September 3, 2015

Exemption No. 12752

Regulatory Docket No. FAA−2015−2400

Mr. Richard Fournier 

Rhody Air LLC

35 Sachuest Way

Middletown, RI 02842

Dear Mr. Fournier:

This letter is to inform you that we have granted your request for exemption. It transmits our 

decision, explains its basis, and gives you the conditions and limitations of the exemption, 

including the date it ends.

By letter dated June 9, 2015, you petitioned the Federal Aviation Administration (FAA) on 

behalf of Rhody Air LLC (hereinafter petitioner or operator) for an exemption. The petitioner

requested to operate an unmanned aircraft system (UAS) to conduct aerial photography and 

videography.

See Appendix A for the petition submitted to the FAA describing the proposed operations and 

the regulations that the petitioner seeks an exemption.

The FAA has determined that good cause exists for not publishing a summary of the petition 

in the Federal Register because the requested exemption would not set a precedent, and any 

delay in acting on this petition would be detrimental to the petitioner.

Airworthiness Certification

The UAS proposed by the petitioner are the Horizon Blade 350 QX3 and the 3D Robotics

Solo.

The petitioner requested relief from 14 CFR part 21, Certification procedures for products 

and parts, Subpart H—Airworthiness Certificates. In accordance with the statutory criteria 

provided in Section 333 of Public Law 112−95 in reference to 49 U.S.C. § 44704, and in 
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consideration of the size, weight, speed, and limited operating area associated with the

aircraft and its operation, the Secretary of Transportation has determined that this aircraft 

meets the conditions of Section 333. Therefore, the FAA finds that the requested relief from 

14 CFR part 21, Certification procedures for products and parts, Subpart H—Airworthiness 

Certificates, and any associated noise certification and testing requirements of part 36, is 

not necessary.

The Basis for Our Decision

You have requested to use a UAS for aerial data collection1

. The FAA has issued grants of 

exemption in circumstances similar in all material respects to those presented in your petition. 

In Grants of Exemption Nos. 11062 to Astraeus Aerial (see Docket No. FAA−2014−0352), 

11109 to Clayco, Inc. (see Docket No. FAA−2014−0507), 11112 to VDOS Global, LLC (see

Docket No. FAA−2014−0382), and 11213 to Aeryon Labs, Inc. (see Docket No. 

FAA−2014−0642), the FAA found that the enhanced safety achieved using an unmanned 

aircraft (UA) with the specifications described by the petitioner and carrying no passengers or 

crew, rather than a manned aircraft of significantly greater proportions, carrying crew in 

addition to flammable fuel, gives the FAA good cause to find that the UAS operation enabled 

by this exemption is in the public interest.

Having reviewed your reasons for requesting an exemption, I find that—

• They are similar in all material respects to relief previously requested in Grant of 

Exemption Nos. 11062, 11109, 11112, and 11213;

• The reasons stated by the FAA for granting Exemption Nos. 11062, 11109, 11112, and 

11213 also apply to the situation you present; and 

• A grant of exemption is in the public interest.

Our Decision

In consideration of the foregoing, I find that a grant of exemption is in the public interest. 

Therefore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701, 

delegated to me by the Administrator, Rhody Air LLC is granted an exemption from 14 CFR 

§§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 91.7(a), 91.119(c), 91.121, 

91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 91.417(a) and (b), to the 

extent necessary to allow the petitioner to operate a UAS to perform aerial data collection. 

This exemption is subject to the conditions and limitations listed below.

 

1 Aerial data collection includes any remote sensing and measuring by an instrument(s) aboard the UA. 

Examples include imagery (photography, video, infrared, etc.), electronic measurement (precision surveying, RF 

analysis, etc.), chemical measurement (particulate measurement, etc.), or any other gathering of data by 

instruments aboard the UA.
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Conditions and Limitations

In this grant of exemption, Rhody Air LLC is hereafter referred to as the operator.

Failure to comply with any of the conditions and limitations of this grant of exemption will be 

grounds for the immediate suspension or rescission of this exemption.

