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May 4, 2015

U.S. Department of Transportation, Docket Operations 

West Building Ground Floor, Room W12-140

1200 New Jersey Avenue, SE

Washington, DC 20590 

Re: Exemption Request; Section 333 of the FAA Modernization & Reform 

Act and Part 11 of the Federal Aviation Regulations from 14 C.F.R. Part 21; 

14 C.F.R. 45.23(b); 14 C.F.R. 61.113(a)&(b); 91.7(a); 91.9(b) (2); 91.103; 

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 

(“Reform Act”) and 14 C.F.R. 11, Aerial Sciences Corporation (“Petitioner”) 

hereby applies for an exemption from Federal Aviation Regulations (“FARs”) 

to allow commercial operation of small unmanned aircraft systems (“sUAS”) in 

airspace regulated by the Federal Aviation Administration (“FAA”) for use in a 

variety of commercial applications so long as such operations are conducted 

within and under the conditions outlined herein or as may be established by 

the FAA as required by Section 333.

As described more fully below, the requested exemption would permit the 

commercial operation of sUAS under controlled conditions in airspace that is: 

1) limited; 2) predetermined; and, 3) controlled as to access. The exemption

would also provide safety enhancements to the safe operations currently 

performed by those presently using conventional manned aircraft. 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.

1. Name and Address of the Petitioner

Aerial Sciences Corporation

Attn: David M. Garrett

5901 E. Lippizan Way

Hereford, AZ 85615

Tel: 520.227.1865

Email: david.garrett@msn.com

2. Company Background
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Aerial Sciences Corporation based in Arizona intends to provide solutions 

supporting development and application of Unmanned Aircraft Systems to 

satisfy Government and Commercial needs. Following approval of this 

exemption request would enable Aerial Sciences the use of our sUAS to 

conduct operations within a variety of industry and business applications such 

as Aerial Survey/Inspection and Imaging, Agricultural, Forestry, Wildlife 

Preservation, Law Enforcement, and Search and Rescue, and Training so 

long as such operations are conducted within and under the conditions 

outlined herein or as may be established by the FAA as required by Section 

333. 

Petitioner is staffed with personnel who hold Airline Transport Pilot (ATP), 

Certified Flight Instructor (CFI) – Instrument (CFII), Commercial, Instrument,

and Private Pilot ratings, Airframe and Powerplant (A&P) Licenses. The 

Petitioner has extensive experience in UAS flight/payload operations, training,

and maintenance of UAS for the US Army. 

This airman, and UAS knowledge and experience will be leveraged to 

maintain and enhance user and public safety throughout all aspects of 

unmanned aircraft (UA) ground and flight operations conducted by Aerial 

Sciences upon approval of this exemption request.

3. Regulations from which the exemption is requested, If such 

regulations apply to sUASs.

14 C.F.R. Part 21;

14 C.F.R. 45.23(b);

14 C.F.R. 61.113(a) & (b);

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

14 C.F.R. 91.9(b)(2);

14 C.F.R. 91.103;

14 C.F.R. 91.109;

14 C.F.R. 91.119;

14 C.F.R. 91.121;

14 C.F.R. 91.151(a);

14 C.F.R. 91.203(a) & (b);

14 C.F.R. 91.405(a);

14 C.F.R. 91.407(a)(1);

14 C.F.R. 91.409(a)(2);

14 C.F.R. 91.417(a) & (b).

4. Statutory Authority for Exemptions

The Federal Aviation Act expressly grants the FAA authority to issue 

exemptions. This statutory authority includes civil aircraft as the term is 
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defined under §40101 of the Act, including sUASs, from the requirement that 

all civil aircraft must have a current airworthiness certificate.

The Administrator may grant an exemption from a requirement of a regulation 

prescribed under subsection (a) or (b) of this section or any sections 44702-

44716 of this title if the Administrator finds the exemption in the public

interest. 49 USC §44701(f). See also 49 USC §44711(a); 49 USC §44704; 

14 CFR §91.203(a)(1).

Section 333(b) of the Reform Act assists the Secretary in determining 

whether sUAS may operate in the National Airspace System (NAS) without 

creating a hazard to the user, the public, or pose a threat to national security. 

