1

December 7, 2015

U.S. Department of Transportation

Docket Management System

1200 New Jersey Ave., SE

Washington, D.C. 20590

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 and 14 CFR Part 11,

Michael Riney Company hereby applies for an exemption from the listed Federal Aviation

Regulations (FARs) to conduct commercial operation of designated Unmanned Aircraft Systems

(referred to as UAS), provided such operations are conducted within and under the conditions

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

Commercial operations of a Michael Riney Company UAS, which are equipped with camera(s)

and sensors, would provide professional services in the following areas:

1. Aerial photography and/or video for public and/or pri vate use including real estate,

architecture, land surveying, engineering and other related professional activities.

2. Aerial video and/or photography for public and/or private use including television, public

events, landscape cinematography and network news imaging.

3. Aerial inspection/photography of residential/commercial structures under contract with the

owners or local government authority.

4. Aerial inspection/photography of residential/commercial utility infrastructure including but not

limited to electrical power lines, wind turbines and cell towers.

5. Aerial video/photography or providing live video feed to assist with search and rescue

operations in cases of an emergency or natural disaster only when the local authorities or

governmen t has requested it by contract or donation.

6. Training to persons individually or belonging to both private and/or public organizations to

increase awareness and improve safety for current and future UAS operations within the

National Airspace System (NAS ).

As described below, the requested exemption would permit the operation of a designated UAS

as set forth in this document under controlled conditions in the NAS that would be compliant

with all local, state, and federal regulations. Appro val of this exemption would further the

positive public image of UAS operations in a safe and responsible manner and further the

seamless integration of these aircraft types into the National Airspace System. Additionally,

because of the electric propulsio n systems and their reduced impact on the environment (both

in economic terms and ecological disruptions), a reasonable level of benefit to the public good

would also be provided as Michael Riney Company would be able to operate on a significantly2

minim ized infrastructure while providing the same level of safety and service currently

performed by conventional aerial p hotography and filming aircraft.

The name and address of the applicant is:

Michael Edward Riney

M i chael Riney Company

1515 Virginia Ave,

Palm Harbor, Florida 34683

Phone: 727

- 643

- 1185

Email: mriney@tampabay.rr.com

Regulations from which the exemption is requested:

14 CFR Part 21 subpart H

14 CFR 45.23 (b)

14 CFR 61.113 (a) & (b)

14 CFR 91.7 (a)

14 CFR 91.9 (b) (2)

14 CFR 91.103

14 CFR 91.109

14 CFR 91.119 (c)

14 CFR 91.121

14 CFR 91.151 (a)

14 CFR 91.203 (a) & (b)

14 CFR 91.405 (a)

14 CFR 91.407 (a) (1)

14 CFR 91.409 (a) (2)

14 CFR 91.417 (a) & (b)

It is the request the Michael Riney Company that it will operate two of the following model type

of UAS:

DJI Phantom 3 Professional (please refer to the following complete specifications )

UAS DJI Phantom 3 Professional Specifications:

Type Quad rotor, fixed gear and propellers

Weight (Including Ba ttery And Propellers) 1280 g

Diagonal Size (Including Propellers) 590 mm

Max Ascent Speed 5 m/s

Max Descent Speed 3 m/s

Hover Accuracy

• Vertical: +/

- 0.1 m (when Vision Positioning is active) or +/

- 0.5 m

• Horizontal: +/

- 1.5 m

Max Speed 35 miles per hour, or 16 m/s (ATTI mode, no wind)

Max Altitude Above Sea Level 6000 m3

Operating Temperature 0°C to 40°C

GPS Mode GPS/GLONASS

Camera Sensor Sony EXMOR 1/2.3 ” Effective pixels: 12.4 M (total

pixels: 12.76 M)

Lens FOV 94° 20 mm (35 m m format equivalent) f/2.8,

focus at ∞

Iso Range 100

- 3200 (video) 100

- 1600 (photo)