1. Operations authorized by this grant of exemption are limited to the Horizon Blade 350 

QX3 and 3D Robotics Solo when weighing less than 55 pounds including payload. 

Proposed operations of any other aircraft will require a new petition or a petition to 

amend this exemption.

2. Operations for the purpose of closed-set motion picture and television filming are 

not permitted. 

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The 

exemption holder may use either groundspeed or calibrated airspeed to determine 

compliance with the 87 knot speed restriction. In no case will the UA be operated at 

airspeeds greater than the maximum UA operating airspeed recommended by the 

aircraft manufacturer.

4. The UA must be operated at an altitude of no more than 400 feet above ground level 

(AGL). Altitude must be reported in feet AGL.

5. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. 

This requires the PIC to be able to use human vision unaided by any device other than 

corrective lenses, as specified on the PIC’s FAA-issued airman medical certificate or

U.S. driver’s license.

6. All operations must utilize a visual observer (VO). The UA must be operated within 

the 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; 

electronic messaging or texting is not permitted during flight operations. The PIC 

must be designated before the flight and cannot transfer his or her designation for the 

duration of the flight. The PIC must ensure that the VO can perform the duties 

required of the VO.

7. This exemption and all documents needed to operate the UAS and conduct its 

operations in accordance with the conditions and limitations stated in this grant of 

exemption, are hereinafter referred to as the operating documents. The operating 

documents must be accessible during UAS operations and made available to the 

Administrator upon request. If a discrepancy exists between the conditions and 

limitations in this exemption and the procedures outlined in the operating documents, 
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the conditions and limitations herein take precedence and must be followed. 

Otherwise, the operator must follow the procedures as outlined in its operating 

documents. The operator may update or revise its operating documents. It is the 

operator’s responsibility to track such revisions and present updated and revised 

documents to the Administrator or any law enforcement official upon request. The 

operator must also present updated and revised documents if it petitions for extension 

or amendment to this grant of exemption. If the operator determines that any update 

or revision would affect the basis upon which the FAA granted this exemption, then 

the operator must petition for an amendment to its grant of exemption. The FAA’s 

UAS Integration Office (AFS−80) may be contacted if questions arise regarding 

updates or revisions to the operating documents.

8. Any UAS that has undergone maintenance or alterations that affect the UAS operation 

or flight characteristics, e.g., replacement of a flight critical component, must undergo 

a functional test flight prior to conducting further operations under this exemption. 

Functional test flights may only be conducted by a PIC with a VO and must remain at 

least 500 feet from other people. The functional test flight must be conducted in such 

a manner so as to not pose an undue hazard to persons and property.

9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is 

in a condition for safe operation.

10. Prior to each flight, the PIC must conduct a pre-flight inspection and determine the 

UAS is in a condition for safe flight. The pre-flight inspection must account for all 

potential discrepancies, e.g., inoperable components, items, or equipment. If the 

inspection reveals a condition that affects the safe operation of the UAS, the aircraft is 

prohibited from operating until the necessary maintenance has been performed and the 

UAS is found to be in a condition for safe flight.

11. The operator must follow the UAS manufacturer’s maintenance, overhaul, 

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

aircraft components.

12. Each UAS operated under this exemption must comply with all manufacturer 

safety bulletins.

13. Under this grant of exemption, a PIC must hold either an airline transport, 

commercial, private, recreational, or sport pilot certificate. The PIC must also hold a 

current FAA airman medical certificate or a valid U.S. driver’s license issued by a 

state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal 

government. 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 certificate.
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14. The operator may not permit any PIC to operate 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 emergency maneuvers and 

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

qualification flight hours and currency must be logged in a manner consistent with 

14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs 

(training, proficiency, and experience-building) and determining the PIC’s ability to 

safely operate the UAS in a manner consistent with how the UAS will be operated 

under this exemption are permitted under the terms of this exemption. However, 

training operations may only be conducted during dedicated training sessions. During 

training, proficiency, and experience-building flights, all persons not essential for 

flight operations are considered nonparticipants, and the PIC must operate the UA 

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

15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All 

operations must be conducted under visual meteorological conditions (VMC). Flights 

under special visual flight rules (SVFR) are not authorized.

