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December 16, 2015

U.S. Department of Transportation, Docket Operations

West Building Ground Floor, Room w12-140

1200 New Jersey Avenue, SE.,

Washington, DC 20590

Petition for Exemption Under Section 333 of the FAA Reform Act and Part 11 of the Federal 

Aviation Regulations from 14 C.F.R. 45.23(b);14 CFR Part 21;14 CFR 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);91.417 (a) & (b).

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform Act) and 14 C.F.R. 

Part 11, ADSK Solutions (hereinafter referred to as PETITIONER), operator of Small Unmanned Aircraft 

Systems (“sUASs”) equipped to conduct aerial data collection, 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 their supplied Flight Operations Manual, and associated Aircraft Flight 

Manuals and as may be established by the FAA as required by Section 333.

Approval of this exemption would thereby enhance safety and fulfill the Secretary of Transportation’s (the 

FAA Administrator’s) responsibilities to “...establish requirements for the safe operation of such aircraft 

systems in the national airspace system.” Section 333(c) of the Reform Act.

The name and address of the applicant is:

CLIENT

Attn: ADSK Solutions

Phone: 248-906-2375

Email: michelle@adsksolutions.com

Address: 560 Kirts Blvd, Ste 101, Troy, MI, 48083

The proposed aircraft utilized are:

DJI Phantom 2 Vision+

DJI Inspire 1

PrecisionHawk Lancaster

This exemption application is expressly submitted to fulfill Congress’ goal in passing Section 333(a) 

through (c) of the Reform Act. This law directs the Secretary of Transportation to consider whether certain 

unmanned aircraft systems may operate safely in the national airspace system (NAS) before completion 

of the rulemaking required under Section 332 of the Reform Act. In making this determination, the 

Secretary is required to determine which types of UASs do not create a hazard to users of the NAS or the 

public or pose a threat to national security in light of the following:

• The UAS’s size, weight, speed, and operational capability;

• Operation in close proximity to airports and populated areas; and

• Operation within visual line of sight of the operator.
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The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This statutory 

authority by its terms includes exempting civil aircraft, as the term is defined under §40101 of the Act, 

that includes sUASs, from the requirement that all civil aircraft must have a current airworthiness 

certificate.

PETITIONER sUASs weigh less than 55 lbs. and operate, under normal conditions at a speed of no more 

than 100 kts with the capability to hover, and move in the vertical and horizontal plane simultaneously. 

All operations will be conducted within line of sight and will operate within the sterile area described in 

the Flight Operations Manual (FOM). As a result, the proposed operations will insure that the sUAS will 

“not create a hazard to users of the national airspace system or the public.”

Given the above, PETITIONER services falls squarely within the intended level of safety Congress 

envisioned that the FAA must allow commercial operations of UASs to commence. Given the clear 

direction in Section 333 of the Reform Act, and subsequent grants of approval, the achieved equivalent 

level of safety surrounding the proposed operations, the public benefit, the enhanced safety, associated 

with allowing UASs operations for aerial data collection purposes, the grant of the requested exemptions 

is in the public interest. Accordingly, the applicant respectfully requests that the FAA grant the requested 

exemption without delay.

Relevant Statutory Authority

This petition for exemption is submitted to fulfill Congress' goal in passing Section 333(a) through (c) of 

the Reform Act. In the Reform Act, Congress directed the FAA "to safely accelerate the integration of civil 

unmanned aircraft systems into the national airspace system" and, under Section 333 of that law, directed 

the Secretary of Transportation ("FAA Administrator") to consider whether certain unmanned aircraft 

systems may operate safely in the National Airspace System ("NAS") before completion of the rulemaking 

required under Section 332 of the Reform Act.

In making this determination, the Secretary is required to determine which types of UASs do not create a 

hazard to users of the NAS or the public or pose a threat to national security in light of the following:

The UAS's size, weight, speed, and operational capability;

Operation of the UAS in close proximity to airports and populated areas; and

Operation of the UAS within visual line of sight of the operator.

If the Secretary determines that such vehicles "may operate safely in the National Airspace System, the 

Secretary shall establish requirements for the safe operation of such aircraft in the National Airspace 

System". 