Shutter Speed 8s

- 1/8000s

Image Max Size 4000 x 3000

Still Photography Modes

• Single Shot

• Burst Shooting: 3/5/7 shots

• Auto Exposure Bracketing (AEB): 3/5

• Bracketed Fr ames at 0.7EV Bias

• Time

- lapse

Video Recording Modes

Phantom 3 Professional

• UHD: 4096x2160p 24/25, 3840x2160p 24/25/30

• FHD: 1920x1080p 24/25/30/48/50/60

• HD: 1280x720p 24/25/30/48/50/60

Supported SD Card Types Micro SD

Max capacity 64 GB. Class 10 or UHS

- 1 rating required

Max Bitrate o f Video Storage 60 Mbps

Supported File Formats

• FAT32/exFAT

• Photo: JPEG, DNG

• Video: MP4, MOV (MPEG

- 4 AVC/H.264)

Operating Temperature 0°C to 40°C

Gimbal Controllable Range Pitch

- 90° to +30°

Stabilization 3

- axis (pitch, roll, yaw)

Vision Positioning (VPS) Max Velocity Less than 8 m/s (when 2 m above

ground)

Altitude Range 30 cm

- 300 cm

Operating Range 30 cm

- 300 cm

Operating Environment Surface with clear pattern and adequate lighting

(Lux > 15)4

DJI Phantom 3 Remote Controller Specifications:

Operating Frequency 2.400 GHz

- 2.483 GHz

Max Distance 2000m (outdoors and unobstructed)

Video Output Port USB

Operating Temperature 0°C

- 40°C

Battery 6000 mAh LiPo 2S

Mobile Device Holder For tablet or phone

Receiver Sensitivity (1%Per)

- 101 dBm ±2 dBm

Transmitter Power (Eirp)

• FCC: 20 dBm

• CE: 16 dBm

Working Voltage 1.2 A @7.4 V

Battery Charger Specifications:

Battery Charger Voltage 17.4 V

Rated Power 100 Watts

Intelligent Flight Battery Ca pacity 4480 mAh

Voltage 15.2 V

Battery Type LiPo 4S

Energy 68 Wh

Net Weight 365 g (per battery)

Max Flight Time Approximately 23 minutes

Operating Temperature

- 10°C to 40°C

Max Charging Power 100 W

Mobile Viewing Device Specifications:

App / Live View Mobile App

DJI Pilot Eirp 100 Mw

Live View Working Frequency 2.4GHz ISM

Live View Quality 720P @ 30fps (depending on conditions and

mobile device)

Latency 220ms (depending on conditions and mobile

device)5

Required Operating Systems iOS 8.0 o r later, Android 4.1.2 or later

Recommended Devices

• iOS: iPhone 5s, iPhone 6, iPhone 6 Plus, iPad Air, iPad Air Wi

- Fi + Cellular, iPad mini 2,

iPad mini 2 Wi

- Fi + Cellular, iPad Air 2 , iPad Air 2 Wi

- Fi + Cellular, iPad mini 3, and iPad

mini 3 Wi

- Fi + Cellular. This app is optimized for iPhone 5s, iPhone 6, and iPhone 6 Plus

• Android: Samsung S5, Note 3, Sony Xperia Z3, Google Nexus 7 II, Google Nexus 9, Mi

3, Nubia Z7 mini

Operations and Regulatory Compliance Specificati ons

The UAS will be operated in full compliance with all manufacturer guidelines, but not to exceed

any limitations or restrictions as defined by approved operating documents or Federal Aviation

Regulations.

The mobile viewing device used with the controll er shall be of a type that is

specifically recommended for use by the manufacturer (currently an Samsung Note 3 running

the latest Android software and DJI Pilot application program).

Software and/or firmware updates will also be completed as required to ensure optimal

operation of the system.

Due to the small size of Michael Riney Company UAS aircraft and the restricted environment

within which they will operate, Michael Riney Company UAS operations will remain well within

the Reform Act ’ s safety requirements. Secondly, due to the small size of the UAS platform and

the predetermined areas in which it will operate, approval of this application presents no

national security issues.

