Aerial Concepts LLC Section 333 Exemption Petition

Re: Exemption Request Pursuant To Section 333 of the FAA Reform Act of 2012

Dear Sir or Madam,

Pursuant to §333 of the FAA Modernization and Reform Act of 2012 (the Reform Act) and 14 

C.F.R. Part 11, Aerial Concepts LLC, operator of Small Unmanned Aircraft Systems (sUASs) 

equipped to conduct aerial photography for the media and advertising industries for pre-planned, 

controlled area, photographic and surveying services, hereby applies for an exemption from the 

listed Federal Aviation Regulations (FARs) to allow commercial operation of its sUASs, so long 

as such operations are conducted within and under the conditions outlined herein or as may be 

established by the Federal Aviation Administration (FAA) as required by §333. Aerial Concepts’

current operation of sUASs for commercial purposes has been halted to comply with recently

enacted federal aviation regulations pertaining to sUASs.

As described more fully below, the requested exemption would permit the operation of small, 

unmanned and relatively inexpensive multi-rotor aircraft under controlled conditions in airspace 

that is 1) contained 2) predetermined 3) has on-site safety personnel controlling access, and 4) 

would provide increased safety and enhancements to clients' business operations.

The name and address of the applicant is:

Aerial Concepts LLC

ATTN: Brad Gibson 

Ph: (918) 691-3420

Email: bradgibson@aerialconceptsok.com

Address: 6924 S 67th East Avenue Tulsa, OK 74133

Web: www.aerialconceptsok.com

Aerial Concepts LLC respectfully requests a grant of an exemption of the following sections of 

Title 14 of the Code of Federal Regulations:

14 CFR 21; 14 CFR 91, et seq., 14 CFR 45.23

Aerial Concepts also respectfully requests an Exemption from Section 333 of the FAA Reform 

Act and Part 11 of the Federal Aviation Regulations from:

14 CFR 45.23(b);14 CFR Part 21;14 CFR 61.1 13 (a) & (b); 91.7 

(a);91.9(b)(2);91.103(b);91.109;91.119;91.121;91.151(a);91.203(a) & (b); • 91.405 (a) 

91.407 (a) (1);91.409 (a) (2);91.417 (a) & (b).
I. The Extent of Relief Aerial Concepts LLC Seeks and the Reason It Seeks Such Relief

Aerial Concepts submits this application in accordance with the Reform Act, 112 P.L. 95 §§331-

334, seeking relief from any currently applicable federal aviation regulations PARs pertaining to 

UASs (unmanned aircraft systems) and operating to prevent Aerial Concepts contemplated 

commercial photography, Photographic mapping, and other flight operations within the U.S. 

national airspace system.

The Reform Act in §332 provides for such integration of civil UASs into our national airspace 

system as it is in the public's interest to do so. Aerial Concepts lightweight UASs meet the 

definition of "small unmanned aircraft" as set forth in §331 and combined with a sterling safety 

record in similar industries, the light duty UASs used by Aerial Concepts are ideal recipients of 

exemption by the intent of the Reform Act.

Considerations for relief include a combination of sUAS physical characteristics, safety features, 

and safe practices identified in §333:

• sUAS weight,

• sUAS overall size,

• sUAS speed over ground,

• sUAS flight zone characteristics,

- Non-operation near airports (civilian or military), 

- Tightly controlled operation in populated areas, 

Specific consideration is outlined below.

• Operation of the UAS by VLOS.

• Coordination by a minimum of two (2) persons, two (2) staff members of Aerial Concepts and 

one (1) safety official from the client.

14 C.F.R. Part 21, Subpart H: Airworthiness Certificates14 C.F.R. §91.203 (a) (1) Subpart H, 

entitled Airworthiness Certificates, establishes the procedural requirements for the issuance of 

airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and limited 

operating area associated to sUASs, an exemption from Part 21 Subpart H meets the 

requirements of an equivalent level of safety under Part 11 and §333 of the Reform Act. 1l1e 

Federal Aviation Act (49 U.S.C.§4470 1 (f)) and §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. In all cases, an analysis of these 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.