In addition, the FAA Administrator has general authority to grant exemptions from its safety regulations 

and minimum standards when the Administrator decides a requested exemption is in the public interest. 

See 49 U.S.C. § 44701(f) (authorizing the grant of exemptions from a requirement of regulations 

prescribed pursuant to section 44701(a)–(b) and sections 44702–44716). A party requesting an 

exemption must explain the reasons why the exemption: (1) would benefit the public as a whole, and; (2) 

would not adversely affect safety (or how it would provide a level of safety at least equal to the existing 

rules). See 14 C.F.R. § 11.81; FAA, Petition for Exemptions.
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Qualification for Approval Under Section 333 of The Reform Act 

The proposed operations in this petition for exemption qualify for expedited approval under Section 333 

of the Reform Act. Each of the statutory criterial and other potentially relevant factors are satisfied. 

The proposed operations would permit the use of small and relatively inexpensive UAS under controlled 

conditions in airspace that is: (1) limited; (2) predetermined; (3) controlled as to access, and; (4) would 

provide an increased level of safety beyond that existing when fixed or rotor wing aircraft are used to 

accomplish the same purpose. 

As discussed in Subsection A below, PETITIONER's sUAS, weighting 55 lbs. or less, including payload

operates, under normal conditions, at a speed of no more than 100 knots and has the capability to hover, 

and move in the vertical and horizontal plane simultaneously. 

PETITIONER's sUASs will operate in line of sight and will operate only within a sterile area described in 

their Flight Operations Manual. Such operations will insure that the sUAS will "not create a hazard to users 

of the National Airspace System or the public."

Given the size of the sUASs involved and the restricted sterile environment within which they will operate, 

this petition for exemption falls squarely within that zone of safety i.e., an equivalent level of safety, in 

which Congress envisioned that the FAA must, by exemption, allow commercial operations of UASs to 

commence immediately. Also, due to the size of the UASs and the restricted areas in which the sUASs will 

operate, approval of the application presents no national security issue. 

Considering the clear direction in Section 333 of the Reform Act, the authority contained in the Federal 

Aviation Act, as amended, the equivalent level of safety surrounding the proposed operations, and the 

significant public benefit, including enhanced safety, reduction in environmental impacts, including 

reduced emissions associated with allowing UASs for the proposed operations, the grant of the requested 

exemptions is also in the public interest. 

Accordingly, PETITIONER respectfully requests that the FAA grant the requested exemption without delay.

Aircraft & Equivalent Level of Safety

PETITIONER proposes that the recent standard of limitations for UAS Section 333 Grants, and the 

conditions listed within the provided FOM, and AFMs, provide for at least an equivalent or even higher 

level of safety to operations under the current regulatory structure that utilizes conventional fixed wing 

or rotorcraft aircraft.

As a result of recent Section 333 Exemptions, PETITIONER agrees to abide by the limitations and conditions 

afforded to other recent Grant recipients conducting commercial operations with sUAS aircraft. 

Introduction and Interest of PETITIONER

PETITIONER, is a sUAS operator and professional organization with a culture of safety and compliance 

in the conduct of their operations, training, and safety and management programs as evidenced in 

the structure of their submitted documentation. The mission of PETITIONER is to support, develop 

and validate unmanned system operations while providing unmatched quality and safety for their 

business. 
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General Information Pertaining to Aircraft Operations 

PETITIONER intends to operate a sUAS less than fifty-five pounds, with the ability to conduct under 

the command of the PETITIONER Pilot In Command (PIC) and perform operations consistent with 

conducting aerial data collection.

Prior to each flight the PIC shall inspect the sUAS to ensure it is in a condition for safe flight. If the 

inspection reveals a condition that affects the safe operation of the sUAS, the aircraft will be 

prohibited from operating until the necessary maintenance has been performed and the sUAS is 

found to be in a condition for safe flight. The Ground Control Station (if utilized) shall be included in 

the preflight inspection. All maintenance and alterations shall be properly documented in aircraft 

records as indicated in the Flight Operations Manual. All discrepancies noted shall be documented as 

described in the PETITIONER Flight Operations Manual (FOM).