16. The UA may not operate within 5 nautical miles of an airport reference 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 with that airport’s 

management is obtained or otherwise permitted by a COA issued to the exemption 

holder. The letter of agreement with the airport management must be made available 

to the Administrator or any law enforcement official upon request.

17. The UA may not be operated less than 500 feet below or less than 2,000 feet 

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

18. If the UAS loses communications or loses its GPS signal, the UA must return to a 

pre-determined location within the private or controlled-access property.

19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies.

20. The PIC is prohibited from beginning a flight unless (considering wind and forecast 

weather conditions) there is enough available power for the UA to conduct the 

intended operation and to operate after that for at least five minutes or with the reserve 

power recommended by the manufacturer if greater.

21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All 

operations shall be conducted in accordance with an ATO-issued COA. The 

exemption holder may apply for a new or amended COA if it intends to conduct 

operations that cannot be conducted under the terms of the attached COA.
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22. All aircraft operated in accordance with this exemption must be identified by serial 

number, registered in accordance with 14 CFR part 47, and have identification 

(N−Number) markings in accordance with 14 CFR part 45, Subpart C. Markings must 

be as large as practicable.

23. Documents used by the operator to ensure the safe operation and flight of the UAS and 

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 the aircraft is operating. 

These documents must be made available to the Administrator or any law enforcement 

official upon request.

24. The UA must remain clear and give way to all manned aviation operations and 

activities at all times. 

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

26. All Flight operations must be conducted at least 500 feet from all nonparticipating 

persons, 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 nonparticipating 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 must cease immediately in a manner ensuring the safety 

of nonparticipating persons; and

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 does 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 property owner/controller or authorized representative. 

Permission from property owner/controller or authorized representative will be 

obtained for each flight to be conducted.

28. Any incident, accident, or flight operation that transgresses the lateral or vertical 

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 

contained on the NTSB Web site: www.ntsb.gov.
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If this exemption permits operations for the purpose of closed-set motion picture and 

television filming and production, the following additional conditions and limitations apply.

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, the operator of the UAS affected by this 

exemption must 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 

must include at least 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 of 

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, 

town, 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 filming production, as specified in the 

exemption holder’s MPTOM.

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

operations must comply with all applicable parts of 14 CFR including, but not limited to, 

parts 45, 47, 61, and 91.
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This exemption terminates on September 30, 2017, unless sooner superseded or rescinded.

Sincerely,

/s/

John S. Duncan

Director, Flight Standards Service

Enclosures
Rhody Air LLC 

35 Sachuest Way 

Middletown, Rl 02842 

. ; ' 401.258.6695 

June 9, 2015 

U.S. Department of Transportation, Docket Operations 

West Building Ground Floor, Room W12-140 

1200 New Jersey Avenue, SE 

Washington, DC 20590 

Dear Sir or Madam: 

r.4nier@cox. net 

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform 

Act), Rhody Air, LLC (the operator) and Richard Fournier and Barry Schubert (the 

applicants and co-owners) hereby apply for an exemption from Federal Aviation 

Regulations (FARs) detailed below to allow for commercial operations of a Horizon 

Blade 350 QX3, a four rotor UAS with an attached CG02 Camera and integrated 3-axis 

gimbal, and a 3D Robotics Solo, a four rotor UAS with a custom Solo gimbal holding a 

GoPro Hero 4 camera for the purpose of aerial photography and video for a variety of 

industries. 

As the Reform Act allows the FAA to "establish requirements for the safe operation of 

such aircraft systems in the national airspace system", Rhody Air's use of the Blade 350 

QX3 and the 3D Robotics Solo will provide the following benefits and enhance or 

provide an equivalent level of safety. 

1. The Blade 350 QX3 and the 3DR Solo have a maximum takeoff weight of less 

than 3 pounds and thus offers a lightweight, small and compact video platform 

compared to manned aircraft. 

