February 2 6 , 2016

U.S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590

Re: Petition of Drone Shots f or an Exemption Pursuant to Section 333 of the FAA

Modernization and Reform Act of 2012

Direct or: Flight Standards Service:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 ("Reform Act") and
14 C.F.R. Part 11, Drone Shots (“ Petitioner ”) hereby applies for an exemption from the Federal Aviation Regulations ("FARs") identifie d below to allow commercial operation of small unmanned aerial vehicles ( i.e., "small unmanned aircraft" or "UAS") for the purpose o f conducting a erial photography

, videography

, c inematography , inspection, mapping and imaging

for the motion picture, televi sion , real estate, construction and web industr ies

.

This petition for exemption is made based on information outlined in this Petition for Exemption, as well as the accompanying Petitioner documents;

1. PIC Flight Operations Manual and;

2. Operations M anuals (C ollectively 2 and 3 are referred to as Documents & Manuals")

3. User Guide and;

4. Flight Manual 1 (Collectively 3 and 4 are referred to as "Manufacturer's Manuals")

Petitioner submits these supporting materials as confidential documen ts pursuant to 14 C.F.R. § 11.35(b), as the materials contain confidential commercial and/or proprietary information that

Petitioner has not and will not share with other requesting parties. Additionally, these d ocuments contain operating conditions and pr ocedures that are not generally available to the public and are protected from release under the Freedom of Information Act, 5 U.S.C. § 552 et. seq.



### NOTE: ALL ATTACHMENTS SET FORTH IN SUPPORT OF THIS LETTER OF

PETITION ARE CONFIDENTIAL AND SHALL NOT BE RELEASED TO THE

PUBLIC WITHOUT WRITTEN AUTHORIZATION FROM THE PETITIONER.

1 . The term "Manufacturer's Manual" also includes all relevant manufacturer publications, including, but not limited to: operations and flight manuals, user guides, component maintenance manuals, pilot training manuals, service

inf ormation letters and, safety/service bulletins

.U.S Department of Transportation

February 2 6 , 2016 Page 2

For your convenience, this Petition is organized as follows:

I. De scription of Petitioner

II. Description of Proposed Operations

A. Aerial Videography

, Photography

, Cinematography

, Inspecti on, Mapping and Imaging

III. Relevant Statutory Authority

IV. Petitioner ’ s Proposed UAS Operations Meet the Requirements of

Section 3 33 of the Reform Act

A. Approval is Warranted Based on the UAS's Size, Weight, Speed, and Operational Capability

B. Approval is Warran ted Based on the Operational Restrictions Set Forth in the Operations Manuals

V. Regulations From Which Exemption is Requested

A. 14 C.F.R. Part 21, Subpart H

– Airworthiness Certificates and 14 C.F.R. § 91.203(a)(1)

B. 14 C.F.R. Part 27 Airworthiness Standards: Normal Category Rotorcraft

C. 14 C.F.R. §§ 91.9(c), 45.23(b) and 45.27(a): Aircraft Marking and Identification Requirements

D. 14 C.F.R. § 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2); 91.417(a) and (b): Maintenance Inspections

E. 14 C.F.R. Part 61, 14 C.F.R. § 61 .3, 14 C.F.R. § 61.113: Private Pilot Privileges and Limitations

F. 14 C.F.R. § 91.7(a): Civil Aircraft Airworthiness

G. 14 C.F.R. § 91.9(b)(2): Civil Aircraft Flight Manual in the Aircraft and 14 C.F.R. § 91.203(a) and (b): Carrying Civil Aircraft Certification and Registration

H. 14 C.F.R. § 91.103: Preflight Action

I. 14 C.F.R. § 91.109(a): Flight Instruction

J. 14 C.F.R. § 91.119(c): Minimum Safe Altitudes

K. 14 C.F.R. § 91.121: Altimeter Settings

L. 14 C.F.R. § 91.151(a): Fuel Requirements for Flight in VFR Conditions

V I

. Drug and Alcohol Program

VII. Public Interest

VIII. Privacy

IX. Federal Register Summary

X. ConclusionU.S Department of Transportation

February 2 6 , 2016 Page 3

I. DESCRIPTION OF PETITIONER

Petitioner is based in Sun Valley

, CA and provides aerial photography, videography,

c inematography , inspect ion, mapping and imaging for the motion picture, television, real estate

and web industries

. T he Company’s Principal and Chief Pilot Erwin S. Aviles has been flying UAV Quadcopters as a hobby for more than year without incident, logging hundreds of hours

f lying

. He also has experience as a student pilot since 1998 flying in five different model airplanes.

Upon the grant of the 333 Exemption the Company’s business will specialize in aerial photography, videography, c inematography , inspection, mapping and i maging for the motion picture, television, real estate and web industries

.

Petitioner ’s staff are well trained and experienced in providing support as visual observers (“VO”) for the pilot in command (“PIC”) in addition to any other needed on site assis tance

.
All of the equipment owned by Petitioner is of the highest quality gear and ha s been able to provide these services safely and without any claims or incident

. Petitioner ’s goal is to advise the perspective client that Petitioner is following all th e applicable state and federal rules to ensure the safety of the public while providing the client with a competitive and cost effective product.

Petitioner seeks an exemption to allow for aerial photography, videography , cinematography

, inspection

, mappi ng and imaging and other related media products.

The contact information for Petitioner is as follows:

Erwin S. Aviles

Drone Shots 10860 Stagg Street Sun Valley, CA 91352

Phone: 818 .653.9183: Email: steveaviles@droneshot

. co

II. DESCRIPTION OF PROPOSED OPERATION

Petitioner seeks an exemption pursuant to Section 333 of the Reform Act to operate the DJI

Blade Chroma (referred to DS

- UAS ) (under 55lbs) for the proposed operations discussed herein

below. All UAS operations will occur under tightly controlle d conditions on private property or approved location where Petitioner has received verifiable permission to operate from the landowner, controller or authorized representative. The proposed UAS operations will be

conducted in accordance with the condition s and limitations of this Petition for Exemption and

Petitioner ’s Operations Manuals. As detailed in Petitioner ’s Operations Manuals, all UAS operations will be limited to daytime VFR conditions, within visual line

- of

- sight ("VLOS") of the operator, in un controlled airsp ace, and will occur at least 5 n m away from an airport reference point

. Moreover, Petitioner ’s Operations Manuals incorporate redundant safeguards to assure the aircraft does not travel outside the controlled area of UAS operations, includi ng GPS "geo

- fencing" technologies.U.S Department of Transportation

February 2 6 , 2016 Page 4

A. Aerial Videography, Photography, Cinematography, Inspection, Mapping

and Imaging

Petitioner seeks to use small DS

- UAS for the purpose of conducting aerial photography, videography, c inematography , inspection, mapping, im aging and for the motion picture,

televis ion, real estate and web industries

. Petitioner has purposefully tailored its operations to meet the requirements established by the FAA in prior grants of exem p tion authorizing

commercial use of UAS in the real es tate indu s try, including :

 Astraeus Aerial (Exemption No. 11062)

 Aerial MOB, LLC (Exemption No. 11066)