Based upon the elevated level of safet y surrounding the proposed operations, the significant

public benefit of these enhanced safety procedures, and the reduction in environmental impacts

(reduced emissions and noise), the grant of the requested exemption is believed to be in the

public intere st.

Accordingly, Michael Riney Company respectfully requests that the FAA grant the requested

333 exemption.

The applicant proposes that the exemption requested apply to UAS that have the characteristics

and that operate with the limitations listed. The se limitations provide for at least an equivalent or

higher level of safety to operations under the current regulatory structure because the proposed

operations represent a safety enhancement to the existing aerial photography and aerial filming

for movie and television filming operations conducted with conventional aircraft.

These limitations and conditions to which Michael Riney Company agrees to be bound

when conducting commercial operations under an FAA issued 333 exemption include,

but are not limit ed to :

1. Operations authorized by this grant of exemption will be limited to the DJI Phantom 3 series

and a ramp weight of less than 55 pounds, including payload. Proposed operations of any other

UAS type at Michael Riney Company will require a new pet ition or an amendment to this

exemption.6

2. The UAS will not be operated at a speed exceeding 87 knots (100 miles per hour). The pilot

may use either groundspeed or calibrated airspeed (as presented via telemetry data on the

mobile viewing device) to deter mine compliance with the 87 knot speed restriction. In no case

will the Phantom 3 be operated at airspeeds greater than the maximum operating airspeed

recommended by the aircraft manufacturer.

3. The UAS must be operated at an altitude of no more than 400 feet above ground level (AGL).

Altitude must be reported in feet AGL (as presented via telemetry data on the mobile viewing

device).

4. The UA will be operated within visual line of sight (VLO S) of the PIC at all times.

5. All operations will utilize a visual observer (VO). The UAS will be operated within visual line of

sight (VLOS) of the PIC and VO at all times. The VO may be used to satisfy the VLOS

requirement as long as the PIC always maintains VLOS capability. The VO and PIC must be

able to communicate verbally at all times. The PIC must ensure that the VO is qualified to

perform the duties required of the VO.

6. This exemption and the operating documents needed to operate this UAS must be accessible

during all operations, and if a discrepancy exists between the conditions and limitations in this

exemption and the procedures outlined in the operating documents, the conditions and

limitations herein will take precedence.

7. I f the approved UAS has undergone maintenance or alterations that affect the UAS operation

or flight characteristics, e.g., replacement of a flight component, it must undergo a functional test

flight prior to conducting further operations under this exempti on. Functional test flights may only

be conducted by a PIC with a VO and must remain at least 500 feet from other people or

structures. The test flight must be conducted in such a manner so as to not pose a hazard to

persons and property.

8. The operator w ill be responsible for maintaining and inspecting the UAS to ensure that it is in

an airworthy condition for safe operation.

9. Prior to each flight, the PIC will conduct a pre

- flight inspection and determine the UAS is in a

condition for safe flight. The pre

- flight inspection will be used to determine if any potential

discrepancies, e.g., inoperable components, items, or equipment exists. If the inspection reveals

a condition that affects the safe operation of the UAS, the aircraft is prohibited from opera ting

until the necessary maintenance and/or corrective action has been performed and the UAS is

determined to be in a condition for safe flight.

10. Michael Riney Company will follow the UAS manufacturer ’ s maintenance, overhaul,

replacement, inspection, and life limit requirements for the aircraft and aircraft components.

11. Each UAS operated under this exemption will comply with all manufacturer safety bulletins.

12. The PIC must hold either an airline transport or commercial ce rtificate. The PIC must also

hold a current FAA airman medical certificate or a valid U.S. driver ’ s license. The PIC must also

meet the flight review requirements specified in 14 CFR § 61.56 in an aircraft in which the PIC is

rated on his or her pilot cert ificate.7

13. Michael Riney Company will not permit any PIC to commence operations unless the PIC

demonstrates the ability to safely operate the UAS in a manner consistent with how the UAS will

be operated under this exemption, including evasive and emer gency maneuvers and

maintaining appropriate distances from persons, vessels, vehicles and structures.

