September 22

, 2015

Exemption No. 12958 Regulatory Docket No. FAA

− 20 15

− 2717

Mr. Edgar F. Heiskell, IV CEO Aeronautic Imagery, LLC 87 Canyon Road Morgantown, WV 26508

Dear Mr. Heiskell :
This letter is to inform you that we have granted your request for exemption. It transmits our decision, explains its basis, and gives you the conditions and limitations of the exemption, including the date it ends.

By letter dated June 4, 2015 , you petitioned the Federal Aviation Administration (FAA) on behalf of Aeron autic Imagery, LLC ( hereinafter petitioner or operator ) for an exemption . The petitioner requested to operate an unmanned ai rcraft system (UAS) to conduct aerial photography and video, as well as to assist in the evaluation of infrastructure and operation s

. See Appendix A for the petition submitted to the FAA des cribing the proposed operations and the regulations that the petitioner seeks an exemption

. The FAA has determined that good cause exists for not publishing a summary of the petition in the Federal Register because the requested exemption would not set a precedent, and any delay in acting on this petition would be detrimental to the petitioner.

Airworthiness Certification

The UAS proposed by the petitioner is a DJI Phantom 3 Professional

. In accordance with the statutory criteria provided in Section 333 of P ublic Law 112

− 95 in reference to 49 U

. S

. C

. § 44704, and in consideration of the size, weight, speed, and limited operating area associated with the aircraft and its operation, the Secret ary of Transportation has determined that this aircraft meets the conditions of Section 333. Therefore, the FAA finds that relief from 14 CFR part 21

, C ertification procedures for products and parts,2

Subpart H

— Airworthiness Certificates , and any associated noise certification and testing requirements of part 36, is not necessary.

The Basis for Our Decision

You have requested to use a UAS for aerial data collection 1

. The FAA has issued grants of exemption in circumstances similar in all material respects to those presented in your petition. In Grants of Exemption No s

. 11062 to Astraeus Aerial ( see Docket No. FAA−2014−0352), 11109 to Clayco, Inc. ( see Docket No. FAA

− 2014

− 0507), 11112 to VDOS Global, LLC ( see Docket No. FAA−2014−0382), and 11213 to Aeryon Lab s , Inc. ( see Docket No. FAA−2014−0642), the FAA found that the enhanced safety achieved using an unmanned aircraft (UA) with the specifications described by the petitioner and carrying no passengers or crew, rather than a manned aircraft of s ignificantly greater proportions, carrying crew in addition to flammable fuel, gives the FAA good cause to find that the UAS operation enabled by this exemption is in the public interest.

Having reviewed your reasons for requesting an exemption, I find th at

—

 They are similar in all material respects to relief previously requested in Grant of Exemption Nos. 11062, 11109, 11112, and 11213 ;

 The reasons stated by the FAA for granting Exemption Nos. 11062, 11109, 11112, and 11213 also apply to the situation yo u present; and

 A grant of exemption is in the public interest.

Our Decision

In consideration of the foregoing, I find that a grant of exemption is in the public interest. Therefore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701, delegated to me by the Administrator, A eronautic Imagery , LLC is granted an exemption from 14 CFR §§ 61.23(a) and ( c ), 61.101(e)(4 ) and (5), 61.113(a), 61.315(a) , 91.7(a), 91.119(c), 91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 91.417(a) and (b), to the extent necessary to allow the petitioner to operate a UAS to perform aerial data collection

. This exemption is subject to the conditions and limi tations listed below.

Conditions and Limitations

In this grant of exemption, Aeronautic Imagery , LLC is hereafter referred to as the operator.

1 Aerial data collection includes any remote sensing and measuring by an instrument(s) aboard the UA. Examples include imagery (photography, video, infrared, etc.), electronic measurement (precision surveying, RF analysis, etc.), chemical measurement (part iculate measurement, etc.), or any other gathering of data by instruments aboard the UA.3

Failure to comply with any of the conditions and limitations of this grant of exemption will be grounds for the immediate suspension or rescission of this exemption.

1. Operations authorized by this grant of exemption are limited to the DJI Phantom 3 Professional when weighing less than 55 pounds including payload. Proposed operations of any other aircraft will r equire a new petition or a petition to amend this exemption

.

2. Operations for the purpose of closed

- set motion picture and television filming are
not permitted.

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The exemption holder may use either groundspeed or calibrated airspeed to determine compliance with the 87 knot speed restriction. In no case will the UA be operated at airspeeds greater than the maximum UA operating airspeed recommended by the aircraft manufacturer.

4. The UA must be operated at an altitude of no more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL.

5. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. This requires the PIC to be able to use human vision unaided by any device other than corrective lenses, as specified on the PIC’s FAA

- issued airman medical certificate or U.S. driver’s license.

6. All operations must utilize a visual observer (VO). The UA must be operated within the visual line of sight (VLOS) of the PIC and VO at all times. The VO may be used to satisfy the VLOS requirement as long as the PIC always maintains VLOS capability. The VO and PIC must be able to communicate verbally at all times ;

e lectronic messaging or texting is not permitted during flight operations. The PIC must be designated before the flight and cannot transfer his or her designation for the duration of the flight. The PIC must ensure that the VO can perform the duties required of the VO.

7. This exemption and all documents needed to operate the UAS and conduct its operations in accordance with the conditions and limitations stated in this grant of exemption, are hereinafter referred to as the operating documents. The operating documents must be accessible dur ing UAS operations and made available to the Administrator upon request. If a discrepancy exists between the conditions and limitations in this exemption and the procedures outlined in the operating documents, the conditions and limitations herein take pr ecedence and must be followed. Otherwise, the operator must follow the procedures as outlined in its operating documents. The operator may update or revise its operating documents. It is the operator’s responsibility to track such revisions and present updated and revised4

documents to the Administrator or any law enforcement official upon request. The operator must also present updated and revised documents if it petitions for extension or amendment to this grant of exemption. If the operator determine s that any update or revision would affect the basis upon which the FAA granted this exemption, then the operator must petition for an amendment to its grant of exemption. The FA A’s UAS Integration Office (AFS− 80) may be contacted if questions arise regar ding updates or revisions to the operating documents.

8. Any UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics, e.g.

, replacement of a flight critical component, must undergo a functional test flight pr ior to conducting further operations under this exemption. Functional test flights may only be conducted by a PIC with a VO and must remain at least 500 feet from other people. The functional test flight must be conducted in such a manner so as to not po se an undue hazard to persons and property.

9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is in a condition for safe operation.

10. Prior to each flight, the PIC must conduct a pre

- flight inspection and determine the UA S is in a condition for safe flight. The pre

- flight inspection must account for all potential discrepancies, e.g.

, inoperable components, items, or equipment. If the inspection reveals a condition that affects the safe operation of the UAS, the aircraft is prohibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight.

11. The operator must follow the UAS manufacturer’s maintenance, overhaul, replacement, inspection, and life limit requi rements for the aircraft and aircraft components.