 Pictorvision, Inc. (Exemption No. 11067)

 HeliVideo Productions, LLC (Exemption No. 11065)

 Snaproll Media, LLC (Exemption No. 11063)

 RC Pro Productions Co nsulting, LLC d/b/a Vortex Aerial (Exemption No. 11064)

 Flying

- Cam, LLC (Exemption No. 11080)

 Aerocine, LLC (Exemption No. 11150)

 Team 5, LLC (Exemption No. 11158)

 Alan D. Purwin (Exemption No. 11161)

 Helinet Aviation Services, LLC (Exemption No. 11160)

 Pi cture Factory, Inc. (Exemption No. 11178)

 Airshark (Exemption No. 11 651 )

 Trudeau, Realtor® (Exemption No. 11138)

 Alon Sicherman (Exemption No. 11728)

All UAS photography

, videography

, cinematography , mapping, imaging and inspection operations will occur o n private property or approved location in a controlled area away from spectators and persons not involved in the recording process . In addition, the operations will be

conducted between dawn and dusk to ensure maximum safety for the public and those invol ved in the manipulation and operation of the UAS ; VFR conditions, at altitudes below 400' above ground level (“AGL”).

As set forth below, Petitioner ’s operations provide an equivalent level of safety which is superior to performing the same work using co nventional fixed

- wing aircraft or helicopters.

Small UAS recording operations is also safer than traditional manned aircraft perfor m ing the

same function. Videographer , photographers and inspectors also frequently need to climb roof

tops , trees, ladders o r otherwise perform elevated work, which exposes them to the risk of dangerous falls, ele c trocution or other work related injuries . In addition, depending on the nature of the video needed and inspection, proximity to equipment, and other mechanical

hazard s associated with industrial sites and construction facilities often involves a risk of exposure to hazardous cond i tions . The use of DS

- UAS mitigates these hazards and is ultimately a much safer and cost e f ficient method of performing these and most other types of recording operations.

Moreover, c onventional operations using rotorcraft and fixed

- wing aircraft in low level operations present risks associated with vehicles weighing tens of thousands of poundsU.S Department of Transportation

February 2 6 , 2016 Page 5

(including payload) and carrying large amounts o f fuel which inherently presents significant fire hazards as well as exposure to other chemical contaminates

. It is important to note the use of small UAS in this area will not only be safer and more cost effective to the perspective user or purchaser of the service , but the quality and expanse of acquired information will be far more robust given the low cost associated with its acquisition and other potential consumers an inexpensive product

.

UAS video production is more reliable, and allows for the co llection, dissemination, and storage

of visual and other sensory data with greater precision and duration at a very low cost . Small UAS will also be capable of accessing and inspecting areas that would otherwise be inaccessible or highly dangerous using c onventional aircraft or other inspection methods.

III. RELEVANT STATUTORY AUTHORITY

This Petition for Exemption is submitted pursuant to Section 333(a) through (c) of the FAA Modernization and Reform Act of 2012 ("Reform Act"). Congress has directed the FAA "to safely accelerate the integration of civil unmanned aircraft systems into the national airspace system." Pursuant to Section 333 of the Reform Act, the FAA Administrator is to permit

u nmanned aircraft systems to operate in the National Air s pace Sys tems ("NAS") where it is safe

to do so b ased on the following considerations:

● The UAS's size, weight, speed and operational capability; ● Operation of the UAS in close proximity to airports and populated areas; and ● Operation of the UAS within the visu al line of sight of the operator.

Additionally, the FAA Administrator has general authority to grant exemptions from the agency's safety regulations and minimum standards when the Administrator decides a requested exemption is in the public interest. See 49 U.S.C. § 106(f) (defining the authority of the Administrator); 49 U.S.C. § 44701(f) (permitting exemptions from §§ 44701(a), (b) and §§ 44702

– 44716, et seq.). A party requesting an exemption must explain the reasons why the exemption: (1) would benefi t the public as a whole, and (2) would not adversely affect safety (or how it would provide a level of safety at least equal to the existing rules). See 14 C.F.R. § 11.81 (petitions for exemption).

IV. PETITIONER ’S PROPOSED DS

- UAS OPERATIONS MEET THE REQU IREMENTS OF SECTION 333 OF THE REFORM ACT

The small DS

- UAS operations proposed by Petitioner as noted above in this Petition for Exemption qualify for expedited approval pursuant to Section 333 of the Reform Act as each of the statutory criteria and relev ant factors are satisfied.

A. Approval is Warranted Based on the UAS's Size, Weight, Speed, and Operational Capability

A Grant of Exemption is appropriate for operations conducted using the UAS s due to their size weight, speed, and operational capability.U.S Department of Transportation

February 2 6 , 2016 Page 6

 The DS

- UAS utilize d by Petitioner ha s been approv ed for use in prior Section 333

Grants of Exemption from the FAA. 2

 The DS

- UAS weigh s less th an 55 pounds, including payload

 The DS

- UAS will not be flown at a ground speed in excess of 87 knots (100 mph)

. T he exemption holder may use either groundspeed or calibrated airspeed to determine compliance with the 87 knot speed restriction

 Altitude information will be generated by equipment onboard the UA S as specified using GPS triangulation, digitally encoded ba rometric altimeter, radio altimeter, or any combination thereof. This information will be transmitted to the pilot

via telemetric data feed.

 The DS

- UAS will have system redundancies and independent functionality to ensure the overall safety and predictabi lity of the system. If connection to the remote control or ground control station is lost, failsafe systems will permit the UAS to return to a predetermined location and safely land without injury or damage.

 The radio frequencies used for operations and c ontrol of the DS

- UAS comply with the Federal Communications Commission ("FCC") and other appropriate government oversight agency requirements. T he operating frequency for the DS

- UAS

is 2.4 and 5.8 GHz frequency bands.

If the same operations were conducted using a helicopter, the aircraft's take

- off weight would likely exceed 6,000 pounds depending on payload . The difference in weight between the DS

UAS and a helicopter significantly reduces the potential harm to the participating and non

participating ind ividuals and/ or surrounding property in the event of an unintended accident or incident. In addition, the risk to the onboard pilot and camera operator is eliminated.

B. Approval is Warranted Based on the Operational Restrictions Set Forth in

Petitioner ’s O perations Manuals

Operations Manuals and the Manufacturer's Manual for the selected DS

- UAS will contain all the procedures and limitations necessary to safely and successfully perform the operations specified in this Petition for Exemption. To assist the FAA in making a safety assessment of Petitioner ’s proposed operations, below is a summary of operational limitations and conditions that Petitioner will adhere to, and which will ensure an equivalent or higher level of safety to operations

conducted under current regulatory guidelines:

1. The DS

- UAS weighs less than 55 pounds, with payload

.

2 See e.g., Grant of Exemption to Shotover Camera Systems L.P. (Exemption No. 11159); Grant of Exemption to VDOS Global, LLC (Exemption No. 11112); Grant of Exemption to LowCountryRC, Corp. (Exemption No. 11 184); Grant of Exemption to Alan Purwin (Exemption No. 11161); Grant of Exemption to Helinet Aviation Services (Exemption No. 11160); Grant of Exemption to Total Safety U.S., Inc. (Exemption No. 11156).

