UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION WASHINGTON, DC

Regulatory Docket No. _______________

IN THE MATTER OF THE PETITION FOR EXEMPTION OF: David J. Tester FOR AN EXEMPTION SEEKING RELIEF FROM THE REQUIREMENTS OF TITLE 14 OF THE CODE OF FEDERAL REGULATIONS SECTIONS 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), AND 91.417(a) & (b) CONCERNING COMMERCIAL OPER
ATION OF DJI PHANTOM 2 VISION+ AND DJI INSPIRE 1 UNMANNED AIR
CRAFT SYSTEMS PURSUANT TO SECTION 333 OF THE FAA MODERNIZATION AND REFORM ACT OF 2012 (PUBLIC LAW 112-95)

Submitted on August, 7 2015 David J. Tester 12216 Chesterfield Ln. Oklahoma City, OK 73173 Tel: (405) 315-0197TABLE OF CONTENTS Page GLOSSARY OF ABBREVIATIONS...................................................................................3
SUMMARY...........................................................................................................................4
INTRODUCTION AND INTERESTS OF PETITIONER....................................................4
BACKGROUND....................................................................................................................5
BASIS FOR PETITION.........................................................................................................5
NAME AND ADDRESS OF PETITIONER.............................................................7 THE SPECIFIC SECTIONS OF 14 C.F.R. FROM WHICH David J. Tester SEEKS EXEMPTION.................................................................8 THE EXTENT OF RELIEF David J. Tester SEEKS AND THE REASON David J. Tester SEEKS THE RELIEF.........................11 THE REASONS WHY GRANTING David J. Tester’S REQUEST WOULD BE IN THE PUBLIC INTEREST .........................................................15 THE REASONS WHY GRANTING THE EXEMPTION WOULD NOT AD

VERSELY AFFECT SAFETY..........................................................................19 SUMMARY THAT CAN BE PUBLISHED IN THE FEDERAL REGISTER......34 ANY ADDITIONAL INFORMATION, VIEWS, OR ARGUMENTS AVAILABLE TO SUPPORT David J. Tester’S REQUEST.........34 CONCLUSION....................................................................................................................36 APPENDICES........................................................................................38

2GLOSSARY OF ABBREVIATIONS AGL Above Ground Level AOI Area of Interest ATC Air Traffic Control ATO Air Traffic Organization AV Aerial Vehicle CFR Code of Federal Regulations COA Certificate of Authorization FAA Federal Aviation Administration FAR Federal Aviation Regulation GCS Ground Control Station GPS Global Positioning System LOL Loss of Link NAS National Airspace System NOTAM Notice to Airman PIC Pilot In Command Section 333 FAA Modernization and Reform Act of 2012 (FMRA) Sec

tion 333 SO Safety Observer SOP Standard Operating Procedures UA Unmanned Aircraft UAS Unmanned Aircraft System VFR Visual Flight Rules VLOS Visual Line of Site VMC Visual Meteorological Conditions VTOL Vertical Takeoff and Landing

3SUMMARY David J. Tester seeks exemption from the requirements of 14 C.F.R §§ 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), to operate an Unmanned Aircraft System pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (FMRA). This exemption will permit David J. Tester to operate an Unmanned Aircraft System (UAS) for the commercial purpose of conducting aerial video and photography of construction sites, real estate, and landscape over certain areas of the United States.
INTRODUCTION AND INTERESTS OF THE PETITIONER David J. Tester provides its clients with expertise and knowledge in advanced tech

nologies and solutions to increase efficiency, productivity and effectiveness. David J. Tester has over 8 years of professional experience in Information Technology. He has over 3 years recreational/hobby experience in all aspects of aerial video and photography. The objective of David J. Tester’s aerial video and photography operations is to provide high quality imaging for a variety of commercial, public, and residential uses, specifically tar

geting:

• Sourcing GIS tagged aerial images for use in Computer Assisted Mass Ap

praisal (CAMA) systems.

• Motion Picture Filming

• Aerial acquisitions used for inspections of public and private structures.

4• Increase public knowledge of UAS and promote safe UAS operations.

• Search and Rescue operations BACKGROUND Unmanned Aircraft Systems: DJI Phantom 2 Vision+, DJI Inspire 1 UASs David J. Tester seeks an exemption to operate DJI systems for compensation or hire within the NAS. The DJI Phantom 2 Vision+ and DJI Inspire 1 are vertical takeoff and landing (VTOL) Unmanned Aircraft (UA) with a Ground Control Station (GCS) utilizing electronic tablet or smart phone systems. The DJI Phantom 2 Vision+ has a maximum gross weight of approximately 2 pounds 11 ounces, while having a length of 16 inches width of 16 inches, height of 8 inches, and a maximum speed of approximately 29 knots. The DJI Inspire 1 has a maximum gross weight of 6 pounds 7.5 ounces, a length of 17.3 inches, width of 17.7 inches, height of 11.8 inches, and a maximum speed of approximate

ly 42 knots. The DJI Phantom 2 Vision+ and DJI Inspire 1UAs are equipped with four main rotors; driven by Lithium Polymer battery powered electric motors. The DJI Phantom 2 Vision+ and DJI Inspire 1 UAs that will be operated by David J. Tester will be registered in accordance with 49 U.S.C. 44103, Registration of Aircraft , as well as 14 C.F.R Part 47, Aircraft Registration , and marked in accordance with 14 C.F.R. Part 45, Identification and Registration Marking

. BASIS FOR PETITION Petitioner, David J. Tester, pursuant to the provisions of the Federal Aviation Regu

lations (14 C.F.R. § 11.61) and the FAA Modernization and Reform Act of 2012 (FMRA), Section 333, Special Rules for Certain Unmanned Aircraft Systems , hereby petitions the