12. Each UAS operated under this exemption must comply with all manufacturer safety bulletins.

13. Under this grant of exemption, a PIC must hold either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC must also hold a current FAA airman medical certificate or a valid U.S. driver’s license issued by a state, the District of Col u mbia, Puerto Rico, a territory, a possession, or the Federal government. The PIC must also m eet the flight revi ew requirements specified in 14 CFR § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

14. The operator may not permit any PIC to operate unless the PIC demonstrates the ability to safely operate the UAS in a manner consistent with how the UAS will be operated under this exemption, including evasive and emergency maneuvers and maintaining approp riate distances from persons, vessels, vehicles and structures. PIC qualification flight hours and currency must be logged in a manner consistent with5

14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs (traini ng, proficie ncy, and experience

- building) and determining the PIC’s ability to safely operate the UAS in a manner consistent with how the UAS will be operated under this exemption are permitted under the terms of this exemption. However, training operations may only be conducted during dedicated training sessions. During traini ng, proficiency, and experience

- building flights, all persons not essential for flight operations are considered nonparticipants, and the PIC must operate the UA with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All operations must be conducted under visual meteorological conditions (VMC). Flights under special visual flight rules (SVFR) are not authorized.

16. The UA may not operate within 5 nautical miles of an airport reference point (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) or for airports not denoted with an ARP, the center of the airport symbo l as denot ed on the current FAA

- published aeronautical chart, unless a letter of agreement with that airport’s management is obtained or otherwise permitted by a COA issued to the exemption holder. The letter of agreement with the airport management must be made ava ilable to the Administrator or any law enforcement official upon request.

17. The UA 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.

18. If the UAS loses communications or loses its GPS sign al, the UA must return to a
pre

- determined location within the pr ivate or controlled

- access property.

19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies.

20. The PIC is prohibited from begi nning a flight unless (considering wind and forecast weather conditions) there is enough available power for the UA to conduct the intended operation and to operate after that for at least 5 minutes or with the reserve power recommended by the manufacturer if greater.

21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All operations shall be cond ucted in accordance with an ATO

- issued COA. The exemption holder may apply for a new or amended COA if it intends to conduct operations that cannot be conducted under the terms of the enclosed COA

.

22. All aircraft operated in accordance with this exemption must be identified by serial number, registered in accordance with 14 CFR part 47, and have identification (N− Number) markings in accord ance with 14 CFR part 45, Subpart C. Markings must be as large as practicable.6

23. Documents used by the operator to ensure the safe operation and flight of the UAS and any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the PIC at the Ground Control Station of the UAS any time the aircraft is operating. These documents must be made available to the Administrator or any law enforcement official upon request.

24. The UA must remain clear and give way to all manned aviation operations and activities at all times.

25. The UAS may not be operated by the PIC from any moving device or vehicle.

26. All Flight operations must be conducted at least 500 feet from all nonpartici pating persons, vessels, vehicles, and structures unless:

a. Barriers 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 r emain under such protection. If a situation arises where nonparticipating persons leave such protection and are within 500 feet of the UA, flight operations must cease immediately in a manner ensuring the safety of nonparticipating persons ; and b. The owner/ controller of any vessels, vehicles or structures has granted permission for operating closer to those objects 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

. The PIC, VO, operator trainees or essential persons are not considered nonparticipating persons under this exemption.

27. All operations shall be conducted over private or control led

- access property with permission from the property owner/controller or aut horized representative. Permission from property owner/controller or authorized representative will be obtained for each flight to be conducted.

28. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of the opera tional area as defined by the applicable COA must be reported to the FA A's UAS Integration Office (AFS− 80) within 24 hours. Accidents must be reported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

. If this exemption permits operations for the purpose of closed

- set motion picture and television filming and production, the following additional conditions and limitations apply.

29. The operator must have a motion picture and television operations manual (MPTOM) as documented in this grant of exemption.7

30. At least 3 days before aerial filming, the operator of the UAS affected by this exemption must submit a written Plan of Activities to the local Flight Standa rds District Office (FSDO) with jurisdiction over the a rea of proposed filming. The 3

- day notification may be waived with the concurrence of the FSDO. The plan of activities must include at least the following:

a. Dates and times for all flights; b. Name and phone number of the operator for the UAS aerial filming conducted under this grant of exemption;

c. Name and phone number of th e person responsible for the on

- scene operation of the UAS; d. Make, model, and serial or N− Number of UAS to be used;

e. Name and certific ate number of UAS PICs involved in the aerial filming; f. A statement that the operator has obtained permission from property owners and/or local officials to conduct the filming production event; the list of those who gave permission must be made available t o the inspector upon request;
g. Signature of exemption holder or representative; and h. A description of the flight activity, including maps or diagrams of any area, city, town, county, and/or state over which filming will be conducted and the altitudes essenti al to accomplish the operation.

31. Flight operations may be conducted closer than 500 feet from participating persons consenting to be involved and necessary for the filming production, as specified in the exemption holder’s MPTOM.

Unless otherwise specifie d in this grant of exemption, the UAS, the UAS PIC, and the UAS operations must comply with all applicable parts of 14 CFR including, but not limited to, parts 45, 47, 61, and 91.

This exemption terminates on September 30, 2017 , unless sooner superseded o r rescinded.

Sincerely,

/s/ John S. Duncan Director, Flight Standards Service

EnclosuresJune 4, 2015

Unmanned Aircraft Sy stems Integration Office Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591

U.S. Department of Transportation, Docket Operation West Building Ground Floor, Room w12

- 140 1200 New Jersey

Avenue, SE Washington, DC 20590

To whom it may

concern,

Aeronautic I

magery , LLC (A.I .) respectfully requests an exemption from several provisions of Title 14 of the Code of Federal Regulations (C.F.R.) to permit the use of small unmanned aerial systems (sUAS) to provide aerial photograph y and video, as well

as to assist in the evaluation of infrastructure and operations for our cl ients. This request is motivated primarily

b y the desire to maximize safet y in infrastructure and operations. An exemption would allow A.I. to broadl y evaluate assets and operations with sUAS, resulting in a safer and more efficient infrastructure network. Accordingl y, the grant of an exemption is consistent with Congress’ intent, reflected in Section 333 of the FAA Modernization and Reform Act of 2012 (Modernization Act), 1 that safe sy stems be permitted in the national airspace prior to the issuance of fin al regulations governing general use of these s ys tems. 2 A summary of this request suitable for publication in the Federal Register is provided as Appendix A.

Appendix B provides the manufacturers information regarding the design, aircraft performance, and fail

- safe features. We have provided manufacturer information related to operating limitations, normal and emergency procedures, and maintenance and inspection procedures. As we add aircraft designs, we will update this appendix appropriately.

Appendix C provides the Aeronautic I magery , LLC Operations Manual for flights covered under this Exemption Request.

1 P.L. 112

- 95, 126 Stat 11, February 14, 2012.

2 Section 333(b) (2) specifically contemplates that the FAA may issue a certificate of waiver upon a f inding that a type of UAS, as a result of its size, weight, speed, operational capacity, proximity to airports and populated areas, and operations within visual line of sight do not create a hazard to users of the NAS or the public or pose a threat to national security. Edgar F. Heiskell , IV Aeronautic I magery, LLC. 87 Cany on Road Morgantown, WV 26508 (304) 290

- 7547 Skipheiskell2@yahoo.com**Background Information**

Aeronautic I magery , LLC is in the business of Consulting on, Building & Maintaining Mission Specific sUAS for our clients. A.I. c lients look to us for Safe Operations of sUAS. We have developed specific Aeronautic Imagery , LL C Safe UAV Operational Procedures. Increasingl y, we have clients looking to operate sUAS for Infrastructure Safety & Maintenance In spections.