.U.S Department of Transportation

February 2 6 , 2016 Page 7

2. All operations shall be conducted over private or controlled

- access property with

verifiable permission from the land owner/controller or authorized representative.

Permis sion from land owner/controller or authorized representative will be obtained

for each scheduled flight prior to operation

.

3. All UAS operated under the Grant of Exemption will be identified by serial number, registered in accordance with 14 CFR part 47, an d have identification (N

- Number) markings in accordance with 14 CFR part 45, Subpart C. Markings will be as large as practicable.

4. Minimum crew for each flight operation will consist of a pilot, who will be Pilot

- in Command ("PIC") of the DS

- UAS , and one o r more Visual Observers ("Observer") as necessary to safely conduct the mission.

5. PICs shall possess either a private, recreational, or sport pilot certificate. The PIC

must also hold a current FAA airman medical certificate or a valid U.S. driver’s

licens e issued by a state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal government. The PIC will also meet the flight review requirements specified in 14 C.F.R 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate

.

6. The DS

- UAS shall be operated within VLOS of the PIC and Observer at all times. The PIC must use human vision unaided by any device other than corrective lenses, as specified on the PIC's FAA

- issued medical certificate.

7. The PIC and Observe r designated for any operation will be able to communicate verbally at all times.

8. Electronic messaging or texting will not be permitted during flight operations.

9. The additional requirements identified in the Grant of Exemption shall be added to

the Petit ioner ’s Operations Manuals. The Operations Manuals will be maintained and made available to the Administrator upon request. If a discrepancy exists between the conditions and limitations in the Grant of Exemption and Petitioner ’s Operations Manuals, the c onditions and limitations in the Grant of Exemption shall take precedence and must be followed. Otherwise, Petitioner shall follow the procedures outlined in their Operations Manuals.

10. Petitioner may update or revise its Operations Manuals. Revisions will be tracked and a revised copy of the Manual will be provided to the Administrator upon request.

Petitioner will also present an updated and revised Operations Manuals if it petitions for extension or amendment to its Grant of Exemption. If an update or re vision would

a f fect the basis upon which the FAA grants the exemption, Petitioner will seek an amendment to its Grant of Exemption. Petitioner will contact the FAA’s UAS Integr a tion Office (AFS

- 80) if questions arise regarding updates or revisions to the

o pe r ating documents.U.S Department of Transportation

February 2 6 , 2016 Page 8

11. Petitioner Operations Manuals and its Grant of Exemption will be available to the

PIC at the ground control station anytime the DS

- UAS is operating.

12. The PIC is prohibited from beginning a DS

- UAS flight unless (considering wind and

fo recast weather conditions) there is enough power to fly to the first intended point of landing, and assuming normal cruising speed, to fly after that for at least 10 minutes.

13. Maximum total flight time for each operational flight using the DS

- UAS will be

limited to 40 minutes or the amount of time the UAS can be flown and still maintain a reserve battery power of no less than 25%, whichever occurs first.

14. Flights will be operated at an altitude of no more than 400 feet AGL and will never enter navigable co ntrolled airspace without timely prior written authorization and approval from the FAA. In the event the structure being inspected exceeds 400 feet AGL, the UAS will not be operated more than 100 feet above the highest point on the structure, and no more t han 50 feet horizontally from the structure.

15. Flight operations must be conducted at least 500 feet from all nonparticipating persons. (persons other than the PIC, VO, operator trainees or essential persons), vessels, vehicles, and structures unless:

a. Barr iers or structures are present that sufficiently protect nonparticipating persons from the UA and/or debris in the event of an accident. The operator must ensure that nonparticipating persons remain under such protection. If a situation arises where nonpar ticipating persons leave such protection and are within 500 feet of the UA, flight operations must cease immediately and/or;

b. The aircraft is operated near vessels, vehicles or structures where the owner/controller of such vessels, vehicles or structures h as granted permission and the 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, and;

c. Operations nearer to the PIC, VO, operator trainees or essential persons do not

p resent an undue hazard to those persons per § 91.119(a).

16. The DS

- UAS may 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.

17. The DS

- UAS may not operate wi thin 5 nm of an airport reference point as denoted on

a current FAA

- published aeronautical chart unless a letter of agreement with that airport’s management is obtained, and the operation is conducted in accordance with a NOTAM as required by the Petitione r COA. The letter of agreement with the airport management will be made available to the Administrator upon request.

18. Prior to each flight the PIC shall inspect the DS

- UAS to confirm that it is in a condition safe for flight. The pre

- flight inspection wil l account for all discrepancies, e.g. inoperable components, items, or equipment, not already covered in the relevant sections of the operating documents as well as equipment updates . The PIC shall notU.S Department of Transportation

February 2 6 , 2016 Page 9

operate any DS

- UAS if the inspection reveals a conditi on that affects the safe

operation of the DS

- UAS until the necessary maintenance has been performed and the

DS

- UAS is found to be in a condition for safe flight. The ground control station shall be included in the preflight inspection. All maintenance and alternations must be properly documented in the UAS ’s records as required by Petitioner ’s Operations

Manuals.

19. Petitioner will timely carry out its maintenance, inspections, and record keeping requirements in accordance with the Operations Manuals. Mainten ance, inspection,

and alterations will be fully noted in the DS

- UAS records, including total time in service, description of work accomplished, date completed and the signature of the authorized person returning the DS

- UAS to service.

20. Any DS

- UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics (e.g., replacement of a flight critical component)

must timely undergo a functional test flight in accordance with Petitioner ’s Operations Manuals. The PIC who con ducts the functional test flight must make an entry in the UAS aircraft records of the flight. The requirements and procedures for a functional test flight and DS

- UAS record entry shall be included in the Petitioner ’s Operations Manuals.

21. The DS

- UAS will b e operated and maintained according to the Manufacturer's Manuals and any required manufacturer Safety/Service Bulletins and product updates

.

22. Prior to the operation, a Mission Packet will be created in accordance with the requirements on Petitioner ’s Oper ations Manuals.

23. Petitioner will obtain an Air Traffic Organization ("ATO") issued Certificate of Waiver or Authorization, otherwise known as a COA, prior to conducting any operations under this Grant of Exemption. A NOTAM will be issued as required by

the COA. All operations will be conducted in accordance with airspace requirements in the ATO issued COA including class of airspace, altitude level and potential transponder requirements.

24. All required permissions and permits will be obtained from territoria l, state, county or city jurisdictions, including local law enforcement, fire or other appropriate governmental agencies.

25. If the DS

- UAS loses communication with the PIC , it will have the capability to safely

return to a pre

- determined location within the operational area and land safely.

26. Contingency plans will be in place to safely terminate flight if there is a loss of

communication between the PIC and the Observer.

27. The DS

- UAS will have the capability to safely abort flight in the case of unpredicted

ob stacles or emergencies.U.S Department of Transportation

February 2 6 , 2016 Page 10

28. PICs and Observers will have at least a curren t Class III Medical Certificate or a valid

and current state driver’s license issued within the United States

.