Any sUAS that has undergone maintenance or alterations that affect the sUAS operation or flight 

characteristics, e.g. replacement of a flight critical component, shall undergo a functional test flight 

in accordance with the manufacturer’s manual and PETITIONER FOM. 

PETITIONER shall follow the manufacturer’s sUAS aircraft/component, maintenance, overhaul, 

replacement, inspection and life limit requirements, with particular attention to flight critical 

components that may not be addressed in the manufacturer’s manuals. Each sUAS operated under 

the proposed exemption shall comply with all manufacturer System and Safety Bulletins as well as 

the PETITIONER AFM for that Aircraft.

Flight Team: Aircraft Pilot in Command (PIC) & Visual Observer (VO)

All PETITIONER Flight Crews, including PIC and Visual Observer(s) (VO), will be qualified as directed 

by PETITIONER FOM. 

PETITIONER requests exemption from the following sections of Title 14:

Part 21 prescribes the procedural requirements for issuing and changing design approvals, productions

approvals, airworthiness certificates, and airworthiness approvals. Regulations from which the exemption 

is requested:

a) 14 CFR Part 21, Subpart H – Airworthiness Certificates & 14 C.F.R. 91.203(a)(1)

b) 14 CFR 91.9 (b) (2), 14 C.F.R. 45.23(b)

c) 14 CFR 61.113 (a) & (b)

d) 14 C.F. R. 91.119

e) 14 CFR 91.151 (a)

f) 14 CFR 91.203 (a) & (b)

g) 14 CFR 91.405 (a), 14 CFR 407 (a) (1), 14 CFR 409 (a) (2), 14 CFR 417 (a) & (b)

h) 14 C.F.R. 91.7 (a)

i) 14 C.F.R. 91.103

j) 14 C.F.R. 91.109

k) 14 C.F.R. 91.121

a) 14 C.F.R. Part 21, Subpart H—Airworthiness Certificates & 14 C.F.R. § 

91.203(a)(1). 
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This petition seeks an exemption from 14 C.F.R. Part 21, Subpart H, which establishes the procedural 

requirements for the issuance of airworthiness certificates as required by 14 C.F.R. §91.203(a)(1). Given 

the size and limited operating area associated with the sUAS to be utilized by the PETITIONER, an 

exemption from Part 21 Subpart H meets the requirements of an equivalent level of safety 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 UAS. 

In all cases, an analysis of these criteria demonstrates that the sUAS 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 rotorcraft operating with an airworthiness certificate without the restrictions 

and conditions of the proposed sUAS operations.

Equivalent Level of Safety 

PETITIONER intends to use the proposed aircraft to perform the proposed operations. 

These aircraft have a demonstrated safety track record. These aircraft are equipped with advanced safety 

features such as intelligent fault handling—the system will automatically fly home and land if the 

communication link is broken, if battery levels get too low or if pre-defined wind thresholds are exceeded.

The sUAS to be operated hereunder weighs than 55 lbs. fully loaded, carries neither a pilot nor passenger, 

carries no explosive materials or flammable liquid fuels, and operates exclusively within a secured area as 

set out in the Manual.

Unlike other civil aircraft, the proposed operations in this petition for exemption will be controlled and 

monitored by the operator, pursuant to the PETITIONER Flight Operations Manual and associated Aircraft 

Fight Manual’s requirements. 

These safety enhancements, which already apply to civil aircraft operated in connection with existing 

inspection operations, provide a greater degree of safety to the public and property owners than 

conventional 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 credible threat to national 

security posed by the sUAS, due to its size, speed of operation, location of operation, lack of explosive 

materials or flammable liquid fuels, and inability to carry a substantial external load.

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

and 45.27(a).

Section 45.23(b) prescribes that 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,” “light-sport,” “experimental,” or “provisional,” as applicable.
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Equivalent Level of Safety 

An equivalent level of safety for exemptions to the aircraft marking and identification requirements of §§ 

91.9(c), 45.23(b) and 45.27(a), 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 sUAS will see the identification of the 

UAS as "Experimental." Additionally, PETITIONER will ensure compliance with any requests of sUAS 

marking by the FAA. 

