M atthew R. Engel Tree Top View Media 1866 Germany Rd. Williamston, Michigan 48895

N ovember 23, 2015

U. S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590

RE: Exempti on Request Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation Regulations from 14 C.F.R. 45.23(b); 14 CFR Part 21; 14 CFR 61.113 (a) & (b); 91.7 (a); 91.9 (b) (2); 91.103(b); 91.109; 91.119; 91.121; 91.151(a); 91.203(a) & (b); 91.405 (a) ; 91.407(a) (1); 91.409 (a) (2); 91.417 (a) & (b).

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, Tree Top View Media (“the applicant”), developer and operator of Small Unmanned Aircraft Systems (“sUASs”) equipped to conduct R eal Estate, Marketing,

Infrastructure and Construction I nspection and assist Business O perations, hereby applies for an exemption from the listed Federal Aviation Regulations (“FARs”) to allow commercial operation of its sUASs, so long as such operations are conducted within and under the conditions outlined herein or as may be established by the FAA as required by Section 333.

As described more fully below, the requested exemption would permit the operation of smal l, unmanned, and relatively inexpensive sUAS under controlled conditions in airspace that is 1) limited, 2) predetermined, 3) controlled as to access, and 4) would provide safety enhancements to the already safe operations in the infrastructure and busines s operations industry presently using conventional aircraft. Approval of this exemption would thereby enhance safety and fulfill the Secretary of Transportation’s (the FAA Administrator’s) responsibilities to “...establish requirements for the safe operation of such aircraft systems in the national airspace system.” Section 333(c) of the Reform Act.

The name and address of the applicant is:

Tree Top View Media

Attn: M atthew R. Engel

Ph o ne : ( 517 ) 285

- 0307

Email: men gel@treetopviewmedia .com Address: 1866 Germany Rd. Williamston, Michigan 48895Regulations from which the exemption is requested:

• 14 CFR Part 21

• 14 C.F.R. 45.23(b)

• 14 CFR 61.113 (a) & (b)

• 14 C.F.R. 91.7 (a)

• 14 CFR 91.9 (b) (2)

• 14 C.F.R. 91.103

• 14 C. F.R. 91.109

• 14 C.F. R. 91.119

• 14 C.F.R. 91.121

• 14 CFR 91.151 (a)

• 14 CFR 91.203 (a) & (b)

• 14 CFR 91.405 (a)

• 14 CFR 407 (a) (1)

• 14 CFR 409 (a) (2)

• 14 CFR 417 (a) & (b)

This exemption application is expressly submitted to fulfill Congress’ goal in pa ssing Section 333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to consider whether certain unmanned aircraft systems may operate safely in the national airspace system (NAS) before completion of the rulemaking required under Section 332 of the Reform Act. In making this determination, the Secretary is required to determine which types of UASs do not create a hazard to users of the NAS or the public or pose a threat to national security in light of the following:

• The UAS’s size, weight, spe ed, and operational capability;

• Operation of the UAS in close proximity to ai rports and populated areas; and

• Operation of the UAS within visual line of sight of the operator.

Reform Act § 333 (a). Lastly, if the Secretary d etermines that such vehicles “may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft in the national airspace system.” Id. §333(c) (emphasis added). 1

The Federal Aviation Act e xpressly grants the FAA the authority to issue exemptions. This statutory authority by its terms includes exempting civil aircraft, as the term is defined under §40101 of the Act, which includes sUASs, from the requirement that all civil aircraft must have a current airworthiness certificate.

The Administrator may grant an exemption from a requirement of a regulation prescribed under subsection (a) or (b) of this section or any sections 44702

- 44716 of this title if the Administrator

1 Applicant interprets this provision to place the duty on the Administrator to not only process applications for exemptions under section 333, but for the Administrator to craft conditions for the safe operation of the UAS, if it
should be determined that the conditions set forth herein do not fulfill the statu tory requirements for approval.finds the exemption in the public interest. 49 U.S.C. §44701(f) See also 49 USC §44711(a); 49

USC §44704; 14 CFR §91.203 (a) (1).