5Administrator to commercially operate the DJI Phantom 2 Vision+, DJI Inspire 1 UASs in the National Airspace System (NAS), and for an exemption from the requirements of 14 C.F.R §§ 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). In consideration of the speed, weight, size, and limited operating area associated with the unmanned aircraft and its operation, David J. Tester’s operation of DJI Phantom 2 Vision+ and DJI Inspire 1 UASs meets the conditions of FMRA Section 333 and therefore, will not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart
H. Accordingly, David J. Tester requests relief from Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), as these sections set forth requirements for maintenance that only apply to aircraft with an airworthiness certificate. David J. Tester submits that the requested relief is proper since an equivalent level of safety will be ensured. David J. Tester will use experienced personnel or technicians to perform maintenance, alterations, or preventive maintenance on the UASs using the meth

ods, techniques, and practices prescribed in the operating documents (i.e., Monthly Main

tenance Log, and DJI Phantom 2 Vision+ and DJI Inspire 1 Instruction Manual). Further

more, David J. Tester will document and maintain all maintenance records for the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs. Relief from certain requirements of Section 61.113(a) and (b), entitled Private pilot privileges and limitations: Pilot in command , is requested by David J. Tester to the extent necessary to allow a Pilot in Command (PIC) holding a private pilot or higher level certifi

6cate, as well as an airman medical certificate, and who has demonstrated, by meeting min

imum flight- hour and currency requirements, that the PIC is able to safely operate the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs in a manner consistent with this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicles and structures. David J. Tester seeks relief from Section 91.7(a), entitled Civil aircraft airworthi

ness , because the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs do not require an airwor

thiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. As such, David J. Tester submits that he will ensure that the DJI Phantom 2 Vision+ and DJI Inspire 1UASs are in an airworthy condition, prior to every flight, by determining that the UASs are in compliance with the operating documents (i.e., Monthly Maintenance Log, and DJI Phan

tom 2 Vision+ and DJI Inspire 1 Instruction Manual), and that the aircraft are in a condi

tion for safe flight. David J. Tester also seeks an exemption from the requirements of Section 91.121, entitled Altimeter Settings , as the DJI Phantom 2 Vision+ and DJI Inspire 1 UAs will not have a typical barometric altimeter onboard. However, altitude information of the DJI Phantom 2 Vision+ and DJI Inspire 1UAs will be provided to the PIC via Global Position

ing System (GPS) equipment and radio communications telemetry data link, which down

links from the UA to the GCS for active monitoring of the flight path. This altitude infor

mation, combined with David J. Tester’s operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs within visual line of sight, at or below 500 feet AGL, will ensure a level of safety equivalent to Section 91.121.

7Additionally, David J. Tester seeks an exemption from the requirements of Section 91.151(b), entitled Fuel requirements for flight in VFR conditions . David J. Tester submits that safety will not be affected by operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UAs during daylight hours in visual meteorological conditions (VMC) under visual flight rules (VFR), with enough battery power to fly for a total duration of approximately 13.5 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 4.5 minutes. In accordance with 14 C.F.R. § 11.81, David J. Tester provides the following in

formation in support of its petition for exemption:
A. Name And Address Of The Petitioner. The name and address of the Petitioner and point of contact is: David J. Tester 12216 Chesterfield Ln. Oklahoma City, OK 73173 73078 Tel: (405) 315-0197 Email: dave@1577productions.com B. The Specific Sections Of 14 C.F.R. From Which David J. Tester Seeks Exemption. 1. David J. Tester Seeks Exemption From The Requirements Of Section 61.113(a) And (b). Section 61.113, entitled Private pilot privileges and limitations: Pilot in command , subsections (a) and (b) prescribe the following, in relevant part: (a) No person who holds a private pilot certificate may act as a pilot in command (PIC) of an aircraft that is carrying passengers or property for compensation or hire; nor may that person, for compensation or hire, act as PIC of an aircraft. (b) A private pilot may, for compensation or hire, act as PIC of an aircraft in con

nection with any business or employment if— (1) The flight is only incidental to that business or employment; and

8(2) The aircraft does not carry passengers or property for compensation or hire. 2. David J. Tester Seeks Exemption From The Requirements Of Section 91.7(a). Section 91.7, entitled Civil aircraft airworthiness , subsection (a), states the follow

ing: (a) No person may operate a civil aircraft unless it is in an airworthy condition.
3. David J. Tester Seeks Exemption From The Requirements Of Section 91.121. Section 91.121, entitled Altimeter settings, subsection (a), states the following, in part: (a) Each person operating an aircraft shall maintain the cruising altitude or flight level of that aircraft, as the case may be, by reference to an altimeter that is set, when operating-- (1) Below 18,000 feet MSL, to-- (i) The current reported altimeter setting of a station along the route and within 100 nautical miles of the aircraft; (ii) If there is no station within the area prescribed in paragraph (a)(1)(i) of this section, the current reported altimeter setting of an appropriate available station; or (iii) In the case of an aircraft not equipped with a radio, the elevation of the departure airport or an appropriate altimeter setting available before departure. 4. David J. Tester Seeks Exemption From The Requirements Of Section 91.151(b). Section 91.151, entitled Fuel requirements for flight in VFR conditions , subsection (b), states the following:

(b) No person may begin a flight in a rotorcraft under VFR conditions unless (con

sidering wind and forecast weather conditions) there is enough fuel to fly to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 20 minutes.

95. David J. Tester Seeks Exemption From The Requirement Of Section 91.405(a). Section 91.405, entitled Maintenance required , subsection (a), states the following: Each owner or operator of an aircraft— (a) 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 sec

tion, have discrepancies repaired as prescribed in part 43 of this chapter[.] 6. David J. Tester Seeks Exemption From The Requirements Of Section 91.407(a)(1) Section 91.407, entitled Operation after maintenance, preventive maintenance, re

building, or alteration , subsection (a)(1), states the following: (a) No person may operate any aircraft that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless-- (1) It has been approved for return to service by a person authorized under § 43.7 of this chapter[.] 7. David J. Tester Seeks Exemption From The Requirements Of Sections 91.409(a)(1) And 91.409(a)(2). Section 91.409, entitled Inspections , subsection (a), states the following: (a) Except as provided in paragraph (c) of this section, no person may operate an aircraft unless, within the preceding 12 calendar months, it has had -- (1) An annual inspection in accordance with part 43 of this chapter and has been approved for return to service by a person authorized by § 43.7 of this chapter; or (2) An inspection for the issuance of an airworthiness certificate in accordance with part 21 of this chapter. 8. David J. Tester Seeks Exemption From The Requirements Of Sections 91.417(a) And 91.417(b). Section 91.417, entitled Maintenance records , subsections (a) and (b), state the fol

lowing: (a) Except for work performed in accordance with §§ 91.411 and 91.413, each reg

istered owner or operator shall keep the following records for the periods speci

fied in paragraph (b) of this section:

