May 18, 2015 Flight Ventures Ltd Page: 1

Flight Ventures Ltd

4827 McDonald Drive Cir N

Stillwater, MN 55082

651-351-2929

Robert Zarracina – President

Robertz@FlightVenturesLtd.com

May 29, 2015

U.S. Department of Transportation

Docket Management System

1200 New Jersey Ave., SE Washington, DC 20590

Re: Exemption Request Pursuant to Section 333 of the FAA Modernization and Reform Act of

2012, 49 U.S.C. § 44701(f), and Part 11 of the Federal Aviation Regulations

Dear Sir or Madam:

Flight Ventures Ltd, pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 

(Reform Act), Subsection (f) of 49 U.S.C. § 44701, and 14 C.F.R. Part 11, requests an exemption

from the Federal Aviation Regulations (FARs) listed below and discussed in Appendix A to allow

Flight Ventures Ltd to conduct commercial operations with small Unmanned Aircraft System (sUAS) 

to provide aerial film making, photography, videography, surveying, data acquisition, site, structural 

and patrolling inspections for pipeline, energy, utility, construction, real estate, precision agriculture 

and other industries, search and rescue, remote sensing, community awareness, education, training 

and research operations.

Performing these services with a sUAS is in the public interest for several reasons, which are

detailed further herein and include: (1) dramatically reducing safety risks inherent in manned 

operations, both in the air and on the ground; (2) inspecting locations where humans are not able 

visit without incurring substantial risk; (3) enhancing capabilities to utilize the sUAS to assist first

responders on safety or environmental incidents; (4) and improving access to and control of 

various sites and operations.

The use of the sUAS for these services will reduce the need to either operate manned aircraft in a

difficult environment and reduce the environmental impact of conventional aircraft operations or add 

to the safety when other non-aircraft related methods prove hazardous or risky. In addition, the

small, lightweight, and easily controllable operating characteristics of the sUASs’ provide for safe

operations over site locations.
May 18, 2015 Flight Ventures Ltd Page: 2

Exemptions Requested

Flight Ventures Ltd requests exemptions from the following regulations:

14 C.F.R. Part 21;

14 C.F.R. 45.23(b);

14 C.F.R. 61.113(a) and (b);

14 C.F.R. 91.7(a);

14 C.F.R. 91.119(c);

14 C.F.R. 91.121;

14 C.F.R. 91.151(a);

14 C.F.R. 91.203(a) and (b);

14 C.F.R. 91.405(a);

14 C.F.R. 91.407(a)(1);

14 C.F.R. 91.409(a)(1) and (2);

14 C.F.R. 91.417(a) and (b).

Operating Conditions

Flight Ventures Ltd requests an exemption subject to the conditions listed in Appendix B, which

are substantially similar to the operating conditions required for the FAA’s previous grants of 

exemptions under Section 333.

In accordance with the conditions approved in previous exemption grants, Flight Ventures Ltd is 

requesting authority to operate the sUAS within visual line of sight and below 400 feet AGL

except as provided by FAA Air Traffic Control via COA. Flight Ventures Ltd will use the elevation of

the highest predominant terrain within 1 mile of the launch point and within the visual line of sight

(VLOS) as a ground reference point to establish the 400 feet ceiling. In other words, Flight Ventures 

Ltd will not operate the sUAS any higher than 400 feet above the highest point within 1 mile from

the launch point, and will only do so provided the sUAS is within the line of sight. These operating

conditions, along with those listed in Appendix B, would provide an equivalent level of safety for the

reasons described below. The sUAS is visible up to 2,000 meters (1.24 miles) in a clear sky, making

the selection of the predominant terrain within 1 mile of the launch point as a ground reference a 

logical and easily manageable reference.

Operator Requirements

As a condition to the grant of the exemptions, Flight Ventures Ltd will require that the PIC hold at 

least a private pilot certificate and a valid third-class medical certificate. The PIC will have

accumulated and logged a minimum number of flight cycles and hours for daytime operations, as

required by the FAA. The PIC will also be subject to the FAA flight review requirements.

The PIC and all observers will be required to have completed a Flight Ventures Ltd training

program.