Tree Top View Media ’s sUAS ’ s (Appendix 1) are rotorcraft, weighing 55 or fewer lbs. including payload. They operate under normal conditions at a speed of no more than 25 knots and have the capability to hover and mo ve in the vertical and horizontal plane simultaneously. They will operate only in line of sight and will operate only within the sterile area described in the • TREE

TOP VIEW MEDIA

- Attachment 1

- sUAS Operating Manual , attached as Ap pendix 2 (hereinafter “the Manual”) . Such operations insure that the sUAS does “not create a hazard to users of the national airspace system or the public.” 2 Given the small size of the sUAS ’ s involved

and the restricted sterile environment within which th ey will operate, the applicant falls squarely within that zone of safety (an equivalent level of safety) in which Congress envisioned that the FAA must, by exemption, allow commercial operations of s UASs to commence immediately.

Also due to the size of the s UASs and the restricted areas in which the relevant sUAS ’ s will operate, approval of the application presents no national security issue. Given the clear direction in Section 333 of the Reform Act, the authority contained in the Federal Aviation Act, as

ame nded; the strong equivalent level of safety surrounding the proposed operations, and the significant public benefit, including enhanced safety, reduction in environmental impacts, including reduced emissions associated with allowing s UAS ’ s for R eal Estate, Marketing,

Infrastructure and Construction I nspection , and B usiness O perations, the granting of the requested exemptions is in the public interest. Accordingly, the applicant respectfully requests that the FAA grant the requested exemption without delay.

Background Information

Tree Top View Media is in the business of consulting on v ideo inspection of building and maintaining mission specific sUAS R eal Estate, Marketing, Infrastructure and Construction

I nspection , and Public S afety. Tree Top View Media ’ s clients look to us for safe operations of sUAS. We have developed specific safe UA V operational procedures. Increasingly, we have clients looking to operate sUAS for infrastructure and maintenance inspections, construction documentation, public safety, and business operations.

2 Reform Act Section 333 (b).Operations performed by Tree Top View Media include:

• Real Estate/Architecture

• Marketing

- Tourism

- Hotel/Resort

- Golf Course Management

• Aerial Data Collection

• Surveying and Mapping

• Agriculture Crop Management

• Agriculture Inspection

• Aerial Filmmaking and Photography

• Construction S ite I nspections and M onitoring

• I ndustrial Surveying

• Manufa cturing Inspection

• Construction Site Documentation

• Land Development

• Public Safety

As part of this

, Tree Top View Media is requesting FAA Exempti on for sUAS operations for safety, m arketing, inspection and video capture usage.

AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY

The applicant proposes that the exemption requested herein apply to civil aircraft that have the characteristics and that operate within the limi tations listed herein. These limitations provide for at least an equivalent or even higher level of safety to operations under the current regulatory structure because the proposed operations represent a safety enhancement to the already safe

infrastructur e, construction, and business operations conducted with conventional aircraft.

These limitations and conditions to which Tree Top View Media agrees to be bound when conducting commercial operations under an FAA issued exemption include:

1. The sUA S will weigh less than 55 lbs.

2. Flights will be operated within line of sight of a pilot and/or observer.

3. Maximum total flight time for each operational flight will be 30 minutes. Flights will be terminated at 25% battery power reserve should that occ ur prior to the 30 minute limit.

4. Flights will be operated at an altitude of no more than 400 feet AGL or, not more than 200 feet above an elevated platform from which flight is planned.

5. Minimum crew for each operation will consist of the sUAS Pilot a nd the Visual

Observer.

6. The sUAS pilot will be a specially trained staff member of Tree Top View Media knowledgeable of the airspace within which the operation will take place and how that airspace fits into the NAS.7. The sUAS Pilot will be t he Pilot in Command (PIC). If a pilot certificate holder other than the sUAS Pilot, who possess the necessary PIC qualifications, is also present on site, that person can also be designated as PIC.