In making this determination the Secretary must consider:

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

• Whether the sUAS operates within visual line of sight of the operator;

• Operation of the sUAS in close proximity to airports and populated 

areas.

Lastly, 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.” Id. 

§333(c).

5. Secondary Documentation (Proprietary)

The following secondary documentation is provided for reference as 

supplemental information pertaining to this Petition:

1. ASC-sUAS Flight Standards 

2. ASC-Preflight Inspection & Operations Check List

3. ASC-RVJET Manual 

These documents will be retained at the ground control point accessible by 

the pilot in command (PIC).

6. Unmanned Aircraft Systems

Aerial Sciences Corporation designs and purpose builds its sUAS for mission 

specific applications utilizing commercially available airframes, flight 

controllers, electronics, and components. The proposed aircraft within this 

exemption request is a fixed wing ASC-RVJET that weighs less than 55 

pounds in weight including payload, and operates at a speed of no more than

54 knots. It is equipped with GPS Flight Controller and data link 

communications capability for operator control via ground control station or 

hand radio transmitter controllers and has battery-limited flight duration of less 

than two hours. The GPS Flight Controller can be programmed to limit flight 
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duration, and limits for flight distance and above ground level (AGL) altitude, 

and has return-to-home, loiter, and predetermined landing location functions 

in the event of lost data link communications or flight anomalies. Operating 

within visual line of sight (VLOS) of the PIC and visual observer (VO) at no 

more than 500 feet AGL and will operate only within the areas described 

herein. Such operations will ensure that the sUAS will not create a hazard to 

users of the NAS or the public as described in the FMRA §333(b). 

Aerial Sciences proposes within this petition the use of the ASC-RVJET fixed 

wing aircraft to support varied mission, payload configurations, and training 

purposes -- see the provided supplemental Manual. General specifications 

are as follows: 

• ASC-RVJET Aircraft: 

Airframe: EPO Foam and Carbon Fiber

Wing Span: 1.95 Meter

Weight: 10 pounds (maximum with payload)

Propulsion: Single - 900KV Electric Motor 

Propellers: Carbon Fiber 12” – 13” 

Power: (3S) 11.1 Volt or (4S) 14.8 Volt Lithium-Polymer batteries

Max Speed: 54 knots

Flight Time: 2 Hours

Autopilot: GPS Flight Controller/Autopilot

Data Link: FCC approved 433 MHz or 2.4 GHz

Video: FCC approved 1.3 GHz or 5.8 GHz 

Telemetry: Voltage, Current, Altitude, GPS Lat/Long, Ground Speed

Aerial Sciences maintains a maintenance log book for its sUAS that 

documents maintenance history. In addition to PIC pre-flight inspections 

conducted before each flight our FAA licensed A&P personnel conduct annual

aircraft inspection and maintenance checks. This includes review of system 

and telemetry data files logged from prior flights, inspection for loose or worn 

components, balancing of props, cleaning of motors, battery voltage and cell 

balancing checks, etc., and performing any needed system repair and 

upgrades to include software/firmware for the GPS, Flight Controller/Autopilot, 

Radio Transmitter, and Ground Control Station. All scheduled or 

unscheduled maintenance and repair actions are documented within the 

sUAS maintenance log book. Upon completion of any repair, modification or 

upgrade, the aircraft is test flown by a qualified PIC and documented within 

the maintenance log book prior to return to service. 

7. Operation of the Unmanned Aircraft

The PIC will be an FAA licensed airman with at least a private pilot’s 

certificate and third class medical. Additionally, the PIC will have a minimum 
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of 10 hours sUAS fixed wing experience of which at least 5 hours are with the 

specific make/model sUAS to be operated per the Aerial Sciences sUAS 

Flight Standards document. 