29. Prior to conducting operations for filming, the PIC will have accumula ted and logged, in a manner consistent with 14 CFR § 61.51(b), a minimum of 200 flight cycles and 25 hours total time as a UAS rotorcraft pilot and at least 10 hours logged as a UAS

p i lot with a similar DS

- UAS type platform

. This requirement can be achieve d by flights conducted and logged as a hobbyist

.

30. Prior to conducting operations for filming, the PIC will have accumulated and logged,

in a manner consistent with 14 CFR § 61.51(b) , a minimum of hours pursuant to 54 CFR § 61.51(b) as UAS pilot operating t he make and model of DS

- UAS to be utilized for operations under the exemption and three take

- offs and three landing in the preceding 90 days

.

31. Operations shall occur during daytime VFR Meteorological Conditions; flights under special visual flight rules (" SVFR") shall not be conducted.

32. The DS

- UAS shall remain clear and yield the right of way to all other manned operations and activities at all times (including, but not limited to, ultralight vehicles, parachute activities, parasailing activities, hang glid ers, etc.).

33. DS

- UAS Operations under Instrument Flight Rules, at night, or beyond VLOS are prohibited.

34. T he UAS will not be operated from an elevated platform unless designed and engineered specifically for such purposes and be in compliance with the gener al restrictions imposed by the applicable regulations . Additionally no PIC will provide any film

- flight operations while in motion from atop any elevated platform vehicle or

device.

35. Before conducting operations, the radio frequency spectrum used for opera tion and

control of the DS

- UAS will comply with the Federal Communications Commission (FCC) or other appropriate government oversight agency requirements.

V

. REGULATIONS FROM WHICH EXEMPTION IS REQ UESTED

The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This statutory authority, by its terms, includes exempting civil aircraft, as the term is defined under § 40101 of the Act, including UASs, from its safety regulations and minimum standards when the

Administrator decides a requested exemption is in the public interest. 3

Petitioner seeks an exemption from several interrelated provisions of Title 14 of the Code of Federal Regulations ("14 C.F.R") Parts 21, 45, 61 and 91 for purposes of conducting the

3 49 U.S.C. § 44701(f) (authorizing the grant of ex emptions from requirements of regulations prescribed pursuant to Sections 44701(a) and (b) and Sections 44702

- 44716).U.S Department of Transportation

February 2 6 , 2016 Page 11

requested operations u sing DS

- UAS platforms noted above . Listed below are: (1) the specific sections of 14 C.F.R for which exemption is sought, and (2) the operating procedures and safeguards that Petitioner has established which will ensure a level of safety better than or equ al to the rules from which exemption is sought. 4

UNMANNED AIRCRAFT SYSTEM

A. 14 C.F.R. Part 21, Subpart H

– Airworthiness Certificates and 14 C.F.R. §91.203(a)(1)

The FAA has stated that no exemption is needed from this section if a finding is made under t he Reform Act that the UAS selected provides an equivalent level of safety when compared to aircraft normally used for the same application. These criteria are met and in point of fact

exceeded

, and therefore no exemption is needed. 5 If, however, the FAA determines that there are some characteristics of the chosen UAS that fail to meet the requirements of the Reform Act, an exemption is requested.

Equivalent Level of Safety

Petitioner ’s use of the DS

- UAS is safe when taking into account its size, weight , speed, and operational capability. As set forth in the description of proposed operations in Section IV(A),

the DS

- UAS weigh s less than 55 poun ds , including payload and will not be flown at a ground speed in excess of 87 knots (100 mph)

. The DS

- UAS is a lso equipped with safety features which will allow Petitioner to operate the DS

- UAS safely after experienc ing certain in

- flight

4 14 C.F.R § 11.81(e), which requires a petition for exemption to include: The reasons why granting the exemption would not adversely a ffect safety, or how the exemption would provide a level of safety at least equal to that provi d ed by the rule from which you seek exemption.

5 See Grant of Exemption No. 11062 to Astraeus Aerial (FAA

- 2014

- 0352 at pgs. 13

- 14, 22).U.S Department of Transportation

February 2 6 , 2016 Page 12

contingencies or failures as noted below

. 6 7 Additionally, the DS

- UAS carr ies neither pilots nor

passengers, carr ies no explosive materials or flammable liquid fuels, or other elements identified by Homeland Security as being prohibitive and operate exclusively within the parameters stated

in Petitioner ’s Operations Manuals

.

Operations conducted under this exemp tion will be closely controlled and monitored by the PIC operator and will be conducted in compliance with local public safety requirements, to provide security for the area of operation. Petitioner will also provide the FAA with advance notice of all

oper ations via NOTAMs as required by the applicable COA. In all cases, operation of the DS

UAS under the proposed conditions will be at least as safe as, or safer than, conventional rotorcraft operating with an airworthiness certificate

. Lastly, the DS

- UAS do not need a means to communicate with other aircraft or ATC, because those capabilities will be solely possessed by the PIC and Observer, who are not onboard the DS

- UAS

. 8 In addition, no sense

- and

- avoid technology is necessary for the DS

- UAS because they w ill be operated at all times in VFR conditions and within VLOS of the PIC and Operator

. 9

B. 14 C.F.R. Part 27 Airworthiness Standards: Normal Category Rotorcraft

Title 14 C.F.R. Part 27 sets forth the procedural requirements for airworthiness certification of normal category rotorcraft. To the extent that Petitioner ’s small DS

- UAS would otherwise require certification under Part 27, Petitioner seeks an exemption from Part 27's airworthiness standards for the same reasons identified in the request for exempt ion from 14 C.F.R. R. Part 21, Subpart H, supra

.

6 See e.g., Grant of Ex emption No. 11184 to Low Country RC, Corp. (FAA

- 2014

- 0803 at pg. 3): "The [DJI S1000] has the capability to operate safely after experiencing certain in

- flight contingencies or failures and uses an auto

pilot system to maintain UAS stability and control. T he UAS is also able to respond to a loss of global positioning system (GPS) or a lost

- link event with a pre

- coordinated, predictable, automated flight maneuver, and manual flight control functionality as a backup. These safety features provide an equivalen t level of safety compared to a manned aircraft performing a similar operation."

7 See e.g., Grant of Exemption No. 11184 to VDOS Global, LLC. (FAA

- 2014

- 0382 at pgs. 4

- 5): "The DS

- UAS can be operated entirely by a touch

- screen, map

- based interface. This m eans the operator only needs to command the system where to go, and the system does all the flying for the operator. The DS

- UAS can be operated in both semi and fully autonomous flight modes, with the operator simply clicking on a map to create a pre

- plann ed flight path for a flight. In addition, the operator can create no fly zones or maximum flight ranges and altitudes so the system cannot enter areas deemed unsafe or unnecessary to fly over. The petitioner states further that the UAS has built

- in

intelli gent fault handling which allows the DS

- UAS to detect a system fault while in the air and automatically fly back to its takeoff location and land. Faults that can be detected include: loss of communication; exceeding pre

- set wind thresholds; and low batter y levels.