The sUAS to be operated by Aerial Concepts is less than 11kg. with maximal payload consisting 

of remote sensing instrumentation, carries neither no persons, carries no explosive or flammable 

materials including combustible fuels, and operates exclusively within a secured area. Unlike 

other civil aircraft, operations under this exemption will be tightly controlled and monitored by

both the pilot (PIC), 'spotter' role designated to act as both the remote sensing controller and 

secondary monitor for safety issues, and a technician, which assists in matters related to 

maintaining the sUAS and also monitors for safety concerns and liaisons to the on-site safety 

officials. These enhancements to current safety practices and regulations, which already apply to 

civil aircraft, provide a greater degree of safety to the public and property owners than 

conventional aircraft operations conducted with airworthiness certificates issued under 14 C.F.R. 

Part 21, Subpart H. 

Lastly, application of these same criteria demonstrates that there is no intrinsic credible threat to 

national security posed by the UAS, due to its size, speed of operation, location of operation, 

lack of intrinsic explosive materials or flammable liquid fuels, and inability to carry a substantial 

external load.

14 C.F.R. §45.23 (b). Marking of the Aircraft The regulation requires: 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 provisionally certificated aircraft, the operator

must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in 

letters not less than 2 inches nor more than 6 inches high, the words "limited;' "restricted;' "lightsport;' "experimental;' or "provisional;' as applicable.

Even though the sUAS will have no airworthiness certificate, an exemption may be needed as the 

sUAS will have no entrance to the cabin, cockpit or pilot station on which the word 

"Experimental" can be placed. Given the size of the sUAS, two-inch lettering will be impossible. 

The word "Experimental" will be placed on the frame in compliance with §45.29 (f) at a size 

suitable for the available space.

The equivalent level of safety will be provided by having the sUAS marked on its fuselage as 

required by §45.29 (f) where the pilot, observer and others working with the sUAV will see the 

identification of the UAS as "Experimental." The FAA has issued the following exemptions to 

this regulation to Exemptions Nos. 10700, 8738, 10167 and 10167A.

Further markings include the use of flashing green LED illumination on the underside of the 

sUAS frame, which stands at contrast against a blue or white sky.
14 C.P.R. §61.113 (a) & (b): Private Pilot Privileges and Limitations: Pilot in Command. 

§61.113 (a) & (b) limit private pilots to non-commercial operations. 

Because the sUAS will not carry a pilot or passengers, the proposed operations can achieve the 

equivalent level of safety of current operations by requiring a ground crew member to have a 

private pilot's license rather than a commercial pilot's license to operate this sUAS. Unlike a 

conventional aircraft that carries the pilot and passengers, the sUAS is remotely controlled with 

no persons on board. The area of operation is controlled and restricted, and all flights are planned 

and coordinated in advance. The risks associated with the operation of the sUAS are so 

diminished from the level of risk associated with commercial operations contemplated by Part 61 

when drafted, that allowing operations as requested with a private pilot in the ground crew 

exceeds the present level of safety achieved by 14 C.P.R. §61.1 13 (a) & (b).

14 C.P.R. §91.7(a): Civil aircraft airworthiness. The regulation requires that no person may

operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness 

certificate issued for the aircraft, should this exemption be granted, no FAA regulatory standard 

will exist for determining airworthiness. Given the size of the aircraft and the requirements 

contained in the Manual for maintenance and use of safety check lists prior to each flight, a 

subset of which are provided in enclosed Supplemental material, an equivalent level of safety 

will be provided.

14 C.F.R. §91.9 (b) (2): Civil Aircraft Flight Manual in the Aircraft. §91.9 (b) (2) provides: No 

person may operate a U.S.-registered civil aircraft ... (2) For which an Airplane or Rotorcraft 

Flight Manual is not required by §21.5 of this chapter, unless there is available in the aircraft a 

current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and 

placards, or any combination thereof.