Training of PICs who do not meet the sUAS experience will be gained within 

dedicated training sessions through use of a fixed wing computer simulator

(ground training) and the sUAS platform(s) (logged flight time) as requested 

through this exemption. Upon meeting the sUAS flight hour requirements, 

logged in a consistent manner per 14 CFR §61.5(b), a flight proficiency check 

will be conducted by a Aerial Sciences FAA rated CFI prior to allowing a PIC 

to conduct flight operations. Flight currency will be maintained by the PIC 

having logged 30 minutes flight time within the proceeding 90 days with the 

specific make/model UAS platform. Regaining currency will be achieved in 

dedicated training/currency sessions. In addition to flight proficiency, the PIC 

will be trained in use of the radio control transmitter, ground control station, 

pre-flight inspection of the sUAS, and operational procedures per Aerial 

Sciences sUAS Flight Standards document paraphrased as follows.

Minimum crew for each flight operation will consist of the sUAS PIC and 

Visual Observer (VO). Flights will be conducted within VLOS of the PIC at all 

times with VO duties assisting PIC in maintaining VLOS and situational 

awareness of obstructions, hazards and avoiding other aircraft. 

Communication between the PIC and VO will be maintained through direct 

voice communications and/or through use of two-way radio or cell phone 

throughout the duration of flight.

Prior to each flight the PIC will conduct a thorough pre-flight inspection, per 

the Aerial Sciences Preflight and Operations Checklist, to ensure the sUAS is 

in safe condition for flight. The pre-flight will include physical inspection of 

components, battery voltage level checks, motor run-up, payload system, 

ground control station and communications checks in preparation of flight. If 

the inspection reveals a condition that prohibits safe operation, the PIC will 

remove the aircraft from service until the necessary maintenance has been 

performed and documented and the sUAS is found to be in a condition for 

safe flight.

The PIC will conduct pre-flight planning to include obtaining weather briefings, 

identifying hazards and obstructions, and establishing predetermined mission 

flight path and limited and controlled area for safe operation. The Petitioner

will submit to the Air Traffic Organization (ATO) a Certificate of Waiver or 

Authorization (COA) prior to conducting any flight operations. The Petitioner

will request a Notice to Airman (NOTAM) not more than 72 hours in advance, 

but not less than 48 hours prior to the operation.

All flight operations will be conducted within a limited area that is strictly 

controlled over private or controlled-access property with permission from the 
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land owner or their authorized representative for each flight to be conducted. 

The PIC will conduct pre-flight safety briefings with all personnel supporting 

flight activities in regard to the planned sUAS operations and mission plan 

prior to each flight. Flight operations will typically be conducted at least 500 

feet from all nonparticipating flight operation people, vessels, vehicles, and 

structures unless there are barriers or structures that safely protects 

nonparticipating persons in event of accident. In the event nonparticipating 

persons leave such protection and are within 500 feet of the sUAS, the PIC 

will immediately cease flight operations. Additionally, if owner of vessels, 

vehicles, or structures provides permission and the PIC determines safe 

operations can be conducted with undue risk to operating personnel then 

flight operations may be conducted closer than 500 feet. 

Aerial Sciences will not conduct flight operations over congested or densely 

populated areas, or within 5 miles of an airport unless a letter of agreement is 

obtained from the airport management and per NOTAM. All flights will be 

conducted under visual meteorological conditions (VMC) during daylight 

hours, at less than 87 knots airspeed and an altitude no greater than 500 feet 

AGL, and will not be operated less than 500 feet below or less than 2,000 feet 

horizontally from a cloud or when visibility is less than 3 statute miles from the 

PIC. Maximum flight time for each operational flight will be 120 minutes and 

allowing for no less than 20% battery as indicated by real-time telemetry 

voltage/current data relayed by the aircraft sensors to the PIC control station.