All flight operations are global positioning system (GPS) controlled, making the system easy to navigate. At any point if the operator is not explicitly commanding the system to move, the system automatically holds its GPS position. The flight c ontrol system employs not only GPS positioning but a variety of sensors including sonar, barometric pressure, temperature, wind speed and others to ensure stability so long as wind thresholds are not exceeded. Also a flight termination link

– to prevent a 'fly away' or other potentially dangerous situation

– is available to the operator."

8 See Grant of Exemption No. 11062 to Astraeus Aerial (FAA

- 2014

- 0352 at pg. 13).

9 . IdU.S Department of Transportation

February 2 6 , 2016 Page 13

C. 14 C.F.R. §§ 91.9(c), 45.23(b) and 45.27(a): Aircraft Marking and Identification Requirements

Petitioner seeks an exemption from the aircraft marking and identification requirements contained in 14 C.F.R. § § 91.9(c), 45.23(b) and 45.27(a).

● 14 C.F.R. § 91.9(c), Civil Aircraft Flight Manual, Marking and Placard requirements, provides that:

No person may operate a U.S.

- registered civil aircraft unless that aircraft

is identified in accordance with Part 45 o f this chapter.

● 14 C.F.R. § 45.23(b), Markings of the Aircraft, states:

When 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 provisiona lly 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 nor more than 6 inches high, the words "limited," "restricted," "light

- sport, "experime ntal," or "provisional," as applicable.

● 14 C.F.R. § 45.27(a), Rotorcraft, states:

Each operator of a rotorcraft must display on that rotorcraft horizontally on both surfaces of the cabin, fuselage, boom, or tail the marks required by § 45.23.

In a previous Grant of Exemption, the FAA determi ned that exemption from these requirements was warranted provided that the aircraft "have identification (N

- Number) markings in accordance with 14 C.F.R Part 45, Subpart C if the markings are as large as practicable." 10

Equivalent Level of Safety

All DS

- U AS flown by Petitioner will bear N

- number markings that are as large as practicable in accordance with 14 C.F.R. Part 45, Subpart C. 11

D. 14 C.F.R. § 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2); 91.417(a) and (b): Maintenance Inspections

Petitioner seeks a n exemption from the maintenance inspection requirements contained in 14 C.F.R. § 91.405(a), 91.407(a) (1), 91.409(a)(2); 91.417(a) and (b). These regulations specify maintenance and inspection standards in reference to 14 C.F.R. Part 43. See, e.g., 14 C.F .R. § 91.405(a) (stating that each owner or operator of an aircraft "[s]hall have the aircraft inspected as

10

. FAA Docket No. FAA

- 2014

- 0352.

11

. See, e.g., FAA D ocket No. FAA

- 2014

- 0352, at 14.U.S Department of Transportation

February 2 6 , 2016 Page 14

p rescribed in subpart E of this part and shall between required inspections ...have discrepancies repaired as prescribed in part 43 of this chapter"). An exemption from these regulations is needed because Part 43 and these sections only apply to aircraft with an airworthiness certificate, which

the UAS platforms to be operated under this grant of exemption will not have

. ( Emphasis added)

Equivalent Le vel of Safety

An equivalent level of safety will be achieved or exceeded because maintenance and inspections

will be timely performed in accordance with the Manufacturer's Manual and any required manufacturer Safety or Service Bulletins. Further, as requi red by Petitioner ’s Operations Manuals, the PIC will conduct a pre

- flight inspection of the DS

- UAS and all associated equipment to account for all discrepancies and/or inoperable components. Maintenance will be performed and verified to address any conditi ons potentially affecting safe operation of the DS

UAS and no flights will occur unless, and until, all flight critical components of the DS

- UAS have been found to be airworthy and in a condition safe for operation. A functional test flight will

be conduct ed following the replacement of any flight

- critical components. As required by

Petitioner ’s Operations Manuals, the PIC who conducts the functional test flight will make an entry in the DS

- UAS aircraft records of the flight.

Petitioner ’s Operations Manual also includes requirements to follow the manufacturer’s UAS aircraft/component, maintenance, overhaul, replacement, inspection, and life limit requirements for the following applicable components: powertrain system (powerplant), propellers, avionics

and c ontrol surfaces (including ailerons/elevons), structures & airframe, camera system, electrical systems (including batteries), ground control station, hazard accessories , and spare parts. Further, Petitioner ’s Operations Manuals also include procedures to d ocument and

maintain a record of the DS

- UAS ’s maintenance, preventative maintenance, alterations, status of replacement /overhaul component parts, and the total time in service of the DS

- UAS used under this Grant of Exemption. As a whole, the maintenance a nd inspection procedures required in

Petitioner ’s Operations Manuals ensure that an equivalent or higher level of safety will be

achieved.

PILOT

- IN

- COMMAND OF THE UAS

E. 14 C.F.R. § 61.113: Private Pilot Privileges and Limitations

Petitioner seeks exemption from 14 CFR § 61.113, which restricts private pilot certificate holders from flying aircraft for compensation or hire, and would also require a second class medical certificate. The purpose of Part 61 is to ensure that the skill and competency of any PIC matches the airspace in which the PIC will be operating, as well as requiring certifications if the private pilot is carrying passengers or cargo for hire. In this case, while the DS

- UAS will be operated as part of a commercial oper ation, they carr y neithe r passengers nor cargo. In the Grant of Exemption to Astraeus Aerial, the FAA determined that the unique characteristics of UAS operation outside of controlled airspace did not warrant the addition al cost and restrictions attendant with requiring the PIC to have a Commercial Pilot Certificate and Class II I Medical

Certificate. 12 The fulfillment of the additional requirements for a private pilot to become qualified as a commercial pilot would not lead to any additional safety benefits when UAS operations are involved.

12 Exemption No. 11062 (FAA Docket No. FAA

- 2014

- 0352).U.S Department of Transportation

February 2 6 , 2016 Page 15

Equivalent Level of Safety

The restrictions Petitioner has placed on its DS

- UAS operations meet or exceed the restrictions similarly imposed on Astraeus Aerial. Petitioner will operate on private property or approved

location away from person s and property not involved in the operation. Petitioner will also obtain an ATO issued COA prior to conducting any operations under this Grant of Exemption. All operations will be conducted in accordance with airspace requirements in the ATO issued

COA i ncluding class of airspace, altitude level and potential transponder requirements. A NOTAM will also be issued as required by the applicable COA.

In addition to these flight restrictions, Petitioner will further ensure safe operation by requiring that any PIC be thoroughly versed not only in airspace and communication issues pertaining to all aircraft operators but also in the unique aspects of DS

- UAS flight. As set forth in the Operations Manuals, pilots will have experience not only in DS

- UAS operations generally but have logged flight time in the specific make and model used for the operations before they are permitted to participate in commercial flights on behalf of Petitioner . The pilot qualification, training, and currency requirements in the Operat ions Manuals ensure that Petitioner pilots are competent and proficient in the DS

- UAS they are operating. Petitioner ’s training and qualification requirements are consistent with those contained in prior FAA Section 333 Grants of Exemption, and will provid e a higher level of competency and proficiency for its pilots and will ensure at least an equivalent level of safety to the public

.