The sUAS, given its size and configuration has no ability to carry a physical flight manual on the 

aircraft. The equivalent level of safety will be maintained by keeping the flight manual at the 

ground control point where the pilot flying the sUAS will have immediate access to it. The FAA 

has issued the following exemptions to this regulation: Exemption Nos. 8607,8737,8738,9299, 

9299A, 9565,95658, 10167, 10167A, 10602,32827, and 10700.

14 C.F.R. §91.103: Preflight action. This regulation requires each PIC to take certain actions 

before flight to insure the safety of flight. As FAA approved rotorcraft flight manuals will not be 

provided for the aircraft an exemption will be needed. The PIC will take all actions including 

reviewing weather, flight battery requirements, landing and takeoff distances and aircraft 

performance data before initiation of flight. Further, we have proprietary manuals created with 

the help of sUAS experts, the manufacturer, the regional sUAS vendor and policy holding 

insurer and continue to work with these organizations to ensure best safe practices are adhered 

to.
14 C.P.R. §91.109: Flight instruction.§91.103 provides that no 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 sUASs and remotely piloted aircraft, 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. The FAA has approved 

exemptions for flight training without fully functional dual controls for a number of aircraft and 

for flight instruction in experimental aircraft. See Exemption Nos. 5778K & 9862A. The 

equivalent level of safety provided by the fact that neither a pilot nor passengers will be carried 

in the aircraft and by the size and speed of the aircraft.

Enhancing this safety is the technology inherent in the remote controls utilizing digital 

communications, which is paired to the sUAS making it nearly impossible to unintentionally or 

intentionally have the control communications interrupted.

14 C.F.R. §91.119: Minimum safe altitudes.§91.119 establishes safe altitudes for operation of 

civil aircraft. §91.119 (d) allows helicopters to be operated at less than the minimums prescribed, 

provided the person operating the helicopter complies with any route or altitudes prescribed for 

helicopters by the FAA. As this exemption is for a sUAS that closely mimics the behavior of a 

helicopter, and the exemption requests authority to operate at altitudes up to 400 AGL, an 

exemption may be needed to allow such operations. As set forth herein, the UAS will never

operate at higher than 400 AGL or beyond unaided visual line of sight, whichever is closer. It 

will however be operated in a restricted area with security officials tasked with ensuring public 

safety, and where buildings and people will not be exposed to operations without their preobtained consent and training.

The equivalent level of safety will be achieved given the size, weight, speed of the UAS as well 

as the location where it is operated. No flight operation will be taken without the permission of 

the property owner in the case of private property or local officials i the case of public property

or private property with public interests. Because of the advance notice to the property owner 

and participants in the remote sensing activity, all affected individuals will be aware of the 

planned flight operations. Compared to flight operations with aircraft or rotorcraft weighting far 

more than the maximum 11kg of Aerial Concepts sUASs proposed herein and the lack of 

flammable fuel, any risk associated with these operations is far less than those presently 

presented with conventional aircraft operating at or below 500 AGL. In addition, the low-altitude 

operations of the sUAS will ensure separation between these small- UAS operations and the 

operations of conventional aircraft that must comply with §91.119.

14 C.F.R. §91.121 Altimeter Settings. §91.121 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 safety will be achieved by the operator, 

confirming the altitude of the launch site shown on the GPS altitude indicator before flight. The 

PIC and Technician will also ensure effective pairing with multiple GPS sources to guarantee 

accurate detection of height.

14 C.F.R. §9 1.15l (a): Fuel Requirements for Flight in VFR Conditions.§91.151 (a) prohibits 

an individual from beginning ‘a flight in an airplane under VFR conditions unless (considering 

wind and forecast weather conditions) there is enough fuel to fly to the first point of intended 

landing, and, assuming normal cruising speed- (1) During the day, to fly after that for at least 30 

minutes; or (2) At night, to fly after that for at least 45 minutes.’