10(1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. The records must include-- (i) A description (or reference to data acceptable to the Administrator) of the work performed; and (ii) The date of completion of the work performed; and (iii) The signature, and certificate number of the person approving the air

craft for return to service. (2) Records containing the following information: (i) The total time in service of the airframe, each engine, each propeller, and each rotor. (ii) The current status of life-limited parts of each airframe, engine, pro

peller, rotor, and appliance. (iii) The time since last overhaul of all items installed on the aircraft which are required to be overhauled on a specified time basis. (iv) The current inspection status of the aircraft, including the time since the last inspection required by the inspection program under which the air

craft and its appliances are maintained. (v) The current status of applicable airworthiness directives (AD) and safety directives including, for each, the method of compliance, the AD or safety directive number and revision date. If the AD or safety directive involves recurring action, the time and date when the next action is re

quired. (vi) Copies of the forms prescribed by § 43.9(d) of this chapter for each ma

jor alteration to the airframe and currently installed engines, rotors, propellers, and appliances. (b) The owner or operator shall retain the following records for the periods pre

scribed: (1) The records specified in paragraph (a)(1) of this section shall be retained until the work is repeated or superseded by other work or for 1 year after the work is performed. (2) The records specified in paragraph (a)(2) of this section shall be retained and transferred with the aircraft at the time the aircraft is sold.

11(3) A list of defects furnished to a registered owner or operator under § 43.11 of this chapter shall be retained until the defects are repaired and the aircraft is approved for return to service. C. The Extent Of Relief David J. Tester Seeks And The Reason David J. Tester Seeks The Relief. 1. Extent Of Relief David J. Tester Seeks And The Reason David J. Tester Seeks Relief From Section 61.113(a) And (b). Relief from Section 61.113(a) and (b) entitled Private pilot privileges and limita

tions: Pilot in command , is requested to the extent necessary to allow a PIC holding a pri

vate pilot or higher level certificate, as well as a current and valid airman medical certifi

cate, and who has met certain flight-hour and currency requirements, to conduct the pro

posed UAS flight operations for compensation or hire. This relief is requested since the limitations set forth in Section 61.113(a) and (b) state that a private pilot may, for compensation or hire, act as PIC of an aircraft in connec

tion with any business or employment if: (1) The flight is only incidental to that business or employment; and (2) The aircraft does not carry passengers or property for compensa

tion or hire. As set forth more fully below, David J. Tester submits that an equivalent level of safety will be maintained because no PIC will be allowed to operate the DJI Phantom 2 Vision+ UAS or DJI Inspire 1 UAS unless that PIC has met certain flight-hour and curren

cy requirements, demonstrating that the PIC is able to safely operate either the DJI Phan

tom 2 Vision+ or DJI Inspire 1 UAS in a manner consistent with the operations specifica

tions as described in this exemption, including evasive and emergency maneuvers, as well as maintaining appropriate distances from people, vessels, vehicles and structures.

12Further, David J. Tester submits that all flights of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, conducted by the PIC pursuant to the grant of this Petition: (1) will be incidental to David J. Tester’s business; and (2) will not carry passengers or property for compensation or hire.
2. Extent Of Relief David J. Tester Seeks And The Reason David J. Tester Seeks Relief From Section 91.7(a). Relief from Section 91.7(a) entitled Civil aircraft airworthiness , is requested to the extent required to allow David J. Tester to determine that the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs are in airworthy condition prior to every flight by ensuring that the UAS is in compliance with the operating documents (i.e., the David J. Tester Aerial Opera

tions Manual, Monthly Maintenance Log, and DJI Phantom 2 Vision+ and DJI Inspire 1 Instruction Manual). David J. Tester seeks the requested relief because the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs do not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. Therefore, David J. Tester will ensure that the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs are in airworthy condition based upon its compliance with the operating documents (i.e., Monthly Maintenance Log, and DJI Phantom 2 Vision+ and DJI Inspire 1 Instruction Manual) prior to every flight, and further, determine that the air

craft are in condition for safe flight, as stated in the conditions and limitations below.
3. Extent Of Relief David J. Tester Seeks And The Reason David J. Tester Seeks Relief From Section 91.121. Relief from Section 91.121, entitled Altimeter settings, may be required to allow flight operations of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, which utilize a

13barometric pressure sensor, GPS equipment, and a radio communications telemetry data link to downlink altitude information from the UA to the PIC at the ground control station (GCS). Since the FAA requires that any altitude information concerning UAS operations be reported to air traffic control (ATC) in feet above ground level (AGL), David J. Tester seeks the requested relief because the DJI Phantom 2 Vision+ and DJI Inspire 1 UA’s al

timeter may be set on the ground to zero feet AGL, rather than the local barometric pres

sure or field altitude, before each flight. Considering the limited altitude of the proposed operations, relief from 14 CFR 91.121 is sought to the extent necessary to comply with the applicable conditions and limi

tations stated below. As more fully set forth herein, an equivalent level of safety will be maintained since the DJI Phantom 2 Vision+ and DJI Inspire 1 UAs are equipped with a barometric pressure sensor and GPS equipment, which automatically ensures that a ground level pressure setting will be established prior to each flight, and provides the PIC with al

titude information of the UA on the heads-up display of the GCS.
4. Extent Of Relief David J. Tester Seeks And The Reason David J. Tester Seeks Relief From Section 91.151(b). Relief from Section 91.151(b) entitled Fuel requirements for flight in VFR condi

tions, is requested to the extent required to allow flights of the battery powered DJI Phan

tom 2 Vision+ and DJI Inspire 1 UAs during daylight hours in visual meteorological condi

tions (VMC), under visual flight rules (VFR), for a total duration of 13.5 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 4.5 minutes. David J. Tester seeks the requested relief because without an exemption

14from Section 91.151(b), the flight time duration of the battery powered DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UAs will severely constrain the practicality of any aerial video or still photo flight operations that David J. Tester proposes to conduct pursuant to this Peti

tion. Significantly, as set forth below, the technical specifications of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, the DJI Phantom 2 Vision+ and DJI Inspire 1 operating documents, and David J. Tester’s proposed operating limitations, ensure that David J. Tester will safely operate the battery powered DJI Phantom 2 Vision+ and DJI Inspire 1 UAs during daylight hours in visual meteorological conditions (VMC), under visual flight rules (VFR), with enough battery power to fly for a total duration of 13.5 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 4.5 minutes.
5. Extent Of Relief David J. Tester Seeks And The Reason David J. Tester Seeks Relief From Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), And 91.417(a) & (b). Since Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) only apply to aircraft with an airworthiness certificate, David J. Tester requests relief from these Sections because the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs do not require airworthiness certificates. As set forth more fully below, the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs meet the conditions of FMRA Section 333 for operation without an airworthiness certificate. Accordingly, David J. Tester will use trained technicians to per

form maintenance, alterations, or preventive maintenance on the UASs using the methods, techniques, and practices prescribed in the UAS operating documents (i.e., the David J.