In event the PIC losses data link communications, the GPS equipped sUAS 

have the capability to return to a pre-determined location and loiter and 

provides the PIC capability to abort flight and return-to-home functions. If an 

in-flight emergency occurs, the PIC will immediately abort flight and initiate 

landing procedures. 

By adhering to these operational procedures, Aerial Sciences, will achieve a 

safety level equivalent to, or greater than that, directed by the rules in which 

they seek exemption. sUAS are inherently safer in all facets due to the fact 

they are much smaller, fly at much slower speeds, have no human operators 

or occupants on board and no flammable fuels to be concerned of in event of 

crash. As sUAS processes are further refined, and commercial flight 

experience gained, the operations will serve to enhance an already higher 

level of safety compared to manned flight operations in which serves the 

public’s best interest in the FAA’s pursuit to integrate UAS into the NAS.

Due to the small size of the sUAS involved, ability of the PIC to control and 

set flight parameters, and the controlled and limited environment in which 

they will operate, the Petitioner falls squarely within that zone of safety (an 

equivalent level of safety) in which Congress envisioned that the FAA must, 

by exemption, allow commercial operations of sUAS to commence 

immediately. Additionally, due to the Private Pilot rating of the PIC, the size 
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of the sUAS, limited payload capacity and flight durations, the use of batteries 

versus flammable fuels, and the limited and tightly controlled areas in which 

the sUAS will operate, approval of the application presents no national 

security issue.

Given the clear direction in FRMA §333, the authority contained in the 

Federal Aviation Act, as amended, the strong equivalent level of safety 

surrounding the proposed operations, and the significant public benefit, 

including enhanced safety, reduction in environmental impacts due to battery 

operation, and reduced costs of sUAS aircraft assets as compared to 

conventional aircraft, the grant of the requested exemptions is in the public 

interest. Accordingly, Aerial Sciences respectfully requests that the FAA 

grant the requested exemption without delay.

8. Description of Specific Regulations 

Pursuant to 14 C.F.R. § 11.81(e), Aerial Sciences seeks exemption from the 

below mentioned regulations and provides reason as to why the exemption 

should be approved based on the level of safety at least equal to that of which 

the rules require.

• 14 C.F.R. Part 21 Subpart H – Airworthiness Certificates

Ø Establishes: The procedural requirements for the issuance of 

airworthiness certificates as required by 14 C.F.R. § 

91.203(a)(1)

Given the small size of the sUAS, the controlled operating areas, 

limitations and conditions Aerial Sciences will adhere to during flight 

operations, 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” with consideration “of the size, weight, speed, 

operational capability, and proximity to airports and populated areas of 

the particular UAS.”

• 14 C.F.R. § 45.23(b) – Aircraft Marking and Identification 

Requirements

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

When marks include only the Roman capital letter "N" and the 

registration number is displayed on limited, restricted or lightsport 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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The sUAS to be flown by Aerial Sciences has no airworthiness 

certificate, an exemption may be needed as the sUAS have no 

entrance to the cabin, cockpit, or pilot station on which the word 

“Experimental” can be placed. The FAA has issued the following 

exemptions to this regulation to Exemptions Nos. 10700, 8738, 10167 

and 10167A.

• 14 C.F.R. § 61.113(a) and (b): Private Pilot Privileges and 

Limitations: Pilot in Command

Ø Sections 61.113 (a) and (b) limit private pilots to noncommercial 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 the PIC operating the aircraft to have a private 

pilot’s license rather than a commercial pilot’s license to operate a 

sUAS. Unlike a conventional manned aircraft, a sUAS is remotely 

controlled by a ground-based operator. The operational area is 

controlled and restricted, and all flights are planned and coordinated in 

advance. The level of safety exceeds that provided by a single 

individual holding a commercial pilot’s certificate operating a 

conventional aircraft. The risks associated with the use of a sUAS are 

so diminished from the level of risk associated with commercial 

operations contemplated by Part 61 allowing sUAS use by a private 

pilot as the PIC exceeds the present level of safety sought by 14 

C.F.R. §61.113 (a) and (b). 

