Dan M. Hagin

DnL Strategies 1018 Natural Springs Way
Leland, NC 28451 (p) ( 910 ) 547

- 9808 (e) danh@itscarolinagolf.com

January 20 , 2016

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

Re: Exemption Request pursuant to Section 333 of FAA Reform Act and Title 14, Code of Federal Regulations (14CFR): §§ 21 subpart H; 45.23(b); 61.113 (a) and (b); 91.7(a); 91.9(b)(2); 91.103; 91.109; 91.119; 91.121; 91.151(b ); 91.203(a) and (b); 91.405(a);

9 1.407(a)(1); 91.409(a)( 1) and (2); and 91.417(a) and (b).

Dear Sir or Madam: Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (“the FMRA”) and 14 CFR Part 11

, Dan M. Hagin (DnL Stratagies)

, (referred to herein as “applicant”), PIC of small Unmanned Aircraft Systems (sUAS), hereby applies for an exemption from the listed Federal Aviation Regulations to allow commercial operation of its sUAS, so long as such operations are conducted within and under the conditions stipulated herein o r as may be established by the FAA as required by

Section 333.

Commercial operation of sUAS, as described herein, which are equipped with cameras and sensors, would operate in the following manner:

Public Benefits: The requested exemption would allow us to use the UAS for aerial image acquisition to support analysis of golf courses (and affiliated partners in marketing). General maintenance, water retention, water distribution, playability would all be enhanced. Typical applications would include, but ar e not limited to:

Aerial Photography Preventive maintenance of grounds Videography/Film making
Marketing

EducationThe inherent ability of the UAS to capture imagery from a low altitude including

oblique photos and video from several angles is complimentary but yet far more versatile than ground

- based or boom based imagery for analyzing golf course and their maintenance, as well as redesign and educating customers on the facilities. The applicant intends to use unmanned systems on golf courses t o enhance and market our products. The public will benefit as a result of this analysis through improved golf facilities. In addition, the golf industry is related to products, hotels, restaurants, theme parks, places of interest and applicate would work with these other industries to coordinate marketing efforts.

Aerial photography and/or video for public and/or private use including real estate,

architectu re, land surveying, agriculture, engineering, closed set television and motion picture filming , p ub lic events

, residential/commercial structures

, golf

courses, and providing live video feed to assist with search and rescue operations in cases of an emergency or natural disaster. All are part of the golf community.

Request: As described below, the requested exemption would permit the operation of sUAS under controlled conditions in the NAS that would be a) limited b) controlled c) predetermined and d) will provide safety enhancements to the already safe operations in the indu stry 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.”

The name, address, phone, and email of the applicant:

Dan M. Hagin 1018 Natural Springs Way
Leland, NC 28451 ( 910 ) 547

- 9808 danh@itscarolinagolf.com

Regulations from which the exemption is requested:

14 CFR Part 21 subpart H 14 CFR 45.23(b) 14 CFR 61.113(a)
14 CFR 91.7(a) 14 CFR 91.9(b)(2)

14 CFR 91.103

14 CFR 91.10914 CFR 91.119(c)

14 CFR 91.121 14 CFR 91.151(b) 14 CFR 91.203(a) and (b) 14 CFR 91.405(a)

14 CFR 91.407(a)(1) 14 CFR 91.409(a)(1) and (2) 14 CFR 91.417(a) and (b)

The sUASs the applicant will be using are multi

- rotor craft weighing no more than

55 lbs including payload. Under normal conditions, they operate at speeds of no more than 45 mph or 39 knots and have the ability to hover and move along a vertical and horizontal plane simultaneously. They will be operated in visual line of sight only and in ac cordance with all other local and federal laws.

Given the small size of the sUAS and the controlled environment provided, the proposed operations will adhere to the Reform Act’s safety requirements. The approval of this application presents no national se curity issues. Regarding the level of safety surrounding the proposed operations and the public benefit, reduction in environmental impacts, including but not limited to reduced emissions and noise, the grant of the requested exemption is in the public int erest. Accordingly, the applicant requests that the FAA grant the requested exemption with minimum delay.

THE UNMANNED AIRCRAFT (UAS):

 The UAS is lightweight (under 55lb. gross weight), battery operated multi

rotor copter that takes off and land vertical ly and has the ability to hover in one location during flight.

THE UAS INCLUDES:

 An on

- board flight computer with GPS navigation and location ability that receives signals for flight control from a ground

- based transmitter/controller.