The FAA has issued the following exemptions to the aircraft marking requirements of § 45.23(b): 

Exemptions Nos. 10700, 8738, 10167 and 10167A.

c) 14 C.F.R. § 61.113 (a) & (b): Private Pilot Privileges and Limitations: Pilot in 

Command.

Section 61.113(a) and (b) prescribes that—

(a) no person who holds a private pilot certificate may act as a pilot in command of an aircraft that is 

carrying passengers or property 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 employment if:

(1) The flight is only incidental to that business or employment; and

(2) The aircraft does not carry passengers or property for compensation or hire.

Section 91.7(a) prescribes that no person may operate a civil aircraft unless it is in an airworthy condition.

Section 91.7(b) prescribes that the pilot in command of a civil aircraft is responsible for determining

whether that aircraft is in condition for safe flight and that the PIC shall discontinue the flight when not 

airworthy mechanical, electrical, or structural conditions occur.

Section 91.9(b)(2) prohibits operation of U.S.-registered civil aircraft 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.

Section 91.103(b) prescribes that a pilot shall for any flight, become familiar with runway lengths at

airports of intended use, and takeoff and landing distance information.

Section 91.109(a) prescribes, in pertinent part, 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.

Equivalent Level of Safety 
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As required by the Manual, PETITIONER's sUAS operators acting as PIC will hold a sport pilot certificate or 

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

equivalent level of safety to § 61.113 (a) and (b), by requiring the PIC operating the sUAS to have a Sport 

Pilot certification or higher. 

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

no living thing on board. Moreover, the area of operation is controlled and restricted, and all flights are 

planned and coordinated in advance as set forth in the Flight Operations Manual.

The level of safety provided by the requirements included in the Flight Operations Manual exceeds that 

provided by a single individual holding a commercial pilot's certificate operating a conventional aircraft in 

accordance with § 61.113 (a) & (b). The risks associated with the operation of small, lightweight UAS are 

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

drafted, that allowing the proposed operations in this petition for exemption with a private pilot as the 

PIC exceeds the present level of safety achieved by § 61.113 (a) & (b).

d) 14 C.F.R. § 91.119: Minimum Safe Altitude

Section 91.119 prescribes that, except when necessary for takeoff or landing, no person may operate an

aircraft below the following altitudes:

(a) Anywhere. An altitude allowing, if a power unit fails, an emergency landing without undue hazard 

to persons or property on the surface.

(b) Over congested areas. Over any congested area of a city, town, or settlement, or over any open 

air assembly of persons, an altitude of 1,000 feet above the highest obstacle within a horizontal 

radius of 2,000 feet of the aircraft.

(c) Over other than congested areas. An altitude of 500 feet above the surface, except over open

water or sparsely populated areas. In those cases, the aircraft may not be operated closer than

500 feet to any person, vessel, vehicle, or structure.

(d) Helicopters, powered parachutes, and weight-shift-control aircraft. If the operation is

conducted without hazard to persons or property on the surface—

(1) A helicopter may be operated at less than the minimums prescribed in paragraph (b)

or (c) of this section, provided each person operating the helicopter complies with any

routes or altitudes specifically prescribed for helicopters by the FAA; and

(2) A powered parachute or weight-shift-control aircraft may be operated at less than the 

minimums prescribed in paragraph (c) of this section.

Section 91.121 requires, in pertinent part, 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.”

Equivalent Level of Safety 
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Compared to flight operations with rotorcraft weighting far more than 55 lbs. proposed herein, and the 

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

with conventional aircraft. An equivalent level of safety will be achieved given the size, weight, speed of 

the UAS as well as the location where it is operated. 

As set forth in the Flight Operations Manual, the sUAS will be operated in a restricted area, where 

buildings and people will not be exposed to operations without their pre-obtained consent. No flight will 

be taken without the permission of the property owner and/or local officials. Because of the advance 

notice to the property owner and participants, all affected individuals will be aware of the planned flight 

operations as set forth in the Flight Operations Manual. Furthermore, by operating at such lower 

altitudes, the sUAS will not interfere with other aircraft that are subject to the minimum safe altitude 

regulations. 