15Tester Aerial Operations Manual, Monthly Maintenance Log, and DJI Phantom 2 Vision+ and DJI Inspire 1 Instruction Manual). Furthermore, David J. Tester will document and maintain all maintenance records for the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs. D. The Reasons Why Granting David J. Tester’s Request Would Be In The Public In
terest; That Is, How It Would Benefit The Public As A Whole. Granting the present Petition will further the public interest by allowing David J. Tester to safely, efficiently, and economically perform aerial video and photography of construction sites, real estate, and landscape over certain areas of the United States. Additionally, use of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs will de

crease congestion of the NAS, reduce pollution, and provide significant benefits to the economy. Notably, the benefits of David J. Tester’s proposed operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs will be realized without implicating any privacy issues. 1. The Public Will Benefit From Decreased Congestion Of The NAS. The DJI Phantom 2 Vision+ and DJI Inspire 1 UAs are battery powered and serve as a safe, efficient, and economical alternative to the manned aircraft traditionally utilized to obtain aerial imagery. By reducing the amount of manned aircraft needed to perform aerial acquisitions, an exemption allowing the use of a DJI Phantom 2 Vision+ or DJI In

spire 1 UAS would reduce the amount of manned aircraft in the NAS, reduce noise and air pollution, as well as increase the safety of life and property in the air and on the ground. Furthermore, by reducing the number of manned aircraft operating in the NAS, congestion around airports caused by arriving and departing aircraft will be reduced. The DJI Phantom 2 Vision+ and DJI Inspire 1 UAs do not require an airport to takeoff or land.

16Likewise, a reduction of manned aircraft conducting aerial video and photography mis

sions would result in fewer aircraft that must be handled by air traffic control during the ground, takeoff, departure, arrival, and landing phases of flight operations. 2. The Public Will Benefit From The Safety And Efficiency Of The DJI Phan
tom 2 Vision+ and DJI Inspire 1 UASs. Conducting aerial acquisitions with the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, instead of manned aircraft, will greatly benefit the public by drastically reducing the levels of air and noise pollution generated during traditional aerial video and still photog

raphy flight operations. By using battery power and electric motors, the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs produce no air pollution, and is the most viable environmen

tally conscious alternative to the cabin class, six cylinder internal combustion engine air

craft that are typically utilized for aerial video and photography, while burning approxi

mately 20-30 gallons per hour of leaded aviation fuel. The DJI Phantom 2 Vision+ and DJI Inspire 1 UAs, while reducing the carbon footprint of aerial acquisitions, also eliminates noise pollution, as the UAs are propelled by battery powered electric motors, rather than an internal combustion engine. By using the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs to perform aerial ac

quisitions, the substantial risk to life and property in the air and on the ground, which is usually associated with traditional manned aircraft flight operations, will be substantially reduced or completely eliminated. Aside from the lack of flight crew members located on

board the aircraft, the DJI Phantom 2 Vision+ and DJI Inspire 1 UAs (weighing approxi

mately 2 pounds 11 ounces and 6 pounds 7.5 ounces respectively, at their maximum gross

17weights with lengths of 16 inches and 17.3 inches respectively, widths of 16 inches and 17.7 inches respectively, and with no fuel on board), has less physical potential for collat

eral damage to life and property on the ground, and in the air, compared to the manned air

craft that typically conduct similar operations (weighing approximately 6,000 pounds with a wingspan of approximately 42 feet, a length of 34 feet, and a fuel capacity of 180 gal

lons). 3. Performing Aerial Video and Photography Operations With The DJI Phan
tom 2 Vision+ and DJI Inspire 1 UASs Will Benefit The Economy. In addition to being safe and efficient, the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs are also an economical alternative to using manned aircraft to conduct similar aerial operations. As such, operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs will allow United States based companies, like David J. Tester, to remain competitive and con

tribute to growth of the U.S. economy. Specifically, with the rising cost of aviation fuel and the Environmental Protection Agency (“EPA”) regulatory actions phasing out leaded avia

tion fuels, U.S. owned and operated companies must adopt new and alternative technology in order to remain competitive. Operating the battery powered DJI Phantom 2 Vision+ and DJI Inspire 1 UASs is one such technology that not only allows companies greater opera

tional flexibility compared to manned aircraft, but provides such flexibility without the high operational cost of a traditional manned aircraft. By operating the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, companies such as David J. Tester, can remain competitive and profitable, and therefore, provide greater job stability to employees and contractors, which will ultimately contribute to growth of

18the U.S. economy. Improved financial performance of U.S. companies, through commer

cial use of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, provides a stable workforce that increases consumer spending; improves local, state, and federal tax revenues; and al

lows companies to invest in research and development in order to remain competitive both in the United States and abroad. 4. There Are No Privacy Issues. Similar to the manned aerial acquisition flight operations that have been conducted for decades, David J. Tester’s proposed operation of the DJI Phantom 2 Vision+ and DJI In

spire 1 UASs will not implicate any privacy issues. Specifically, the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs will be operated only in compliance with operating docu

ments (i.e., the David J. Tester Aerial Operations Manual, Monthly Maintenance Log, and DJI Phantom 2 Vision+ and DJI Inspire 1 Instruction Manual) which requires property owner involvement as well as local law enforcement notification, and in accordance with the Federal Aviation Regulations, including the minimum altitude requirements of 14 C.F.R. § 91.119. E. The Reasons Why Granting The Exemption Would Not Adversely Affect Safety, Or How The Exemption Would Provide A Level Of Safety At Least Equal To That Provided By The Rule From Which David J. Tester Seeks Exemption. 1. Reasons Why The DJI Phantom 2 Vision+ and DJI Inspire 1 UAs Meet The Conditions Of The FAA Modernization and Reform Act of 2012 (FMRA) Section 333. In consideration of the size, weight, speed, and limited operating area associated with the unmanned aircraft and its operation, David J. Tester’s operation of the DJI Phan