An on

- board camer a or sensor package used to document physical and/or environmental
conditions of structures and the natural environment.

 An on

- board telemetry system that delivers flight data from the on

- board flight computer to the radio transmitter including altitude AGL, horizontal and vertical speed, compass direction of flight and direction back to its launch site.

 A 2.4GHz on

- board r adio transmitter that transmits live video from the on

- board camera plus all the flight data from the telemetry system described above.

THE GROUND STATION PART OF THE SYSTEM:

 A Pilot in Command (PIC) in operational control of a mission from beginning to end,

and who controls the UAS while in the air.

 A 2.4GHz radio transmitter/controller operated by the PIC to control the UAS while in flight. Ground Station (computer, tablet or smart phone based app) which receives and displays video and system telemet ry real time from the UAS.

PILOT IN COMMAND (PIC): The PIC will meet the requirements outlined in FAA Policy N 8900.227 Section 16 Personnel Qualifications. Additionally, the PIC will perform maintenance on the system and will complete a course of mainte nance instruction as part of their initial training.

I submit that the combination of the UAS light weight, flight performance and ability, fully qualified flight crew and strict operation under the guidelines established in 8900.227, and

under all of the Restrictions listed above, the FAA can have full confidence that the operation will be safe and in compliance.

AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY The operation limitations proposed for an equivalent or higher level of safety because operations will further enhance the safety of the persons and/or property using conventional aircraft. These limitations and conditions to which the applicant agrees to adhere to when conducting commercial operations under the FAA issued exemption as set forth in the Flight Operations Manual (FOM) include:

(Please see Exhibits I, II, III, IV, V for actual pre/post flight and flight log information)

1) The UA may not be operated at a speed exceeding 5 0 miles per hour). The exemption holder may use either groundspeed or calibrated airspeed to determine compliance with the 50 mph speed restriction. In no case will the UA be operated at airspeeds greater than the maximum UA operating airspeed recommended by the aircraft manufacturer. 2) The UA mu st be operated at an altitude of no more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL. 3) The UA must be operated within visual line of sight (VLOS) of the PIC at all times. This requires the PIC to be able to use human visio n unaided by any device other than corrective lenses, as specified on the PIC’s FAA

- issued airman medical

certificate or U.S. driver’s license. 4) The exemption and all documents needed to operate the UAS and conduct its operations in accordance with the conditions and limitations stated in the grant of exemption, are hereinafter referred to as the operating documents. The operating documents must be accessible during UAS operations and made available to the Administrator upon request. If a discrepancy exists between the

conditions and limitations in the exemption and the procedures outlined in the operating documents, the c onditions and limitations o f the exemption take precedence and must be followed. Otherwise, the PIC must follow the procedures as outlined in its operating documents. The PIC may update or revise its operating documents. It is the PIC ’s responsibility to track such revisions and

pre sent updated and revised documents to the Administrator or any lawenforcement official upon request. The PIC must also present updated and

revised documents if it petitions for extension or amendment to this grant of exemption. If the PIC determines that any update or revision would affect the

basis upon which the FAA granted the exemption, then the PIC must petition for an amendment to its grant of exemption. The FAA’s UAS Integration Office (AFS−80) may be contacted if questions arise regarding updates or revisions to the operating documents. 5) Any UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics, e.g., replacement of a flight critical component, must undergo a functional test flight prior to conducting further operations under this exemption. Functional test flights may only be conducted by a PIC and must remain at least 500 feet from other people. The functional test flight must be conducted in such a manner so as to not pose an undue hazard to persons and property. 6) The PIC is responsible for maintaining and inspecting the UAS to ensure that it i s in a condition for safe operation. 7) Prior to each flight, the PIC must conduct a pre

- flight inspection and determine the UAS is in a condition for safe flight. The pre

