (or 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 manner consistent with the operating documents, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicles and structures.17. UAS operations will not be conducted during night hours, as defined in 14

CFR 1.1 All operations will be conducted under visual meteorological conditions (VMC).

18. The UAS will not operate within five nautical miles of an airport referen ce point as denoted on a current FAApublished aeronautical chart.

19. 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 three statute miles from the PIC.

20. If a UAS l oses communications or loses its GPS signal, it will return to a predetermined location within the planned operating area and land or be recovered in accordance with the operating documents.

21. The PIC will abort a flight in the event of unpredicted obstacles or emergencies in accordance with the operating documents.

22. The PIC will not begin a flight unless, considering wind and forecast weather conditions, there is enough power to fly at a normal cruising speed to the intended landing point and land the UAS with 30 percent battery power remaining.

23. 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 oversigh t agency requirements.

24. The documents required under 14 CFR 91.9 and 14 CFR 91.203 would be available to the PIC at the Ground Control Station of the UAS at any time the UAS is operating. These documents will be made available to the Administrator or a ny law enforcement official upon request.

25. The UAS will remain clear and yield the right of way to all manned aviation operations and activities at all times.

26. The UAS will not be operated by the PIC from any moving device or vehicle.

27. The UAS will not be operated over congested or densely populated areas unless contracted out to do events.

28. Flight operations will be conducted at least 500 feet from all nonparticipating persons, vessels, vehicles and structures unless:a. Barriers or structu res are present that sufficiently protect nonparticipating

persons from the UAS and/or debris in the event of an accident. Wewill 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 cease immediately. b. The aircraft is operated near vessels, vehicles or structures where the owner/controller of such vessels, vehicles or structures has granted permission and th e PIC has made a safety assessment of the risk of operating closer to those objects and determined that it does not present an undue hazard. c. Operations near to the PIC, VO, operator trainees or essential persons do not present an undue hazard to those p ersons per 14 CFR 91.119(a).

29. All operations will be conducted over private or controlled access property with permission from the landowner/controller or authorized representative. Permission from land owner/controller or authorized representative wil l be obtained for each flight to be conducted.

30. Any incident, accident or flight operation that transgresses the lateral or vertical boundaries of the operational area as defined by the applicable certificate of authorization (COA) will be reported to the FAA’s UAS Integration Office (AFS80) within 24 hours. Accidents will be reported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB website: www.ntsb.gov

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On behalf of Alacrity Productions, Inc. , I would like to thank you for your consideration in granting this exemption.

Steven D. Johnson President Alacrity Productions, Inc.

AIRCRAFT

– DJI Inspire1 Model T600 We ight (Battery Included) 2935 g Hovering Accuracy (GPS mode) Vertical: 0.5 m Horizontal: 2.5 m Max Angular Velocity Pitch: 300°/s Yaw: 150°/s Max Tilt Angle 35° Max Ascent Speed 5 m/s Max Descent Speed 4 m/s Max Speed 22 m/s (ATTI mode, no wind) Max Service Ceiling Above Sea Level 4500 m (Default altitude limit: 120 m above takeoff point)Max Wi nd Speed Resistance 10 m/s

Max Flight Time Approximately 18 minutes Motor Model DJI 3510H Propeller Model DJI 1345T Indoor Hovering Enabled by default Operating Temperature Range

- 10° to 40° C Diagonal Distance 559 to 581 mm Dimensions 438x451x301 mm Power Spectral Density 9.06mW/MHz