The battery powering the sUAS provides approximately 15 minutes of powered flight in hover 

mode without payload. Aerial Concepts sUAS will not be able to meet the 30-minute reserve 

requirement in 14 CPR §91.151. Operating the small UAS, in a tightly controlled area where 

only people and property owners or official representatives who have signed waivers will be 

allowed, with less than 30 minutes of reserve power, does not engender the type of risks that 

Section 9l.l51(a) was intended to alleviate given the size and speed of the small UAS. Aerial 

Concepts believes that an equivalent level of safety can be achieved by limiting flights to » 10 

minutes or 25% of battery power whichever happens first. This restriction would be more than 

adequate to return the sUAS toils planned landing zone from any where in its limited operating 

area. Similar exemptions have been granted to other operations, including Exemptions 2689F, 

5745, 10673, and10808.

14 C.P.R. §91.203 (a) & (b): Carrying Civil Aircraft Certification and Registration. The 

regulation provides in pertinent part:

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

within it the following: (1) An appropriate and current airworthiness certificate... 

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

paragraph (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. 

The sUAS fully loaded weighs no more than llkg and is operated without an onboard pilot. As 

such, there is no ability or place to carry certification and registration documents or to display

them on the sUAS. An equivalent level of safety will be achieved by keeping these documents at 

the ground control point where the pilot flying the sUAS will have immediate access to them, to 

the extent they are applicable to the sUAS. The FAA has issued numerous exemptions to this 

regulation. A representative sample of other exceptions includes Exemption Nos. 9565, 9665,

9789, 9789A, 9797, 9797A, 9816A and 10700.
14 C.P.R. §91.405 (a); 407 (a) (1); 409 (a) (2); 417(a) & (b): Maintenance Inspections. These 

regulations require that an aircraft operator or owner "shall have that aircraft inspected as 

prescribed in subpart E of this part and shall between required inspections, except as provided in 

paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this 

chapter...;' and others shall inspect or maintain the aircraft in compliance with Part 43. 

Given that these section and Part 43 apply only to aircraft with an airworthiness certificate, these 

sections will not apply to the applicant. Maintenance will be accomplished by the operator 

pursuant to the flight manual. An equivalent level of safety will be achieved because these small 

UASs are very limited in size and will carry a small payload and operate only in restricted areas 

for limited periods of time. If mechanical issues arise the UAS can land immediately and will be 

operating from no higher than 400 feet AGL. The operator will ensure that the UAS is in 

working order prior to initiating flight, perform required maintenance, and keep a log of any 

maintenance performed. Moreover, the operator is the person most familiar with the aircraft and 

best suited to maintain the aircraft in an airworthy condition to provide the equivalent level of 

safety.

An exemption granted to Aerial Concepts would permit its operation of lightweight, unmanned, 

remotely controlled, sUASs in a tightly controlled environment with limited airspace. Aerial 

Concepts utilizes local business' safety officers in specifically determined areas (designed flight 

zone) to mitigate injury and property damage while fulfilling clients' goals. Technical 

enhancements to current safety controls will allow Aerial Concepts to operate exceeding current 

safety specifications, and stay ahead of, or meet, new ones being implemented by the FAA and 

Department of Transportation. Further, Aerial Concepts conducts its operations in compliance 

with protocols described herein or as otherwise established by the FAA.

II. Commercial and Public Benefits

We at Aerial Concepts believe that granting this exemption request furthers the public interest by

providing safe (by way of an unmanned system) and efficient means to meet technical problems 

solvable by elevated data collection instruments. Aerial Concepts client base are typically small 

to medium sized business' looking to increase their awareness of structures or landscape on their 

respective properties through data collection other Public Interest 

Aerial videography for geographical awareness and for real estate marketing has been around for 

a long time through manned fixed wing aircraft and helicopters, but for small business owners, 

its expense has been cost-prohibitive. Granting this exemption to the petitioner would allow him 

to provide this service at a much lower cost. Furthermore, the petitioner indicates his small UAS 

will pose no threat to the public given its small size and lack of combustible fuel when compared 

to larger manned aircraft. The petitioner also states that the operation of his UAS will minimize 

ecological damage and promote economic growth by providing information to companies 
looking to relocate or build in the Tulsa, OK metro area by photographic, video graphic or lidarbased surveying. 