- flight inspection must account for all potential discrepancies, e.g., inoperable compo nents, items, or equipment. If the inspection reveals a condition that affects the safe operation of the UAS, the aircraft is prohibited from operati ng until the necessary maintenance has been performed and the UAS is found to be in a condition for safe fl ight. 8) The PIC must follow the UAS manufacturer’s maintenance; overhaul, replacement, inspection, and life limit requirements for the aircraft and aircraft

components. 9) Each UAS operated under the exemption must comply with all manufacturer safety bulletin s. 10) Under t he grant of exemption . The PIC must hold a current and valid U.S. driver’s license issued by a state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal government. 11) The PIC may not operate unless the PIC demonstrat es the ability to safely operate the UAS in a manner consistent with how the UAS will be operated under the exemption, including evasive and emergency maneuvers and maintaining appropriate distances from persons, vessels, vehicles and structures. PIC quali fication flight hours and currency must be logged in a manner consistent with 14 CFR § 61.51(b). Flights for the purposes of training

the PICs (training, proficiency, and experience

- building) and determining the PIC’s ability to safely operate the UAS in a manner consistent with how the UAS will be operated under the exemption are p ermitted under the terms of the exemption. However, training operations may only be conducted during dedicated training sessions. During training, proficiency, and experience

bui lding flights, all persons not essential for flight operations are considered nonparticipants, and the PIC must operate the UA with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.12) UAS operations may not be conducted during ni ght, 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. 13) The UA may not operate within 5 nautical miles of an airport reference poi nt (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) or for airports not denoted with an ARP, the center of the airport symbol as denoted on

the current FAA

- published aeronautical chart, unless a letter of agreement with that airport’s m anagement is obtained or otherwise permitted by a COA issued to the exemption holder. The letter of agreement with the airport management must be made available to the Administrator or any law enforcement offi cial

upon request. 14) The UA may not be operated less than 500 feet below or less than 2,000 feet horizontally from a cloud or when visibility is less than 3 statute miles from the

PIC. 15) For tethered UAS operations, the tether line must have colored pennants or

streamers attached at not more than 50 foot intervals beginning at 150 feet

above the surface of the earth and visible from at least one mile. This requirement for pennants or streamers is not applicable when operating exclusively below the top of and within 250 feet of any structure, so long as th e UA operation does not obscure the lighting of the structure. 16) If the UAS loses communications or loses its GPS signal, the UA must return to a

pre

- determined location within the private or controlled

- access property. 17) The PIC must abort the flight in the event of unpredicted obstacles or emergencies. 18) The PIC is prohibited from beginning a flight unless (considering wind and forecast weather conditions) there is enough available power for the UA to conduct the intended operation and to operate after that for at least 5 minutes or with the reserve power recommended by the manufacturer if greater. 19) Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All operations shall be conducted in accordance with an ATO

- issued COA. The exemption holder may apply for a new or amended COA if it intends to conduct operations that cannot be conducted under the terms of the enclosed COA. 20) All aircraft operated in accordance with the exemption must be identified by serial number, registered in accordan ce with 14 CFR part 47, and have identification (N−Number) markings in accordance with 14 CFR part 45, Subpart C. Markings must be as large as practicable. 21) Documents used by the PIC to ensure the safe operation and flight of the UAS and any documents requ ired 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. 22) The U A must remain clear and give way to all manned aviation operations and

activities at all times. 23) The UAS may not be operated by the PIC from any moving device or vehicle. 24) All Flight operations must be conducted at least 500 feet from all nonparticipating persons, vessels, vehicles, and structures unless:a) Barriers or structures are present that sufficiently protect nonparticipating persons from the UA and/or debris in the event of an accident. The PIC must ensure that nonparticipating persons remain under such protection. If a situation arises where nonparticipating persons leave such protection and are within 500 feet of the UA, flight operations must cease immediately in a manner ensuring the safety of nonparticipating persons; and b) The owner/controller of any vessels, vehicles or structures has granted permission for operating closer to those objects and the PIC has made a safety assessment of the risk of operating closer to those objects and determined that it does not present an un due hazard. c) The PIC, trainees

, or essential persons are not considered nonparticipating persons under this exemption. 25) All operations shall be conducted over private or controlled

- access property with permission from the property owner/controller or autho rized representative. Permission from property owner/controller or authorized representative will be obtained for each flight to be conducted. 26) 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 repor ted to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

. 27) For the purpose of closed

- set motion picture and television filming and production, the PIC must have a motion picture and television ope rations manual (MPTOM) as documented in the grant of exemption. 28) At least 3 days before aerial filming, the PIC of the UAS affected by the exemption must submit a written Plan of Activities to the local Flight Standards District Office (FSDO) with jurisdic tion over the area of proposed filming. The 3

- day notification may be waived with the concurrence of the FSDO. The plan of activities must include at least the following: a) Dates and times for all flights; b) Name and phone number of the PIC for the UAS aeria l filming conducted under the grant of exemption; c) Name and phone number of the person responsible for the on