Flight Ventures Ltd respectfully submits that the operator qualifications takes into account the

operating conditions and characteristics of the particular sUAS in use.
May 18, 2015 Flight Ventures Ltd Page: 3

Public Interest

Flight Ventures Ltd respectfully submits that its use of the sUAS in lieu of manned operations, which

are currently conducted with conventional fixed and rotary winged aircraft, offers increased

safety benefit and will achieve an enhanced level of safety, as mandated under Section 333(c) of

the Reform Act. Approval of this application also will benefit the public interest by allowing better,

safer, and more cost efficient information gathering for various industries.

Conventional aerial survey and inspection operations using manned aircraft involve very heavy

aerial vehicles that must transit to the operational location and carry significant quantities of

combustible fuels and a multi-person crew in piloting and observation roles. These operations

become even more difficult if the terrain is mountainous. By contrast, the sUAS light weight,

including its payload and use of batteries for power, allows it to be carried to and from the area of

activity, removing the need for airborne pilots and observers, and poses less risk to people and

infrastructure on the ground, as well as other aircraft.

Additionally, no national security issues are or will be raised by the grant of the requested

exemptions due to the sUAS small size and extremely limited load-carrying capacity, as well as its

operational limitations and absence of flammable fuel. On the other hand, the sUAS is likely to

enhance national security through better and more accurate monitoring of critical national

infrastructure.

The grant of the requested exemption is in the public interest based on the clear direction in

Section 333 and 49 U.S.C. § 44701(f), the equivalent and enhanced level of safety of the 

proposed operations, the significant public benefit, and cost savings to be realized as a result of the

use of sUAS for aerial inspection and survey services. Moreover, the FAA has already granted 

similar exemptions for sUAS used to conduct high-resolution aerial imaging and surveying 

operations. Accordingly, the applicant respectfully requests that the FAA grant the requested

exemption without delay.

Privacy Concerns

The proposed operations will take place only in largely unpopulated, remote areas that are 

owned or leased, controlled by Flight Ventures Ltd or the owner of record. Access to these areas

is restricted to employees and authorized personnel only. No privacy issues are raised by this

application.

Federal Register Summary

Pursuant to 14 C.F.R. § 11.81(f), the following summary is provided for publication in the Federal

Register, should the FAA determine that publication is needed:

Docket No.: No. FAA-2015- Petitioner: Flight Ventures Ltd. Section of 14 CFR: Part 21, § 45. 23(b), 

§ 61.113(a) and (b), § 91.7(a), § 91.119(c), § 91.121, § 91.151(a), § 91.405(a), § 91.407(a)(1), § 

91.409(a)(2), § 91.417(a) and (b). Description of Relief Sought: Flight Ventures Ltd is seeking an

exemption to conduct commercial operations using a small-unmanned aircraft (55 pounds or less) in

remote areas of the United States.
May 18, 2015 Flight Ventures Ltd Page: 4

Under 49 U.S.C. § 44701(f), the “Administrator may grant an exemption from a requirement of a 

regulation prescribed under subsection (a) or (b) of this section or any of sections 44702-44716 of

[Title 49] if the Administrator finds the exemption is in the public interest.” See Exemption Nos.

11109, 11110, 11136, 11166, 11167, 11170, 11172. Flight Ventures Ltd requests that the FAA not 

request public comment on its application because it would not set a precedent and because the

relief requested is identical to exemptions granted previously. 14 C.F.R. § 11.87.

Sincerely,

Robert A Zarracina

Flight Ventures Ltd
May 18, 2015 Flight Ventures Ltd Page: 5

APPENDIX A

EXEMPTION REQUEST AND EQUIVALENT LEVEL OF SAFETY SHOWINGS UNDER

APPLICABLE RULES SUBJECT TO EXEMPTION

Flight Ventures Ltd requests an exemption from the following regulations as well as any additional 

regulations that may technically apply to the operation of the sUAS:

14 C.F.R. Part 21, Subpart H: Airworthiness Certificates

Part 21, Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements for

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

weight of the aircraft, the operating conditions, design safety features, and the proposed conditions

and limitations, it is unnecessary to go through the certificate of airworthiness process under Part 21 

Subpart H to achieve or exceed current safety levels.

Such an exemption meets the requirements of an equivalent level of safety under Part 11 and 

Section 333. Section 333 and 49 U.S.C. § 44701(f) both authorize the FAA to exempt 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 sUAS involved.