• 14 C.F.R. 91.7(a) – Civil Aircraft Airworthiness

Ø No person may operate a civil aircraft unless it is in an airworthy 

condition.

There is no airworthiness certificate for the sUAS to be operated by 

Aerial Sciences. To provide an equivalent level of safety, the PIC will 

conduct pre-flight inspections to ensure airworthiness. During flight, 

the PIC will adhere to § 91.7(b) and abort air operations immediately 

upon identification of an in-flight anomaly or emergency. Licensed A&P 

staff will conduct annual inspections. Maintenance log books will be 

maintained for each sUAS thereby achieving an equivalent level of 

safety.

• 14 C.F.R. § 91.9 (b) (2): Civil Aircraft Flight Manual in the Aircraft. 

Ø Section 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, 
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and placards, or any combination thereof.

The sUAS, given their size and configuration have no ability or place to 

carry such a flight manual on the aircraft, not only because there is no 

pilot on board, but because there is no room or capacity to carry such 

an item on the aircraft platform. The equivalent level of safety will be

maintained by keeping the sUAS documentation at the ground control 

point where the PIC will have 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 – Pre-flight Action

Ø Each pilot in command shall, before beginning a flight, become 

familiar with all available information concerning that flight. This 

information must include- (paragraphs a, b, 1 and 2)

The PIC will take all actions, to include flight and mission planning, 

reviewing weather, flight battery requirements, safe take-off and 

landing areas, and aircraft performance data before commencement of 

flight. In addition, the PIC will verify the sUAS is ready for flight by 

conducting a pre-flight inspection and run up of systems and data-link

communications checks prior to each flight.

The exemption requested for this section is specifically addressed 

toward the requirements which do not apply to sUAS operations such 

as runways and air traffic control integration. The airport manager will 

be notified and approval obtained prior to any operations being 

executed less than five statute miles of an operating airport.

14 C.F.R. §91.109: Flight instruction

Ø Section 91.109 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.

sUAS and remotely piloted aircraft, by their design do not have fully 

functional dual controls. Flight control is accomplished through the use 

of a radio transmitter or ground control station that communicates with 

the aircraft via a receiver in the sUAS. 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 numbers 5778K & 9862A. The equivalent level of safety 

provided by the fact that neither a pilot nor passengers will be 

occupants in the aircraft and by the small size and slow speed of the 

sUAS.
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• 14 C.F.R. 91.119 – Minimum Safe Altitudes

Ø 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 sparsely populated areas. In those 

cases, the aircraft may not be operated closer than 500 feet to 

any person, vessel, vehicle, or structure.

Section 91.119 establishes safe altitudes for operation of civil aircraft. 

Section 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. This exemption is for a sUAS and the exemption requests 

authority to operate at altitudes up to 500 AGL underneath navigable 

airspace and in class E and G airspace maintaining safe separation 

from manned aircraft, an exemption may be needed to allow such 

operations.

The equivalent level of safety will be achieved given the size, weight, 

speed of the sUAS as well as the limited and controlled location 

where it is operated. Compared to flight operations with manned 

aircraft weighing far more than the maximum 55 pounds proposed 

herein, and the lack of flammable fuel, any risk associated with these 

operations is far less than those presently presented with 

conventional manned aircraft. In addition, the low-altitude operations 

of the sUAS will ensure separation between it and operations of 

conventional manned aircraft that must comply with Section 91.119.

• 14 C.F.R. §91.121 Altimeter Settings

Ø 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 do not have an adjustable barometric altimeter an 

exemption is required. An equivalent level of safety will be achieved 

by the PIC, confirming the altitude of the launch site via the sUAS

GPS.

• 14 C.F.R. 91.151(a) – Fuel Requirements for Flight in VFR 

Conditions

Ø 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;
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This regulation is written based on the capabilities of a traditional 

aircraft which have flight times of several hours or greater; therefore, 

with the majority of sUAS which have flight times of only two hours or 

less, this regulation would effectively deny the ability of the air vehicle 

to operate.