14. PIC qualification flight hours and currency will be logged in a manner consistent with

14 CFR § 61.51(b). During training, proficiency, and experience

- building flights, all persons not

essential for flight operations are considered nonparticipants, and the PIC will operate the UAS

with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

15. UAS operations will not be conducted during night as part of this exemption, as defined in

14 CFR § 1.1. All operations will be conducted under visual meteorological conditions (VMC).

16. Michael Riney Company UAS will not operate within 5 nautical miles of an airport

refer ence point (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) or for

airports not denoted with an ARP, the center of the airport symbol as denoted on the current

FAA

- published aeronautical chart, unless a letter of agreement (LOA) with th at airport ’ s management is obtained or otherwise permitted by a COA issued to the exemption holder.

17. The UAS will not operate 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 and VO.

18. If the UAS loses communications or loses its GPS signal, the PIC will initiate a Return to

Home (RTH) to it ’ s known takeoff point. Further, the UAS will utilize the manufacturer ’ s failsafe

flight profile that requires the UAS to initia te a climb to the maximum altitude (400 feet AGL),

then proceed to the pre

- determined home point, and then initiate a vertical descent to landing to

avoid potential obstacles along it ’ s return path.

19. The PIC will immediately abort the flight in the event of unpredicted obstacles or

emergencies.

20. The PIC will not operate the UAS unless (considering wind and forecast weather conditions)

there is enough available power for the UA to conduct the int ended operation and to operate

after that for at least five minutes or with the reserve power recommended by the manufacturer

if greater. Low power warning will be set to 25% (termination of operations and an immediate

return to the takeoff point), and cri tical power will be 10% (automatic auto land sequence is

initiated).

21. All operations shall be conducted in accordance with an ATO (air traffic organization)

- issued

COA (certificate of waiver or authorization). Michael Riney Company will apply for a n ew

COA u pon FAA approval of this 333 exemtion.

22. All UAS operated in accordance with this exemption will be identified by serial number,

registered in accordance with 14 CFR part 47, an d have identification (N

− Number) markings in

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

23. All documents and manuals used to ensure the safe operation and flight of the UAS as well

as any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the PIC at

the Ground Control Station of the UAS any time it is operating. These documents and manuals

will be presented to the Administrator or any law enforcement official upon request.8

24. The UAS will rema in clear and give way to all manned aviation operations and activities at

all times.

25. The UAS will not be operated by the PIC from any moving device or vehicle.

26. All flight operations will be conducted at least 500 feet from all nonparticipating pers ons,

vessels, vehicles, and structures unless:

A. Barriers or structures are present that sufficiently protect nonparticipating persons

from the UA and/or debris in the event of an accident. The operator must ensure that

n onparticipating persons remain under such protection. If a situation arises where

nonparticipating persons leave such protection and are within 500 feet of the UA, flight

operations will cease immediately to ensure the safety of nonpartici pating persons.

B. The owner/controller of any vessels, vehicles or structures has granted permission for

operating closer to those objects and the PIC has made a safety assessment of the risk

of operating closer to those objects and determined that it doe s not present an undue

hazard.

The PIC, VO, operator trainees or essential persons are not considered nonparticipating

persons under this exemption.

27. All operations shall be conducted over private or controlled

- access property with permission

from the p roperty owner/controller or authorized representative. Permission from property

owner/controller or authorized representative will be obtained for each flight to be conducted.

Any incident, accident, or flight operation that transgresses the lateral or ver tical boundaries of

the operational area as defined by the applicable COA must be reported to the FAA's UAS

Integration Office (AFS

− 80) within 24 hours. Accidents must be reported to the National

Transportation Safety Board (NTSB) per instructions containe d on the NTSB Web site:

www.ntsb.gov

.

28. If operations for television filming and production are approved, the following additional

conditions and limitations will apply.

29. Michael Riney Company must have exemption permits for operations for the purp ose of

closed

- set motion picture and television filming.

29. The operator must have a motion picture and television operations manual (MPTOM) as

documented in this grant of exemption.