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

Section 91.151(a) prescribes that 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 fly after that for at least 30 minutes.

Equivalent Level of Safety 

An equivalent level of safety can be achieved by limiting flights to their low voltage warning at which time 

a return to land must be accomplished. This restriction would be more than adequate to return the sUAS 

to its planned landing zone from anywhere within its limited operating area. Operation of the sUAS with 

less than 30 minutes of reserve fuel does not engender the type of risks that Section 91.151(a) was 

intended to alleviate given the size and speed of the small UAS. Moreover, operation will be limited to 

controlled areas where only people and property owners, or official representatives who have signed 

waivers will be allowed.

This request for exemption falls within the scope of prior exemptions. See e.g. Exemption 10673 (allowing 

PETITIONER to operate without compliance with § 91.151 (a)); see also Exemptions 2689F, 5745, 10673, 

and 10808.

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

Section 91.203(a) prohibits, in pertinent part, any person from operating a civil aircraft unless it has within 

it (1) an appropriate and current airworthiness certificate; and (2) an effective U.S. registration certificate 

issued to its owner or, for operation within the United States, the second copy of the Aircraft registration 

Application as provided for in § 47.31(c).

Section 91.203(b) prescribes, in pertinent part, that no person may operate a civil aircraft unless the

airworthiness certificate 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.
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Equivalent Level of Safety

To the extent these regulations are applicable to the proposed sUAS operations, 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. 

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.

g) 14 C.F.R. §§ 91.405(a); 91.407(a)(1); 91.409(a)(2); 91.417 (a) & (b): Maintenance 

Inspections.

Section 91.405(a) requires, in pertinent part, that an aircraft operator or owner shall have that aircraft

inspected as prescribed in subpart E of the same part and shall, between required inspections, except as

provided in paragraph (c) of the same section, have discrepancies repaired as prescribed in part 43 of the 

chapter.

Section 91.407(a)(1) prohibits, in pertinent part, any person from operating an aircraft that has undergone 

maintenance, preventive maintenance, rebuilding, or alteration unless it has been approved for return to 

service by a person authorized under § 43.7 of the same chapter.

Section 91.409(a)(2) prescribes, in pertinent part, that no person may operate an aircraft unless, within

the preceding 12 calendar months, it has had an inspection for the issuance of an airworthiness certificate 

in accordance with part 21 of this chapter.

Section 91.417(a) and (b) prescribes, in pertinent part, that—

(a) Each registered owner or operator shall keep the following records for the periods specified in 

paragraph (b) of this section:

(1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, 

annual, progressive, and other required or approved inspections, as appropriate, for each aircraft 

(including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. The records must 

include—

(i) A description (or reference to data acceptable to the Administrator) of the work performed; 

and

(ii) The date of completion of the work performed; and

(iii) The signature, and certificate number of the person approving the aircraft for return to 

service.

(2) Records containing the following information:

(i) The total time in service of the airframe, each engine, each propeller, and each rotor.

(ii) The current status of life-limited parts of each airframe, engine, propeller,rotor, and appliance.

(iii) The time since last overhaul of all items installed on the aircraft which are required to be 

overhauled on a specified time basis.

(iv) The current inspection status of the aircraft, including the time since the last inspection 

required by the inspection program under which the aircraft and its appliances are maintained.

(v) The current status of applicable airworthiness directives (AD) and safety directives including, 

for each, the method of compliance, the AD or safety directive number and revision date. If the 
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AD or safety directive involves recurring action, the time and date when the next action is 

required.

(vi) Copies of the forms prescribed by § 43.9(d) of this chapter for each major alteration to the 

airframe and currently installed engines, rotors, propellers, and appliances.

(b) The owner or operator shall retain the following records for the periods prescribed:

(1) The records specified in paragraph (a)(1) of this section shall be retained until the work is repeated or 

superseded by other work or for 1 year after the work is performed.