19tom 2 Vision+ and DJI Inspire 1 UASs meet the conditions of FMRA Section 333, and will not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. Section 333 provides authority for a UAS to operate without airworthiness certifi

cation and sets forth requirements for considering whether a UAS will create a hazard to users of the NAS or the public, or otherwise pose a threat to national security. Specifically, FMRA Section 333 states the following, in part: (a) In General.--Notwithstanding any other requirement of this subtitle, and not later than 180 days after the date of enactment of this Act, the Secretary of Transportation shall determine if certain unmanned aircraft systems may oper

ate safely in the national airspace system before completion of the plan and rulemaking required by section 332 of this Act or the guidance required by sec

tion 334 of this Act. (b) Assessment of Unmanned Aircraft Systems.--In making the determination under subsection (a), the Secretary shall determine, at a minimum-- (1) which types of unmanned aircraft systems, if any, as a result of their size, weight, speed, operational capability, proximity to airports and populated areas, and operation within visual line of sight do not create a hazard to users of the national airspace system or the public or pose a threat to national security; and (2) whether a certificate of waiver, certificate of authorization, or airwor

thiness certification under section 44704 of title 49, United States Code, is required for the operation of unmanned aircraft systems identified under paragraph (1). (c) Requirements for Safe Operation.--If the Secretary determines under this sec

tion that certain unmanned aircraft systems may operate safely in the national airspace system, the Secretary shall establish requirements for the safe opera

tion of such aircraft systems in the national airspace system. In seeking this exemption, David J. Tester submits that the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs can operate safely in the NAS pursuant to FMRA Section 333, as

20demonstrated by: (a) the characteristics of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs; (b) the pilot certification requirement; and (c) the specific operating limitations. a. The Specifications Of The DJI Phantom 2 Vision+ and DJI Inspire 1 UASs Demonstrate Its Safe Characteristics. The DJI Phantom 2 Vision+ and DJI Inspire 1 UASs do not create a hazard to users of the NAS or the public, or otherwise pose a threat to national security considering its size, weight, speed, and operational capability. i. Technical Specifications Of The DJI Phantom 2 Vision+ and DJI In
spire 1 UASs. The technical specifications of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs are set forth by the DJI Phantom 2 Vision+ and DJI Inspire 1 Specifications and Data Sheet, attached hereto as Exhibit A and B. ii. The DJI Phantom 2 Vision+ and DJI Inspire 1 UASs Autonomous Flight And Navigation Modes Enable The UASs To Remain Within A Defined Operational Area. The DJI Phantom 2 Vision+ and DJI Inspire 1 UASs may be operated in both man

ual and fully autonomous flight modes. A complete description of the flight and naviga

tional modes of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs is provided at pages 25-35 of the DJI Phantom 2 Vision+ and pages 12-16 and 45-50 of the DJI Inspire 1 User Manuals, attached hereto as Exhibit C and D. iii. The DJI Phantom 2 Vision+ and DJI Inspire 1 UASs Are Designed For Automatic Return To Home Point Or Hover In The Event Of Loss Of The Control Link Or Navigation. When the Control Link is lost, the DJI Phantom 2 Vision+ and DJI Inspire 1 UAs will remain stationary, in flight, for 3 seconds or more. If, after 3 seconds, the DJI Phantom

212 Vision+ and DJI Inspire 1 UAs do not reacquire control link data from the GCS, the UAs will assume that the Control Link is lost and the UAs will return to the home position (i.e., failsafe mode) via GPS, and will descend to the takeoff position and shutdown. A complete description of the Failsafe Functions of the DJI Phantom 2 Vision+ UAS are set forth at pages 27 through 29 and for the DJI Inspire 1 at pages 13 through 15 of the DJI Phantom 2 Vision+ and DJI Inspire 1 User Manuals, attached hereto as Exhibit C and D. iv. The DJI Phantom 2 Vision+ and DJI Inspire 1 GCS And Its Opera
tion. A complete description of the operation and specifications of the DJI Phantom 2 Vision+ and DJI Inspire 1 GCS and flight control software is provided at pages 32 through 43 of the DJI Phantom 2 Vision+ User Manual and pages 40 through 47 of the DJI Inspire 1 User Manual. DJI Phantom 2 Vision+ and DJI Inspire 1 User Manuals are attached here

to as Exhibits C and D. b. Flight Operations Of DJI Phantom 2 Vision+ and DJI Inspire 1 UASs Are Limited To The Line Of Sight Of A Certificated Pilot in Command With A Safety Observer. David J. Tester will only utilize certificated pilots who possess a current and valid airman medical certificate to act as a pilot in command (PIC) of the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs. Additionally, a safety observer will assist all pilots during flight time. c. Flights Of DJI Phantom 2 Vision+ and DJI Inspire 1 UASs Will Be Con
ducted Pursuant To Specific Operating Limitations.

22In seeking this exemption, David J. Tester proposes to commercially operate DJI Phantom 2 Vision+ and DJI Inspire 1 UASs for the special purpose of conducting aerial video and photography over certain areas of United States, pursuant to the following spe

cific operating limitations: 1. Operations authorized by this grant of exemption will be limited to the following aircraft described in the operating documents, rotorcraft UASs weighing less than 55 pounds maximum gross weight: DJI Phantom 2 Vision+ and DJI Inspire 1 Unmanned Aircraft Systems. Proposed operations of any other aircraft will re

quire a new petition or a petition to amend this grant. 2. UAS operations under this exemption will be limited to conducting operations for the purpose of aerial video and photography. 3. The UAs may not be flown at an indicated airspeed exceeding 20 knots. 4. The UA must be operated at an altitude of no more than 500 feet above ground level (AGL), as indicated by the procedures specified in the operating docu

ments unless a special request is made and approved by ATC. All altitudes re

ported to ATC must be in feet AGL. 5. The UAs must be operated within visual line of sight (VLOS) of the PIC at all times. This requires the PIC to be able to use human vision unaided by any de

vice other than corrective lenses, as specified on the PIC’s FAA-issued airman medical certificate. 6. The use of first person view (FPV) by the PIC or safety observer (SO) is not permitted. 7. All operations must utilize a safety observer (SO). The SO may be used to satisfy the VLOS requirement as long as the PIC always maintains VLOS capability. The SO and PIC must be able to communicate verbally at all times. Electronic messaging or texting is not permitted during flight operations. The PIC must be designated before the flight and cannot transfer his or her designation for the du