By moving these functions onto sUAS based aircraft, the potential for loss of life or property is 

diminished due to the greater control in a smaller and safer aircraft that holds no persons. 

Second, there are no reactive or combustible materials on board the sUAS and thus the potential 

for fire or explosions is greatly diminished. Third, the small size and extreme maneuverability of

Aerial Concepts UASs allow the PIC to avoid hazards. 

Lastly, due to the nature of the remote sensing instrumentation onboard, the sUAS can maintain 

quite a safe distance between the aircraft and the object(s) undergoing scrutiny. Accordingly,

Aerial Concepts UASs have operated and will continue to operate at and above current safety

levels.

A. The costs and benefits of your proposed action to society in general and specific groups 

within society.

As described above, Aerial Concepts past customers have been small to medium business 

seeking a remote sensing solution to specific issues. Examples include aerial inspection of 

residential and commercial buildings to survey current conditions, surveying of large land lots, 

visual and photographic evidence of land locked properties, collection of video and images for 

tree removal services in remote, private areas, and searching for missing cattle in dense foliage 

areas.

The impact to society, financial and otherwise, would be extremely minimal. Indeed, it's been 

demonstrated that sUASs have the ability to drastically increase the information available to 

policymakers at a fraction of the cost of measuring this data by terrestrial means. One such 

impact would be inconvenience to directly proximal and non-essential personnel that would be 

displaced from public or business owned property if it is deemed to be unsafe. In this case we 

relay our needs for a f1ight zone with the requirement that it be safe from casual intrusions and 

allow the business time to shift operations in order to minimize potential safety issues. This is 

best performed with the aid of safety personnel that actively steer non-essential persons around 

the flight zone.

B. The effect of an exemption for Aerial Concepts on the quality of the natural and social 

environments.

Utilizing sUASs minimizes the requirement for conventional aircraft. This eliminates the need 

for an onboard pilot, time-consuming adherence to regulations surrounding bookkeeping and 

submission of flight paths to local civilian or military airports, and detrimental effects to the 
environment caused by operating a combustible fuel based, large scale aircraft, with restrictions 

on the proximity to the target for remote sensing.

Ill. Flight Capabilities and Characteristics of Aerial Concepts UASs pursuant to 112 P.L. 95 

§333 (a), concerns for public safety are mitigated by the overall capabilities and characteristics 

of the sUAS.

Aerial Concepts utilizes four (4) counter-rotating propellers paired oppositely to each other for 

balance, control and stability. The total span of the sUAS is less than 1.2 meters allowing for 

stable flight or landing even with the sudden onset of detrimental environmental conditions. The

sUAS's have a maximal unit+ payload mass of 11kg, including cinematic/photographic or other 

surveying equipment.

Aerial Concepts sUAS is designed to primarily hover in place to capture photographic data and 

then operate at less than a 35 knot maximum speed to the next point of interest. They are capable 

of vertical and horizontal operations but, in practice, is operated only within unaided VLOS of 

the PIC. In addition to the PIC, Aerial Concepts employs a spotter (VOS role) and a technician 

(secondary VOS and on-site personnel liaison), which are within unaided verbal communication 

range. These personnel are supplemented by safety officials provided by the client.

More characteristics have been outlined in the enclosed supplemental materials.

We also otherwise minimize pedestrian access in the flight zone of the client's grounds. In the 

event of visual loss with the UAS, the PIC can change flight controls from Cartesian (X,Y,Z) 

based controls to radial (r,a,h) based controls which allows the PIC to utilize one controller axis 

to recall the VAS to the PIC's position without concern to the current heading of the sUAS. In 

the event of loss of sight of the sUAS into an area containing hazards or possible hazards, the 

spotter has a heads-up-display containing a live video feed which can be used to locate the UAS 

while it maintains it's position in hover mode. The sUAS has demonstrated it's ability to maintain 

it's position by GPS coordinates in hover mode in "-'2Skph wind gusts at rv25 feet representing 

an extreme environmental condition beyond the range of conditions within the scope for sUAS 

operation.