**Infrastructure Safety Inspection Operations**  : Real Estate Pipeline In s pection Oil

- Field Inspection Petro/Chemical/Manufacturing Inspection Construction Site In spection Agriculture Inspection Utility Inspection

As part of this Aeronautic I magery , LL C is requesting FAA Exemption for sUAS operations for safet y, inspection and video capture usage.
**Regulatory Basis for Exemption Request**  In addition to the waiver authority provided in §333 of the Modernization Act, the FAA may grant an exemption under 49 U.S.C. §44701(f) if it has determined that such an exemption is in the public interest. The FAA has imposed a separate requirement in its procedural regulations, providing that the petitioner shall explain why granting the exemption would not adversel y affect safet y or how the exemption would provide at least an equivalent le vel of safety as compliance with the underl yi ng regulation. In this case, approval of this exemption would advance the public interest by significantly enhancing the safet y and efficiency of infrastructure operations and by providing the FAA with valuable user experience on sUAS in a context with appreciable economic and societal benefits. As described more full y below, the requested exemption would permit the operation of sUAS under tightly controlled conditions, thus ensuring that operations will not have an adverse impact on safet y. To the contrary , as explained below, Aeronautic Imagery , LLC anticipates that use of sUAS will enhance safet y in infrastructure operations. Granting an Exemption is in the Public Interest. The safet y and efficiency of infrastr ucture operations is heavily dependent upon constant anal ys is of assets, right

- of

way , infrastructure and other assets/facilities. There are a wide variet y of factors that can affect conditions and cause problems for infrastructure. Even relativel y small o bjects or minor failures can lead to accidents or other incidents causing downtime of infrastructure. Extreme weather events can lead to flooding or overheating infrastructure. For example earthquakes, landslides, and abandoned vehicles at grade crossings can block infrastructure. The potential for sabotage and terrorism

– or even just trespassing

– are also among the many risks that modern infrastructure faces.

As a result, pursuant to federal regulations and company policy , our client’s maintenance employ ees routinel y inspect the infrastructure, such as bridges, tunnels, support structures, and signals. At present, this work is done primaril y b y compan y personnel inmotor vehicles, on foot, in specialized equipment. This is often a labor

- in tensive and

sometimes arduous job. While our clients do all they can to make these inspections as safe as possible, there is an irreducible element of risk involved whenever employ ees are required to go out on structures. Employ ees may need to climb over o r onto structures, which can be slippery , rough, and/or exposed to the elements. Some structures, such as bridges, are high above the ground. Equipment moving through inspection zones can increase risk as well, especiall y in high

- traffic areas. While the u se of sUAS for supplemental infrastructure and general asset evaluation would not eliminate these risks entirel y (as it is an additive safet y measure), it would reduce the risks to employ ees by

allowing for remote aerial review.

Additionally , the sheer amount of assets and the widely dispersed locations

– in many instances far from sizeable population centers

– means that visual inspection in all instances b y compan y personnel can be inefficient. Aerial analy sis by traditional fixed wing aircraft is impr actical because the required altitudes for safe flight reduce visibility below meaningful levels

– it is simply not possible to see all asset anomalies from such heights. Helicopters present better vantage points; however manned helicopters are much

more c ostly , subject to human safet y and carry highl y explosive jet fuel making them impractical for deplo ym ent. By using sUAS for supplemental asset evaluation, Aeronautic Im agery , LLC will be able to substantially upgrade its capacity to detect and address iss ues with the right

- of

- way and other assets before they become a problem for safe operations. Thus, the use of sUAS has the potential to improve efficiency , resulting in faster and safer delivery of goods, energy

& natural resources vital to the U.S.

econom y.**Granting an Exemption will not Adversely Affect Safety** 

Aeronautic Im agery , LLC notes that there is no applicable standard for an equivalency determination. Some have argued that the appropriate standard is that for model aircraft, noting that their operations, if conducted for recreational purposes, would fall completely within the allowable operations for model aircraft. We believe it is difficult to argue that there is sufficient correlation between model operations controlled by the Ac adem y of Model Aeronautics and the ones contemplated b y Aeronautic Im agery , LLC . At the same time, it is clear that equivalency cannot be established for traditional, manned civil aircraft because the design and use profiles between traditional aircraft an d sUAS are simply too different. As such, we believe it makes more sense to focus on wh y the contemplated operations would not adversel y affect safet y, which is all that §11.81(e) requires.

Granting an exemption will not adversely affect safety

. Aeronaut ic Imagery, LLC contemplates conducting sUAS operations over client owned or controlled land, solely during day light hours, at altitudes well below 200’ . In general, sUAS operations are intended to be conducted in areas distant from both congested areas an d airports. Moreover, because of the inherent risks presented by standard infrastructure operations, our clients have alread y t aken steps to secure property against unauthorized public access. For example, substantial stretches of pipeline, utilities, and oil and gas production sites are fenced, elevated, or otherwise secured to prevent access. Other long stretches of infrastructure are, as noted above, in very remote wilderness areas. The nature of operations anticipated by Aeronautic Imagery , LLC requires that the sUAS be flown at relatively

low altitu des and relativel y low speeds. Aeronautic Imagery, LLC expects that in most instances, the sUAS will be flown less th an 100 feet from the highest structure along the path of the sUAS. Accordingl y, the risk of interference with another aircraft is minimal. Aeronautic Imagery , LLC also plans to conduct sUAS operations at least three miles from any public airports (includin g heliports). In the event an operation needs to be conducted closer to an airport, Aeronautic Im agery, LLC will inform the airport operator and airport air traffic control tower of the contemplated operation and will comply with any directions issued by

a ir traffic control at that airport.

Approval of exemptions allowing commercial operations of sUASs in the infrastructure aerial inspection industry will enhance safet y b y reducing risk. Conventional operations, using jet or piston power aircraft, operate at extremely low altitudes just feet from the subject being inspected and in extreme proximity to people and structures; and present the risks associated with vehicles that weigh in the neighborhood of 4,000lbs., carr yi ng large amounts of jet A or other fu el (140 gallons for jet helicopters). Such aircraft must fly to and from the inspection site. In contrast, a sUAS weighing fewer than 55 lbs. and powered b y batteries eliminates virtually all of that risk given the reduced mass and lack of combustible fuel carried on board. The sUAS is carried to the inspection site. The sUAS will carry

no passengers or crew and, therefore, will not expose them to the risks associated with manned aircraft flights.

The operation of small UASs, weighing less than 55 lbs., co nducted in the strict conditions outlined above, will provide an equivalent level of safet y supporting the grant of the exemptions requested herein, including 333 Aircraft Exemption Status exempting the applicant from conventional aircraft requirements and allowing commercialoperations. These lightweight aircraft operate at slow speeds, close to the ground, and in

a controlled environment and, as a result, are far safer than conventional operations conducted with turbine helicopters operating in close proximity to the ground and people.

The safet y of those on the ground is protected b y t he fact that no one will be allowed into the area without the permission of the company . Securit y will be established for the flight area as part of the pre

- fligh t control. Each individual within the secure area will be briefed prior to flight and will consent to being in the area. All others will be excluded from the area.

