Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 1 of 12

U.S. Department of Transportation

Docket Management System

1200 New Jersey Ave., SE 

Washington, DC 20590

Date: February 19, 2015

SUBJECT: Exemption Request Under Section 333 of the FAA Reform Act and Part 11 

of the Federal Aviation Regulations

Dear Sir or Madam:

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

and 14 C.F.R. Part 11, Robison Engineering Company, Inc., seeks an exemption from Federal 

Aviation Regulations (“FARs”) detailed below for the eBee RTK Unmanned Aircraft System 

(UAS) manufactured by SenseFly SA of Switzerland.

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

Authorization to use the system in UAS aerial mapping of mine sites in Nevada and California. 

The eBee RTK system consists of a lightweight (1.6 lbs.) battery operated aircraft, a PC-based 

ground control station, and associated communications equipment. The aircraft carries an 

onboard geo-referenced still camera that allows it to conduct precision photogrammetry at the 

resolution necessary for highly accurate topographic mapping. This high-resolution data can be 

used for determining disturbance areas during the mine permitting and reclamation processes. 

This data can also improve efficiency in mining efforts for more accurately tracking movement of 

ore in pits and stockpiles. The use of an airborne survey vehicle also prevents personnel from 

entering dangerous areas of a mine operation. By approving these exemptions, the FAA will 

create benefits to both public agencies and private mine operators which are ultimately in the 

public interest.

The aircraft will be operated in the field with both a Pilot in Command (PIC) and a ground-based 

Visual Observer (VO) in accordance with FAA Policy N 8900.227 Section 14 "Operational 

Requirements for UAS" with the following additional restrictions:

 All operations will occur in Class G airspace at no more than 400 ft. above ground level

(AGL).

 Operations will occur over private property with the permission of the land owner.

 All required permits will be obtained from state and local government prior to operation.

 The aircraft will not be operated over urban or populated areas.

 The aircraft will not be operated at air shows or over an open-air assembly of people.

 The aircraft will not be operated directly over heavily trafficked roads.

 The aircraft will not be operated within 5 nautical miles (NM) of an airport or heliport1

 Operations will be limited to daytime and visual meteorological conditions (VFR flight 

rules).

 

1

10 of the 12 intended mine sites are beyond 5 NM of Class E non-tower controlled airports. Please see Appendix C 

for further information on the remaining two sites.

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 2 of 12

 Aircraft will remain within Visual Line of Sight (VLOS) at no greater than 1/2 NM from the 

PIC at all times.

 While the aircraft is airborne, the VO will be positioned within voice and/or radio distance 

from the PIC.

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 from the 

manufacturer. Due to the simplicity of the system, we do not anticipate the need for a 

supplemental pilot.

While performing UAS mapping operations on active mine sites, the PIC and VO will be under 

the jurisdiction of the Mine Safety and Health Administration (MSHA). Any personnel working on 

an active mine site must obtain an initial 24 hours of safety training and an 8 hour annual 

refresher course. The operator of the UAS must also sign an MSHA Form 5000-23 which states 

the PIC has been trained appropriately before operating equipment on a mine site. While MSHA 

regulations do not apply to the National Airspace System (NAS), we feel these added safety 

regulations further enhance our awareness and intent to operate a UAS with the utmost care, 

attention, and responsibility. Furthermore, the use of a UAS will help eliminate the need for 

personnel to enter hazardous and dangerous mining areas to measure and collect topographic 

data. A UAS can help prevent injury and the loss of life while working on active mine sites.

We submit that the combination of the aircraft's light weight, historically demonstrated flight 

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

8900.227, the FAA can have confidence that the operation will have an equivalent or greater 

level of safety to manned aircraft performing the same mission.

The name and contact information of the applicant are: 

Robison Engineering Company, Inc.

Attn: Michael Detwiler, LSI

Geomatics Professional

Phone: 775-852-2251 ext: 714

Fax: 775-852-9736

Email: michael@robisoneng.com

Or

Nathan Earl Robison, PE

President, Principal Engineer

Phone 775-852-2251 ext: 700

Fax: 775-852-9736

Email: nathan@robisoneng.com

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 3 of 12

The regulations from which the exemption is requested are as follows:

 14 CFR Part 21

 14 CFR 91.203

 14 CFR 45.23, 45.29

 14 CFR 91.9

 14 CFR 61.113, 61.133

 14 CFR 91.109, 91.119

 14 CFR 91.121, 91.151

 14 CFR Subpart E (91.401 - 91.417)

 FAA Policy 8900.227 Paragraph 16(c)(4) and Paragraph 16(e)(1)

We are prepared to modify or amend any part of this request to satisfy the need for an 

equivalent level of safety. We look forward to working with your office. Please contact us at any 

time if you require additional information or clarification.