ration of the flight. The PIC must ensure that the SO can perform the functions prescribed in the operating documents. 8. The SO must not perform any other duties beyond assisting the PIC with seeing and avoiding other air traffic and other ground based obstacles/obstructions and is not permitted to operate the camera or other instruments.
239. The operating documents and the grant of exemption must be accessible during UAS operations and made available to the Administrator upon request. If a dis

crepancy exists between the conditions and limitations contained in the grant of exemption and the procedures outlined in the operating documents, the condi

tions and limitations contained in the grant of exemption take precedence and must be followed. Otherwise, the operator must follow the procedures as out

lined in its operating documents. The operator may update or revise its operating documents. It is the operator’s responsibility to track such revisions and present updated and revised documents to the Administrator upon request. The operator must also present updated and revised documents if it petitions for extension or amendment to the grant of exemption. If the operator determines that any update or revision would affect the basis upon which the FAA granted the exemption, then the operator must petition for amendment to its grant of exemption. The FAA’s UAS Integration Office (AFS-80) may be contacted if questions arise re

garding updates or revisions to the operating documents. 10. Prior to each flight the PIC must inspect the UAS to ensure that it is in a condi

tion for safe flight. If the inspection reveals a condition that affects the safe op

eration of the UAS, the aircraft is prohibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight. The Ground Control Station must be included in the preflight in

spection. All maintenance and alterations must be properly documented in the aircraft records. 11. Any UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics, e.g. replacement of a flight critical compo

nent, must undergo a functional test flight. The PIC who conducts the function

al test flight must make an entry in the aircraft records. 12. The pre-flight inspection must account for all potential discrepancies, e.g. inop

erable components, items, or equipment, not already covered in the relevant sections of the operating documents. 13. The operator must follow the UAS manufacturer’s aircraft/component, mainte

nance, overhaul, replacement, inspection, and life limit requirements. 14. The operator must carry out its maintenance, inspections, and record keeping requirements, in accordance with the operating documents. Maintenance, in

spection, 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 authorized person returning the UAS to service.
2415. Each UASs operated under this exemption must comply with all manufacturer Safety Bulletins. 16. The authorized person must make an entry in the aircraft record of the correc

tive action taken against discrepancies discovered between inspections. 17. The PIC must possess at least a private pilot certificate and at least a current third- class medical certificate. 18. The operator may not permit any PIC to operate unless the PIC meets the opera

tor’s qualification criteria and demonstrates the ability to safely operate the UAS in a manner consistent with how the UAS will be operated under the ex

emption, including evasive and emergency maneuvers and maintaining appro

priate distances from persons, vessels, vehicles and structures. PIC qualification flight hours must be logged in a manner consistent with 14 C.F.R. § 61.51(b). Flights for the purposes of training the operator’s PICs are permitted under the terms of the exemption. However, training operations may only be conducted during dedicated training sessions. During training, proficiency, and experi

ence-building flights, all persons not essential for flight operations are consid

ered nonparticipants, and the PIC must operate the UA with appropriate dis

tance from nonparticipants in accordance with 14 C.F.R. § 91.119. 19. UAS operations may not be conducted during night, as defined in 14 C.F.R. § 1.1. All operations must be conducted under visual meteorological conditions (VMC). If flight at night is required, a special request will be made at the FAA office closest to proposed area of operations. Flights under special visual flight rules (SVFR) are not authorized. 20. The UA 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 agree

ment with that airport’s management is obtained, and the operation is conducted in accordance with a NOTAM as required by the operator’s COA. The letter of agreement with the airport management must be made available to the Adminis

trator upon request. 21. 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.22. If the UA loses communications or loses its GPS signal, it must return to a predetermined location within the planned operating area and land or be recovered in accordance with the operating documents.
2523. The PIC must abort the flight in the event of unpredicted obstacles or emergen

cies in accordance with the operating documents. 24. The PIC is prohibited from beginning a flight unless (considering wind and forecast weather conditions) there is enough power to fly at normal cruising speed to the intended landing point and land the UA with 25% battery power remaining. 25. The operator must obtain an Air Traffic Organization (ATO) issued Certificate of Waiver or Authorization (COA) prior to conducting any operations under the grant of exemption. This COA will also require the operator to request a Notice to Airman (NOTAM) not more than 72 hours in advance, but not less than 48 hours prior to the operation. All operations shall be conducted in accordance with airspace requirements in the ATO issued COA including class of airspace, altitude level and potential transponder requirements. 26. All aircraft operated in accordance with the exemption must be identified by serial number, registered in accordance with 14 C.F.R. part 47, and have identi

fication (N- Number) markings in accordance with 14 C.F.R. part 45, Subpart C. Markings must be as large as practicable. 27. Before conducting operations, the radio frequency spectrum used for operation and control of the UA must comply with the Federal Communications Commis

sion (FCC) or other appropriate government oversight agency requirements. 28. The documents required fewer than 14 C.F.R. 91.9 and 91.203 must be avail

able to the PIC at the Ground Control Station of the UAS any time the UAS is operating. These documents must be made available to the Administrator or any law enforcement official upon request. 29. The UA must remain clear and yield the right of way to all manned aviation op

erations and activities at all times. 30. The UAS may not be operated by the PIC from any moving device or vehicle. 31. Flight operations must be conducted at least 500 feet from all nonparticipating persons (persons other than the PIC, SO, operator trainees or essential 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 opera

tor must ensure that nonparticipating persons remain under such protec

26tion. If a situation arises where nonparticipating persons leave such pro

tection and are within 500 feet of the UA, flight operations must cease immediately and/or; b. The aircraft is operated near vessels, vehicles or structures where the owner/controller of such vessels, vehicles or structures has granted per

mission and the PIC has made a safety assessment of the risk of operat

ing closer to those objects and determined that it does not present an un

due hazard, and; c. Operations nearer to the PIC, SO, operator trainees or essential persons do not present an undue hazard to those persons per § 91.119(a). 32. All operations shall be conducted over private or controlled-access property with permission from the land owner/controller or authorized representative. Permission from land owner/controller or authorized representative will be ob

tained for each flight to be conducted. 33. Any incident, accident, or flight operation that transgresses the lateral or verti

cal boundaries of the operational area as defined by the applicable COA must be reported to the FAA's UAS Integration Office (AFS-80) within 24 hours. Accidents must be reported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

. 2. Reasons Why An Exemption From The Requirements Of Section 61.113(a) And (b) Would Not Adversely Affect Safety. David J. Tester submits that the equivalent level of safety established by Section 61.113(a) and (b) will be maintained because no PIC will be allowed to operate the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs unless that PIC has demonstrated, by meeting minimum flight-hour and currency requirements, that the PIC is able to safely operate the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS in a manner consistent with the exemption, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicles and structures.