Aeronautic Im agery , LLC initially intends to use a dedicated staff for sUAS operations. All operations will be within visual line

- of

- sight (i.e., no more than approximately 0.5 miles from the manipulator of the controls, or pilot in command (PI C)). Each PI C will conduct at least three take

- offs and landings with the sUAS on which he or she is tr ained
every 90 day s. PIC’s will establish their qualifications thru a combination of aeronautical knowledge, UAS	airmanship	skills,	and	verification	through	testing	of	flight ability	before infrastructures	operations	have	commenced. Depending on the ty pe of operation, additional ground

- based visual observers may be employ ed as well. These observers will be within constant visual line of sight and in constant contact with the PI C. The visual observers will assist the PI C in avoiding objects near the sUAS.

There are no standards for either Private or Commercial sUAS pilot certificates. The safe operation and control of the UAS as described in this application does not depend on the ty pe of FAA license held by the PIC. Given the restricted and controlled air space within which operations will take place, the key factors needed b y the PIC are knowledge of the airspace within which the operation will take place and how that airspace fits into the National Airspace Sy stem (NAS). That knowledge can be and is gaine d primarily through ground school and not through flight training in fixed wing or rotor aircraft, nor is it dependent on the acquisition of a commercial or private pilot’s certificate. Those certificates demonstrate knowledge of the factors and skills nee ded for the safe operation of those ty

pes of aircraft (fixed wing or rotorcraft). I t cannot be assumed that a commercial pilot, approved to operate a helicopter or fixed wing aircraft, has the skill or ability to safel y operate a small unmanned aerial vehicle, operating at 400 AGL or lower, within strictly

controlled pre

- approved airspace. Besides knowledge of airspace regulations, dexterity

in the control and operation of the sUAS acquired from actual operation of the aircraft is the most important fac tor in establishing an equivalent level of safet y.

If the PI C has acquired the necessary knowledge of airspace requirements, the relevant issues are (1) where the aircraft will be flown, (2) the size of the aircraft relative to what is being used today

to accomplish the same mission, and (3) what precautions will be taken to ensure the safety of those in the area of operation. We propose that the aircraft be operated within a secure environment; and that no one be allowed to enter the secure envir onment unless they

are part of the operation, have been fully briefed of the risks prior to operation of the sUAS, and have consented to the risks associated with being in theoperating area. Should there be a mishap, the sUAS being flown pose signific antly less of a threat than the helicopters and fixed wing aircraft now being employ ed because they are a fraction of the size, carry no flammable fuel, do not carry crew or passengers, and pose an infinitesimal risk to others. This is in stark contrast t o conventional aircraft that are flown to the site, carry

explosive fuel, carry

passengers and crew, and operate in a much larger area.
From a practical standpoint, there are relatively few licensed full

- scale aircraft pilots who are also qualified to fl y the ty pe of sUAS that are utilized for infrastructure image

- capture operations. There are even fewer commercial pilots that can fl y these sUAS

– to the point that to do both is considered rare. Assuming that it is unlikely for a company

to find a pilot that has both qualifications, that compan y would either have to source a qualified sUAS pilot to train and obtain a commercial certificate, or find a commercial certificated pilot who would be willing to learn to fl y a sUAS to the competency level re quired for professional use.
Minimum requirements for the PI C include: 1) A minimum of 200 flight cy cles and 25 hours of total time as a sUAS rotorcraft pilot; 2) A minimum of 5 hours as sUAS pilot with the make and model of sUAS to be utilized for operations under the exemption and 3 take offs and landings in the preceding 90 day s; 3) Have undergone a qualification process as specified in the Flight Operations & Procedures Manual consisting of a knowledge & skill test of the aircraft to be used.

Another consideration supporting the certificate requirement is that pilots are subject to securit y screening b y the Department of Homeland Security . This requirement should ameliorate securit y concerns over UAS operations under this exemption.

Aeronautic Im agery , LLC int ends to use commercially available sUAS Components for sUAS. These sUAS s ys tems will be tested for quality & safety in our test facility

before being deploy ed to the field. The sUAS is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, and operates exclusively within a secured area. We have a routine maintenance schedule to verify that the sUAS will remain in safe and operational condition. Please see **Appendix B** , for Specific Types of sUAS.

Notes Regarding: 14 C.F.R. Part 21, Subpart H I n a cc o r dan c e w it h t h e s t a t u t o r y crit e ri a p r ov i de d i n Se cti o n 33 3 o f P L 11 2

- - - 9 5 i n

r e f e r en c e t o 4 9 US C 44704
, an d i n c ons i de r a ti o n o f t h e s i ze , w e i gh t, speed

, an d li m it e d
ope r a ti n g a r e a a ss o ci a t e d w it h t h e a ircr a f t an d it s ope r a ti on , w e r eques t t ha t t h i s

a ir c r a f t exe m p ti o n m ee t s t h e c ond iti on s o f Se cti o n 333

. The r e f o r e , i f g r an t e d Se cti o n 33 3 r e li e f o f 1 4 CF R pa r t 21
, an d an y a ss o ci a t e d no is e c e rtific a ti o n an d t e sti ng

r equ ir e m en t s o f pa r t 36
, i s no t ne c essa r y

.Notes Regarding: 14 C.F.R. § 45.23 (b). Marking of the Aircraft

G ive n the s ize of the sUAV, two

- inc h letteri ng w ill be imposs ible

. U A w il l b e i den tifi e d b y s e ri a l nu m be r , r eg ist e r e d i n a cc o r dan c e w it h 1 4 CF R pa r t 47
, an d hav e i den tific a ti o n ( N

- - - N u m be r ) m a r k i ng s i n acco r danc e w it h 1 4 CF R pa r t 45

, Subpa r t C

. M a r k i ng s w il l b e

a s l a r g e a s p r ac ti cab l e

.

Notes Regarding: 14 CFR § 91.7(a) Civil Aircraft Airworthiness Aeronautic Im agery , LLC ’s request is based on the fact that no airworthiness certificate will be issued for the UAS. Aeronautic Imagery , LLC ’s UAS will not require an airworthiness certificate in accordance with 14 CFR part 21, Subpart H. Based on the fact that an airworthiness certificate will not be issued, exemption from § 91.7(a) is not
necessary

. Notes Regarding: 1 4 CFR § 91.9(b)(2) Civil aircraft flight manual, marking & placard Certifications required, the original intent of these regulations was to display an aircraft’s airworthiness, certification, and registration documents so they would be easily available
to inspectors and passengers. Based on the FAA Memorandum subject “Interpretation regarding whether certain required documents may be kept at an unmanned aircraft’s control station,” dated August 8, 2014, the requested relief from 14 CFR §§ 91.9(b)(2) and 91. 203(a) and (b) is not necessary

. Notes Regarding: §91.109 Flight instruction; Simulated instrument & certain flight tests Small UASs, by

their design, do not have fully functional dual controls. Flight control is accomplished through the use of a control box that communicates with the aircraft via radio communications. Aircraft being considered for use by Aeronautic Imagery , LLC allow the UAS I nstructor to place the aircraft into ‘loiter’ mode (fixed altitude stationary hold). In the event of the student l osing control, the UAS Instructor can quickly and via alternate equipment (equipment not in the hands of the student) place the aircraft into a mode that then allows the instructor to bring the aircraft back into control and back to the
pre

- determined and

/or safe landing location. Aeronautic Im agery , LLC does not describe training scenarios in which a dual set of controls would be utilized or required, i.e. dual flight instruction, provided by a flight instructor or other company

- designated individual, tha t would require that individual to have fully

functioning dual controls. Rather, Aeronautic I magery , LL C evaluates the qualification of its PI Cs based on their experience with the UAS to be operated and verifies through testing, in lieu of formalized train ing. As such, Aeronautic Imagery
, LLC does not seek relief from 14 CFR § 91.109.