Sincerely,

Nathan Earl Robison

President

Appendices:

A. Exemption Request and Equivalent Level of Safety

B. Public Interest

C. Supporting Information from Manufacturer’s Section 333 Application

D. Mine Location Information

E. Map of Intended UAS Operating Locations (Mines)

F. Maintenance Procedures

G. User Manual

H. Manufacturer Airworthiness Justification

I. Training Documentation

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154

2/19/2015 
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 4 of 12

APPENDIX A - EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY

Robison Engineering Company requests an exemption from the following regulations as well as 

any additional regulations that may technically apply to the operation of the SenseFly eBee 

RTK:

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 UAS, we request an experimental 

certificate be issued for the SenseFly eBee RTK under either or both of the following provisions:

21.191 Experimental certificates.

Experimental certificates are issued for the following purposes:

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

new aircraft installations, new aircraft operating techniques, or new uses for aircraft.

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

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

issuance of type and supplemental type certificates, flights to substantiate major design 

changes, and flights to show compliance with the function and reliability requirements of the 

regulations.

Since the experimental certificate can be used for commercial purposes such as market 

surveys, sales demonstrations, and customer crew training, we would expect that an 

experimental certificate would permit our commercial purpose as well.

The aircraft will not carry persons or property, will not carry fuel, and will only fly under strict 

operational requirements. Combined with the fact that the aircraft weighs only 1.6 pounds and 

is constructed primarily out of foam, we propose that the eBee RTK 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 requirements for an airworthiness 

certificate in general, citing the equivalent level of safety outlined in the previous paragraph.

We would also like to site the proposal made in the Notice of Proposed Rule Making on 

February 15, 2015 (Appendix 5 – Alternative 2) that the FAA allows all UAS under 55 pounds 

exempt from an airworthiness certificate. 

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". At 1.6 lbs., the eBee RTK is too small to 

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 5 of 12

carry documentation, does not have an entrance, and is not capable of carrying passengers or 

crew.

To obtain an equivalent level of safety and meet the intent of 91.203, we propose that 

documents deemed appropriate for this aircraft by the FAA will be co-located with the crew at 

the ground control station and available for inspection upon request. In order to identify the 

aircraft, we propose that the information found on airworthiness and registration certificates be 

permanently affixed to the aircraft via placard: 

EXPERIMENTAL

Manufacturer: SenseFly SA 

Model: eBee RTK

Serial Number: ER-01-23715

FAA Registration: N846RE

Registered to:

Robison Engineering Company, Inc.

846 Victorian Ave. Suite 20

Sparks, NV. 89431

If found please contact: (775)-852-2251.

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 1.6 lb. eBee RTK does not have an entrance in which the word "EXPERIMENTAL" can be 

placed, and may not have a registration number assigned to it by the FAA.

We propose to achieve an equivalent level of safety by including the word "EXPERIMENTAL" 

on the top of the aircraft, 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, the permanent placard 

discussed in the previous paragraph will provide the aircraft's registration information should it 

be found on the ground. Finally, we will display at the ground control station a high contrast flag 

or banner that contains the words "Unmanned Aircraft Ground Station" in letters 12 inches high. 

Since the aircraft will operate within VSOL of the ground station, the banner should be visible to 

anyone that observes the aircraft and chooses to investigate its point of origin.

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

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

manual is in the aircraft. 

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 6 of 12

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 too small to carry documentation.

To obtain an equivalent level of safety and meet the intent of 91.9, we propose that a current, 

approved Airplane Flight Manual (Appendix G) be available to the crew at the ground control 

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

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

Commercial pilot privileges and limitations.

The regulation provides that no person may serve as a required pilot flight crewmember of a 

civil aircraft of the United States, unless that person:

(1) Has a pilot certificate or special purpose pilot authorization issued under this part in 

that person's physical possession or readily accessible in the aircraft when exercising the 

privileges of that pilot certificate or authorization. However, when the aircraft is operated 

within a foreign country, a pilot license issued by that country may be used.

The regulation provides also that no person that holds a private pilot certificate may act as pilot 

in command of an aircraft for compensation or hire. Subparagraph (b) allows a private pilot to 

act as pilot in command of an aircraft in connection with any business or employment if:

(1) The flight is only incidental to that business or employment;

(2) The aircraft does not carry passengers or property for compensation or hire.