2. Alex Paiva, a licensed FAA pilot with a Commercial grade pilot certificate will be 

the primary PIC (Pilot in Command) of all of Rhody Air operations. In addition, 

Barry Schubert is a licensed FAA pilot with a Private grade pilot certificate, along 

with John Felisberto, another member of the LLC with a Private grade pilot 

certificate. 

3. Both the Blade 350 QX3 and the 3DR Solo offer significant safety, noise, 

emission, security and environmental benefits not available to larger manned 

aircraft. 
4. Both the Blade 350 QX3 and the 3DR Solo have numerous safety features such 

as Failsafe mode, automatic landing should signal between PIC and UAS be 

interrupted, GPS based altitude and distance locks, Flight Limits function and low 

battery warnings. We feel that these features addressed in more detail below and 

in the Blade 350 QX3 and the 3DR Solo User Manuals provide an equivalent 

level of safety. 

5. Operations utilizing both the Blade 350 QX3 and the 3DR Solo will provide a 

benefit to the general public and serve the public interest by providing the service 

of aerial photographic images and videos to numerous businesses and 

individuals for considerably less than the previously only available option of 

utilizing manned aircraft at an equivalent level of safety. 

The Aircraft, Operations and an Equivalent Level of Safety 

1. The safe operation of the UAS will be the first priority before, during and after every 

operation. 

2. The UAS pilot will be an FAA licensed Commercial grade airman and will be 

considered the PIC whether flying or supervising and will be responsible for the safe 

operation of the UAS at all times. 

3. Both the Blade 350 QX3 and the 3DR Solo have a maximum takeoff weight of 1300 

grams or approximately 2.9 pounds. They both have a diagonal length of 350mm and a 

maximum speed of 15 meters per second. 

4. The UAS's utilize GPS coordinated location sensors and are controlled by a 2.4 GHz 

transmitter. 

5. All UAS operations will be conducted at Visual Line Of Sight (VLOS) at no more 

than 200 feet AGL. 

6. No UAS operations will be conducted within 5 NM of an airport. 

7. No UAS operations shall occur over densely populated areas, large assemblies of 

people, stadiums, government buildings, power lines, or major roads. 

8. All nonparticipating persons shall be a minimum of 500 feet from the UAS. 

9. If a nonparticipating person comes within 500 feet of the UAS, flight operations will 

cease immediately. 

10. All UAS operations shall take place during daylight hours under conditions 

equivalent to Visual Flight Rules (VFR) with the UAS no more than 1/4 NM from the 

PIC. 
11. All UAS operations will have a PIC and a Visual Observer (VO) present and all 

operations will be within line of sight (LOS) of the PIC and VO. 

12. The UAS will yield to all manned aircraft at all times. 

13. All required permits and permissions will be obtained from local and state 

government should they be required. 

14. A pre-flight inspection by the PIC will be performed prior to each flight to assure that 

the UAS is safe for flight. A post-flight inspection will also be performed as an added 

level of safety. An aircraft check will also occur after every two hours of flight. See 

Appendix B for aircraft checklist. 

15. At no time shall the UAS be operated with missing or manufacturer unapproved 

parts, or in any condition that could pose a hazard to any other aircraft or structure or 

person on the ground. 

16. Prior to all UAS operations a pre-flight meeting will be held by the PIC to determine 

the parameters of flight in a given location, any hazards present, weather conditions, 

safety procedures at the specific location and approximate duration and route of 

flight. 

17. The PIC will have accumulated and accurately logged a minimum of 25 hours total 

time as a UAS rotorcraft pilot with a minimum of 10 hours as a UAS pilot with a 

multi-rotor UAS and 5 hours as a UAS pilot operating the same make and model of 

UAS to be used for operations under the exemption. 

18. The Blade 350 QX3 and the 3DR Solo UAS's will utilize GPS location, auto return 

home and will never be operated at below 20% batter capacity. 

Both the Blade 350 QX3 and the 3DR Solo UAS's are small and safe sub 3 pound 

plastic and composite aircraft utilizing four propellers driven by a 2800mAh, 11.1 V, LiPo 

smart battery with an average flight time of 17-18 minutes. 

