April 18, 2015

U.S. Department of Transportation

Docket Management System

1200 New Jersey Ave. SE 

Washington, DC 20590

Re: Exemption Request Section 333 of the FAA Reform Act

Dear Sir/Madam:

This petition is being submitted on our own behalf without legal counsel or consulting services. 

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the “Reform Act”), and 

14 C.F.R. Part 11, Aerial West, LLC (“Aerial West”), a California based limited liability company

operating a Small Unmanned Aircraft System (“sUAS”) equipped to conduct aerial photography and 

survey for various industries, hereby applies for an exemption from the Federal Aviation Regulations 

(“FARs”) listed below to allow operation of our sUAS commercially in airspace regulated by the 

Federal Aviation Administration (“FAA”) so long as such operations are conducted with and under

the conditions outlined herein or as may be established by the FAA as required by Section 333.

The requested exemption would permit Aerial West to pursue its commercial interests in providing 

services to consumers’ interested aerial data capture using a small advanced sUAS in the following 

areas:

• Agricultural Surveying

• 3D Mapping

• Aerial video/photography or providing live video feed 

• Closed Set Film Cinematography

• sUAS Operator Training

• Real Estate Photography

• Product Demonstrations

• Research and Development

Aerial West states that all sUAS flights that will occur over private or controlled access property will do 

so with the property owner's prior consent and knowledge and that only people who have consented or

otherwise have agreed to be in the area where photography and videography will take place will be 

captured.

Aerial West understands the proper roles of an observer, communication procedures, proper visual 

scan techniques, operations at non-towered airports, and appropriate sections of the Aeronautical 

Information Manual.
Regulations from which the exemption is requested:

14 C.F.R. Part 21

14 C.F.R. 45.23 (b)

14 C.F.R. 61.113(a) and (b)

14 C.F.R. 91.7 (a)

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

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. 91.205 (b)

14 C.F.R. 91.215

14 C.F.R. (91.401 - 91.417)

Unmanned Aircraft System

sUAS are a feasible method to obtain information of agricultural cropland to determine optimum 

inputs that result in cost savings to farmers, yield security, and reduce environmental impact of 

excess fertilizers and chemicals in the soil.

We are petitioning for exemption to enable Aerial West to operate a DJI Phantom 3 multi-rotor 

equipped with a three-axis gimbaled camera, a DJI Inspire 1 multi-rotor equipped with a three-axis 

gimbaled camera, a DJI S-900 multi-rotor equipped with a three-axis gimbaled camera, and a DJI

S-1000 multi-rotor equipped with a three-axis gimbaled camera. These sUAS all weigh less than 25 

lbs., have a built-in capability to limit the height it flies above the ground, to limit the radius of the 

distance it flies from the operator and to exclude it from Class B, C and D airspace including a no 

fly zone feature. Each system also has the failsafe function of the autopilot system, which means 

when the communication between the Main Controller and the transmitter is lost; the system will 

automatically trigger Return to Home and will land safely.

The above specifications meet standards listed below, some derived in accordance with the Model

Aircraft Operating Standards:

• The petitioner will only operate its sUAS in line of sight of a pilot and/or observer and

will operate at sites that are a “sufficient distance” from populated areas within the sterile 

area described in the operators manual. Such operations will insure that the sUAS will "not 

create a hazard to users of the national airspace system or the public."

• When flying sUAV within 3 miles of an airport, airport operators will be notified and the 

operator will give the right of way to avoid flying in the proximity of full-scale aircraft.

• Maximum flight time for each operational flight will be 60 minutes.

• Flights will be terminated at 25% battery power reserve should that occur prior to the 60 

minute limit.
• The sUAV will be programmed so that it will not be operated at an altitude of no more than

400 feet AGL, and not more than 200 feet above an elevated platform from which filming 

is planned.

• The sUAS operated by the petitioner weighs less than 55 pounds, including the payload

(i.e. camera, lens, and gimbal).

• The sUAS will operate at speeds of no more than 55 knots.

• Given the small size of the sUAS and the restricted sterile environment within which they 

will operate, our sUAS operations adhere to the Reform Act's safety requirements.

Under the requested exemption Aerial West ensures that all operators have completed a small 

unmanned aircraft systems (UAS) education and training program including all applicable 

regulations and guidance documents; including aeronautical background information such as 

charts, NOTAMS and Aircraft Circulars; Radio Communications Procedures; Human Factors and 

Crew Resource Management; Basic Small UAS Aerodynamics; Weather factors; Airmanship and 

Decision-making and Safe Operating Procedures.