30. At least 3 days before aerial filming, Michael Riney Company will submit a written Plan of

Activities to the local Flight Standards District Office (FSDO) with jurisdiction over the area of

proposed filming. The 3

- day notification may be waived with the concurrence of the FSDO. The

plan of activities will include at lea st the following:

a. Dates and times for all flights;

b . Name and phone number of the operator for the UAS aerial filming conducted

under this grant of exemption;

c. Name and phone number of the person responsible for the on

- scene operation of9

the UAS;

d. Make, model, and serial or N

− Number of UAS to be used;

e. Name and certificate number of UAS PICs involved in the aerial filming;

f. A statement that the operator has obtained permission from property owners

and/or local officials to conduct the filming production event; the list of those

who gave permission must be made available to the inspector upon request;

g. Signature of exemption holder or representative; and

h. A description of the flight activity, including maps or diagrams of any area, city,

to wn, county, and/or state over which filming will be conducted and the altitudes

essential to accomplish the operation.

31. Flight operations may be conducted closer than 500 feet from participating persons

consenting to be involved and necessary for the fi lming production, as specified in the

exemption holder ’ s MPTOM.

32. Unless otherwise specified in this grant of exemption, the UAS, the UAS PIC, and the UAS

operations will comply with all applicable parts of 14 CFR including, but not limit ed to, parts 45,

47, 61, and 91.

33. The UAS will only operate within a defined boundary area throughout all phases of flight.

Security will be monitored by the operator and designated security personnel.

34. A preflight briefing will be conducted in regar d to the day ’ s planned UAS operations. All

personnel who will be performing duties within the boundaries of the safety perimeter be present

for this briefing. Preflight briefing items will include, but are not limited to:

a. Authorized UAS flight operation s, mission plan of activities, and special provisions

issued by the Flight Standards District Office having jurisdiction over the photo /

filming area.

b. Radio communications (if required for operations permitted within 5 miles of an

airport).

c. Takeoff procedures.

d . Maneuvering of the UAS to be conducted during the event.

e. Approach and landing procedures.

f. Alternate landing zone in the event of emergency or security breach.

g. Weather and special considerations.

h. Emergency procedures.

i . Safety briefing for participating personnel.10

j. Safety procedures of non

- participating persons.

k. Definition of operational boundaries.

l. Regulatory requirements: local, state, or federal.

m.Any additional limitations or procedures unique to the operat ions.



### Regulations from which the exemption is requested:

14 CFR Part 21 subpart H

14 CFR 45.23 (b)

14 CFR 61.113 (a) & (b)

14 CFR 91.7 (a)

14 CFR 91.9 (b) (2)

14 CFR 91.103

14 CFR 91.109

14 CFR 91.119 (c)

14 CFR 91.121

14 CFR 91.151 (a)

14 CFR 91.203 (a) & (b)

14 CFR 91.405 (a)

14 CFR 91.407 (a) (1)

14 CFR 91.409 (a) (2)

14 CFR 91.417 (a) & (b)

4 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. §91.203 (a) (1)

Subpart H, ent itled Airworthiness Certificates, establishes the procedural requirements for the

issuance of airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and

limited operating area associated with the aircraft to be utilized by the Applic ant, an exemption

from Part 21 Subpart H meets the requirements of an equivalent level of safety under Part 11

and Section 333 of the Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section

333 of the Reform Act both authorize the FAA to exe mpt aircraft from the requirement for an

airworthiness certificate, upon consideration of the size, weight, speed, operational capability,

and proximity to airports and populated areas of the particular UAS. In all cases, an analysis of

these criteria demo nstrates that the UAS operated without an airworthiness certificate, in the

restricted environment and under the conditions proposed will be at least as safe, or safer, than

a conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate

without the restrictions and conditions proposed. The UAS to be operated hereunder is less

than 55 lbs. including payload, carries neither a pilot nor passenger, carries no explosive

materials or flammable liquid fuels, and operates exclusivel y within a secured area as set out in

the Manual. Unlike other civil aircraft, operations under this exemption will be tightly controlled

and monitored by both the operator, pursuant to the Manual ’ s requirements, and under the

requirements and in complianc e with local public safety requirements, to provide security for the

area of operation as is now done with conventional filming. The FAA will have advance notice of

all operations. These safety enhancements, which already apply to civil aircraft operated i n connection with motion picture and television production, provide a greater degree of safety to

the public and property owners than conventional operations conducted with airworthiness

certificates issued under 14 C.F.R. Part 21, Subpart H. Lastly, appli cation of these same criteria11

demonstrates that there is no credible threat to national security posed by the UAS, due to its

size, speed of operation, location of operation, lack of explosive materials or flammable liquid

fuels, and inability to carry a s ubstantial external load.