- scene operation of the UAS; d) Make, model, and serial or N−Number of UAS to be used; e) Name and certificate number of UAS PICs involved in the aeria l filming; f) A statement that the PIC has obtained permission from property owners and/or local officials to conduct the filming production event; the list of those who gave permission must be made available to the inspector upon request; g) Signature of exem ption holder or representative; and h) A description of the flight activity, including maps or diagrams of any area, city, town, county, and/or state over which filming will be conducted and the altitudes essential to accomplish the operation. 29) Flight operat ions may be conducted closer than 500 feet from participating persons consenting to be involved and necessary for the filming production, as specified in the exemption holder’s MPTOM.Unless otherwise specified in the 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.

14 CFR Part 21, Subpart H: Airworthiness Certificates 14 CFR 91.203(a)(1) Subpart H, entitled 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 applicant, an exemption from Part 21 Sub part 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 33 of the Reform Act both authorize the FAA to exempt aircraft from the requirement f or an airworthiness certificate, upon consideration of the size, weight, speed, operational capability, and proximity to airports and populated areas of the particular sUAS. In all cases, an analysis of these criteria demonstrates that the sUAS operated wi thout 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 restrict ions and conditions proposed.

The sUAS to be operated her e under is less than 55 pounds fully loaded, carries neither a pilot nor passenger, carries no explosive materials or fla mmable liqui d fuels, and operates exclusively within a secured and designated area. Unlike other civil aircraft, operations under this exemption will be tightly controlled and

monito red by both the PIC and und er the requirements and in compliance with local public safety requirements. These safety enhancements provide a greater deg ree of safety to the public and property owners than con ventional operations conducted

with airworthiness certificates issu ed under 14 CFR Part 21, Subpart H. Lastly, applic ation of these same criteria demonstrates that there is no credible threat to

natio nal security posed by the sUAS, due to its size, speed of operation, location of operation, lack of explosive mat erials or flammable liquid fuels , and inability to carry a substantial external load.

14 CFR 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 certificat e d aircraft, the PIC must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches not more than 6 inches high, the words “limited,” “restricted,” “light

- sport,” “experimental,” or “provisional,” as applicable.

Even though the sUA S will have no airworthiness certificate, an exemption may be needed as the sUAS will have no entrance to the cabin, cockpit or pilot station on which the word “Experimental” can be placed. Given the size of the sUAS, two

- inch lettering will be impossible. All aircraft will have identification (N−Number)markings in accordance with 14 CFR part 45, Subpart C. Markings will be as large as

practicable.

14 CFR 61.113(a) Private Pilot Privileges and Limitations: Pilot in Command

Pursuant to 14 CFR 61.113(a), no person who holds a private pilot certificate may act as a pilot in command of an aircraft that is carrying passengers or property for compensation or hire. Our sUASs do not carry any pilots or passengers nor property therefore the ap plicant seeks an exemption to 14 CFR 61.113(a). The risks attendant to the operation of sUAS is far less than the risk levels inherent in the commercial

activit i es outlined in 14 CFR 61. I feel the operation and limitations sets forth in the FOM will equat e to the safe operation of the sUAS.

14 CFR 91.7(a) Civil Aircraft Airworthiness The regulation requires that no person may operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for the

aircraft , should this exemption be granted, no FAA regulatory standard will exist for determining airworthiness. Given the size of the aircraft for maintenance and use of safety checklists prior to each flight, an equivalent level of safety will be provided.

14 CFR 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 Section 21.5 of this chapter, unless there is available in the aircraft a current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or any combination thereof. The sUAS, given its size and configuration has no ability or place to carry such a fli ght 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 po int where the pilot flying the sUAS will have

immediate access to it.

14 CFR 91.103 Preflight Action This regulation requires each pilot in command to take certain actions before flight to ensure the safety of flight. As FAA approved rotorcraft flight ma nuals will not be provided for the aircraft an exemption will be needed. 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 FR 91.109 Flight Instruction

Section 91.109 provides that no person may operate a civil aircraft (except a manned free balloon) that is being used for flight instruction unless that aircraft has fully functioning dual controls. Small UAS 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 wit h out fullyfunctional dual controls for a number of aircraft and for flight instruction in

experimental aircraft . The equivalent level of safety is 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 CFR 91.119 Minimum Safe Altitudes Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119(d) allows helicopters to be operated at less than the minimums prescribed, provided the person opera ting the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. As this exemption is for a sUAS that is a helicopter and the exemption requests authority to operate at altitudes up to 400 feet AGL, an exemption may be needed to allow such operations. As set forth herein

, the sUAS will never operate at higher than 400 feet AGL with out a COA specifically authorizing an altitude above 400 feet AGL. The equivalent level of safety will be achieved given the size, weight and speed of the sUAS as well as the location where it is operated. In addition, the low

- altitude operations of the sUAS will ensure separation between these sUAS operations and the operations of conventional aircraft that must comply with Section 91.119.