All of Aerial Concepts sUASs utilize LiPo (lithium polymer) battery based power sources, 

decreasing safety risks from more easily combustible, fuel based, power sources. Flight times 

generally last between eight (8) to ten (10) minutes allowing the staff to work with small flight 

areas per phase. The maximum flight time without payload is 15 minutes, however practical safe 

operation limits this to 10 to give ample time to control the sUAS to a safe landing zone. Aerial 

Concepts further restricts flight time by not operating its sUASs with less than twenty five 

percent battery capacity. Further safety management systems in place include a GPS mode that 

allows Aerial Concepts sUASs to hover in place if communication with the PIC is lost and 
optionally follow a set of waypoints at a set speed and height to a 'home base' pre-designated safe 

landing zone. In the event of UN-foreseen motor(s) failure, the system will enter into a 

controlled descent while allowing full use of all UAS flight controls by the PIC. All commands 

sent via remote controller received during a controlled descent are translated to an 'as meant' 

paradigm meaning the flight control package will use it's real time 3 dimensional position and 

compensate rotors control the sUAS regardless of spin velocity. This assures that if one system is 

compensated a safe and successful landing can still occur.

III. Emergency Procedures 

In the event of emergencies related to the operation of the UAS, Aerial Concepts LLC has 

enacted various equipment and tactics to minimize issues during flight. They include:

• Loss of Remote Signal

- The flight package features an optional enhanced fail-safe system, which returns the 

UAS to the home base waypoint via the same path taken to the point of lost signal.

- The UAS will then perform a hover over this waypoint and then a controlled landing.

• Loss of GPS Signal

- The system will operate in assisted mode with three (3) GPS satellites.

- The flight package features an optional enhanced fail-safe system, which returns the 

UAS to the home base waypoint via the same path taken to the point of lost signal.

- In the event of signal loss with the three (3) GPS satellites, manual mode can be 

activated or the flight package can be programmed to perform a controlled landing to 

the home base waypoint.

- Ground based height ranging is preformed by a separate system and so loss of the 

GPS single will not impact a controlled and safe landing.

• Loss of Engine Power

- In the event of one (1) (or to two oppositely positioned) rotor or motor failure the

system will enter into a controlled spin where all controls are translated based on the 

current orientation and will behave as normal operation to the PIC to ensure a safe

landing.

- In the event of multiple rotor or motor failure, the flight package can be configured to

perform a safe landing or attempt operation to a home base waypoint.

- Note: Behavior of the landing location is highly dependent on the position and 

number of rotors/motors that are affected. 

• Loss of Ground Control Software 

- This will not affect operation of the flight. The unit will be piloted to a safe landing 

area and then landed so that examination of the link can be made.
IV. Reasons Why an Exemption to Aerial Concepts Will Not Adversely Affect Safety 

Standards

Aerial Concepts contends that operation of it's sUASs will not "create a hazard to users of the 

national airspace system or the public:' as stated in 112 P.L. 95 §333 (b). Given the diminutive 

size and weight of Aerial Concepts sUASs, combined with their operation in cordoned off and 

well-controlled areas, Aerial Concepts sUASs falls within Congress's contemplated safety zone.

Aerial Concepts sUASs have an established safety record bolstered by multi-point preflight 

checklist, awareness of their surroundings and intimate knowledge of the behavior of the sUAS 

platform in many weather conditions. TI1is safety record and implemented operational practices

demonstrate an awareness of public safety. Aerial Concepts operations routinely provide a 

level of safety at least equal to existing rules, and in nearly every instance, exceeds existing 

rules. Aerial Concepts has worked very closely with the regional vendors and support for this 

unit to create a tightly integrated and highly tolerant platform that has been tested thoroughly by

a vendor with a proven record for safety and solid designs.

Aerial Concepts also continues to work closely with organizations to identify and mitigate sUAS 

platform risk due to their expertise in several industries closely related to the aviation and 

transportation. Aerial Concepts does not operate its UASs on or near airports and generally has 

only operated its fleet on private grounds with cordoned off areas or areas under the control of 

the property owner I client with assistance by safety officials employed by the business. Aerial 

Concepts determines the areas needed to fulfill the clients' goals and only operates its UASs in 

these flight zones and only in compliance with well regarded safety protocols set forth initially

by the RC UAS trade and hobby groups and recently codified by relevant FARs.