In this case, an analysis of these criteria demonstrates that the sUAS operated without an 

airworthiness certificate, under the conditions proposed herein, will be at least as safe, or safer,

than a conventional aircraft (fixed wing or rotorcraft) with an airworthiness certificate. The sUAS

weighs less than 10 pounds fully loaded. It will not carry a pilot, passenger or flammable fuel. The

sUAS operates exclusively within a controlled area pre-disclosed and in compliance with conditions

set forth herein. Unlike other civil aircraft, operations under this exemption will be tightly controlled

and monitored by the PIC and observer(s), pursuant to the conditions set forth in Appendix B, the

Operator’s Manual, and local public safety requirements. The FAA will have advance notice of all

operations through the filing of NOTAMs. The lack of flammable fuel and the fact that the aircraft is

carried to the location and not flown there all establish the equivalent level of safety. The sUAS

provides at least an equivalent level of safety to that of such operations being conducted with

conventional aircraft that would be orders-of-magnitude larger and would be carrying passengers,

cargo, and flammable fuel.

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

The regulation requires that 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 nor 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 cabin, 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 safety 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 this regulation to Exemptions Nos. 10700, 8738, 

10167 and 10167A. 
May 18, 2015 Flight Ventures Ltd Page: 6

14 C.F.R. §§ 61.113(a) & (b): Commercial Pilot Privileges

Sections 61.113(a) & (b) limit private pilots to non-commercial operations. Unlike a conventional 

aircraft that carries a pilot, passengers, and cargo, the sUAS is remotely controlled with no

passengers or property of others on board. The area of operation is controlled and restricted,

and all flights are planned and coordinated in advance as set forth in the Operator’s Manual. In

conjunction with the required training of the PIC and observers, the level of safety provided by the

requirements included in the Operator’s Manual exceeds that provided by a single individual holding

a commercial pilot certificate operating a conventional aircraft. The proposed operations will

achieve at least an equivalent level of safety.

14 C.F.R. § 91.7(a): Minimum Safe Altitudes

Section 91.7(a) prohibits an individual from operating a civil aircraft unless it is in an airworthy

condition. No FAA standard exists for determining an aircraft’s airworthiness when an

airworthiness certificate is not issued. As the FAA has done with previous exemption grants,

airworthiness will be ensured and an equivalent level of safety will be achieved by compliance

with the operating documents prior to every flight.

14 C.F.R. § 91.119(c): Minimum Safe Altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. Specifically, Section

91.119(c) limits aircraft flying over areas other than congested areas to an altitude of 500 feet above

the surface, except over open water or sparsely populated areas. In those cases, the aircraft may 

not be operated closer than 500 feet to any person, vessel, vehicle, or structure. Because some of

the aerial inspection and survey work must be accomplished at altitudes less than 500 feet AGL and

nonparticipating employees may be working within 500 feet of the sUAS, an exemption from

Section 91.119(c) is needed.

The equivalent level of safety will be achieved because the sUAS, given its size, weight, speed, and

materials, does not pose a serious risk. Also, every flight will be conducted over land controlled by

Flight Ventures Ltd. Flight Ventures Ltd will notify all effected individuals of sUAS operations in 

advance to ensure they are aware of the planned flights. Compared to aerial inspection operations

conducted with aircraft or rotorcraft weighing far more than 10 pounds and carrying flammable fuel,

any risk associated with these operations will be far less than those currently allowed with

conventional aircraft operating at or below 500 feet AGL. Exemption Nos. 11156, 11158, 11159.

14 C.F.R. § 91.121: Altimeter Setting

Section 91.121 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 sUAS may not have a barometric altimeter, but instead a GPS

altitude read out, an exemption is required. An equivalent level of safety will be achieved by the

operator, pursuant to the Operator’s Manual, confirming the altitude of the launch site shown on the

GPS altitude indicator before flight.
May 18, 2015 Flight Ventures Ltd Page: 7

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

This regulation 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) During 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 sUAS

batteries provide approximately 50 minutes of powered flight. Without an exemption from 14

C.F.R. § 91.151, the sUAS’s flights would be limited to approximately 10 minutes in length

because the PIC would require the last 30 minutes to satisfy section 91.151(a). Given the

limitations on its proposed operations, a longer time frame for flight in VFR conditions is reasonable.

Flight Ventures Ltd believes that an exemption from 14 C.F.R. § 91.151(a) provides an equivalent

level of safety and is consistent with prior exemptions. Operating the sUAS, without 30 minutes of

reserve fuel does not engender the type of risks that Section 91.151(a) was meant to prevent

given the size and speed at which the sUAS operates. In the unlikely event that the sUAS’ battery

runs low, it would simply follow the pre-programmed command to land at a designated location, 

usually the departure point. Given its weight and construction material, the risks are less than 

contemplated by the current regulation.