8. The sUAS will only operate within defined boundaries as outlined in the company Manual.

9. A briefing will be conducted in regard to the planned sUAS operations prior to each mission. It will be mandatory that all personnel who will be performing duties within the boundaries of the safety perimeter be p resent for this briefing.

10. The operator will file a FAA Form 7711

- 1, or its equivalent, as modified in light of the requested exemption, with the appropriate Flight Standards District Office (FSDO).

11. The operator will obtain the consent of all persons involved in the mission and ensure that only consenting persons will be allowed within 100 feet of the flight operation, and this radius may be reduced to 30 fe et based upon an equivalent level of safety determination, as required by the company m anual. With the advanced permission of the relevant FSDO, operations at closer range can be approved.

12. The operator will submit a written Plan of Activities to the FSDO three days before the proposed mission as required in the company m anual. Items will include:

a. Dates and times for all flights;

b. Name and phone number of the operator for the s UAS mission conducted under this petition of exemption;

c. M ake, model, and serial or N

- number of UAS to be used;

d. Name and certificate number of s UAS PICs involved in the mission;

e. A statement that the operator has obtained permission from property owners and/or local officials to conduct the mission;

f. The li st of those who gave permission 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 whi ch the mission will be conducted and the altitudes essential to accomplish the operation.

13. Pilot and observer will have been trained in operation of s UAS generally and received

up

- to

- date information on the particular s UAS to be operated as required in t he company

manual

. 14. Observer and pilot will at all times be able to communicate by voice.

15. Written and/or oral permission from the relevant property holders will be obtained.

16. All required permissions and permits will be obtained fr om territorial, state, county or city jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies.

17. If the sUAS loses communications or loses its GPS signal, the UAS will have the capability to return to a pre

- determ ined location within the Security Perimeter and land.

18. The sUAS will have the capability to abort a flight in case of unpredicted obstacles or emergencies.14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. §91.203 (a) (1)

Subpart H, ent itled Airworthiness Certificates, establishes the procedural requirements for the issuance of airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and limited operating area associated with the aircraft to be utilized by the Applic ant, an exemption from Part 21 Subpart H meets the requirements of an equivalent level of safety under Part 11 and Section 333 of the Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333

of the Reform Act both authorize the FAA to exe mpt aircraft from the requirement for an airworthiness certificate, upon consideration of the size, weight, speed, operational capability, and proximity to airpor ts and populated areas of the particular UAS. In all cases, an analysis of these criteria demonstrates that the UAS operated without an airworthiness certificate, in the restricted environment and under the conditions proposed will be at least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate without the restrictions and conditions proposed.

The sUAS to be operated hereunder is less than 55 lbs. fully loaded, carries neither a pilot nor

pa ssenger, carries no explosive materials or flammable liquid fuels, and operates exclusively within a secured area as set out in the Manual. Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by both the op erator and observer, pursuant to the Manual’s policies, and under and in compliance with local public safety requirements, to provide security for the area of operation as is now done with conventional infrastructure and construction inspections and busine ss operations. The FAA will have advance notice of all operations. These safety enhancements, which already apply to civil aircraft operated in connection with infrastructure and construction inspections and business operations, provide a greater degree of safety to the public and property owners than conventional operations conducted with airworthiness certificates issued under 14 C.F.R. Part 21, Subpart H.

Lastly, application of these same criteria demonstrates that there is no credible threat to national security posed by the UAS, due to its size, speed of operation, location of operation, lack of explosive materials or flammable liquid fuels, and inability to carry a substantial external load.

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

The regulation requires:

When marks include only the Roman capital letter "N" and the registration number is displayed on limited, restricted or light

- sport category aircraft or experimental or provisionally certificated aircraft, the operator must also display

on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches 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 a cabin, cockpit or pilot station on which the word “Experimental” can be placed. Given the size of the sUA S , 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 sUA S marked on its fuselage as required by §45.29 (f) where the pilot, observer and others working with the sUA S 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 101 67A.

