January 21, 2016

U.S. Dept. of Transportation, Docket Operations

West Building Ground Floor, Room w12

- 140

1200 New Jersey Avenue, SE.,

Washington, DC 20590

Botos Design & Distribution Inc.

2836 County Road 43

Wadley, Alabama 36276

VIA FEDERAL DOCUMENT MANAGEMENT SYSTEM

Re: Exemption Request under Section 333 of the FAA Reform Act and Part 11 of the Federal

Aviation Regulations

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the "Reform Ac t")

and 14 C.F. R. Part 11, Botos Design & Distribution Inc., seeks an exemption from Federal

Aviation Regulations ("FARs") detailed below for the following described Unmanned Aerial System

called in this application Synergy System, which includes an Unm anned Aircraft (UA) and ground

station

- based equipment and crew:

THE UNMANNED AIRCRAFT (UA):

[~]A lightweight (20 lb gross weight with all on

- board equipment), manufactured by DJI, Inspire

1

- t

- 600, that includes the following equipment in flight;

[¥] An o n

- board flight computer with GPS navigation and location ability that receives signals for

flight controls from a ground

- based transmitter/controller;

[~]An on

- board camera capable of capturing imagery in the form of full color, high definition still

photo s and video;[~ An on

- board telemetry system that delivers flight data from the on

- board flight computer to

the on

- board radio transmitter including altitude AGL, horizontal and vertical speed, compass

direction of flight and direction back to its launch site;

~ A 2.4GHz on

- board radio transmitter that transmits live video from the on

- board camera plus

all the flight data from the telemetry system described above;

THE GROUD STATION

- BASED PART OF THE SYS TEM:

t~] A Pilot in Command (PIC) in operational control of a flight operation from beginning to end

and who controls the UA while in the air;

[~A 2.4GHz radio transmitter/controller operated by the PIC to control the UA while in flight;

["?J A radio recei ver receiving live video and flight data from the on

- board camera and computer

projects it all together onto a screen for the PIC to view during flight;

t?.J A Visual Observer (VO) is a person who provides a second pair of eyes to visually track the

UA whi le in flight.

The requested exemption would support an application for a commercial Certificate of

Authorization to use the above described Synergy System to support Production of promotional

materials (video and/or still images) for Real Estate sales Pro duction of promotional

materials, (video and/or still images) for Travel and Tourism industries production of promotional

materials, (video and/or still images) for commercial businesses, Photography and videography

of social events, while never operating over persons not directly involved with the

Synergy system.

The UA, powered by batteries, is smaller, lighter and more maneuverable than larger aircraft

running on combustible fuel, it operates at lower altitudes with no people on board and will

thereby re duce current risk levels and thereby enhance safety and diminish the likelihood of

death or serious bodily injury. With a small payload and maximum flight time of only 18 minutes,

this is offers little or no risk to national security.

Low level oblique pho tos and video from several angles are far more effective than groundbased

imagery for displaying the characteristics of large, complex properties with several

buildings and large trees. The alternative could be to charter a full

- sized helicopter for thisp urpose, which has proven more costly than many potential clients are able to afford. The

benefits of reduced cost and improved quality of presentation from the UA will be valuable to

and benefit many buyers and sellers of real property and marine property.

Additionally, we request that we be allowed to use our system to benefit first responders nearby

who might require assistance, including fire fighters, the police, the sheriff, et al., while

remaining subject to all limitations cited in this application a s we do so.

The Synergy System will be operated in the field with both a PIC and a VO in accordance with

FAA Policy N 8900.227 Section 14 "Operational Requirements for UAS" and with the following

Restrictions:

a) No flight will be made with a UA Gross wei ght exceeding 55 pounds;

b) All operations must occur in FAA Class G airspace at no more than 400ft AGL, at an

airspeed of no more than 50 knots and no further than 3/4 NM from the PIC;

c) All operations must utilize a visual observer (VO). The VO and PIC must be able to

communicate by voice at all times during a flight operation;

d) Operations will be restricted to flights over property with the permission of the property owner;

e) The PIC must have accumulated and logged, in a manner consistent with 14 CF R § 61.51

(b), a minimum of 100 flight cycles and 25 hours of total time as a UA rotorcraft pilot and at least

ten hours logged as a UA pilot with a similar UA type;

f) All required permits will be obtained from state and local government prior to operatio n;
g) The Synergy System will not be operated over densely populated areas;

h) The Synergy System will not be operated at air shows;

i) The Synergy System will not be operated over any open

- air assembly of people;

j) The Synergy System will not be operated over heavily trafficked roads;

k) The Synergy System will not be operated within 5NM of an airport or heliport;

I) Operations will be restricted to day only and weather conditions equivalent to VFR;

m) The PIC will brief the VO and property owner about th e operation and risk before the first

flight at each new location;

n) No flight may be made without a Pre

- Flight Inspection by the PIC before each operation toascertain that the UA is in a condition safe for flight (see Appendix A).