The remote control/transmitter operates at 2.4 GHz. The aircraft's software can be 

calibrated to limit both AGL and distance from the transmitter. The aircraft will 

automatically return to point of origin or descend in place should signal with the 

transmitter be lost. 

The UAS is unmanned, operates at low altitudes, does not run on combustible fuel, has 

very low decibel level noise emissions and has a small payload capacity and short flight 

time, thus significantly reducing current risk levels involved with utilizing manned aircraft 

for aerial photography. Additionally, past purchasers of aerial photography have had to 

contract with manned aircraft operations at a significant expense. 
Rhody Air's UAS operations will provide a public benefit in allowing more people to 

access aerial photography images and videos at a significantly lower price and in the 

process we will be providing that data at a greater or at least equivalent level of safety 

as compared to similar manned operations. 

It is the applicants belief that the small size of the Blade 350 QX3 and the 3DR Solo 

UAS's, the basic operating parameters outlined above, the specific exemptions 

discussed below, the fully trained, certified and vetted crew and the equivalent level of 

safety provided at a much lower cost to the general public will allow the FAA to grant an 

exemption to Rhody Air LLC for commercial UAS aerial photography operations under 

the Reform Act of 2012. 

The exemption requests follow below as well as Appendix A and Appendix B. The Blade 

350 QX3 and the 3DR Solo User's Manuals are available upon request.. 

Sincerely, 

r.4nier@cox.net 
EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY 

Rhody Air, LLC, requests an exemption from the following regulations as well as any 

additional regulations that may technically apply to the operation of the Blade 350 QX3 and 

he 3DR Solo UASs. 

14 CFR Part21, 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 UAS, we 

request an experimental certificate be issued for the UAS operated by the applicant! 

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 and will only fly under strict operational 

requirements. As the Blade 350 QX3 and the 3DR Solo UAS also carries no combustible 

fuel, weighs less than3 pounds and is constructed primarily of plastics and composites, we 

propose the UAS is at least as safe, if not significantly safer than conventionally certified aircraft 

used within similar parameters. 

If an experimental airworthiness certificate is not appropriate for this application, then we! 

request an exemption of 14 CFR Part21, 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 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." 

As the UAS is too small to carry documentation, does not have an entrance and does 

not carry a crew, we propose the following in order to meet the intent of 91.203 and 

provide an equivalent level of safety. All documents deemed appropriate by the FAA for 

this aircraft will be located at the operational ground station for each flight in proximity to 

the PIC and VO and will be available for inspection on request. In order to identify the 

aircraft, we propose to use the manufacturers model and production codes located on 

the aircraft as well as appropriate registration numbers and the telephone number of the 

manufacturer and Rhody Air LLC affixed to the aircraft as well. Should the FAA deem 

appropriate, we will also affix the word "EXPERIMENTAL" in the largest possible 

lettering given the size of the UAS, as discussed further below. 

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. 

As the UAS does not have an entrance, may not have an FAA assigned registration 

number and is of such small size, we propose to affix the word "EXPERIMENTAL" in the 

largest possible lettering appropriate for the aircraft. Additionally, for each operation the 

ground station will be clearly identified with a banner containing the words "UAS Ground 

Station" that will be of appropriate size to be seen by any observer of the aircraft 

operations. The ground station will also have all registration and identity documents 

relating to the UAS. 

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. The intent of this requirement is to ensure that 

flight manual information is available to the aircrew while operating the aircraft. 

Rhody Air LLC requests an exemption to this requirement as the UAS cannot, given its 

size, carry the flight manual. To meet an equivalent level of safety, we propose to have 

the current manufacturers flight manual and the Rhody Air flight manual at the 

operational ground station of each flight, available to both the PIC and VO. 
14 CFR 91.109 Flight instruction; Simulated instrument flight and certain flight 

tests. 

The regulation provides that "No person may operate a civil aircraft that is being used for 

flight instruction unless that aircraft has fully functioning dual controls." 