To meet the intent, Aerial Sciences, will limit its sUAS flights to 120

minutes, or no less than 20% remaining battery power, which ever 

occurs first, to ensure safe landing and retrieval of the air vehicle and 

providing at least an equal level of safety. Similar exemptions have 

been granted to other operations, including Exemptions 2689F, 5745, 

10673, and 10808.

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

and Registration

Ø 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 55 lbs. 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 PIC 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 

numbers 9565, 9665, 9789, 9789A, 9797, 9797A, 9816A, and 10700.

• 14 C.F.R. 91.405(a), 91.407(a)(1), 91.409(a)(2) and 91.417(a) & (b) –

Maintenance Inspections

Ø 91.405(a) States: 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.

Ø 91.407(a)(1) States: (a) No person may operate any aircraft 

that has undergone maintenance, preventive maintenance, 
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rebuilding, or alteration unless—(1) It has been approved for 

return to service by a person authorized under § 43.7 of this 

chapter.

Ø 91.409(a)(2) States: (a) Except as provided in paragraph (c) of 

this section, no person may operate an aircraft unless, within 

the preceding 12 calendar months, it has had—(2) An 

inspection for the issuance of an airworthiness certificate in 

accordance with part 21 of this chapter. No inspection 

performed under paragraph (b) of this section may be 

substituted for any inspection required by this paragraph unless 

it is performed by a person authorized to perform annual 

inspections and is entered as an ‘‘annual’’ inspection in the 

required maintenance records.

Ø 91.417(a) & (b) States: (a) Except for work performed in 

accordance with §§ 91.411 and 91.413, each registered owner 

or operator shall keep the following records for the periods 

specified in paragraph (b) of this section: (paragraphs 1 (i – iii), 

2 (i – vi)); (b) The owner or operator shall retain the following 

records for the periods prescribed: (paragraphs 1 – 3)

Pre-flight inspections and routine maintenance will be accomplished by 

the PIC to ensure the sUAS is in good working order prior to flight. If 

mechanical issues or emergency situations arise the sUAS can land 

immediately and given its small size poses very little risk to persons or 

property. Upon completion of any repair, modification or upgrade, the 

aircraft is test flown by a qualified PIC and documented within the 

maintenance log book prior to return to service. Annual inspections

and maintenance will be conducted and documented within the sUAS 

maintenance log book by licensed A&P personnel to meet the intent of 

these regulations and provide an equivalent level of safety.

9. Summary the FAA may publish in the Federal Register

Aerial Sciences seeks an exemption from the following Regulations: 14 

C.F.R. Part 21; 14 C.F.R. 45.23(b); 14 C.F.R. 61.113(a)&(b); 91.7(a); 91.9(b) 

(2); 91.103; 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) to commercially operate its small 

unmanned aircraft systems to support a variety of industry and business 

applications, to include, but not limited to, Aerial Survey/Inspection and 

Imaging, Agricultural, Forestry, Wildlife Preservation, Law Enforcement, and 

Search and Rescue, and Training. Granting Aerial Sciences request for 

exemption will reduce current risk levels and thereby enhance safety.

Further, Aerial Sciences sUAS operates at lower altitudes, up to 500 feet 

AGL, in predetermined and controlled airspace, weighing less than 55 pounds 
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and traveling at speeds less than 87 knots. They will provide at least an 

equivalent level of safety as that achieved under current FARs.

Aerial Sciences Corporation respectfully requests that the FAA grant its 

exemption request without delay. The FAA has the authority to issue the 

exemption sought by Aerial Sciences pursuant to the Federal Aviation Act, 85 

P.L. 726 (1958), as amended (the "Act").

By__________________________ for: Aerial Sciences Corporation

David M. Garrett 5901 E. Lippizan Way

Hereford, AZ 85615

Tel: 520.227.1865

david.garrett@msn.com