The PIC and VO will meet the requirements outlined in FAA Policy N 8900.227 Section 16

personnel Qualifications. Additionally, the PIC and VO will perform maintenance on the system

and will complete a course of maintenance instruction as part of their init ial training.

We submit that the combination of the UA's light weight, flight performance and ability, fully

qualified flight crew and strict operation under the guidelines established in 8900.227, and under

all of the Restrictions (a) through (n) listed a bove, the FAA can have full confidence that the

operation will have an equivalent or greater level of safety than manned aircraft performing the

same mission.

The name and contact information of the applicant are:

Matthew Botos, DBA, Botos Design & Distri bution Inc.

2836 County Road 43

Wadley, Alabama 36276
matthew_botos@yahoo.com

The regulations from which the exemption is requested are listed below. Beside each regulation

number is the page of the attached Addendum upon which each may be found together with our

proposed equivalent level of safety for each regulation:

- 14 CFR Part 21 ................................. Addendum Page 1

- 14 CFR 91.203 ................................. Addendum Page 1

- 14 CFR 45.23, 45.29 .......................... Addendum Page 2

- 14 CFR 91.9 .................................... Addendum Page 2

- 14 CFR 61.113, 61.133 ....................... Addendum Page 2

- 14 CFR 91.109, 91.119, 91.121 .............. Addendum Page 3

- 14 CFR 91.151 ................................. Adde ndum Page 3

- 14 CFR Subpart E (91.401

- 91.417) ...... Addendum Page 3

- FAA Policy 8900.227 Paragraph 16(c)(4) and Paragraph 16(e)(1) ... Addendum 1We are prepared to modify or amend any part of this request to satisfy the need for an

equivalent level of safety. Please contact us at any time if you require additional information or

clarification. We look forward to working with your office.

Sincerely,

Matthew Botos, Botos Design & Distribution Inc.

Addendum containing Exemption Request s and Equivalent Level of Safety Appendix A

- Flight

Manual's

Appendix B

- Owner's Manual for UA

ADDENDUM EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY

Matthew Botos, DBA, Botos Design & Distribution Inc. requests an exemption from the following

regul ations as well as any additional regulations that may technically apply to the operation of the

Synergy System:

14 CFR Part 21, Subpart H: Airworthiness Certificates

This part establishes the procedures for the issuance of an airworthiness certificate. Wh ile the

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

request an experimental certificate be issued for the Synergy System under either or both of the

following provisions: 21.191 Experimental certificates.

Experi mental 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 comp liance 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 c hanges, 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 wo uld 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

carbon fiber and 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 91.203(a) & (b) Civil aircraft: Certifications required.

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

to the aircr..aft 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."

At a maximum gross weight of 6.5 pounds, the UA is too small to carry documen tation, 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 t he 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 cont aining the following information plus the word "EXPERIMENTAL" to

satisfy the requirement of 14 CFR 45.23, which follows immediately after the proposed placard

description below:

Appendix A

EXPERIMENTAL

Manufacturer: OJI Innovations, Inc. 950 E Baseline Av e. Ste. 210 Apache Junction AZ 85119

Models: Inspire 1

- t

- 600,

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

These regulations provide that each aircraft must display 11N'' and the aircraft's registrationnumber in letters at least 3 inch es 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 UA 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 th e
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 91.9 Civil aircraft flight manual, marking, and placard requirements.

This regulation provides that no person may operate an aircraft unless a cur rent, 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 aircr aft 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 UA Flight Manual (Appe ndix A) must be available to the crew at the ground station

anytime the aircraft is in, or preparing for, flight.

14 CFR 61.113 Private pilot privileges and limitations: Pilot in Command and 61.133

Commercial pilot privileges and limitations.

The regulatio n 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 emplo yment if: (1) The

flight is only incidental to that business or employment; and (2) The aircraft does not carrypassengers or property for compensation or hire.