Robison Engineering Company requests the FAA to consider manufacturer training highlighted 

and detailed in Appendix I, as sufficient training for staff members intended to act as PIC of the 

eBee RTK. Siting the Notice of Proposed Rulemaking issued on February 15, 2015 (Appendix 5 

– Alternative 3) and the proposed rules for a micro UAS class for aircraft less than 4.4 pounds, 

The eBee RTK weighing only 1.6 pounds would fall in this category. We feel at this time the 

training we have received is sufficient to safely and responsibly operate in the NAS.

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 eBee ground control station is based on a small hand-held computer and includes a manual 

joystick-style override set of controls. With the PIC and VO having both real-time computer 

control and the option of "hands-on" the controls during flight, we feel that this technique meets 

the intent 91.109 and provides an equivalent level of safety.

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 7 of 12

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 aircraft will be operating at a maximum of 400 feet AGL, we cannot comply with this 

requirement.

To provide an equivalent level of safety we will only fly over private property with the permission 

of the land owner or mine operator. The land owner and mine operations department will be 

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

ground. We maintain that due to the small size of the eBee RTK, the hazard to persons, 

vessels, vehicles, and structures is not comparable to manned aircraft and this physical limit to 

risk should be considered in granting the exemption.

The aircraft will not be operated over congested areas nor over any open air assembly of 

persons. The aircraft will be operated at an altitude allowing, if a power unit fails, an emergency 

landing without undue hazard to persons or property on the surface.

14 CFR 91.121 Altimeter 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 aircraft will fly below 400 feet AGL and will not need to maintain hemispherical cruising 

altitudes in order to de-conflict with other aircraft. As such, an appropriate altimeter 

measurement presented to the pilot should be Above Ground Level and should be based on the 

barometric pressure at the point of launch. To provide an equivalent level of safety, the UAS's 

AGL altimeter will be set to zero on the ground prior to every flight. Since the aircraft will fly no 

more than 50 minutes, even rapid changes in barometric pressure will have limited effect on the 

safety of the flight. 

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, Visual Flight 

Rules (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 presume the intention of this paragraph is to provide a reserve of energy as a safety buffer 

for go-arounds and other delays to landing.

The eBee RTK is battery operated and the maximum duration of flight from a single battery 

charge is 50 minutes. The eBee RTK has a thoroughly tested safety system that calculates 

remaining battery time and distance from ground control station and based on those 

parameters, calculates the duration needed to return to the ground control station with enough 

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 8 of 12

battery time to land safely. Since the aircraft will never fly more than 1/2 NM from the point of 

intended landing, a full battery charge at launch will ensure that we meet the reserve energy 

requirement of this paragraph. We request an exemption to the word "fuel" and ask for an 

equivalent interpretation with the word "energy".

14 CFR Subpart E (91.401 - 91.417) - 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. 

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 attached Maintenance Procedures (appendix D), the PIC will ensure that the 

aircraft is in an airworthy condition prior to flight and conduct detailed inspections after every 10 

hours. Maintenance performed by the PIC is limited to repairing small damage, typically 

scraping of Styrofoam during landing, replacing a propeller, and updating software and 

firmware. All other maintenance will be performed by the manufacturer. 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 the PIC must have a valid FAA third-class medical certificate issued 

under part 67 in order to perform as a pilot. 

The eBee RTK aircraft weighs 1.6 lbs., is constructed out of foam composite materials, and is 

unmanned. Requiring the crew 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 be:

1) vision corrected to 20/20

2) a valid state issued driver's license

3) current first aid/CPR training.

Due to the size and weight of the aircraft, the greatest hazard of our proposed operation will be 

driving to the launch site on active mine sites. A licensed driver is medically qualified to operate 

a much larger vehicle. The 20/20 vision requirement will ensure that the PIC and VO can see 

and avoid air traffic. Given the unlikely event that both the PIC and VO become medically 

incapacitated while the aircraft is in flight, the eBee RTK will recover autonomously to the 

landing location designated prior to launch without crew intervention. 

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 9 of 12

It is furthermore our intention to hire and train military veterans that have experience operating 

or otherwise familiar with electric UAS. Some of these veterans are disabled. Despite such

disability, a military veteran will bring invaluable operational experience ultimately making our

operations safer. This request is in the public interest as it opens aviation related jobs to a 

section of the public that would not otherwise be medically qualified.