OPERATING PARAMETERS OF THE UAS

F. 14 C.F.R. § 91.7(a): Civil Aircraft Airworthiness

I nasmuch as there will be no airworthin ess certificate issued for the UAS, Petitioner seeks an exemption from 14 C.F.R. § 91.7(a), which requires that a civil aircraft be in airworthy condition to be operated. The FAA has stated that no exemption is required for 14 C.F.R. § 91.7(a) to the

exten t that the requirements of Part 21 are waived or found inapplicable. 13 Accordingly, Petitioner requests that the requirements for § 91.7(a) be treated in accordance with

Section V ( A), supra.

G. 14 C.F.R. § 91.9(b)(2): Civil Aircraft Flight Manual in the Air craft and 14 C.F.R. § 91.203(a) and (b): Carrying Civil Aircraft Certification and Registration

Title 14 C.F.R. § 91.9(b) (2) and § 91.203(a) and (b) require the operator to carry airworthiness

documents and other aircraft manuals onboard the aircraft. Pu rsuant to 14 C.F.R. § 91.9(b) (2):

(b) No person may operate a U.S.

- registered civil aircraft

–

... (2) For which an Airplane or Rotorcraft Flight Manual is required by § 21.5 of this chapter, unless there is available in the aircraft a current approved Ai rplane or Rotorcraft

f light Manual, approved manual material, markings, and placards, or any combination

thereof.

13 See Id. at 13

- 14, 22.U.S Department of Transportation

February 2 6 , 2016 Page 16

Pursuant to 14 C.F.R. § 91.203(a) and (b):

(a) Except as provided in § 91.715, no person may operate a civil aircraft unless it has

within i t the following:

(1) An appropriate and current airworthiness certificate...

(b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) 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.

Given the small size and configuration of the DS

- UAS , it would be impossible to keep

airworthiness documents and other aircraft manuals on board the DS

- UAS because there is simply no room and the DS

- UAS has no cabin or cockpit. As a way to comply with the code

Petitioner will maintain the documents with the PIC and make them available for inspection.

Equivalent Level of Safety

In an FAA Office of Chief Counsel's O pinion dated August 8, 2014, and prepared by Dean E. Griffith, Attorney, AGC

- 220, it was acknowledged that the intent of 14 C.F.R. 91.9(b) and 91.203(a) and (b) is met if the pilot of the unmanned aircraft has access to the UAS flight manual, registration certificate, and other required documents from the ground control station from which he or she is operating the aircraft. 14 As this FAA Office of Chief Counsel Opinion clarifies, the intent of the rule is to ensure the pilot has access to these key docume nts during flight. Therefore, an equivalent level of safety will be achieved by ensuring that the pilot has access to the documents at the ground control station from which he or she is piloting the UAS.

H. 14 C.F.R. § 91.103: Preflight Action

Petitioner seeks an exemption from 14 C.F.R. § 91.103, which requires a PIC to become familiar with specific information before each flight, including information contained in the FAA

approved Flight Manual on board the aircraft. While the PIC will be familiar with all information necessary to safely conduct the flight, an exemption is requested to the extent that an FAA

approved Flight Manual is required.

Equivalent Level of Safety

An equivalent level of safety will be provided by following the Petitioner ’s Operat ions Manuals and the Manufacturer's Manual. The PIC will perform a series of checklists designed to identify any defects or inoperable components in accordance with the Petitioner ’s Operations Manuals, including checklists covering Pre

- Flight, Launch, Land ing, and Post

- Flight procedures. The PIC will also be required to review weather, flight requirements, battery charge, landing and takeoff distance, UA performance data, and contingency landing areas

— before initiation of flight.

14 Memorandum from Mark Bury, FAA Assistant Chief Counsel for International Law, Legislation and Regulation, to John Duncan, FAA Flight Standards Service (Aug. 8, 2014); see also Docket No. FAA

- 2014

- 0352 at 16

- 18.U.S Department of Transportation

February 2 6 , 2016 Page 17

Petitioner ’s Operations Man uals and the Manufacturer's Manual will be kept at the ground control station and will be accessible to the PIC at all times while operating the UAS.

I. 14 C.F.R. § 91.109(a): Flight Instruction

Petitioner seeks an exemption from 14 C.F.R. § 91.109(a), which provides in pertinent part that "[n]o 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." UASs and remotely piloted aircraft, by their design, do not have functional dual controls. Instead, flight control is accomplished through the use of a device that communicates with the aircraft via radio communications. Accordingly, an exemption will be required for the flight instruction requireme nts of 14 C.F.R. § 91.109(a).

Equivalent Level of Safety

Given the size and speed of the UASs that Petitioner intends to use, an equivalent level of safe training can still be performed without dual controls because no pilot or passengers are aboard

the UAS, and as required by the Petitioner ’s Operations Manuals, all persons will be a safe distance away in the event that the UAS experiences any difficulties during flight instruction. Moreover, as required by the Petitioner ’s Operations Manuals, all flight training will be conducted in controlled and sterile environment. As a whole, the safety procedures provided for

in Petitioner ’s Operations Manuals ensure that the proposed UAS operations provide an equivalent or higher level of safety than that provided by the flight instruction regulations.

J. 14 C.F.R. § 91.119(c): Minimum Safe Altitudes

Petitioner requests an exemption from the minimum safe altitude requirements of 14 C.F.R. § 91.119(c). 15 Section 91. 119 prescribes the minimum safe altitudes under which aircraft may not operate, including 500 feet above the surface and away from any person, vessel, vehicle, or

structure in non

- congested areas. See 14 C.F.R. § 91.119(c). Section 91.119(d) allows for a helicopter to operate at less than those minimum altitudes when it can be operated "without hazard to persons or property on the surface," provided that "each person operating the helicopter complies with any routes or altitudes specifically prescribed for helicopters by the FAA."

An exemption is requir ed because the proposed DS

- UAS operation will normally need to o c cur below 400 feet AGL. In circumstances where the DS

- UAS is used to inspect a structure whose height exceeds 400 feet AGL, the DS

- UAS will not be operated more than 100 feet above the highes t point on the structure, and within 50 feet horizontally of the structure. Add i tionally, due the nature of the proposed operations, the Pilot and/or Observers(s) may need to be less than 500 feet away from the DS

- UAS

.

15 Relief from § 91.119(a) will not be necessary because Petitioner will be able to perform an emergency landing without undue hazard to persons or property on the ground in the event of a failure. Petitioner's propo sed UAS operations will not occur over congested areas, and therefore an exemption from § 91.119(b) will not be necessary. See e.g., Grant of Exemption No. 11157 to Slugwear, Inc., dba Like on a tree Aerial (FAA

- 2014

- 0534 at 15).U.S Department of Transportation

February 2 6 , 2016 Page 18

Equivalent Level of Safety

Compare d to flight operations with rotorcraft weighing far more than the maximum weights

pr o posed herein, and given the lack of flammable fuel with the above noted UASs, any risk

assoc i ated with these operations is far less than those which presently exist with c onventional

ai r craft. An equivalent level of safety will be achieved given the size, weight, and speed of the

DS

- UAS , as well as the controlled location where the operations will occur. In order to avoid any risk to manned aircraft, flight operations will be restricted to 400 feet AGL or below, or when inspec t ing a U.S. structure whose height exceeds 400 feet AGL, within 100 feet above the highest point on that structure and 50 feet horizontally of the structure.