We respectfully request exemption under Section 333 to enable Aerial West to operate safe, lowrisk commercial sUAV operations for the activities stated. Aerial West at all times will respect the 

space and privacy of citizens and property whilst keeping our skies safe.

Sincerely,

Bill Palmatary

Owner

Aerial West, LLC

834 15th PL Suite B

Hermosa Beach, Ca 90254

323-539-8828 office

818-429-1174 cell
EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY

Aerial West requests an exemption from the following regulations as well as any 

additional regulations that may technically apply to the operation of the sUAV System:

14 CFR Part 21, Airworthiness Certificates

This part establishes the procedures for the issuance of an airworthiness certificate. While the FAA 

continues to work to develop airworthiness standards for Unmanned Aerial Systems, we request an 

experimental certificate be issued for the DJI Phantom 2 Vision plus, DJI S-900, DJI Inspire, and

RF-70 sUAS under either or both of the following provisions:

21.191 Experimental certificates.

Experimental certificates are issued for the following purposes:

(a) Research and development. Testing new aircraft design concepts, new 

aircraft equipment, new aircraft installations, new aircraft operating techniques, or 

new uses for aircraft.

(b) Showing compliance with regulations. Conducting flight tests and other 

operations to show compliance with the airworthiness regulations including flights to show 

compliance for issuance of type and supplemental type certificates, flights to substantiate 

major design changes, and flights to show compliance with the function and reliability 

requirements of the regulations. Since the experimental certificate can be used for

commercial purposes such as market surveys, sales demonstrations, and customer crew 

training, we would expect that an experimental certificate would permit our commercial 

purpose as well. The aircraft will not carry persons or property, will not carry fuel, and will 

only fly under strict operational requirements. Combined with the UA's light weight, being 

constructed primarily of foam, carbon fiber, and/or plastic, we propose that the UA will be 

at least as safe, if not safer, than a conventionally certificated aircraft performing the same

mission. If an experimental airworthiness certificate is not appropriate for this application, 

then we request an exemption of 14 CFR Part 21, Subpart H, and the requirement for an 

airworthiness certificate in general, citing the equivalent level of safety outlined in the 

previous paragraph.

14 CFR 45.23 Display of marks; general and 45.29 Size of marks.

These regulations provide that each aircraft must display "N" and the aircraft's registration number 

in letters at least 3 inches high. Additionally, the aircraft must display the word "EXPERIMENTAL" 

in letters at least 2 inches high near the entrance to the cabin, cockpit, or pilot station. The sUAV 

does not have an entrance in which the word "EXPERIMENTAL" can be placed, and may not have 

a registration number assigned to it by the FAA. We propose to achieve an equivalent level of 

safety by including the word "EXPERIMENTAL" in the placard on the top of the aircraft, as shown

above, where the PIC, VO and others in the vicinity of the aircraft while it is preparing for launch will 

be able to see the designation. Additionally, we feel that the permanent placard discussed in the 

previous paragraph will provide the aircraft's registration information at the ground station. Finally, 

we will display at the ground station a high contrast flag or banner that contains the words 

"Unmanned Aircraft Ground Station" in letters 3 inches high or greater. Since the aircraft will

operate within 3/4 NM of the ground station, the banner should be visible to anyone that observes

the aircraft and chooses to investigate its point of origin.
14 CFR 61.113 Private pilot privileges and limitations: Pilot in Command and 61.133

Commercial pilot privileges and limitations.

The regulation provides that no person that holds a Private Pilot certificate may act as pilot in 

Command of an aircraft for compensation or hire. Subparagraph (b) allows a private pilot to 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. Our proposed operations require that the PIC must hold at least 

a Private Pilot Certificate issued by the FAA and since the aircraft cannot carry passengers or 

property, we feel we meet the intent of 61.113 Subparagraph (b) even though the intent of this 

application is to conduct a business.

14 CFR 91.7 Prohibits the Operation of an aircraft without an airworthiness certificate. As 

no such certificate will be applicable in the form contemplated by the FARs, this Regulation is 

inapplicable.

14 CFR 91.9 Civil aircraft flight manual, marking, and placard requirements.

This regulation provides that no person may operate an aircraft unless a current, approved flight 

manual is in the aircraft. We assume that the intent of this requirement is to ensure that flight 

manual information is available to the aircrew while operating the aircraft. We request an exemption 

to this requirement since the aircraft is not only too small to carry documentation, the 

documentation would not be available to the crew during flight operations. To obtain an equivalent 

level of safety and meet the intent of 91.9, we propose that a current, approved sUAS Flight 

Manual must be available to the crew at the ground station anytime the aircraft is in, or preparing 

for, flight.