Aerial Concepts has standardized the following practices to ensure safe operation of its UASs:

 Work with on-site personnel to plan flight goals

 Work with on-site personnel to restrict access to non-essential persons

 Operation by unaided VLOS operation only

 Operation in phases 10 minutes in length,

 Operation to minimal 25% battery power,

 Operation of device to GPS aided readout to 300ft at maximum,

 Numerous pre-programmed fail-safes that ensure specific behavior per issue

 Three main roles supplemented by on-site safety personnel,

 Employ controlled lifecycle management of components to guard against multiple failures

 Preform a site check day(s) before flight to identify potential issues

 Subscribe to relevant local weather and safety alerts

 Expertly choose data collection instruments and accessories to minimize flight requirements or expertise

 Aerial Concepts has experience in similar fields and has adapted this experience in it's use of UASs to 

increase safety. 
In combination to the ever-expanding knowledge repositories from hobbyists and experts alike,

Aerial Concepts is constantly evolving its practices when there is a clear benefit to operations or 

increased safety element.

V. Summary

Pursuant to 14 C.F.R. Part 11, the following summary is provided for publication in the Federal 

Register, should it be determined that publication is needed:

Aerial Concepts {applicant) seeks an exemption from the following rules: 14 C.P.R. §21, subpart 

H; 14 C.F.R 45.23(b); 14 C.P.R. §§61.113( a) & (b); 91.7 (a); 91.9 (b) (2); 91.103{b); 91.109; 

91.119; 91.121; 91.151(a); 91.203(a) & (b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2); 91.409 (a) 

{2) and 91.417 (a) & (b) to operate commercially a small unmanned vehicle (11kg or less) in 

elevated photographic and remote sensing operations.

Approval of exemptions allowing commercial operations of sUASs in the media industry will 

enhance safety by reducing risk associated with conventional aircraft operations and other means 

of elevated remote sensing involving persons. The public benefit served by approval of this 

petition is increased awareness of characteristics of difficult imaging targets. A sUAS weighing 

fewer than 1lkg and powered by sealed batteries eliminates virtually all associated risk inherent 

in operating conventional aircraft in close proximity to buildings or persons or otherwise 

elevating persons to a position they would be able to collect needed data.

The operation of small UASs, weighting less than 55lbs., conducted in the strict conditions 

outlined above, will provide an equivalent level of safety supporting the grant of the exemptions 

requested herein, including exempting the applicant from the requirements of Part 21 and 

allowing commercial operations.

As identified and described herein, Brad Gibson, and his company Aerial Concepts LLC, is an 

experienced, recognized media services professional in the various photographic and 

videography industries. Mr. Gibson and his company have been producing and delivering media 

and technical solutions for the media service industry for two (2) years with a spotless safety 

record.

The FAA has been given the authority to issue the exemption to Aerial Concepts pursuant to the 

Federal Aviation Act, 85 P.L. 726 (1958), and as such, we humbly seek your consideration and 

approval of this petition.

Note: All irregular behavior has root cause analysis performed before UAS operation is resumed.
VI. Supplements

The following links are supplements related to the operation of the UASs in operation under the 

control of Aerial Concepts LLC and are specifically related to the SteadiDrone Quad4:

http://www.steadidrone.com/support/QU4DQuickstartGuide.pdf

http://download.dji-innovations.com/downloads/nazam-v2/en/NAZAM_Quick_Start_Guide_v1.26_en.pdf

http://www.steadidrone.com/support/check.jpg

http://www.steadidrone.com/support/PeriodicMaintenanceChecklist.pdf

http://www.steadidrone.com/support/QU4DAirframeAssemblyGuide.pdf

Respectfully submitted,

Brad Gibson

Aerial Concepts LLC

6924 South 67th East Ave

Tulsa, OK 74133-1725

918-691-3420