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

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

- commercial operations. Because the UAS will not carry a pilot or passengers, the proposed operations can ac hieve the equivalent level of safety of current operations by requiring the PIC operating the aircraft to have specially trained staff operate this small UAS. Unlike a conventional aircraft that carries the pilot and passengers, the sUAS is remotely contro lled with no living thing on board. The area of operation is controlled and restricted, and all flights are planned and coordinated in advance as set forth in the Manual. The level of safety provided by the requirements included in the Manual exceeds that provided by a single individual holding a commercial pilot’s certificate operating a conventional aircraft. The risks associated with the operation of the sUAS are so diminished from the level of risk associated with commercial operations contemplated by P art 61 when drafted, that allowing operations of the sUAS as requested by specially trained staff as the PIC exceeds the present level of safety achieved by 14 C.F.R. §61.113 (a) & (b).

14 C.F.R. §91.7(a): Civil aircraft airworthiness.

The regulation requi res that no person may operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for the aircraft, should this exemption be granted, no FAA regulatory standard will exist for determining airworthines s. Given the size of the aircraft and the requirements contained in the Manual for maintenance and use of safety checklists prior to each flight, as set forth in t he company manual , an equivalent level of safety will be provided.

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

Section 91.9 (b) (2) provides:

No person may operate a U.S.

- registered civil aircraft ... (2) For which an Airplane or Rotorcraft Flight Manual is not required by §21.5 of this chapter,

unless there is availabl e in the aircraft a current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or any

combination thereof.

The sUAS, given its size and configuration has no ability or place to carry such a flight manual

on the aircraft, not only because there is no pilot on board, but because there is no room or capacity to carry such an item on the aircraft.The equivalent level of safety will be maintained by keeping the flight manual at the ground control point where the pil ot flying the sUAS will have immediate access to it.

The FAA has issued the following exemptions to this regulation: Exemption Nos. 8607, 8737, 8738, 9299, 9299A, 9565, 9565B, 10167, 10167A, 10602, 32827, and 10700.

14 C.F.R. § 91.103: Preflight action

This regulation requires each pilot in command to take certain actions before flight to insure the safety of flight. As FAA approved rotorcraft flight manuals will n ot be provided for the aircraft, an exemption will be needed. An equivalent level of safety will be provided as set forth in the

company Manual. The PIC will take all actions including reviewing weather, flight battery requirements, landing and takeoff distances, and aircraft performance data before initiation of flight.

14 C.F.R. §91.109: Flight instruction

Section 91.103 provides that no person may operate a civil aircraft (except a manned free balloon) that is being used for flight instructio n unless that aircraft has fully functioning dual

controls.

sUASs and remotely piloted aircraft, by their design do not have fully functional dual controls. Flight control is accomplished through the use of a control box that communicates with the

aircraft via radio communications. The FAA has approved exemptions for flight training without fully functional dual controls for a number of aircraft and for flight instruction in experimental aircraft. See Exemption Nos. 5778K & 9862A. The equivalent level of sa fety provided by the fact that neither a pilot nor passengers will be carried in the aircraft and by the size and speed of

the aircraft.

14 C.F.R. §91.119: Minimum safe altitudes

Section 91.119 establishes safe altitudes for operation of civil aircraft. Se ction 91.119(d) allows helicopters to be operated at less than the minimums prescribed, provided the person operating the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. As this exemption is for a sUAS that is a helic opter and the exemption requests authority to operate at altitudes up to 400 AGL, or not more than 200 above an elevated platform from which operation is planned, an exemption may be needed to allow such operations. As set forth herein, except for

the limi ted conditions stated in the Manual, the UAS will never operate at higher than 400 AGL. It will, however, be operated in a restricted area with a security perimeter, where buildings and people will not be exposed to operations without their pre

- obtained co nsent.