14 C.F.R. § 45.23 (b). Marking of the Aircraft

When marks include only the Roman capital letter "N" and the registration number is displayed

on limited, restricted or light

- sport category aircraft or experimental or provisionally certificated

aircraft, the operator must also display on that aircraft near each entrance to the cabin, cockpit,

or pilot station, in letters not less than 2 inches no r more than 6 inches high, the words "limited,"

"restricted," "light

- sport," "experimental," or "provisional," as applicable.

Even though the UAS will have no airworthiness certificate, an exemption may be needed as

the UAS will have no entrance to the cab in, cockpit or pilot station on which the word

Experimental ” can be placed. Given the size of the sUAV, two

- inch lettering will be impossible.

The word “ Experimental ” will be placed on the fuselage in compliance with §45.29 (f).

The equivalent level of saf ety will be provided by having the sUAV marked on its fuselage as

required by §45.29 (f) where the pilot, observer and others working with the sUAV will see the

identification of the UAS as “ Experimental. ” The FAA has issued the following exemptions to thi s

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

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

Sections 61.113 (a) & (b) limit private pilots to non

- commercial operations. Because the UAS

will not ca rry 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 this small UAS. Unlike a conventional

aircraft that carries the pilot and passengers, the UAS is remotely controlled with no souls on

Page 1! 0 of !14

board. The area of operation is controlled and restricted, and all flights are planned and

coordinated in advance a s set forth in the Manual. The level of safety provided exceeds that

provided by a single individual holding a commercial pilot ’ s certificate operating a conventional

aircraft. The risks associated with the operation of the UAS are so diminished from the l evel of

risk associated with commercial operations contemplated by Part 61 when drafted, that allowing

operations of the UAS as requested with a private pilot as the PIC exceeds the present level of

safety achieved by 14 C.F.R. §61.113 (a) & (b).

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

The regulation requires that no person may operate a civil aircraft unless it is in airworthy

condition. As there will be no airworthiness certificate issued for the aircraft, should this

exemption be granted, no FAA regulatory standard will exist for determining airworthiness.

Given the size of the aircraft and the requirements contained in the Manufacturers Operating

Manual for maintenance and use of safety check lists prior to each fligh t, an equivalent level of

safety will be provided.

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

Section 91.9 (b) (2) provides: No person may operate a U.S.

- registered civil aircraft ...

(2) For which an Airplane or Rotorcraft Flig ht 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, and placards, or any combination thereof.

The UAS, given its size and configuration has 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. The equivalent level of safety will be mainta ined

by keeping the flight manual at the ground control point where the pilot flying the sUAS will have12

immediate access to it. The FAA has issued the following exemptions to this regulation:

Exemption Nos. 8607, 8737, 8738, 9299, 9299A, 9565, 9565B, 10167 , 10167A, 10602, 32827,

and 10700.

14 C.F.R. § 91.103: Preflight Action

This regulation requires each pilot in command to take certain actions before flight to insure the

safety of flight. As FAA approved rotorcraft flight manuals will not be provided for the aircraft an

exemption will be needed. The PIC will take all actions including reviewing current weather

conditions and forecasts, flight time and battery requirements, establishing a clear takeoff and

landing zone, and aircraft performance data before initiating flight.