As set forth in the Operations Manuals, the DS

- UAS will be operated in a restricted area, and all flights will be operated at a lateral distance of at least 500 feet from any nonparticipating persons, unless that person is in a position where he or she is shielded from the DS

- UAS and any possible d ebris resulting from its failure. As required by the Operations Manuals, flights will be terminated if a nonparticipating person within 500 feet of the DS

- UAS leaves a shielded position. Further, its operations will occur at least 500 feet away from vehic les or structures unless the property owner/controller timely has granted permission and the PIC has made a safety assessment of the risk of operating closer to those objects and, operations near the PIC or Observer will not present an undue hazard per § 9 1.119(a). Adherence to these restrictions in

Petitioner ’s Operations Manuals will ensure operations can be conducted without compromising public safety. 16

K. 14 C.F.R. § 91.121: Altimeter Settings

Petitioner seeks an exemption from 14 C.F.R. § 91.121, wh ich requires a person operating an aircraft to maintain cruising altitude or flight level by reference to an altimeter that is set to the elevation of the departure airport or barometric pressure. An exemption is required to the extent

that the UASs do not have a barometric altimeter, but rather a GPS altitude read out.

Equivalent Level of Safety

The FAA has stated that an equivalent level of safety to the requirements of 14 C.F.R. §91.121 can be achieved in circumstances where: (1) the UASs will be opera ted below 400 feet AGL or

below 17 , (2) within VLOS, (3) where GPS based altitude information is relayed in real time to the

16 See e.g., Grant of Exe mption No. 11138 to Douglas Trudeau (FAA

- 2014

- 0481 at 19): "If ba r riers or structures are present that can sufficiently protect nonparticipating persons from the UA or debris in the event of an accident, then the UA may operate closer than 500 feet to pers ons afforded such protection. The operator must also 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 UA, flight operations must cea se immediately. When conside r ing how to immediately cease operations, the primary concern is the safety of those nonparticipating persons. In add i tion, the FAA finds that operations may be conducted closer than 500 feet to vessels, vehicles and structures when the

ow n er/controller of any such vessels, vehicles or structures grants permission for the operation and the PIC makes a

saf e ty assessment of the risk of operating closer to those objects and determines that it does not present an undue

ha z ard."

17 If the height of the structure being inspected exceeds 400 feet AGL, the UAS will not be ope r ated more than 100 feet above the highest point on the structure.U.S Department of Transportation

February 2 6 , 2016 Page 19

operator at a ground

- based on

- screen display and, (4) where prior to each flight, a zero altitude initiation point is established for the PIC to confirm accuracy of the onboard GPS. 18

The DS

- UAS that Petitioner intends to use for the proposed operations will meet all these operational characteristics. Moreover, as required by Petitioner ’s Operations Manuals, the PIC will be required to calibrate the aircraft's GPS compass prior to each flight operation. Like prior FAA Section 333 Grants of Exemption, the DS

- UAS Petitioner intends to use, and the safety mitigation procedures contained in the Operations Manuals, both ensure that an equival ent level of safety or greater level will be achieved, and a Grant of Exemption to the requirements of § 191.121 is therefore appropriate

.

L. 14 C.F.R. § 91.151(a): Fuel Requirements for Flight in VFR Conditions

Petitioner requests an exemption from 14 C.F. R. § 91.151(a)'s fuel requirements for flight in

VFR conditions. Section 91.151 states:

(a) No person may begin a flight in an airplane under VFR conditions unless (considering wind and forecast weather conditions) there is enough fuel to fly to the firs t 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.

Here, the technological limitations on UAS battery power means t hat no meaningful flight operations can be conducted while still maintaining a 30

- minute battery reserve. An exemption from the fuel requirements of 14 C.F.R. § 91.151(a) is therefore required. Moreover, it is not

Petitioner ’s intention to fly the DS

- UAS at night.

Equivalent Level of Safety

In the Grant of Exemption to VDOS (Exemption No. 11112), the FAA determined that an equivalent level of safety to the fuel requirements for flight in VFR conditions could be achieved by prohibiting the PIC from beginn ing a DS

- UAS flight unless (considering wind and forecast weather conditions) there was enough power to fly to the first intended point of landing and, assuming normal cruising speed, to fly after that for at least 10 minutes. In reaching this conclusion, the FAA considered that the UAS batteries for the DS

- UAS provide approximately 50 minutes of powered flight (with payload) and provided battery level and battery time remaining in minutes and seconds to the PIC. 19 The FAA also considered the fact the DS

- UAS operating manual states: “start every flight with a fully charged battery in the aerial vehicle”, and

that in the event that the DS

- UAS should run low on power, the PIC will be alerted and can safely land the

- DS

- UAS as soon as possible. Like the VDOS Gra nt of Exemption, Petitioner ’s

use of the DS

- UAS , combined with the requirements of Petitioner's Operations Manuals, ensure that an equivalent level of safety can be achieved and in fact exceeded

.

18 See Grant of Exemption No. 11062 to Astraeus Aerial (FAA

- 2014

- 0352 at 21).

19

. Grant of Exemptio n No. 11112 to VDOS Global, LLC (FAA

- 2014

- 0382 at 10).U.S Department of Transportation

February 2 6 , 2016 Page 20

Similarly, in the Grant of Exemption to Alan Purwin (Exempti on No. 11161), the FAA determined that an equivalent level of safety to the fuel requirements for flight in VFR conditions could be achieved by prohibiting the PIC from beginning a flight with the UA unless (considering wind and forecast weather conditions ), there was enough power to safely fly at normal cruising speed to the intended landing point and land the UA with 25% battery power remaining. Petitioner will adhere to this limitation for its DS

- UAS flights.

The DS

- UAS includes a low battery warning s ystem and the amount of battery reserve power remaining is continuously transmitted to the PIC via telemetric data feed, which downlinks from

the DS

- UAS to a ground

- based

- on

- screen display. 20 As required by Petitioner ’s Operations Manuals, the PIC will pro mptly fly the DS

- UAS back to the home launch location or pre

det ermined abort location where it may safely land, while still maintaining a minimum of 25% reserve battery power. Petitioner submits that the procedures requiring flights to be safely

terminate d once the batteries fall below 25% capacity, combined with the requirement that flights only be conducted within a secure, isolated area, using a UAS weighing less than 5 5 pounds, and within VLOS of the PIC and Observer(s), ensure that the proposed operat ion will provide an equivalent or higher level of safety to the public to that provided by the regulations from which exemption is sought

.

VI. DRUG AND ALCOHOL PROGRAM

Petitioner will have policies in place to ensure that no person may participate in DS

- UAS flight operations if they are under the influence of alcohol or any drug.

