10/28/2015 08:38 2092397886 

October 27, 2015 

U.S. Dept. of Transportation, Docket Operations 

West Building Ground Floor, Room w12-140 

BOYCE_RESDURCE ' 

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1200 New Jersey Avenue, SE., 

Washington, DC 20590 VIA FAX (20?> 493-225J & U.S. MAIL· 

PAGE 01/07 

MtP Operating Company 

1670 Honoaplilani Hwy 

Wailuku, HI 96793 

albertboyce@gmail.com 

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 Moderni%ation and Reform Act of 2012 (the "Reform Act") and 14 C.F.R. 

Part 11, MTP Operating Company, LLC, seeks an exemption from Federal Aviation F{egulations ("FARs") 

detailed below for the following described Unmanned Aerial System called in this application the ME System, 

which includes an Unmanned Aircraft {UA) and ground station-based equipment and crew: 

THE UNMANNED AIRCRAFT (UA): 

• A lightweight {3.3 kg gross weight with all on-board equipment), battery operated 6-motor rotorcraft in 

the form of a quadcopter that takes off and lands vertically, manufactured by DJI, Model S900, that 

·Includes the following equipment in flight; 

• An on~ board flight computer with GF'S 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 photos 

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 2.4GH:z: on-board radio transmitter that transmits live video from the on-board camera plus all the 

flight data from the telemetry system described above; 

iHE GROUND STATION -BASED PART OF THE SYSTEM: 

• 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; · 

• A radio receiver 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; 

• A VIsual Observer (VO) Is a person who provides a second pair_of eyes to visually track the UA while in 

flight. 

The requested exemption would support an application for a commercial Certificate of Authorization to use the 

above described ME System to support the rapid delivery of treshly-ha!Vested specialty fruits and vegetables 

from land owned by applicant, to a kitchen owned by applicant, never operating over persons not directly 

involved with the ME 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 reduce 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 no risk to national security . 

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The UA is a safer, more environmentally friendly method to deliver produce from hilly fields and terrain that do 

not benefit from paved or gravel roads. 

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

require assistance, including fire fighters, the pollee, the sheriff, et at, while remaining subject to all limitations 

cited in this application as we do so. 

The ME 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 weight exceeding 5.5 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 wiH 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 ME System will not be operated over densely populated areas; 

h) The ME System will not be operated at air shows: 

i) The ME System will not be operated over any open-air assembly of people; 

J) The ME System will not be operated over heavily trafficked roads; 

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

I) Operations will be restricted to day only arid 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 Pre-Flight Inspection by the PIC before each operation to 

ascertain 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 initial 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 6900.227, and under all of the Restrictions (a) through 

(n) listed above, 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: 

*' MTP Operating Company, LLC 

Attn: Albert Boyce 

Ph: (209) 479M2896 

Email: afbertboyce@gmail.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 pur proposed equivalent level of 

safety for each regulation: 

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~ 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~dum 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 1 Page 4 

We 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 additiona_llnformation or clarification. We look fOI'Vtlard to working 

with your office. 

Sincerely, 

Albert Boyce - Manager 

MTP Operating company. LLC 

Addendum containing Exemption Requests an~ Equivalent Level of Safety 

Appendix A - Flight Manual 

Appendix B - owner's Manual for UA 

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ADDENDUM 

EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY 

MTP Operating Company, LlC, requests an exemption from the following regulations as well as any additional 

regulations that may technically apply to the operation of the ME System: 

14 CFR Part 21, Subpart H: 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 ME System 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 destgn 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, 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 airvvorthiness ~ertificate in general, citing the 

equivalent level of safety outlined in the previous paragraph. 

14 C;FR 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." 

At a maximum gross weight of 3.3 kg., the UA 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 d6cuments deemed appropriate for this aircraft by the FAA will be co~looated 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 "EXPERIMENTALH to satisfy the 

requirement of 14 CFR 4S.23, which follows immediately after the proposed placard description below: 

EXPERIMENTAL Manufacturer: 

OJ! Innovations, Inc. 

950 E Baseline Ave. Ste. 210 

Apache Junction AZ 85119 

Model: 8900 

lff'ound please contact: (808) 244~7643 

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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 UA does not have an entrance In which the 

word "EXPERIMENTAL" oan be placed, and may not have a registration number assigned to it by the FAA. 

We propos~ 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 314 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 1hat 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 ddcumenlation, 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 (Appendix A) must be available to tlie crew at the ground station anytime .the 

aircraft is in, or preparing for, flight. 

14 CFR 61.113 Private pilot privileges and limitations:mand 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 it (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 either 

1, Hold a Commercial Pilot Certificate issued by the FAA, and have logged 25 hours of flight experience in this 

type of UA, or 

2. Meet the requirements of 8900.227 para 16(c)(2}{c) "Operations without a pilot certificate" in which the PIC is 

required to complete "FAA private pilot ground instruction" and pass "the FAA Private Pilot written examination." 

Since there are currently 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 minimum, FAA commercial pilot ground instruction and pass 

the FAA Commercial Pilot written examination in addition 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 ''No person may operate a civil aircraft that is being used for flight instruction unless 

that aircraft has fully functioning dual controls." The ME System ground-based control station consists of a small 

hand-held radio transmitter and while tt 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..{)n" 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. 

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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 maximum 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 

aircraft will not be operated over congested areas or over any open air assembly of persons. The property 

owner will be briefed on the expected route of flight and the associated risks to persons and property on the 

ground. The aircraft wUI 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 takeoff 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 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 reseiVe as a safety 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% 

reserve. Since the aircraft will never fly more than % NM from the point of intended landing, a full battery charge 

at launch will ensure that we meet the rese!Ve energy requirement of tl'lis 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- 91A17) ·Maintenance, Preventive Maintenance, Alterations 

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

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." 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 Paragraph 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 obse!Ver. The UA maximum gross weight is 6.5 pounds, it is 

constructed 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 UAwfll retum autonomously 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 medical requirements 

for the PIC and VO be vision corrected to 20120 and a valid, state issued drivers 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. 

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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 knots and no further than 314 NM from the PIC; 

c) All operations must utilize a visual o'bserver (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 accu~ulated and logged, in a· manner consistent w_ith 14 CFR § 61.51 (b), a minimum of 

100 flight cycles and 25 hours of total time as a UA rotorcratt 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 ME System will not be operated over densely populated areas; 

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

i) The ME System will not be operated over any open-air assembly of people; 

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

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

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

m) PIC will confirm that no people are below or near the direct flight path t!' and from destination. 

n) The PIC will brief the VO and property owner about the operation and risk before the first flight at each new 

location; 

o) No flight may be made withOut a successful 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 firmly. 

3: Micro-so card has been inserted if necessary. 

4. Gimbal is functioning as normal. 

5. Motors can start and are functioning as normal. 

6. OJI Pilot app connected to the aircraft. 

TO REGAIN CONTROL AFTER LOST RAOIO CONTACT 

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

will bring the UAV back to the PIC. 

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