The controls for the UAS do not currently have a set of fully functioning dual controls. If 

a UAS pilot is being trained, the pilot performing the training would be directly 

supervising and could take over the controls from the pilot in training if the need arose. 

This would be similar to the technique of a "throw-over type" control wheel in some fixed 

wing aircraft. We feel that this technique meets the intent 91 .1 09 and provides an 

equivalent level of safety. 

14 CFR 91.119 Minimum safe altitudes: General. 

The regulation provides that over sparsely populated areas the aircraft cannot be! 

operated closer than 500 feet to any person, vessel, vehicle, or structure. 

Since the UAS will be operating at a maximum 200 feet AGL, we cannot comply with 

this requirement and thus ask for an exemption. In order to provide an equivalent 

level of safety, we propose the following. 

A. The UAS will only be operated within VLOS of the PIC and VO at a maximum 

range of 1/4 NM from the ground station. 

B. A preflight safety risk assessment will be completed prior to each flight to ensure 

the UAS is in a condition for safe flight and that the planned operation can be 

completed safely. Rhody Air's Flight Manual and Pre-Flight Checklist is included 

as Appendix A and Appendix B. 

C. The UAS will not be operated within 5 NM of any airport. 

D. The UAS will only operate over private property with the approval of the owner of 

that property. 

E. The UAS will not operate over any open air assemblies of people, congested or 

crowded areas, or within 500 feet of any nonparticipating person. 

Overall, we believe that the above restrictions and the UAS's small size, light weight, low 

maximum speeds, and high degree of maneuverability and stability combine to provide 

an equivalent level of safety compared to manned aircraft. 
14 CFR 91.121Aitimeter settings. 

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

altimeter setting available within 100 nautical miles of the aircraft. 

The UAV will always be flying below 200 feet AGL within VLOS of the PIC and VO that 

will provide separation from terrain, structures and other aircraft. Also, the UAS will 

continually transmit an AGL reading back to the controller at the ground station and the 

AGL lock in the UAS's software will be set to 200 feet, providing an equivalent level of 

safety. 

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 that the intention here is to provide a reserve of fuel to remain aloft should a 

landing be delayed or the landing point changed. The UAS is smart battery powered 

and continually transmits battery charge information back to the ground station to be 

evaluated by the PIC who will return the UAS back to the ground station when the 

battery shows 20% remaining capacity. We feel that this combined with the fact that the 

UAS will have a maximum range of 1/4 NM from the ground station provides an 

equivalent level of safety. 

14 CFR Subpart E (91.401 -91.4171- Maintenance, Preventive Maintenance, and 

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. 

We propose that the PIC perform maintenance and inspection and "be authorized to 

approve the aircraft for return to service." As provided for in Appendix A, the PIC will 

inspect the aircraft prior to every flight to ensure it is in airworthy condition. A 

maintenance check will also be performed after every 2 hours of flight. Any general 

maintenance and repair or replacement of components will be completed by the PIC 

following the manufacturers recommendations and documented in accordance with 

91.417. In any case where the UAS cannot be returned to service by the PIC, or is 

suspected to be unsafe, the UAS will not be operated until returned to all manufacturer 

specifications. We feel that due to the simplicity, size, robustness and construction of 

the aircraft. the PIC can assure an equivalent level of safety. 
8900.227 Paragraph 16(cXa) PIG Medical. and Paragraph 16(eX1) Observer 

Medical. 

This policy provides that both the PIC and observer must have a valid FAA second-class 

medical certificate issued under part 67 in order to perform as a pilot or observer. 

We feel that 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. 

However, in our case, the PIC is a commercial grade airman with the appropriate 

medical certificate, so we would ask for a waiver regarding the VO's medical certificate 

only. 

Since the UAV is of small size, unmanned and required to be in VLOS of the PIC and 

VO at all times and given the highly unlikely scenario of both the PIC and VO becoming 

incapacitated simultaneously, the PIC's medical certificate should be sufficient. 