Using the approved Section 333 exemption submitted by Advanced Aviation Solutions, LLC. as 

a set of guidelines, Robison Engineering Company proposes to adhere to the conditions and 

limitations outlined in the Grant of Exemption under Docket No. FAA-2014-0508 as listed below:

1. Operations authorized by this grant of exemption are limited to the following aircraft 

described in the operating documents which is a fixed-wing aircraft weighing 

approximately 1.6 pounds: senseFly eBee RTK (eBee RTK). Proposed operations of 

any other aircraft will require a new petition or a petition to amend this grant.

2. The UAS may not be flown at an indicated airspeed exceeding 70 knots

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

(AGL), as indicated by the procedures specified in the operating documents. All 

altitudes reported to ATC must be in feet AGL.

4. The UAS 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.

5. All operations must utilize a visual observer (VO). 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 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 functions prescribed in the operating 

documents.

6. The operating documents and this grant of exemption must be maintained 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, 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 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 

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.

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 10 of 12

7. Prior to each flight the PIC must inspect the UAS to ensure it is in a condition for safe 

flight. 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. The Ground Control 

Station must be included in the preflight inspection. All maintenance and alterations 

must be properly documented in the aircraft records.

8. Any UAS 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. The PIC who conducts the functional test flight must make an entry in the 

aircraft records.

9. The pre-flight inspection section in the operating documents must account for all 

discrepancies, i.e. inoperable components, items, or equipment, not already covered in 

the relevant sections of the operating documents. 

10. The operator must follow the UAS aircraft/component, maintenance, overhaul, 

replacement, inspection, and life limit requirements.

11. The operator must carry out its maintenance, inspections, and record keeping 

requirements, in accordance with the operating documents. Maintenance, inspection, 

and alterations must be noted in the aircraft records, including total flight hours, 

description of work accomplished, and the signature of the PIC returning the UAS to 

service.

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

and Safety Bulletins.

13. The PIC must make an entry in the aircraft record of the corrective action taken against 

discrepancies discovered between inspections.

14. The Pilot in Command (PIC) must meet the following medical requirements:

a. vision corrected to 20/20

b. a valid state issued driver's license

c. current first aid/CPR training.

15. The operator may not permit any PIC to operate unless that PIC has demonstrated 

through the operator’s training that the PIC is able 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. A record of training must be documented and 

made available upon request by the Administrator. Flights for the purposes of training 

the operator’s PICs and VOs (training, proficiency, and experience-building), are 

permitted under the terms of this exemption. However, said training operations may only 

be conducted during dedicated training sessions.

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 11 of 12

16. 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.

17. The FAA stipulated Advanced Aviation Solutions will conduct operations in Class G 

airspace. Robison Engineering Company proposes to conduct operations in Class G

airspace.

18. The UAS may not operate within 5 nautical miles of the airport reference point as 

denoted on a current FAA-published aeronautical chart.

19. The UAS 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.

20. If the UAS loses communications or loses its GPS signal, it must return to a predetermined location within the planned operating area and land or be recovered in 

accordance with the operating documents. 

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

accordance with the operating documents.

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

weather conditions) there is enough power to fly at normal cruising speed to the 

intended landing point and land the UAV with 30% battery power remaining.

23. The operator must obtain an Air Traffic Organization (ATO) issued Certificate of Waiver 

or Authorization (COA) prior to conducting any operations under this grant of exemption. 

This COA will also require the operator to request a Notice to Airman (NOTAM) not more 

than 72 hours in advance, but not less than 48 hours prior to the operation.

24. 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 (NNumber) markings in accordance with 14 CFR part 45, Subpart C. Markings must be as 

large as practicable.

25. Before conducting operations, the radio frequency spectrum used for operation and 

control of the UA must comply with the Federal Communications Commission (FCC) or 

other appropriate government oversight agency requirements.

26. The 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.

27. The UAS must remain clear and yield the right of way to all other manned aviation 

operations and activities at all times.

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154
Robison Engineering Company, Inc

846 Victorian Avenue, Suite 20, Sparks, NV 89431

775-852-2251 office, 775-852-9736 fax

www.robisoneng.com

Page 12 of 12

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

29. The UAS may not be operated over congested or densely populated areas.

30. 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 UAS, 

flight operations must cease immediately and/or;

b) the aircraft is operated near vessels, vehicles or structures where the land 

owner/controller has granted permission 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, and 

c) Operations nearer to the PIC, VO, operator trainees or essential persons do not 

present an undue hazard to those persons per § 91.119(a).

31. All operations shall be conducted over private or controlled-access property with 

permission from the land owner/controller or authorized representative. Permission from 

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

conducted.

32. 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.

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.

DocuSign Envelope ID: 77141E8D-E5F1-42CA-8916-9A314457A154