14 C.F.R. §91.109: Flight instruction

Section 91.103 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. UASs and remotely piloted aircraft, by their design do not have fully functional dual

controls. Flight control is accomplished through the use of a control box that communicates with

the aircraft via radio communications. The FAA has approved exemptions for flight training

without fully functional dual controls for a number of aircraft and for flight instruction in

experimental aircraft. See Exemption Nos.5778K & 9862A. The equivalent level of safety can be

achieved as neither a pilot nor passengers will be carried in the aircraft in addition to the small

size and low speed of the aircraft.

Page 1! 1 of 1! 4

14 C.F.R. §91.119: Minimum Safe Altitudes

Section 91.119 establishes safe altit udes 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. As thi s exemption is for a UAS that is not a helicopter and the exemption requests authority to operate

at altitudes up to 400 AGL, or not more than 200 above an elevated platform from which filming

is planned, an exemption may be needed to allow such operations . As set forth herein, except

for the limited conditions stated in the Manual, the UAS will never operate at higher than 400

AGL. It will however be operated in a restricted area with security perimeter, where buildings

and people will not be exposed to op erations without their pre

- obtained consent.

The equivalent level of safety will be achieved given the size, weight, speed of the UAS as well

as the location where it is operated. No flight will be taken without the permission of the property

owner or loca l officials. Because of the advance notice to the property owner and participants in

the filming activity, all affected individuals will be aware of the planned flight operations.

Compared to flight operations with aircraft or rotorcraft weighing more than the maximum 55lbs.

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

operations is far less than those presently presented with conventional aircraft operating at or

below 500 AGL. In addition, the low

- altitude operat ions of the UAS will ensure separation

between these small

- UAS operations and the operations of conventional aircraft that must

comply with Section 91.119.

14 C.F.R. §91.121 Altimeter Settings

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 UAS may not have a barometric altimeter,

but instead a GPS altitude read out, an exemption may be needed. An equivalent level of safety

will be achieved by the operator, pursuant to the Manual and Safety Check list, by receiving

altitude information via a digitall y encoded telemetric data feed, which downlinks from the13

aircraft to a ground

- based on

- screen display. This altitude information will be generated by

equipment installed on board the aircraft, using GPS triangulation, or digitally encoded

barometric altime ter, or radio altimeter, or any combination thereof. Prior to each flight, a zero

altitude initiation point will be established and confirmed for accuracy by the pilot.

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

Section 91.151 (a ) prohibits an individual from beginning “ 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) D uring the day,

to fly after that for at least 30 minutes; or (2) At night, to fly after that for at least 45 minutes. ”

The battery powering a small UAS provides approximately 23 minutes of powered flight. To

meet the 30 minute reserve requirement in 14 CFR §91.151, UAS flights of this type would not

be possible. Given the limitations on the UAS ’ s proposed flight area and the location of its

proposed operations within a predetermined area, a longer time frame for flight in daylight or

night VFR conditions is reasonable Michael Riney Company believes that an exemption from

14 CFR §91.151(a) falls within the scope of prior exemptions. See Exemption 10673 (allowing

Lockheed Martin Corporation to operate without compliance with FAR 91.151 (a)). Operating

the

small UAS, in a tightly controlled area where only people and property owners or official

representatives who have signed waivers will be allowed, with less than 30 minutes of reserve

fuel, does not engender the type of risks that Section 91.151(a) was int ended to alleviate given

the size and speed of the small UAS. Michael Riney Company believes that an equivalent

Page 1! 2 of !14

level of safety can be achieved by limiting flights to 23 minutes or 25% of battery power,

whichever happens first. This restriction would be more than adequate to return the UAS to its

planned landing zone from anywhere in its limited operating area. Similar exemptions have

been granted to other operations, including Exemptions 2689F, 5745, 106 73, and 10808.

14 C.F.R. §91.203 (a) and (b): Civil Aircraft: Certificates Required

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 appropri ate 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 c ockpit entrance so that it is legible to passengers or crew.

A small UAS 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 a sUAS. An equivalent level of safety will be achieved by keeping these documents at

the ground control point where the pilot flying the sUAS will have immediate access to them, to

the extent they are applicable to the UAS. The FAA has issued nume rous exemptions to this

regulation. A representative sample of other exceptions includes Exemption Nos. 9565, 9665,

9789, 9789A, 9797, 9797A, 9816A, and 10700.