14 CFR 91.109 Flight Instruction; Simulated instrument flight and certain flight tests The 

regulation states that "No person may operate a civil aircraft that is being used for flight instruction 

unless that aircraft has fully functioning dual controls." The sUAS System ground-based control 

station consists of a small hand-held radio transmitter and while it does not offer a second set of

"controls", both the student and instructor can, and will, operate the single set of controls 

simultaneously. With both student and instructor having "hands-on" the controls during flight, we 

feel that this technique meets the intent 91.109 and provides an equivalent level of safety.

14 CFR 91.119 Minimum safe altitudes: General.

The regulation states that over sparsely populated areas the aircraft cannot be operated closer

than 500 feet to any person, vessel, vehicle, or structure. Since the typical mission of the sUAS 

would be photography or survey of persons, vessels, vehicles or structures it would be necessary 

to operate closer than 500 feet to the items listed. Operations will only be flown over property or 

persons where permission has been obtained and careful pre-planned has been performed. The 

aircraft will be operated at a low altitude allowing, if a power unit fails, an emergency landing 

without undue hazard to persons or property on the surface. Therefore we maintain that due to the 

small size of the UAS, the hazard to persons, vehicles and structures is minimal compared to 

manned aircraft, which should be considered in granting the exemption.

14 CFR 91.121 Altimeter settings.

The regulation requires that aircraft shall maintain cruising altitudes by reference to an altimeter

setting available within 100 NM of the aircraft. The sUAS will always fly below 600 feet AGL and will 

not need to maintain cruising altitudes in order to prevent conflict with other aircraft. An Above 

Ground Level altimeter measurement above the takeoff point is transmitted via radio from the sUAS 

on-board computer to the display screen held by the PIC, providing a constantly updated AGL 

readout.

14 CFR 91.151 Fuel requirements for flight in VFR conditions.
The regulation provides that no person may begin a flight in an airplane under day-VFR conditions 

unless there is enough fuel to fly to the first point of intended landing and to fly after that for at

least

30 minutes. We feel the intention of this paragraph is to provide an energy reserve as a safety

buffer for delays to landing. The sUAS are battery operated and the maximum duration of flight

from a single battery charge is 12-45 (depending on which sUAS) minutes with a 20% reserve.

Since the aircraft will never fly more than 1/2 NM from the point of intended landing, a full battery

charge at launch will ensure that we meet the reserve energy requirement of this paragraph. We

request an exemption to the word "fuel" and ask for an equivalent interpretation with the word 

"energy". We

also request exemption from the 30 min reserve and ask that our reserve will be to fly the mission to

the point of intended landing and have at least a 20% battery reserve after that.

14 CFR 91.203(a) & (b) Civil aircraft: Certifications required.

The regulation provides that an airworthiness certificate, with the registration number assigned to 

the aircraft and a registration certificate must be aboard the aircraft. Additionally, subparagraph 

(b) provides that the airworthiness certificate be "displayed at the cabin or cockpit entrance so that

it is legible to passengers or crew." With our largest vehicle, the RF-70, at a maximum gross 

weight of

13 pounds, the sUAS is too small to carry documentation, does not have an entrance, and is not

capable of carrying passengers or crew. To obtain an equivalent level of safety and meet the 

intent of 91.203, we propose that documents deemed appropriate for this aircraft by the FAA will 

be co- located with the crew at the ground control station and available for inspection upon 

request. In order to identify the aircraft, we propose that the information found on airworthiness 

and

registration certificates be permanently affixed to the aircraft via placard containing the 

following information plus the word "EXPERIMENTAL" to satisfy the requirement of 14 CFR

45.23.

14 CFR Subpart E (91.401- 91.417) - Maintenance, Preventive Maintenance, Alterations The 

regulation provides that the operator is primarily responsible for maintaining the aircraft in an 

airworthy condition, including compliance with part 39 and 43. Paragraphs 91.407 and

91.409 require that the aircraft be "approved for return to service by a person authorized under

43.7" after maintenance and inspection. It is our intention that the PIC perform maintenance 

and inspection of the aircraft and "be authorized to approve the aircraft for return to service."

The PIC will ensure that the aircraft is in an airworthy condition prior to every flight and in 

addition, conduct detailed inspections after every two hours of flight. Maintenance performed by

the PIC is limited to repairing small cracks, replacing a propeller, checking electrical connections 

and updating software and firmware for the on-board computer. All other maintenance will be 

performed by the manufacturer or their designated repair facility. The PIC will document work 

performed in accordance with 91.417. We feel that due to the size, construction, and simplicity of 

the aircraft, the PIC can ensure an equivalent level of safety.