Flight Ventures Ltd believes that an equivalent or enhanced level of safety can be achieved by 

maintaining 10 minutes of reserve power which, allowing at least 30 minutes of flight time, if not

more, would be more than adequate to return the sUAS to its planned landing zone from anywhere

in its limited operating area. Exemption 10673 (allowing Lockheed Martin Corporation to operate

without compliance with 91.151(a)); see also Exemptions 2689F, 5745, 10673 and 10808.

14 C.F.R. §§ 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 91.417(a) and (b): Maintenance

Inspections

Section 91.405(a) requires 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.”

Section 91.407 similarly makes reference to requirements in Part 43. Section 91.409(a)(2)

requires an annual inspection for the issuance of an airworthiness certificate. Section 91.417(a)

requires the owner or operator to keep records showing certain maintenance work that has been

accomplished by certificated mechanics, under Part 43, or licensed pilots and records of approval

of the aircraft for return to service. A qualified person prior to each flight and at predefined intervals 

as part of the maintenance schedule will perform pre-flight checks.

The pre-flight checklist includes but may not be limited to:

1. Visual inspection of the airframe;

2. Visual inspections of propeller;

3. Verify GPS acquisition;

4. Plan and upload mission;

5. Video and payload check;

6. Controls check;

7. Gyro/control surfaces check;

8. Throttle check

9. Altimeter check;

10. Check sensors; and

11. Verify failsafe’s are set correctly.
May 18, 2015 Flight Ventures Ltd Page: 8

An equivalent level of safety will be achieved because the sUAS will carry no external payload, will

operate only in restricted predetermined areas, and is not a complex mechanical device. In addition,

the operator will ensure that the sUAS is in working order prior to initiating flight, perform required

maintenance, and keep a log of any maintenance that is performed. Moreover, the operator is

the person most familiar with the aircraft and is best suited to maintain the aircraft in an airworthy

condition and to ensure an equivalent level of safety. Last, the Operator’s Manual will have

instructions to develop and document maintenance, overhaul, replacement, and inspection

requirements in the absence of Flight Ventures Ltd requirements, and procedures to document and

maintain maintenance records for the sUAS. The sUAS maintenance guidelines provide an

equivalent level of safety to the maintenance requirements in Part 91.
May 18, 2015 Flight Ventures Ltd Page: 9

APPENDIX B

FLIGHT VENTURES LTD OPERATING LIMITATIONS

1. Operations authorized by the grant of exemption are limited to the sUAS that weigh less

than 55 lbs.

2. The sUAS will not be operated at a speed exceeding 87 knots (100 miles per hour) based on 

either groundspeed or calibrated airspeed to determine compliance with the 87 knot speed 

restriction. In no case will the sUAS be operated at airspeeds greater than the maximum 

sUAS operating airspeed recommended by the aircraft manufacturer. 

3. The sUAS will not be operated at an altitude more than 400 feet above the highest 

predominant terrain except as may be provided by FAA Air Traffic Control (ATC) via COA.

The highest predominant terrain is the defined as terrain within 1 mile of the launch point

and within the visual line of sight of the PIC. All altitudes reported to ATC shall be in feet

AGL.

4. The sUAS 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 use a visual observer (VO). The VO and PIC must be able to

communicate verbally at all times. The PIC must be designated before 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 accessible during sUAS 

operations and made available to the Administrator upon request. If a conflict exists 

between the conditions and limitations in the exemption and the procedures outlined in the

operating documents, the conditions and limitations in the exemption take precedence and

must be followed. Otherwise, Flight Ventures Ltd must follow the procedures as outlined in

its operating documents. Flight Ventures Ltd may update or revise its operating documents.

It is Flight Ventures Ltd’s responsibility to track such revisions and present updated and

revised documents to the Administrator upon request. Flight Ventures Ltd must also present 

updated and revised documents if it petitions for extension or amendment to this grant of

exemption.

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

flight. The PIC shall not operate the aircraft if the inspection reveals a condition that affects

the safe operation of the sUAS until the necessary maintenance has been performed and

the sUAS is found to be in a condition for safe flight. The Ground Control Station, if

utilized, must be included in the preflight inspection. All maintenance and alternations must

be properly documented in the aircraft records.