Our proposed operations require that the PIC must

Meet the requirements of 8900.227 para 16(c)(2)(c) 110perations without a pilot certificate~~ in

which the PIC is required to complete 11 FAA private pilot ground instruction~~ and pass 11 the FAA

Private Pilot written examination.~~ Since there are curr ently no means available for the pilot of a

UAS to gain the experience in an equivalent category and class in order to apply for a

commercial pilot's license, we propose to generate an equivalent level of safety by requiring our

pilots to complete, at a mi nimum, FAA commercial pilot ground instruction and pass the FAA

Commercial Pilot written examination in addition

Appendix A

to completing the private pilot requirements. 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 91.109 Flight Instruction; Simulated instrument flight and certain flight tests

The regulation states that 11No person may operate a civil aircraft that is being used for flight

instruction unless that aircraft has fully functioning dual controls."

The Synergy 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 st udent 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 s afety.

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 aircraft will be operating at a

maxi mum of 400 feet AGL, we cannot comply with this requirement.

In order to provide an equivalent level of safety we will only fly over private property with a size

of at least two acres with the permission of the owner of the property flown over. The aircraf t will

not be operated over congested areas or over any open air assembly of persons. The propertyowner will be briefed on the expected route of flight and the associated risks to persons and

property on the ground. 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 UA, 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 UA will always fly below 400 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 ta keoff point is transmitted via radio from the UA 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 b egin 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 saf ety buffer for delays to landing. The UA is battery operated and the maximum

duration of flight from a single battery charge is 18 minutes with a 20°/o reserve. Since the

aircraft will never fly more than 314 NM from the point of intended landing, a full b attery 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".

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 "beauthorized to approve the aircraft for return to service." As provided in the Pre

- Flight Checklist in

Appendix A, 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.

8900.227 Paragraph 16(c)(4) PIC Medical. and Para graph 16(e)(1) Observer Medical.

This policy provides that both the PIC and VO must have a valid FAA second

- class medical

certificate issued under part 67 in order to perform as a pilot or observer. The UA maximum

gross weight is 6.5 pounds, it is construc ted of carbon fiber and plastic and the PIC is not on

board. Both the PIC and the VO are required to be in VLOS. Given the unlikely event that both

the PIC and VO become medically incapacitated while the aircraft is in flight, the UA will return

autonomous ly to the site of launching and land without crew intervention.

Therefore, requiring the PIC and VO to meet the same medical requirements as a commercial

pilot carrying passengers in a large aircraft is an unnecessary burden.

We propose that the minimum me dical requirements for the PIC and VO be vision corrected to

20/20 and a valid, state issued driver's license. The 20/20 vision requirement will ensure that the

PIC and VO can see and avoid air traffic; a licensed driver is medically qualified to operate a

much larger vehicle.

APPENDIX A

- FLIGHT MANUAL

FLIGHT RESTRICTIONS

a) No flight will be made with a UA Gross weight exceeding 55 pounds;

b) All operations must occur in FAA Class G airspace at no more than 400' AGL, at an airspeed

of no more than 50 knot s and no further than 3/4 NM from the PIC;

c) All operations must utilize a visual observer (VO). The VO and PIC must be able to

communicate verbally at all times during a flight operation;d) Operations will be restricted to flights over property with the permission of the property owner;

e) The PIC must have accumulated and logged, in a manner consistent with 14 CFR § 61.51

(b), a minimum of 100 flight cycles and 25 hours of total time as a UA rotorcraft pilot and at least

ten hours logged as a UA pilot with a similar UA type;

f) All required permits will be obtained from state and local government prior to operation;

g) The Synergy System will not be operated over densely populated areas;

h) The Synergy System will not be o perated at air shows;

i) The Synergy System will not be operated over any open

- air assembly of people;

j) The Synergy System will not be operated over heavily trafficked roads;

k) The Synergy System will not be operated within 5 NM of an airport or helipor t;
I) Operations will be restricted to day only and weather conditions equivalent to VFR;

m) The PIC will brief the VO and property owner about the operation and risk before the first

flight at each new location;

n) No flight may be made without a successf ul Pre

- Flight Inspection by the PIC before each

operation to ascertain that the UA is in a condition safe for flight.

PREFLIGHT CHECKLIST

1. Remote controller, aircraft battery, and mobile device are fully charged.

2. Propellers are mounted correctly and f irmly.

3. Micro

- SD card has been inserted if necessary.

4. Gimbal is functioning as normal.

5. Motors can start and are functioning as normal.

6. DJI Pilot app connected to the aircraft.

TO REGAIN CONTROL AFTER LOST RADIO CONTACT

If radio contact is lost a nd not restored within 3 seconds, an automatic Return to Home feature