Notes Regarding § 14 CFR 91.119(b) Relief from § 14 CFR 91.119(b), operation over congested areas, is not applicable, because the Aeronautic Imagery , LLC operations will only be conducted within the secured area described herein.**Aeronautic Imagery, LLC Safety Operations & Procedures**  **Overview:**

Technology Considerations: Best

- in

- class, tried and proven technologies that are in advanced iterations. Software from highly

- reputable industry partners will include features

- 1. Auto descent (landing) if communication signal were to be severed. If the sUAS loses communications, the sUAS will have capability to return to a pre

- determined location w ithin the Security Perimeter and land. 2. Auto descent (landing) if battery were to drop lower than nominal level. 3. Flights will be terminated at 25% battery power reserve. 4. Live video for operator gives real

- time positioning feedback. In other words, we

can monitor the scene from the vehicle's perspective for collision avoidance, and to maintain spatial orientation. 5. The sUAS will have the capability to abort a flight in case of unpredicted obstacles

or emergencies. 6. On

- Screen

- Display (OSD) contains operating information to ascertain vehicle health at all times: speed, altitude, number of GPS satellites (when available), heading and voltage. 7. GPS lock supplies for return

- to

- home (RTH). Should Command and Control (C2) link failures occur (highly improbable), vehicle returns automatically to the point of launch. 8. Altitude information will be provided to the sUAS pilot via a digitally encoded telemetric data feed, which downlinks from the aircraft to a ground

- based on

- screen display. This altitude information will be generated by equipment installed on board the aircraft, using GPS triangulation, or digitally encoded barometric altimeter, or radio altimeter, or any combination thereof. Prior to each flight, a zero altitude initiation point will be established a nd confirmed for accuracy by the pilot.

Mechanical/Physical: 1. Aeronautic Imagery, LLC will fly line

- of

- sight (LOS) only. The vehicle will always remain in direct LOS to the pilot, thus eliminating the concern of signal severance (flying behind objects/walls). 2. The sUAS will weigh less than 55 lbs and travel at less than 50 knots. 3. Batteries should far exceed the capacity required for actual flight time. 4. Flights will be operated at an altitude of no more than 400 feet AGL. 5. Fireproof bags for storag e and charging of high capacity Lipo batteries on

- site. 6. UA operated under this exemption will be marked in accordance with 14 CFR part	45	or	as	otherwise	authorized	by	the FAA.

Personnel: 1. Spotters ensure safe operation and act as a redundant set of eyes for operators (pilot, gimbal op, director) 2. Radio spectrum analysis for interference on the frequencies utilized for vehicle control/communication. 3. A briefing will be conducted in regard to the planned sUAS operations prior to each day’s activities. It will be mandatory that all personnel who will be performing duties within the boundaries of the safety perimeter be present for this briefing. 4. The operator will obtain the consent of all persons involved in the sUAS operationsand ensure that only consenting persons will be allowed within 100 feet of the flight operations. 5. Observer and pilot will at all times be able to communicate by voice. 6. Written and/or oral permission from the relevant property holders will be obtained. 7. Pilot and observer will have been trained in operation of UAS generally and received up

- to

- date information on the particular UAS to be operated.

Operations: 1. The unmanned aircraft (UA) must weigh less than 55 pounds (25 Kg), including energy

source(s) and equipment. Operations authorized by this petition of exemption are limited to the following aircraft described in Appendix B. Proposed operations of any other aircraft will require a new petition or a petition amendment to this request.

2. The UA may

not be flown at a ground spee d exceeding 50 knots.

3. Flights must be operated at an altitude of no more than 400 feet above ground level (AGL), as indicated by the procedures specified in the operator’s manual. All altitudes reported to ATC must be in feet AGL.

4. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. This requires the PIC to be able to use human vision unaided by an y device other than corrective lenses, as specified on the PIC’s FAA

- issued medical certificate.

5. All operations must utilize a visual observer (VO). The VO may be used to satisfy the VLOS requirement as long as the PI C alway s maintains VLOS capability . The VO and PIC must be able to communicate verbally at all times.

6. The operator’s manual included as Appendix C and this petition of ex emption must be maintained and made available to the Administrator upon request. If a discrepancy

exists between the conditions and limitations in this exemption and the procedures outlined in the operator’s manual, the conditions and limitations here in take precedence and must be followed. Otherwise, the operator must follow the procedures as outlined in its operator’s manual.

The operator may

update or revise its operator’s manual. I t is the operator’s responsibility

to track such revisions and pres ent updated and revised documents to the Administrator upon request. The operator must also present updated and revised documents if it petitions for extension or amendment. If the operator determines that an y update or revision would affect the basis for which the FAA grants this petition for exemption, then the operator must petition for amendment to their exemption. The FAA’s UAS Integration Office (AFS

- 80) may be contacted if questions arise regarding updates or revisions to the operator’s manual.

7. Prio r to each flight the PIC must inspect the UAS to ensure it is in a conditionfor safe flight. If the inspection reveals a condition that affects the safe operation of the UAS, the aircraft is prohibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight. The Ground Control Station, if utilized, must be included in the preflight inspection. All maintenance and alterations must be properly documented in the aircraft records.

8. A ny UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics, e.g. replacement of a flight critical component, must undergo a functional test flight in accordance with the operator’s manual. The PI C who condu cts 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 aircraft record entry must be added to the operator’s manual.

9. The operator must follow the manufacturer’s UAS aircraft/component, maintenance, overhaul, replacement, inspection, and life limit requirements. When unavailable, aircraft maintenance/component/overhaul, replacement, and inspection/maintenance requirements must be established and identified in the operator’s manual. At a minimum, requirements for the following must be included in the operator’s manual:

a. Actuators / Servos; b. Transmission (single rotor);

c. Powerplant (motors); d. Propellers;

e. Electronic speed controller; f. Batteries;
g. Mechanical dy

namic components (single rotor); h. Remote command and control; i. Ground control station (if used); and j. Any other components as determined by the operator;

10. The PI C must meet the flight review requirements specified in 14 CFR § 61.56 in an aircraft in which the PI C is rated on his or her pilot certificate.