27Considering David J. Tester’s proposed area of operations, and the operating limita

tions set forth-above; the parallel nature of private pilot aeronautical knowledge require

ments to those of commercial pilot requirements (See Exemption No. 11062); and the air

manship skills necessary to safely operate the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS, David J. Tester submits that the additional manned airmanship experience of a com

mercially certificated pilot would not correlate to the airmanship skills necessary for David J. Tester’s specific proposed flight operations. The FAA has previously granted relief from Section 61.113(a) and (b) specific to UAS, in circumstances similar, in all material respects, to those presented herein (e.g. Ex

emption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 11136, 11138, 11150, 11153, 11156, 11158, 11159, 11160, 11161). David J. Tester will not allow any PIC to operate the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS unless that PIC has demonstrated, by meeting minimum flight-hour re

quirements or the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS training and currency re

quirements, that the PIC is able to safely operate the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS in a manner consistent with this exemption, including evasive and emergency ma

neuvers and maintaining appropriate distances from people, vessels, vehicles and struc

tures. Specifically, the PIC must have accumulated and logged, in a manner consistent with 14 C.F.R. § 61.51(b), 25 hours of total time as a UAS rotorcraft pilot (with a mini

mum of 5 hours of those hours as a UAS pilot operating the same make and model of UAS to be used for operations under the exemption). In addition to the hour requirements, the

28PIC must accomplish 3 takeoffs and landings in the preceding 90 days (for currency pur

poses). As in Exemption Nos. 11062, 11138, and 11153, prior documented flight experi

ence that was obtained in compliance with applicable regulations will ensure an equivalent level of safety during David J. Tester’s proposed operations. The Administrator has held that prior documented flight experience that was obtained in compliance with applicable regulations would ensure safe operations, stating as follows: In Exemption No. 11062, the FAA required that prior to conducting operations for the purpose of motion picture filming (or similar operations), the PIC must have accumulated and logged, in a manner consistent with 14 CFR 61.51(b), 25 hours of total time as a UAS rotorcraft pilot including at least 10 hours logged as a UAS pi

lot with a multi-rotor UAS. Prior to operations under Exemption No. 11062, the PIC must also have accumulated and logged a minimum of 5 hours as a UAS pilot operating the same make and model of UAS to be used for operations under the exemption. For clarification, the FAA considers these minimum hour requirements to be inclusive rather than additive; i.e. 5 hours make and model time may be in

cluded in the 10 hours of multi-rotor time and the 10 hours may be included in the total 25 hours of UAS rotorcraft time. In addition to the hour requirements, the PIC must accomplish 3 takeoffs and landings in the preceding 90 days (for currency purposes). The FAA finds that at a minimum, the flight-hour requirements in Ex

emption No. 11062 are appropriate to practice and build proficiency in the skills necessary to safely conduct the petitioner’s proposed operations. The FAA also finds that prior documented flight experience that was obtained in compliance with applicable regulations would satisfy this requirement. Training, proficiency, and experience-building flights can also be conducted under the grant of exemption toaccomplish the required flight time. During training, proficiency, and experiencebuilding flights the PIC is required to operate the UA with appropriate distances in accordance with 14 C.F.R 91.119. Exemption No. 11138 at page 15. Accordingly, David J. Tester will ensure safe operations by not allowing any PIC to operate the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS unless that PIC has demonstrat

ed, by meeting minimum flight-hour and currency requirements, that the PIC is able to

29safely operate the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS in a manner consistent with the exemption, including evasive and emergency maneuvers and maintaining appro

priate distances from people, vessels, vehicles and structures. 3. Reasons Why An Exemption From The Requirements Of Section 91.7(a) Would Not Adversely Affect Safety. The equivalent level of safety established by Section 91.7(a) will be maintained because prior to every flight, David J. Tester will ensure that the DJI Phantom 2 Vision+ or DJI Inspire 1 UAS is in an airworthy condition based upon the UAS’s compliance with its operating documents and as stated in the conditions and limitations herein. Additionally, the FAA has previously granted relief from Section 91.7(a) specific to UAS, in circumstances similar, in all material respects, to those presented herein (e.g. Ex

emption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 4. Reasons Why An Exemption From The Requirements Of Section 91.121 Would Not Adversely Affect Safety. The equivalent level of safety established by Section 91.121 will be maintained be

cause the altitude information of the DJI Phantom 2 Vision+ and DJI Inspire 1 UAs will be provided to the PIC via GPS equipment and a radio communications telemetry data link, which downlinks from the UA to the GCS for active monitoring of the flight path and alti

tude. This altitude information, combined with David J. Tester’s operation of the DJI Phan

tom 2 Vision+ and DJI Inspire 1 UAs within visual line of sight, at or below 500 feet AGL, will ensure a level of safety equivalent to Section 91.121. The altitude information will be

30generated by GPS equipment installed onboard the aircraft. Prior to each flight, a zero alti

tude initiation point is automatically established by the UASs at ground level. The FAA has previously granted relief from Section 91.121 specific to UAS, in cir

cumstances similar, in all material respects, to those presented herein (e.g. Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11112, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 5. Reasons Why An Exemption From The Requirements Of Section 91.151(b) Would Not Adversely Affect Safety. A grant of this exemption would ensure an equivalent level of safety established by 14 C.F.R. Section 91.151(b) as a result of (1) the technical specifications of the DJI Phan

tom 2 Vision+ and DJI Inspire 1 UASs; (2) the limitations on the proposed flight opera

tions; and (3) the location of the proposed flight operations. Accordingly, David J. Tester will ensure that it will safely operate the battery powered DJI Phantom 2 Vision+ and DJI Inspire 1 UAs during daylight hours in VFR conditions, with enough battery power to fly for a total duration of 13.5 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 4.5 minutes. Here, as in Exemption No. 11109, the technical specifications of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs; the limitations on the proposed flight operations; and the location of the proposed operations, will ensure an equivalent level of safety established by 14 C.F.R. Section 91.151(b). Furthermore, safety will be ensured as the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs provide audible and visual warnings to the PIC at the GCS when the UAs experiences low battery voltage, the first warning occurring at approximate