The equivalent level of safety will be achieved given the size, weight, and speed of the UAS as well as the location where it is operated. No flight will be taken without the permission of the property owner or local officials. Because of the advanc e notice to the property owner and participants in the mission, all affected individuals will be aware of the planned flight operations

as set forth in t he company manual

.Compared to flight operations with aircraft or rotorcraft weigh ing far more than the maximum 55lbs. proposed herein and the lack of flammable fuel, any risk associated with these operations is far less than those presently pr esented with conventional aircraft operating at or below 500 AGL in the infrastructure and construction inspections and business operations industry. In addition, the low

- altitude operations of the sUAS will ensure separation between these small UAS operat ions and the operations of conventional aircraft that must comply with Section

91.119.

14 C.F.R. §91.121 Altimeter Settings

This regulation requires each person operating an aircraft to maintain cruising altitude by

reference to an altimeter that is set “... to the elevation of the departure airport or an appropriate altimeter setting available before departure.” As the sUAS may not have a barometric altimeter, but instead a GPS altitude read out, an exemption may be needed. An equivalent level of safety

will be achieved by the operator, pursuant to the Manual and safety checklist, confirming the altitude of the launch site shown on the GPS altitude indicator before flight.

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

Section 91.151 (a) prohibits an individual from beginning “a flight in an airplane under VFR conditions unless (considering wind and forecast weather conditions) there is enough fuel to fly to the first point of intended landing, and, assuming normal cruising speed

– (1) Du ring the day, to fly after that for at least 30 minutes; or (2) at night, to fly after that for at least 45 minutes.” The battery powering the sUAS provides approximately 30 minutes of powered flight. To meet

the 30

- minute reserve requirement in 14 CFR §91 .151, sUAS flights would be limited to approximately 20 minutes in length. Given the limitations on the UAS’s proposed flight area and the location of its proposed operations within a predetermined area, a longer time frame for flight in daylight or night VFR conditions is reasonable.

Applicant believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without compliance with FAR 91.151 (a)). Operating th e small UAS, in a tightly controlled area where only people and property owners or official representatives who have signed waivers will be allowed, with less than 30 minutes of reserve fuel, does not engender the type of risks that Section 91.151(a) was i ntended to alleviate given the size and speed of the small UAS. Additionally, limiting sUAS flights to 20 minutes would greatly reduce the utility for which the exemption will be granted.

Applicant believes that an equivalent level of safety can be achieve d by limiting flights to 20 minutes or 25% of battery power whichever happens first. This restriction would be more than adequate to return the sUAS to its planned landing zone from anywhere in its limited operating

area.

Similar exemptions have been granted to other operations, including Exemptions 2689F, 5745, 10673, and 10808.14 C.F.R. §91.203 (a) and (b): Carrying Civil Aircraft Certification and Registration

The regulation provides in pertinent part:

(a) Except as provided in § 91.715, no person may operate a civil aircraft unless it has within it the following:

(1) An appropriate and current airworthiness certificate. . . .

(b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) of this section or a special flight authorization issued under §91.715 is displayed at the cabin or cockpit entrance so that it is legible to

passengers or crew.

The UAS fully loaded w eighs no more than 55 lbs. and is operated without an onboard pilot. As such, there is no ability or place to carry certification and registration documents or to display

them on the sUAS.

An equivalent level of safety will be achieved by keeping these docu ments at the ground control point where the pilot flying the sUAS will have immediate access to them, to the extent they are applicable to the sUAS. The FAA has issued numerous exemptions to this regulation. A representative sample of other exceptions incl udes Exemption Nos.

9565, 9665, 9789, 9789A, 9797, 9797A, 9816A, and 10700.

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

These regulations require that an aircraft operator or owner “shall have that aircraft inspec ted as prescribed in subpart E of this part and shall between required inspections, except as provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and others shall inspect or maintain the airc raft in compliance with Part 43.

Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to the applicant. Maintenance will be accomplished by the operator pursuant to the flight manual and operating handbook as referenced in the Manual (See Sections 8.6 and 9). An equivalent level of safety will be achieved because these small UASs are very limited in size and will carry a small payload and operate only in restricted areas for limited

pe riods of time. If mechanical issues arise the UAS can land immediately and will be operating from no higher than 400 feet AGL. As provided in the Manual, the operator will ensure that the UAS is in working order prior to initiating flight, perform required maintenance, and keep a log of any maintenance performed. Moreover, the operator is the person most familiar with the

aircraft and best suited to maintain the a ircraft in an airworthy condition to provide the equivalent level of safety.Pursuant to 14 C.F.R. Part 11, the following summary is provided for publication in the Federal Register, should it be determined that publication is needed:

Applicant seeks an ex em ption from the following rules:

14 C.F.R. §21, subpart H; 14 C.F.R 45.23(b);14 C.F.R. §§ 61.113( a) & (b);91.7 (a); 91.9 (b) (2);91.103(b);91.109; 91.119; 91.121; 91.151(a);91.203(a) and (b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2); 91.409 (a) (2) and 91.417 (a) & (b) to operate commercially a small unmanned vehicle (55lbs or less) in motion picture and television operations.

Approval of exemptions allowing commercial operations of sUASs in the r eal e state, m arketing,

i nfrastructure and c onstruction i nspection and b usiness o perations will enhance safety by reducing risk. Conventional infrastructure and construction inspections and business operations, using jet or piston power aircraft, operate at extremely low altitudes just feet from the infrastructure being inspected and i n extreme proximity to people and structures; and present the risks associated with vehicles that weigh in the neighborhood of 4,000lbs, carrying large amounts of jet A or other fuel. Such aircraft must fly to and from the work location. In contrast, a

sUA S weighing fewer than 55 lbs. and powered by batteries eliminates virtually all of that risk given the reduced mass and lack of combustible fuel carried on board. The sUAS is carried to the worksite and not flown. The sUAS will carry no passengers or crew and, therefore, will not expose them to the risks associated with manned aircraft flights.

The operation of small UASs, weighing less than 55 lbs., conducted in the strict conditions outlined above, will provide an equivalent level of safety supporting the grant of the exemptions requested herein, including exempting the applicant from the requirements of Part 21 and allowing commercial operations. These lightweight aircraft operate at slow speeds, close to the ground, and in a sterile environment and, as a result, are far safer than conventional operations conducted with turbine helicopters operating in close proximity to the ground and people.

Privacy

All flights will occur over private or controlled access property with the property owner’s prior

consent and knowledge. Infrastructure and construction inspections and business operations will be performed for people who have also consented for work to be performed or otherwise have agreed to be in the area where UAS flight will take place.Conclusion

Satisfaction of the criteria provided in Section 333 of the Reform Act of 2012

– size, weight, speed, operating capabilities, proximity to airports and populated areas and operation within visual line of sight and national security

– provide more than adequate justification for the grant of the requested exemptions allowing commercial operation of applicant’s UAS in the infrastructure and construction inspections and bus iness operations industry pursuant to the Manual appended hereto.

Sincerely,

M atthew R. Engel

Owner Tree Top View Media

Appendix 1

• DJI Phantom 2

o See Attach ed Document:

 TREE TOP VIEW MEDIA

- Attachment 2

- Phantom 2 User Manual v1_4

. pdf

• DJI Phantom 3 Professional

o See Attached Document:

 TREE TOP VIEW MEDIA

- Attachment 3

- Phantom 3 Professional User Manual v1_2

. pdf

• D JI Inspire 1

o See Attached Document s :

 TREE TOP VIEW MEDIA

- Attachment 4

- Inspire 1 User Manual v1_2

. pdf

 TREE TOP VIEW MEDIA

- Attachment 5

- Inspire 1 Safety
Guidelines

. pdf

 TREE TOP VIEW MEDIA

– Attachment 6

- Inspire 1 Maintenance Manual V1_0

. pdf

• 3 DRobotics Solo

o See Attached Document:

 TREE TOP VIEW MEDIA

- Attachment 7

- 3DR Solo User Manual

Appendix 2 Please see the attached Operating Manual :

• TREE TOP VIEW MEDIA

- Attachment 1

- sUAS Operating Manual