11. Prior to operations conducted for the purpose of infrastructure inspections, the PI C must have accumulated and logged, in a manner consistent with 14 CFR § 61.51(b), a minimum of 200 flight cy cles and 25 h ours of total time as a UAS rotorcraft pilot and at least 10 hours logged as a UAS pilot with a similar UAS ty pe (single blade or multirotor). Prior documented flight experience that was obtained in compliance with applicable regulations may satisfy this r equirement. Training, proficiency , and experience

- building flights can also be conducted under this petition of exemption to accomplish the required flight cy cles and flight time. During training, proficiency , and experience

- building flights, all persons n ot essential for flight operations are considered nonparticipants, and the PIC mustoperate the UA with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

12. Prior to operations conducted for the purpose of infrastructure inspection, the PI C must have accumulated and logged, in a manner consistent with 14 CFR § 61.51(b), a minimum of five hours as UAS pilot operating the make and model of UAS to be utilized for operations under the exemption and three take

- offs and three landings in the preceding 90 day s. Training, proficiency
, experience

building, and take

- off and landing currency flights can be conducted under this petition of exemption to accomplish the required flight time and 90 day currency

. During training, profici ency , experience

- building, and take

- off and landing
currency flights all persons not essential for flight operations are considered nonparticipants, and the PI C must operate the UA with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

13. Prior to any

flight operations authorized by this petition of exemption, the PIC and VO must have successfully completed a qualification process, as outlined in the operator’s manual. As this is a requirement stipulated by the operator, the test

m ust be developed and implemented by a qualified person designated at the sole discretion of the operator. A record of completion of this qualification process must be documented and made available to the Administrator upon request.

14. Prior to operations conducted for the purpose of infrastructure inspection, a flight demonstration, administered by an operator

- approved and

- qualified pilot must be successfully completed and documented. This documentation must be available for review upon request by the Adm inistrator. Because the knowledge and airmanship
test qualifications have been developed by the operator, and there are no established practical test standards that support a jurisdictional FAA FSDO evaluation and approval of company designated examiners, the petitioner will conduct these tests in accordance with the operator’s manual.

15. The UA may not be operated directly over any person, except authorized and consenting personnel, below an altitude that is hazardous to persons or property on the surface in the event of a UAS failure or emergency.

16. Regarding the distance from participating persons, the operator’s manual has safety mitigations for authorized and consenting personnel. At all times, those persons must be essential to the operations.

17. Regarding distance from nonparticipating persons, the operator must ensure that no persons are allowed within 500 feet of the area except those consenting to be involved and necessary for the infrastructure inspection operations. This provision
may be reduced to no less than 200 feet if it would not adversely affect safety and the Administrator has approved it. For example, an equivalent level of safety may be determined by an aviation safety inspector’s evaluation of the infrastructure inspection area to note terrain features, obstructions, buildings, safety barriers, etc. Such barriers may protect nonparticipating persons (observers, the public, news media, etc.) from debris in the event of an accident.18. If the UAS loses communications or loses its G PS signal, the UA must return to a pre

- determined location within the security perimeter and land or be recovered in accordance with the operator’s manual.

19. The UAS must abort the flight in the event of unpredicted obstacles or emergencies in accordance with the operator’s manual.

20. Each UAS operation must be completed with 25% battery power remaining.

21. The operator must obtain an Air Traffic Organization (ATO) issued Certificate of Waiver or Authorization (COA) prior to conducting any operations under this petition of exemption. This COA will also require the operator to request a Notice to Airman (NOTAM) not more than 72 hours in advance, but not less than 48 hours prior to the operation.

22. All aircraft operated in accordance with this exemption must be identified by serial number, registered in accordance with 14 CFR part 47, and have identification (N

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

23. The operator must develop procedures to document and maintain a record of the UAS maintenance, preventative maintenance, alterations, status of replacement/overhaul component parts, and the total time in service of the UAS. These procedures must be added to the operator’s manual.

24. Each UAS operated under this exemption must comply with all manufacturer Safety Bulletins.

25. The operator must develop UAS technician qualification criteria. These criteria must be added to the operator’s manual.

26. The preflight inspection section in the operator’s manual must be amended to include the following requirement: The preflight inspection must account for all discrepancies, i.e. inoperable components, items, or equipment, not covered in the relevant preflight inspection sections of the operator’s manual.

27. Before conducting operations, the radio frequency spectrum used for operation and control of the UA must comply with the Federal Communications Commission (FCC) or other appropriate government oversight agency requirements.

28. At least three days before scheduled infrastructure inspection, the operator of the UAS affected by this exemption must submit a written Plan of Activities to the local FSDO with jurisdiction over the area of proposed infrastructure inspection. The 3

- day notification may be waived with the concurrence of the FSDO. The plan of activities must include at least the following:

a. Dates and times for all flights; b. Name and phone number of the operator for the UAS infrastructureinspection operations conducted under this petition of exemption;

c. Name and phone number of the person responsible for the on

- scene operation of the UAS; d. Make, model, and serial or N

- number of UAS to be used;

e. Name and certificate number of UAS PICs involved in the infrastructure inspection event; f. A statement that the operator has obtained permission from property owners and/or local officials to conduct the infrastructure inspection event; the list of those who gave permission must be made available to the inspector
upon request; g. Signature of exemption

- holder or representative; and h. A description of the flight activity, including maps or diagrams of any area, city, town, county, and/or state over which infrastructure inspection will be conducted and the altitudes essential to accomplish the operation.

29. The documents required under 14 CFR §§ 91.9 and 91.203 must be available to the PIC at the Ground Control Station of the UAS any time the aircraft is operating. These documents must be made available to the Administrator or any law enforcement official upon request.

30. The UA must 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 gliders, etc.).

31. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All operations must be conducted under visual meteorological conditions (VMC). Flights under special visual flight rules (SVFR) are not authorized.

32. The UAS may not be operated by the PIC from any moving device or vehicle.

33. The UA 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.

34. The UA may not operate in Class B, C, or D airspace without written approval from the FAA. The UA may not operate within 5 nautical miles of the geographic
center of a non

- towered airport 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 operator’s COA. The letter of agreement with the airport management must be made available to the Administrator upon request.

35. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of the operational area as defined by the applicable COA must be reported to the FAA’s UAS Integration Office (AFS

- 80) within 24 hours. Accidents must be reported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov. Further flight operations may not be conducted until the incident, accident, or transgression is reviewed by AFS

- 80 and authorizatio n to resume operations is provided.**Support for Petition for Exemption** 

In accordance with the procedural requirements of 14 C.F.R. §11.81, Aeronautic Imagery , LLC provides the following information:

**Contact Information:** Edgar F. Heiskell, IV CEO Aeronautic Im agery , LLC 87 Cany on Road Morgantown, WV 26508 (304) 290

- 7547 skipheiskell2@y ahoo.com

**Regulatory Provisions from which Aeronautic Imagery, LLC**  **seeks an Exemption**  Aeronautic Im agery , LLC believes it may need an exemption from the following provisions to conduct the contemplated operations. In some instances, relief is needed because relief from another provision renders compliance with the regulation at hand infeasible. 333 Aircraft Exemp tion Status 14 C.F.R. §61.113(a) and (b) 14 C.F.R. §91.119(c) 14 C.F.R. §91.121 14 C.F.R. §91.151 14 C.F.R. §91.405(a) 14 C.F.R. §91.407(a) 14 C.F.R. §91.409(a)(1)&(2) 14 C.F.R. §91.417(a)&(b)

Aeronautic Im agery , LLC believes an exemption is only needed f rom the above

listed regulatory

provisions. To the extent that the FAA believes that additional relief is required for Aeronautic Imagery , LLC to conduct the operations described here, we request an exemption from any such regulatory provisions as well. 3

3 For example, 14 C.F.R. §91.417(a) imposes certain maintenance record keeping requirements “as applicable”. Since none of the underlying requirements (e.g., inspection intervals) can be met and will require an exemption, Aeronautic Imagery, LLC believes a separate exemption should not be required for §91.417(a).**The Extent of Requested Relief and the Reasons Relief is Needed** 

**Section 333 Aircraft Exemption Status:**  Section 333 of the Modernization Act authorizes the FAA to exempt aircraft from the requirement for an airworthiness certificate based on a consideration of the size, weight, speed, operational capability of the particular UAS, as well as its proximity to airports and populated areas. An analysis of these criteria demonstrates that the sUAS operated without an airworthiness certificate in the areas and under the conditions contemplated by Aeronautic Imagery, LLC will be at least as safe, if not safer, than a conventional aircraft (fixed wing or rotorcraft) operatin g with an airworthiness certificate without the conditions proposed in this request.