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

characteristics (e.g., replacement of a flight critical component) must undergo a functional

test flight in accordance with the Operator’s Manual. The PIC who conducts the functional

test flight must make an entry in the aircraft records of the flight. The requirements and

procedures for a functional test flight and aircraft record entry shall be included in the

Operator’s Manual.
May 18, 2015 Flight Ventures Ltd Page: 10

9. The pre-flight inspection must account for all discrepancies, e.g. inoperable components, 

items, or equipment, not already covered in the relevant sections of the operating

documents.

10. The operator must follow sUAS manufacturers component, maintenance, overhaul, 

replacement, inspection, and life limit requirements.

11. Flight Ventures Ltd must carry out its maintenance, inspections, and record keeping

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

alterations, and status of replacement/overhaul component parts must be noted in the

aircraft records, including total time in service, description of work accomplished, and the

signature of the person authorized to return the sUAS to service.

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

Bulletins or Airworthiness Directives if applicable.

13. The PIC must possess at least a private pilot certificate and at least a current third class

medical certificate. The PIC must also meet the flight review requirements specified in 14

C.F.R. § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

14. Flight Ventures Ltd may not permit any PIC to operate, unless the PIC meets the

operator’s qualification criteria and demonstrates the ability to safely operate, the sUAS in a 

manner consistent with how the sUAS 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 C.F.R. § 61.51(b). The PIC must ensure that the VO

is trained appropriately in order to fulfill his or her duties. A record of training and

qualification must be documented and made available upon prior documented flight

experience obtained in compliance with applicable regulations may satisfy this requirement.

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, 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 these operating conditions.

15. Operations may not be conducted during night, as defined in 14 C.F.R. § 1.1. All 

operations must be conducted under visual flight rules (VFR) conditions. Flights under

special visual flight rules (SVFR) or instrument flight rules (IFR) conditions are not authorized.

16. The sUAS may not operate within 5 nautical miles of an airport reference point as 

denoted on a current FAA published aeronautical chart unless a letter of agreement with

that airport’s management is obtained, and the operation is conducted in accordance with a

NOTAM as required by Flight Ventures Ltd’s COA. The letter of agreement with the airport

management must be made available to the Administrator upon request.

17. The sUAS 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.
May 18, 2015 Flight Ventures Ltd Page: 11

18. If the sUAS loses communications or loses its GPS signal, the sUAS must return to a predetermined location within the security perimeter and land or be recovered in accordance

with the Operator’s Manual.

19. The PIC must abort the flight in the event of unpredicted obstacles, other aircraft incursions

or emergencies in accordance with the Operator’s Manual.

20. sUAS operations must be completed within 50 minutes flight time.

21. Flight Ventures Ltd must obtain an ATC issued COA prior to conducting any operations

under this exemption. This COA will also require the filing of the NOTAM not more than 72 

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

22. All aircraft operated in accordance with the requested exemption must be identified by serial 

number, registered in accordance with 14 C.F.R. Part 47, and have identification (N-Number)

markings in accordance with 14 C.F.R. Part 45, Subpart C. Markings shall be as large as 

practicable.

23. The radio frequency spectrum used for operation and control of the sUAS must comply

with Federal Communication (FCC) or other appropriate government oversight agency

requirements.

24. The documents required under 14 C.F.R. §§ 91.9 and 91.203 must be available to the PIC

at the Ground Control Station of the sUAS any time the aircraft is operating. These

documents shall be made available to the Administrator or any law enforcement official upon 

request.

25. The sUAS must remain clear and yield the right of way to all other manned operations and

activities at all times.

26. The sUAS may not be operated from any moving device or vehicle.

27. The sUAS may not be operated over congested or densely populated areas.

28. Flight operations must be conducted at least 500 feet from all nonparticipating persons,

vessels, vehicles, structures, and public access roads unless if operated near vessels,

vehicles or structures where the owner / controller of such vessels, vehicles or structures

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.

29. Operations nearer than 500 feet to the PIC, VO, operator trainees or essential persons as

defined in the operating documents are permitted if those operations do not present an

undue hazard to those persons per § 91.119(a) as determined by the PIC.

30. All operations must be conducted over private or controlled access property unless an 

exception is granted.