(2) The records specified in paragraph (a)(2) of this section shall be retained and transferred with the 

aircraft at the time the aircraft is sold.

(3) A list of defects furnished to a registered owner or operator under

§ 43.11 of this chapter shall be retained until the defects are repaired and the aircraft is approved for

return to service.

Equivalent Level of Safety

An equivalent level of safety will be achieved because maintenance and inspections will be performed in 

accordance with the Flight Operations Manual and the Aircraft Operations Manual. As provided in the 

Flight Operations Manual, 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. 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. 

If mechanical issues arise, the UAS can land immediately and will be operating from no higher than 400 

feet AGL. Moreover, the UAS's small size, carrying capacity, and the fact that flight operations will only 

take place in restricted areas for limited periods of time, create less risk than the same factors associated 

with conventional fixed-wing aircraft and rotorcraft performing the same operation.

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

This petition seeks an exemption from 14 C.F.R. § 91.7(a), which requires that a civil aircraft be in an 

airworthy condition to be operated. Inasmuch there will be no airworthiness certificate issued for the 

sUAS, should this exemption be granted, no FAA regulatory standard will exist for determining 

airworthiness. 

Equivalent Level of Safety 

PETITIONER pilots that will be flying the sUAS have a stellar safety record. Given the size of the sUAS and 

the requirements contained in the Manual for maintenance and use of safety checklists prior to each 

flight, an equivalent level of safety will be provided.

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

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

i) 14 C.F.R. § 91.103: Preflight Action.
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This petition seeks an exemption from § 91.103, which requires a PIC to become familiar with specific 

information before each flight, including information contained in the FAA-approved Flight Manual on 

board the aircraft. Inasmuch as an FAA approved flight manual will not be provided for the sUAS, an 

exemption will be needed.

Equivalent Level of Safety 

An equivalent level of safety will be provided by following the Flight Operations Manual and Aircraft Flight 

Manual comprehensive preflight checklist. The PIC will take all actions, including reviewing weather, flight 

battery requirements, landing and takeoff distances, and aircraft performance data, before initiation of 

flight.

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

This petition seeks an exemption from 14 C.F.R. § 91.109(a), which provides that “[n]o person may operate 

a civil aircraft (except a manned free balloon) that is being used for flight instruction unless that aircraft 

has fully functioning dual controls.” sUASs and remotely piloted aircraft, by their design do not have fully 

functional dual controls. Instead, flight control is accomplished through the use of a control box that 

communicates with the sUAS via radio communications. 

Equivalent Level of Safety 

Given the size and speed of the sUAS, an equivalent level of safe training can still be performed without 

dual controls because no pilot or passengers are aboard the sUAS, and all persons will be a safe distance 

away should the sUAS experience any difficulties during flight instruction. 

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. 

k) 14 C.F.R. § 91.121 Altimeter Settings.

This petition seeks an exemption from 14 C.F.R. § 91.121, which requires a person operating an aircraft 

to maintain cruising altitude or flight level by reference to an altimeter that is set to the elevation of the 

departure airport or barometric pressure. An exemption is required because the sUAS does not have a 

barometric altimeter, but rather a GPS altitude read out. 

Equivalent Level of Safety 

An equivalent level of safety will be achieved by following the procedures set forth in the Flight Operations 

Manual and Aircraft Flight Manual. The PIC will use the GPS altitude indicator to constantly monitor the 

sUASs height, thus ensuring operation at safe altitudes.
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Public Interest

Consistent with the requirements of 14 C.F.R. §11.81(d), PETITIONER offers the following reasons why 

granting this petition for exemption is in the public interest, i.e., how granting it would benefit the public 

as a whole. 

Approval of exemptions allowing commercial operations of small and lightweight sUAS in the utility aerial 

services industry benefits the public as a whole in the following ways:

• It helps fulfill Congress' goal in passing Section 333(a) through (c) of the Reform Act, namely, 

the FAA Administrator's assessment of whether certain UAS may operate safely in the 

National Airspace System before completion of the rulemaking required under Section 332 of 

the Reform Act. 