Furthermore, given the aircrafts auto return home feature and low operating altitude, we 

feel that the above provide an equivalent level of safety. We propose that the medical 

requirements for the VO be vision corrected to 20/20 and a valid state issued driver's 

license. 
APPENDIX A 

RHODY AIR'S FLIGHT MANUAL 

FLIGHT PARAMETERS AND RESTRICTIONS 

A. The PIC will be an FAA licensed airman with a Commercial Pilot certificate and 

associated medical certificate or the UAS pilot will be directly supervised by an FAA 

licensed airman with a Commercial Pilot certificate and associated medical certificate. 

B. The PIC will have accumulated and logged a minimum of 25 flight hours as a UAS 

rotorcraft pilot and a minimum of 10 hours logged as a UAS pilot with a multi-rotor UAS 

and 5 hours as a UAS pilot operating the same make and model of UAS to be used for 

operations under the exemption. A current logbook of all training flights and all flight 

operations will be at the ground station during all operations. 

C. All flights will occur in FAA Class G airspace at no more than 200 feet AGL and no further 

than 1/4 NM from the PIC. 

D. All operations will utilize a PIC and VO with the PIC and VO able to communicate verbally 

at all times. 

E. All operations will occur only during daylight hours and in weather conditions equivalent to 

VFR. 

F. All operations will occur at VLOS from the PIC and VO. 

G. The PIC and VO will have a pre-flight meeting at the site of the operation just prior to the 

flight to assess weather, area of operation, topography, flight time, route, hazard 

mitigation and overall operational and safety parameters. Also during this meeting, the 

pre-flight aircraft checklist (see Appendix B) will be implemented. 

H. No flight operations shall occur within 5 NM of an airport, nor shall flight operations occur 

over open assemblies of people, congested roadways, densely populated areas, air 

shows, or other restricted areas. 

I. The UAS will always operate at a minimum of 500 feet from any nonparticipating (nonessential 

flight personnel) persons and UAS operations shall cease should a 

nonparticipant be closer than 500 feet to the UAS. 

J. All operations will be conducted over private property with the full permission of the 

property owner and the property owner will be briefed as to the flight parameters. 

K. Flight planning will include the termination of the flight with 20% battery remaining, as 

determined by the data link between the UAS and ground station. 
L. The UAV will at all times give way to manned aircraft. 

M. Prior to every flight, a highly visible banner with the words "UAS Ground Station" will be 

placed at the site of the ground station to allow an outside observer to determine the 

location of the UAS's origin and command point. 

N. All permits required by state and local governments will be obtained prior to any 

operations. 

0. No flight operations will occur without a successful pre-flight inspection by the PIC before 

each flight to determine that the UAS is in a condition for safe flight. 

P. At the conclusion of each flight a post-flight inspection will be done to assess the 

condition of the UAS. 

Q. A full pre-flight check of the aircraft will be performed after every 2 hours of flight. 

R. Replacement of parts shall only be done according to manufacturer's instructions. 

S. All flight operations will be logged in a flight logbook. 

T. All maintenance done and inspections performed will be lodged in a maintenance log. 

U. Check for software updates weekly and upload to UAS as needed to continually keep the 

UAS software as current as possible. 
APPENDIX 8 

RHODY AIR PRE-FLIGHT AIRCRAFT CHECKLIST 

1. Inspect all propellers for proper tightness and that they are free of cracks, dings, chips 

and excessive wear. 

2. Review Rhody Air's Flight Manual. 

3. Review manufacturer's user manual. 

4. Inspect all wiring and motors. 

5. Inspect the airframe for cracks or damage. 

6. Inspect battery voltage of UAS on-board battery and Remote Controller/Transmitter 

battery to ensure there is sufficient energy in both systems for safe flight. 

7. Recalibrate compass according to manufacturer's instructions. 

8. Always turn on Remote Controller/Transmitter before turning on UAS battery. 

9. Ensure that a link between Transmitter and UAS is established and that GPS link is 

established. 

1 O.Engage throttle, lift aircraft off the ground and verify the aircraft responds properly to all 

inputs and hovers accurately. 

11. Adjust transmitter "trims" if required. 

12. Check wind direction and sun glare. 

13. Verify all UAS LED indicators are correct for both color and solid/flashing.