14 CFR 9 1.121 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 depa rture.” 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 PIC

, pursuant to the safety check list and live flight data monitoring, confirmi ng the altitude of the launch site shown on the GPS altitude indicator before each flight.

14 CFR 91.151 (b) Fuel Requirements for Flight in VFR Conditions Section 91.151(b) requires rotorcraft pilots to plan at least a 20 minute fuel reserve. The battery powering the sUAS provides approximately 20 to 23 minutes of flight. To meet the reserve requirement in 14 CFR 91.151(b), sUAS flights would be limited

to less than 3 minutes. Given the limitations on the sUAS’s proposed flight area and

the location of its proposed operations within a predetermined area, a longer time frame for flight in VFR conditions is reasonable. The applicant believes that an exemption from 14 CFR 91.151(b) falls within the scope of prior exemptions. Operating the sUAS in a tightly controlled area with less than 20 minutes of reserve fuel does not engender the type of risks that Section 91.151(b) was intended to alleviate given the size and speed of the small UAS. Additionally, limiting sUAS flights to 3 minutes would greatly reduce the utility for which the exemption will be granted. The applicant believes that an equivalent level of safety can be achieved by prohibiting the PIC from beginning a flight unless (considering wind and forecast weather conditions) there is enough availa ble power for the sUAS to conduct the intended operation and to operate after that for at least 5 minutes or with the reserve power recommended by the manufacturer if greater.14 CFR 91.203(a) and (b) Carrying Civil Aircraft Certification and Registratio n

The regulation provides in pertinent part: (a) Except as provided in § 91.715, no person may operated a civil aircraft unless it has within it the following: (1) An appropriate and current airworthiness certificate... (b) No person may operate a civil a ircraft 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 t hat it is legible to

passengers or crew.

The sUAS fully loaded weighs no more than 55 pounds 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 documents at the ground control point where the pilot flying the sUAS wil l have immediate access to them, to the extent they are applicable to the sUAS.

14 CFR 91.405(a) ; 407(a)(1); 409(a)(2); 417(a) and (b) Maintenance Inspections These regulations require that an aircraft PIC or owner “shall have that aircraft inspected as prescribed in subpart E of this part and shall between required inspections, except as provided in paragraph (c ) of this section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and others shall inspect or maintain the aircraft in compliance with Par 43. Given that these sections and Part 43 apply only to aircraft with an airworthiness certi ficate, these sections will not apply to the applicant. Maintenance will be accomplished by the PIC pursuant to the flight manual and operating handbook. An equivalent level of safety will be achieved because these sUASs are very limited in size and will c arry a small payload and operate only in restricted areas for limited periods of time. If mechanical issues arise, the sUAS can land immediately and will be operating from no higher than 400

feet AGL. The PIC will ensure that the sUAS is in working order p rior to initiating flight, perform required maintenance, and keep a log of any maintenance performed. Moreover, the PIC is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivale nt level of safety.

An equivalent level of safety will be achieved because maintenance and inspections will be performed in accordance with the sUAS Manufacturer’s Manual, as referenced in the Aircraft Operations Manual (AOM). As provided in the FOM, the

PIC will ens u re that the sUAS is in working order prior to initiating flight and perform re q ui r ed maintenance needed.Small UAS information

sUAS’s to be used are as follows but not limited to providing they are within the scope of the exemption grante d by the FAA:

Links to serv ice manuals and safety features 1. DJI Phantom 3 Advanced (P3A) https://dl.djicdn.com/downloads/phantom_3/en/Phantom_3_Advanced_User_Man ual__V1.6.pdf

2. DJI Phantom 3 Pro (P3P) https://dl.djicdn.com/downloads/phantom_3/en/Phantom_3_Professional_User_M anual__V1.6.pdf



### See E xhibits I, II, III, IV, V