The sUAS is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, and operates exclusively within a secured area. Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by the operator and observer. Operations will be conducted in compliance with the FAA and with local public safety requirements to provide security for the area of operation as is now done with conventional equipment, infrastructure, bridge and out building evaluation. These safety enhancements provide an expanded degree of safety to the inspectors over conventional operations. Lastly, application of these same criteria demonstrates that there is no credible threat to national security posed by the sUAS, due to its size, speed of operation, location of operation, lack of explosive materials and inability to carry a substantial external load.

Given the size and limited operating area associated with the aircraft to be utilized by the Applicant, this meets the requirements of an equivalent level of safet y under Part 11 and Section 333 of the Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333 of the Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration of the size, weight, speed, operational capability , and proximity to airports and populated areas of the particular sUAS. I n all cases, an anal ys is of the se criteria demonstrates that the UAS operated without an airworthiness certificate, in the restricted environment and under the conditions proposed will be at least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate without the restrictions and conditions proposed.14 C.F.R. §61.113(a) and (b) **§61.113 Private pilot privileges and limitations: Pilot in command.**  (a) Except as provided in paragraphs (b) through (h) of this section, no p erson who holds a private pilot certificate may act as pilot in command of an aircraft that is carry ing passengers or propert y for compensation or hire; nor may that person, for compensation or hire, act as pilot in command of an aircraft. (b) A private pilot may , for compensation or hire, act as pilot in command of an aircraft in connection with any business or employ

ment if: (1) The flight is onl y incidental to that business or employment; and (2) The aircraft does not carry passengers or property

for compensation or hire.

***** Aeronautic Im agery , LLC anticipates initially using a cadre of speciall y trained staff to conduct the sUAS operations. While these individuals will not hold commercial pilot licenses. The sUAS will not carry propert y for compensation or hire since they will be used solel y to assist in evaluation of the infrastructure, equipment, right

- of

- way , assets, bridges, tunnels and out

- buildings in furtherance of Aeronautic Imagery , LLC ’s client’s primary business, the successful operation of a infrastructure; however, the employ ees’ operation of the sUAS will not be incidental to their employ ment with Aeronautic Im agery , LLC , and they will be compensated for such work. Without an exemption, the pilot woul d be required to hold a commercial pilot certificate under §61.133. However, the risk associated with the contemplated operations is less than the risk posed by

a traditional aircraft. The sUAS will fly at altitudes well below the permissible limits for other civil aircraft, eliminating the risk to other aircraft, and within a geographical envelope under the sole control of Aeronautic Im agery , LLC clients. Accordingl y, the risk would be limited to Aeronautic I magery , LLC personnel, who will be appropriatel y outfitted in safet y gear, and Aeronautic I magery , LL C client’s propert y on the ground. Requiring a commercial pilot certificate would provide no appreciable safet y benefit and would needlessl y impose additional cost on Aeronautic Imagery , LLC

. Because the contemplated operations would not comply with §61.113(b)(1) and none of the other exceptions to paragraph (a) appl y, relief is needed from both paragraphs (a) and (b).14 C.F.R. 91.119(c) **§91.119 Minimum safe altitudes: General.**  Except when necessary

for takeoff or landing, no person may operate an aircraft below the following altitudes:

*** (c) Over other than congested areas. An altitude of 500 feet above the surface, except over open water or sparsel y populated areas. In those cases, the aircr aft
may not be operated closer than 500 feet to any person, vessel, vehicle, or structure.

***** Aeronautic Im agery , LLC submits that the only relief it requires from §91.119 is from the minimum altitudes listed in paragraph (c). Relief is required from paragraph (c) for fixed wing operations because asset evaluation conducted at 500 feet or higher is insufficiently

distinct to be meaningful. Since operations at this altitude also pose a heightened risk of collision with another aircraft, safet y can only be assured through the grant of an exemption. The anticipated rotorcraft operations should be adequately addressed by

paragraph (d) (1). Additionally , relief should not be needed from paragraph (a) because an emergency landing of the aircraft due to a powe r failure will not create an undue hazard to persons or propert y on the surface. As noted in the explanation of wh y an exemption will not adversel y affect safet y, Aeronautic I magery , LL C’s clients have exclusive use of the land over which the sUAS will be operated, and public access is restricted. It also has exclusive use of significant portions of land adjacent to the infrastructure and structures that will be the objects of evaluation and anal ysis. Aeronautic Im agery , LLC’s c lients tightly control access to land and have the ability to assure that no individuals unassociated with the planned operations are on the affected land. As such, the risk of injury is minimal. Aeronautic I magery , LL C does not contemplate conducting operations over congested areas, so relief is not requested from paragraph (b).

14 C.F.R. 91.121 **14 C.F.R. §91.121 Altimeter Settings**  This regulation requires each person operating an aircraft to maintain cruising altitude by

reference to an altimeter that is set “...to the elevation of the departure airport or an appropriate altimeter setting available before departure.”

***** As the sUAS may

not have a barometric altimeter, but instead a GPS altitude read out, an exemption may

be needed. An equivalent level of safet y will be achieved b y the operator, pursuant to the Manual and Safety Check list, confirming the altitude of the launch site shown on the GPS altitude indicator before flight. Altitude information will be provided to the sUAS pilot via a digitally encoded telemetric data feed, which downlinks from the aircraft to a ground

- based on

- screen display. This altitude information will be generated by equipment installed on board the aircraft, using GPS triangulation, or digitally encoded barometric altimeter, or radio altimeter, or any combination thereof. Prior to each flight, a zero altitude initiation point will be established and confirmed for accuracy by the pilot.14 C.F.R. 91.151 **§91.151 Fuel requirements for flight in VFR conditions.**  (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 first point of intended landing and, assuming normal cruising speed

– (1) During the day , to fl y after that for at least 30 minutes. (b) No p erson may

begin a flight in a rotorcraft under VFR conditions unless (considering wind and forecast weather conditions) there is enough fuel to fly to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 2 0 minutes.