14 C.F.R. §91.405 (a); 407 (a) (1); 409 (a) (2); 417(a) & (b): Maintenance Requirements and

Insp ections

These regulations require that an aircraft operator or owner “ 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..., ” and others shall inspect or maintain the aircraft in compliance with Part 43.

Given that these section and Part 43 apply only to aircraft with an airworthiness certificate,14

these sections will not app ly to a UAS operated by Michael Riney Company . Maintenance will

be accomplished by the operator pursuant to the flight manual and operating handbook. As the

manufacturer does not provide specific maintenance instructions, maintenance will be “ on

condition ” for all aircraft and each aircraft will have a maintenance log. An equivalent level of

safety will be maintained because small UASs are very limited in size and will carry a small

payload and operate only in restricted areas for limited periods of time. If mechanical issues

arise the UAS can land immediately and will be operating from no higher than 400 feet AGL. As

provided in the Manual, the operator will ensure that the UAS is in working order prior to

initiating flight as part of a detailed p reflight, perform required maintenance, and keep a log of

any maintenance performed. Moreover, the operator will be the individual most familiar with the

aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivalent

level of safety. If the operator encounters a maintenance issue which cannot be addressed, the

UAS will be returned to the manufacturer or a qualified repair facility where such repairs or

maintenance can be performed. These repairs will also be noted in t he aircraft maintenance log.

Pursuant to 14 C.F.R. Part 11, the following summary is provided for publication in the Federal

Register, should it be determined that publication is needed:

Applicant ( Michael Riney Company ) seeks an exempt ion from the following rules:

14 C.F.R. §21, subpart H; 14 C.F.R 45.23(b);14 C.F.R. §§ 61.113( a) & (b);91.7 (a); 91.9 (b) (2);

91.103(b);91.109; 91.119; 91.121; 91.151(a);91.203(a) and (b); 91.405 (a); 91.407 (a) (1);

91.409 (a) (2); 91.409 (a) (2) and 91 .417 (a) & (b) to commercially operate a small unmanned

aerial system (55lbs or less) in aerial photography and aerial filming operations.

Approval of exemptions allowing commercial operations of sUASs in the aerial photo and film

industry will enhance saf ety by reducing risk. Conventional film operations, using jet or

piston power aircraft, operate at extremely low altitudes close to the subject being filmed and in

near proximity to people and structures and present the risks associated with vehicles that

weigh in excess of 3000 pounds and carry large amounts of fuel. Such aircraft must fly to and

from the film location. In contrast, a small UAS weighing less than 55 lbs. and powered by

batteries eliminates virtually all of that risk given the reduced mass and lack of combustible fuel

carried on board.

The UAS is carried to the film set or location and not flown.

The small UAS will also carry no passengers or crew and, therefore, will not expose them to the

risks associated with manned aircraft flights.

The operation of a small UAS weighing less than 55 pounds, conducted in the strict conditions

outlined above, will provide an equivalent or increased level of safety supporting the grant of the

exemptions requested herein, inc luding the exemption of the applicant from the requirements of

Part 21 and allowing commercial operations.

These small, unmanned aircraft operate at slow speeds in close proximity to the ground, as well

as in a restricted environment. As a result, a small UAS in commercial operations is far safer

than operations conducted with conventional helicopters or aircraft operating in similarly close

proximity to structures and personnel.15

In the matter of privacy, all flights will occur over private or controlled ac cess property with the

property owner ’ s prior consent and knowledge. Filming will be of people who have also

consented to being filmed or otherwise have agreed to be in the area where filming will take

place.

I wil l ensure that all regulatory requirements are met and/or exceeded in the best interests of

professionalism and safety. Michael Riney Company is committed to this philosophy, and will

gladly provide feedback and additional data to further the development of this emerging

industry.

Please forward any request for additional information or questions to:

Michael Riney 727

- 643

- 1185

mriney@tampabay.rr.com

. Sincerely

,

Michael Riney