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

boundaries of the operational area as defined by the applicable COA shall 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.
May 18, 2015 Flight Ventures Ltd Page: 12

APPENDIX C

SMALL UNMANNED AERIAL SYSTEM DESCRIPTION

Flight Ventures Ltd Corporate Overview: Flight Ventures Ltd is a Minnesota company with its

headquarters in Stillwater, Minnesota.

sUAS Operating Overview: The sUAS utilized are either a fixed or rotary-wing aircraft constructed

of foam or rugged polycarbonate materials. The aircraft are easy to assemble or come preassembled. The sUAS can be operated manually or in fully autonomous flight modes. Creating preplanned flight paths in autonomous mode is as simple as clicking on reference points on a georeferenced maps. Pre-mission waypoints, landing zones, and flight area dimensions can be entered 

during preflight planning ensuring the sUAS operates only within specified boundaries and predetermined flight parameters.

The DJI Phantom 3 (Phantom) and Sensefly Exom (Exom) are quad copter drones while the 

Sensefly eBee (eBee), Ag Eagle (Eagle) and Precision Hawk (Hawk) are fixed wing drones.

The Phantom is a battery-powered drone allowing flight times up to 23

minutes. Diagonally it measures approximately 590mm (23.25 inches) 

including rotor blades. Takeoff weight is 1280 grams.

The Exom is a battery-powered drone allowing flight times up to 22 

minutes. It measures approximately 7.0 H x 22 L x 32 W inches. Rotor 

blade diameter measures 13 inches. Takeoff weight is 3.7 pounds.

The eBee is a battery-powered drone allowing flight times up to 50 

minutes. Its wingspan is 38 inches. Takeoff weight is 1.52 pounds.

The Eagle is a battery-powered drone allowing flight times up to 40 

minutes. Its wingspan is 56 inches. Takeoff weight is 3 pounds.

The Hawk is a battery-powered drone allowing flight times up to 40 

minutes. Its wingspan is 48 inches. Takeoff weight is 3 pounds.
May 18, 2015 Flight Ventures Ltd Page: 13

Many advanced safety features makes these drones on of the safest choices for commercial 

operations. Safety features include geo-fencing, position hold and self-leveling, return home, 

emergency landing and stop. The Exom includes rotor blade shrouding.

Operator’s Manual – The respective UAS Operator’s Manual, provided by the respective 

manufacturer, will be followed at all times and available during all appropriate flight operations.

Takeoff and Landing style/type – The sUAS is ground or hand launched and can be tube launched 

with additional equipment. The sUAS lands by returning to a pre-determined rally point. Once it

reaches a pre-selected altitude, it heads toward the landing waypoint, descending until it lands and / 

or skids to a stop.

Navigation System – Specific maps can be downloaded to the display screen (such as VFR air 

sectional and geographic maps), which are overlaid with GPS positional data. Waypoints can be

created before and during flight operations creating specific locations and sequences for the aircraft

in use.

Defined “Keep Out” Areas – The navigation software allows for preplanning Keep Out Areas, also 

know as geo-fencing, that allow the operator to designate airspace he or she does not want the

sUAS to enter. If defined flight paths pass through an area designated as keep-out, the individual 

waypoints and waypoint connection segments turn red as a warning. Additionally, if a mission is

uploaded and intersects with a keep out area, a warning is presented to the user. Also, if an aircraft

in flight is navigated into a designated keep out area, an audible warning is sounded.

Maintenance – The sUAS require very little maintenance, and operators may perform most required

maintenance in the field with the field repair kit.

Command and Control Systems - The sUAS Ground Control Station (GCS) allows the operator

simultaneous control over aircraft and payloads. The display screen provides all essential flight data

to the operator. Telemetry data is transmitted to the command station at least once per second.

Displayed on GCS:

● Current position

● Registered home position

● Any autopilot flight plans

● Registered emergency landing zone

● Aircraft attitude

● Altitude

● Airspeed

● Groundspeed

● Compass reading/heading

● Estimated wind heading

● Communication strength

● Range from home

● Bearing from home

● Duration of current mission

● Rate of climb

● Mode of the aircraft

● Battery level
May 18, 2015 Flight Ventures Ltd Page: 14

Emergency Procedures and System Failures

Loss of Link – The sUAS does not need constant signal from the GCS to continue flying.

Communications outages are detected by the system and are reported to the PIC. During the

communication outage, the sUAS continues on its pre-determined flight path until a failsafe is

triggered. Once a failsafe is triggered, the sUAS will perform in accordance with the failsafe

conditions uploaded before launch. This is accomplished without input from the operator.