VII. PUBLIC INTEREST

The public interest will be served by granting Petitioner ’s Petition for Exemption. Congress has established a national policy that favors early integrat ion of UAS into the NAS in controlled, safe working environments such as those proposed in this Petition. Granting this Petition for Exemption helps fulfill Congress' goal in passing Section 333(a) through (c) of the Reform

Act

— the FAA Administrator's asse ssment of whether certain UAS may operate safely in the NAS before completion of the statutorily required rulemaking.

The proposed DS

- UAS operations in this Petition for Exemption significantly improve s the safety and reduce s risk of harm, physical injury and property damage to the public at large, the property owners from whom permission was granted for use by Petitioner and abutting properties, staff of Petitioner, unsuspecti n g passersby, inspecting engineers from relevant organizations and all those who may be in the local vicinity . Traditional methods of providing surveillance and mapping services location personnel to climb towers

, trees, venture onto precarious roofs and other dangerous scenarios

, perform elevated work for which the individual

is neit her trained n or equipped to perform , which exposes them to unnecessary risk of serious physical injury from dangerous falls or other physical mishaps

. Moreover, inspectors/surv eyors are often unnecessarily exposed to hazardous conditions, unsafe environme nts, culturally tense

situations and other hazards associated with identifying specific locations for potential recording

20 . T he DS

- UAS ground control station displays, the UASs position, navigation route, tail number, altitude, hea d ing, north seeking arrow, range to targets, calculated target position, date/time, and sensor heading and orie n tation

relative to the UASU.S Department of Transportation

February 2 6 , 2016 Page 21

sites to be used in the end product

. The use of small UAS can eliminate these hazards and ultimately creat e a much safer method of pe rforming these types of inspections creating a safer environment for the public as well as Petitioner employees.

The use of small UAS also enhances safety and reduces risk to the surrounding public because, unlike manned aircraft weighing thousands of pou nds, carrying crew in addition to flammable

fue l, the UAS carry no passengers, crew or explosive fuel . Further more , in the unlikely event of an accident, Petitioner ’s small battery powered DS

- UAS presents significantly less danger to persons on the ground when compared to operations by conventional manned aircraft. 21 As

P etitioner's DS

- UAS are battery powered, the public will also benefit from a reduction in

harmful petroleum based emissions associated with conventional aircraft performing in the same

funct ions proposed herein. Air quality will naturally be improved with the reduction of fuel powered vehicles.

Lastly, as recognized by the FAA in prior Section 333 Grants of Exemption to filmmakers, UAS provide an additional economic tool for the aerial fi lming notwithstanding the industry, adding a greater degree of flexibility, which supplements the current capabilities offered by manned

aircraft. 22 The quality of the finished product is enhanced and provides a greater finished product

demand which will a id the current UAS industry and provide additional jobs as the cost of providing the needed product is greatly reduced while reducing the difficulty with which the finished product is created . The demand for the current industrial product is increasing an d will continue to increase given the enhanced flexibility of production ; therefore, given the lower cost, owner/operators and others in the relevant industry will be more inclined to utilize the services of

commercial UAS along with a n appropriate license d PIC’s

.

VIII. PRIVACY

All DS

- UAS operations will be conducted in accordance with applicable federal, state, and local laws regarding privacy. All operations shall be conducted over private or controlled

- access property with permission from the land ow ner/controller or authorized representative. Permission from land owner/controller or authorized representative will be obtained for each flight to be

conducted.

IX. FEDERAL REGISTER SUMMARY

Pursuant to 14 C.F.R. Part 11, the following summary is provid ed for publication in the FEDERAL REGISTER, should it be determined that publication is needed: Petitioner seeks an exemption from the following rules in Title 14 of the Code of Federal Regulations:

21 See Grant of Exemption No. 11158 to Team 5, LLC (FAA

- 2014

- 0783 at 12): "Manned hel i copters conducting aerial filming can weigh 6,000 pounds or more and are operated by an onboard pilot, in addition to other onboard crewmembers, as necessary. The petitioner’s UAs will weigh less than 55 pounds with no onboard pilot or crew. The pilot and crew will be r e motely located fro m the aircraft. The limited weight significantly reduces the potential for harm to participating and nonparticipating individuals or property in the event of an incident or acc i dent. R isk to an onboard pilot and crew during an incident or accident is elimi nated with the use of a UA for the aerial filming operation."

22 See e.g., Grant of Exemption No. 11178 to Picture Factory, Inc. (FAA

- 2014

- 0794 at 18).U.S Department of Transportation

February 2 6 , 2016 Page 2 2

Part 21, Subpart H; Part 27; 45.23(b); 45.27(a); 61.113; 91.7(a); 91.9(b)(2); 91.9(c); 91.103; 91.109(a); 91.119(c); 91.121; 91.151(a); 91.203 (a) & (b); 91.405(a); 91.407(a)(1); 91.409(a)(1) & (2); 91.417 (a) & (b).

The exemption will enhance safety by reducing risk to the aircraft crew, production crew, gener al public, property owners and city structures from the substantial hazards associated with performing equivalent film work and aerial video production with conventional fixed

- wing aircraft, rotorcraft, or other methods.

X. CONCLUSION

Petitioner ’s Petit ion for Exemption satisfies the criteria articulated in Section 333 of the Reform

Act of 2012 which includ es weight ; speed ; operating capabilities ; proximity to airports and populated areas ; operation within VLOS and national security. The proposed DS

- UAS operations will benefit the public as a whole by improving safety and reducing risk by alleviating human exposure to danger while lowering the attendant related costs thereby increasing the demand for the finished product. In consideration of the foregoing , this Petition for Exemption provides the FAA with more than adequate justification for granting the requested exemptions allowing

Petitioner to use small DS

- UAS in the recorded production of its product.

We thank you for your prompt consideration of ou r requested exemptions.

Respectfully Submitted,

Erwin S. Aviles

Drone Shots 10860 Stagg Street Sun Valley, CA 91352

Phone: 818.653.9183

Email: steveaviles@droneshot.coU.S Department of Transportation

February 2 6 , 2016 Page 23

(The following attached items contain proprietary and commercial info rmation exempt from disclosure under the Freedom of Information Act, 5 U.S.C. § 522 et seq., and should be held in a separate file pursuant to 14 C.F.R. § 11.35(b)).

Attachments:

1. General Operations Manual 2. PIC Operating Manual 3. Company Protocols

4 . Location Protocols 5. Flight Communications Protocols 6. Departing Location Protocols

7. Transmitter Protocols 8. Preflight Checklist 9. Post Flight Checklist 10. Equipment Checklist

11. UAS Manufacturer’s Manuals

a. User Manuals

b. UAS Maintenance Manua ls

PETITIONER REQUESTS THAT GOOD CAUSE EXISTS TO EXEMPT ANY PART OF

THIS PETITION FROM BEING PUBLISHED IN THE FEDERAL REGISTER PUBLIC

FORUM BECAUSE THE REQUESTED EXEMPTION WOULD NOT SET A PRECEDENT, AND ANY DELAY IN ACTING ON THIS PETITION WOULD BE

DETRIM ENTAL TO THE PETITIONER.