***** Operating the sUAS in a pre

- defined area with less than 30 minutes of reserve fuel does not raise the type of risk contemplated by §91.151, i.e., that an aircraft could run out of fuel in the event it has to be flown to an alternate airpor t or circle the planned airport in the event of unanticipated conditions. Aeronautic Imagery , LLC does not intend to use the sUAS for point

- to

- point flights and will not operate the sUAS bey ond visual line of sight. Nor will the sUAS require an airport in order to land. Rather, Aeronautic Im agery , LLC will operate the sUAS using pre

- planned flight paths (taking into account weather conditions) designed to allow the sUAS to fly to the point of intended landing. As such, there is no nee d for a time

- based excess fuel requirement. Rather it should be sufficient to require onl y as much additional excess flight capacit y as necessary to safel y land the sUAS. We believe that a 25% battery reserve is more than sufficient to meet this objective

.14 C.F.R. 91.405(a), 91.407(a) (1), 14 C.F.R. 91.409(a) (1)&(2) and 14 C.F.R. 91.417(a) & (b) **§91.405 Maintenance required.**  Each owner or operator of an aircraft

– (a) Shall have that aircraft inspected as prescribed in subpart E of this part and shall between required inspections, except as provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this chapter;

***** **§91.407 Operation after maintenance, preventive maintenance,**  **rebuilding, or alteration.**  (a) No person may

operate any

aircraft that has undergone maintenance, rebuilding, or alteration unless

– (1) It has been approved for return to service b y a person authorized under §43.7 of this chapter;

***** **§91.409 Inspections.** (a) Except as provided i n paragraph (c) of this section, no person may operate an aircraft unless, within the preceding 12 calendar months, it has had (1) An annual inspection in accordance with part 43 of this chapter and has been approved for return to service by a person author ized by

§43.7 of this chapter; or (2) An inspection for the issuance of an airworthiness certificate in accordance with part 21 of this chapter.

***** **§91.417 (a) & (b)**

***** Aeronautic Im agery , LLC believes that an exemption from these three maintenance requirements is appropriate because the FAA has not developed maintenance standards that would allow an operator to meet the part 91 maintenance requirements. In particular, there are no individuals authorized by the FAA to approve a sUAS for return to service under §91.407(a) or to conduct the initial airworthiness and annual return to service inspections required b y §91.409(a). Aeronautic Im agery , LLC will maintain the aircraft as instructed in the owner’s manual, where applicable, and will not operate the aircraft until it has reasonabl y determined that an y needed repairs have been made. However, because of the technical impossibility of meeting the requirements of §§91.405(a), 407(a), 409(a) and 41 7(a)&(b), we believe an exemption from these provisions is appropriate.

Please do not hesitate to contact me at the phone number or via the e

- mail address provided above should you have an y questions or concerns.

Respectfully submitted,

Edgar F. Heiskell, IV CEO, Aeronautic Im agery, LLC.**Appendix A** 

Summary for Federal Register Publication

Pursuant to 14 C.F.R. Part 11, the following summary is provided for publication in the Federal Register should the FAA determine that publication is needed.

Petitioner: Aeronautic Imagery , LLC

Sections of 14 C.F.R. Affected: 333 Aircraft Exemption Status 14 C.F.R. §61.113(a) and (b) 14 C.F.R. §91.119(c) 14 C.F.R. §91.121 14 C.F.R. §91.151 14 C.F.R. §91.405(a) 14 C.F.R. §91.407(a) 14 C.F.R. §91.409(a) 14 C.F.R. §91.417(a)&(b)

Description of Relief Sought:

Petitioner seeks relief from the requirements of 333 Aircraft Exemption Status, 14 C.F.R., 61.113(a)&(b)), 91.119(c), 91.121, 91.151, 91.405(a), 91.407(a), 91.409(a), and 91.417(a)&(b) to conduct sU AS operations over Aeronautic Im agery , LLC Client’s owned or controlled land, solely during day light hours, to assist in the safe evaluation and anal ys is of infrastructure and operations. In general, sUAS operations are intended to be conducted in areas re mote from both congested areas and airports. The nature of operations anticipated b y Aeronautic Im agery , LLC requires that the sUAS be flown at relativel y low altitudes. Aeronautic Im agery , LLC expects that in most instances, the sUAS will be flown less th an 75 feet from the highest structure along the path of the sUAS and in no instances will be flown higher than 400 feet above the ground. Accordingl y, the risk of interference with other aircraft is minimal.**Appendix B** 

**Specific	type(s),	make, and**  **model :** 



### DJI	Phantom	3	Professional

**Aircraft Weight (In**  **cluding Battery And Propellers):** 1280 g **Diago nal Size (Including Propellers):**  590 mm **Max Ascent Speed** : 5 m/s **Max Descent Speed:** 3 m/s **Hover Accuracy:** V ertical: +/

- 0.1 m (when Vision Positioning is active) or +/

- 0.5 m

Horizontal: +/

- 1.5 m Max Speed 16 m/s (ATTI mode, no wind)
**Max Altitude Above Sea Level :**  6000 m **Operating Temperature** : 0°C to 40°C
**GPS Mode:** GPS/GLONASS
**Camera Sensor**  **:** Sony

EXMOR 1/2.3” Effective pixels: 12.4 M (total pixels: 12.76 M)
**Lens :**  FOV 94° 20 mm (35 mm format equivalent) f/2.8, focus at ∞ **ISO Range :**  100

- 3200 (video) 100

- 1600 (photo) **Shutter Speed :**  8s

- 1/8000s **Image Max Size :**  4000 x 3000 **Still Photography Modes :**  Single Shot **Burst Shooting:** 3/5/7 shots **Auto Exposure Bracketing (AEB):** 3/5 Bracketed Frames at 0.7EV Bias
**Time**

**- lapse**  **Video Recording Modes :**  UHD: 4096x2160p 24/25, 3840x2160p 24/25/30 FHD: 1920x1080p 24/25/30/48/50/60HD: 1280x720p 24/25/30/48/50/60

**Supported SD Card Types :**  **Micro SD :**  Max capacity : 64 GB. Class 10 or UHS

- 1 rating required
**Max Bitrate o f Video Storage**  **:** 60 Mbps **Supported File Formats :**  Photo: JPEG, DNG Video: MP4, MOV (MPEG

- 4 **Operating Temperature :**  0°C to 40°C
**Gimbal Controllable Range**  **:** Pitch

- 90° to +30°
**Stabilization :**  3

- axis (pitch, roll, y aw) Vision Positioning **Max Velocity:** Less than 8 m/s (when 2 m above ground) **Altitude Range :**  30 cm

- 300 cm **Operating Range :**  30 cm

- 300 cm **Operating Environment :**  Surface with clear pattern and adequate lighting (Lux > 15)
**Remote Controller Operating Frequency**  **:** 2.400 GHz

- 2.483 GHz
**Max Distance :**  2000m (outdoors and unob structed) **Battery:** 6000 mAh L iPo 2S **Receiver Sensitivity (1%PER) :** 

- 101 dBm ±2 dBm **Transmitter Power (EIRP) :**  FCC: 20 dBm CE: 16 dBm **Working Voltage :**  1.2 A @7.4 V **Battery Charger Voltage**  **:** 17.4 V
**Rated Power :**  100 W **Intelligent Flight Battery Capacity**  **:** 4480 mAh **Voltage:** 15.2 V **Battery Type :**  LiPo 4S **Energy:** 68 Wh **Net Weight** : 365 g **Max Flight Time:** Approximately 23 minutes **Operating Temperature :** 

- 10°C to 40°C