• The operation significantly improves safety and reduces risk by alleviating human exposure 

to danger associated with current aerial data collection methods, namely, full size helicopters. 

Manned helicopters performing aerial data collection and closed set filming, have 

experienced an exceedingly high number of accidents and fatalities. The public's interest is 

furthered by reducing human exposure to death or serious injury associated with such 

activities. 

• PETITIONER's sUASs are battery powered and create no emissions. If PETITIONER's sUAS 

crashes, there is no fuel to ignite and explode. Any impact of PETITIONER's lightweight sUASs 

is, obviously, far less than a full size helicopter. The public's interest is furthered by minimizing 

ecological impact of an accident and by reducing human exposure to potentially harmful 

emissions associated with manned aircraft. 

• Aerial data collection and closed set filming are valuable tools for PETITIONER’s operations. 

However, problems with safety, cost, statistical integrity, and logistics continue to impede 

aerial surveys and inspections from conventional manned aircraft. The use of sUAS addresses 

these problems and is a powerful tool for performing a wide-range of such operations. The 

public as a whole will benefit from the safer and more cost-effective utility aerial services that 

sUAS operations provide. 

PETITIONER supports their request with the following information:

PETITIONER has provided the following information – contained in his petition and supporting

documentation including: (1) Aircraft Flight Manuals(AFM), and (2) PETITIONER Flight Operations Manual. 

Unmanned Aircraft System

The PETITIONER will operate the Aircraft per each appropriate AFM, with the option of an additional 

transportable ground station. PETITIONER will operate this aircraft in accordance with the PETITIONER

Flight Operations Manual, and appropriate Aircraft Flight Manual. 

All aircraft operations will be conducted under visual meteorological conditions (VMC). The sUAS will not 

be operated less than 500 feet below or less than 2000 feet horizontally from a cloud or when visibility is 

less than 3 statute miles from the PIC. 
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The sUAS operated in accordance with this exemption request shall be identified by serial numbers, 

registered in accordance with 14 CFR part 47, and have identification (N-Number) markings in accordance 

with 14 CFR part 45, Subpart C. Markings will be as large as practicable. 

UAS Operating Parameters

The PETITIONER states that he will abide by the FAA granted Section 333 operating conditions under this

exemption and the Flight Operations Manual for PETITIONER. 

Conclusion 

Satisfaction of the criteria provided in Section 333 of the Reform Act of 2012—size, weight, speed, 

operating capabilities, proximity to airports and populated areas, and operation within visual line of sight 

and national security—provides more than adequate justification for the grant of the requested 

exemptions allowing commercial operation of PETITIONER's sUAS in the aerial data collection and closed 

set filming activities of their business.

If additional information is required, or if you have any questions regarding this Petition for Exemption, 

please contact Grady Boyce at:

Grady Boyce, Universal Aviation Solutions, Inc. (dba, SkyGen Aviation)

Phone: 770-733-2939

Email: gboyce@skygenaviation.com

Very truly yours,

Grady Boyce

Submitted on September 7, 2015

Grady Boyce

Attachments (All Subject to Non-Disclosure Under the Freedom of Information Act, 5 U.S.C. § 552 et. 

seq.): PETITIONER Flight Operations Manual, and Aircraft Flight Manuals. 

List of Attachments 

(1) ADSK Solutions Flight Operations Manual

(2) ADSK Solutions Aircraft Flight Manual for DJI Phantom 2 Vision+

(3) ADSK Solutions Aircraft Flight Manual for DJI Inspire 1

(4) ADSK Solutions Aircraft Flight Manual for PrecisionHawk Lancaster

These attachments listed are referenced in the request for exemption and contain trade secret and 

commercial proprietary information that PETITIONER has not and will not share with others except 

under appropriate confidentiality agreements. The PETITIONER Flight Operations Manual (FOM) 
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attachment contains operating conditions and procedures that have been developed exclusively by 

PETITIONER, and that are not available to the public. PETITIONER requests that these attachments be 

treated as proprietary information pursuant to 14 C.F.R. Section 11.35, and maintains that they are 

protected from release under the Freedom of Information Act. See 5 U.S.C. 552 et seq.