31ly 33% remaining battery power, and again at approximately 10% remaining battery pow

er. At the critically low battery level, the DJI Phantom Vision+ and DJI Inspire 1 UASs will descend and land automatically. Significantly, previous exemptions granted by the FAA concerning Section 91.151 establish that safety is not adversely affected when the technical characteristics and operat

ing limitations of the UAS are considered. Relief has been granted for manned aircraft to operate at less than the minimums prescribed in Section 91.151, including Exemption Nos. 2689, 5745, and 10650. Moreover, the FAA has previously granted relief from Section 91.151 specific to UAS, in circumstances similar, in all material respects, to those present

ed herein (e.g. Exemption Nos. 8811, 10808, 10673, 11042, 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 6. Reasons Why An Exemption From The Requirements Of Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), And 91.417(a) & (b) Would Not Adversely Affect Safety. In seeking this exemption, David J. Tester submits that the equivalent level of safe

ty with regard to the regulatory maintenance and alteration requirements established by Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) will be met because David J. Tester will use trained technicians to perform maintenance, alterations, or preventive maintenance on the UASs using the methods, techniques, and practices pre

scribed in the operating documents (i.e., the David J. Tester Aerial Operations Manual, Monthly Maintenance Log, and DJI Phantom 2 Vision+ and DJI Inspire 1 Instruction

32Manual). Furthermore, David J. Tester will document and maintain all maintenance records for the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs. Since the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs will be inspected as pre

scribed by the operating documents, David J. Tester will maintain the equivalent level of safety established by Sections 91.405(a), 91.409(a)(1), and 91.409(a)(2). A copy of the DJI Phantom 2 Vision+ and DJI Inspire 1 User Manuals are attached hereto as Exhibit C and D; a copy of the DJI Phantom 2 Vision+ and DJI Inspire 1 UAS Maintenance LOG is at

tached hereto as Exhibit E. Likewise, the exemption sought will not adversely affect safety because David J. Tester will use trained technicians to perform maintenance, alterations or preventive main

tenance on the UAS using the methods, techniques, and practices prescribed by the operat

ing documents. Furthermore, the exemption sought would maintain an equivalent level of safety established by Sections 91.407, 91.417(a) and 91.417(b), because all maintenance of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs will be performed by trained technicians. Maintenance will be documented and maintained utilizing the monthly maintenance log. Significantly, previous exemptions granted by the FAA concerning Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) establish that safety is not adversely affected when the technical characteristics and operating limitations of the UAS are considered. In consideration of David J. Tester’s proposed operating limitations, the operating documents, and the technical aspects of the DJI Phantom 2 Vision+ and DJI Inspire 1

33UASs, David J. Tester submits that safety will not be adversely affected by granting ex

emption from 14 C.F.R. Sections 91.405(a), 91.407(a)(1) and (a)(2), 91.409(a)(2), and 91.417(a) and (b). The FAA has previously granted relief specific to UAS in circumstances similar, in all material respects, to those presented herein (e.g. Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 7. The FAA May Prescribe Any Other Conditions For Safe Operation. In accordance with Section 333 of the FAA Modernization and Reform Act of 2012 (FMRA) and 14 C.F.R. § 21.16 entitled Special Conditions, David J. Tester requests that the FAA prescribe special conditions for the intended operation of the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs, which contain such safety standards that the Administrator finds necessary to establish a level of safety equivalent to that established by 14 C.F.R. Part 21, Subpart H, and 14 C.F.R §§ 61.113(a) & (b), 91.7 (a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). Such special conditions will permit safe operation of the UAs for the limited purpose of conducting aerial video and photography over certain areas of the United States for compensation or hire. FMRA Sec

tion 333 sets forth the requirements for considering whether a UAS will create a hazard to users of the NAS or the public, or otherwise pose a threat to national security; and further, provides the authority for such UAS to operate without airworthiness certification in ac

cordance with any requirements that must be established for the safe operation of the UAS in the NAS.

34Likewise, the Administrator may prescribe special conditions pursuant to 14 C.F.R. § 21.16, for operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, since the airworthiness regulations of 14 C.F.R. Part 21 do not contain adequate or appropriate safe

ty standards, due to the novel or unusual design features of the aircraft. Section 21.16, enti

tled Special Conditions, states the following: If the FAA finds that the airworthiness regulations of this subchapter do not contain adequate or appropriate safety standards for an aircraft, aircraft engine, or propeller because of a novel or unusual design feature of the aircraft, aircraft engine or pro

peller, he prescribes special conditions and amendments thereto for the product. The special conditions are issued in accordance with Part 11 of this chapter and contain such safety standards for the aircraft, aircraft engine or propeller as the FAA finds necessary to establish a level of safety equivalent to that established in the regulations. See 14 C.F.R. § 21.16. Therefore, in accordance with FMRA Section 333 and 14 C.F.R. § 21.16, the FAA may prescribe special conditions for Mr. Brown’s intended operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs, which contain such safety standards that the Administra

tor finds necessary to establish a level of safety equivalent to that established by 14 C.F.R. Part 21, Subpart H, and 14 C.F.R Sections 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b).
F. A Summary That Can Be Published In The Federal Register, stating: The Rules From Which David J. Tester Seeks Exemption: David J. Tester seeks exemption from the requirements of 14 C.F.R Sections 61.113(a)&(b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). A Brief Description Of The Nature Of The Exemption David J. Tester Seeks:

35This exemption will permit David J. Tester to commercially operate an Unmanned Aircraft System (UAS) for the purpose of conducting aerial video and photography over certain areas of the United States.
G. Any Additional Information, Views, Or Arguments Available To Support David J. Tester’s Request. This Petition is made pursuant to the FAA Modernization and Reform Act of 2012 (FMRA) Section 333, which directs the Secretary of Transportation to determine if certain UAS may operate safely in the NAS. As such, David J. Tester’s request for exemption may be granted pursuant to the authority of FMRA Section 333 and 14 C.F.R. Part 11, as set forth above. FMRA Section 333 sets forth the requirements for considering whether a UAS will create a hazard to users of the NAS or the public, or otherwise pose a threat to national se

curity; and further, provides the authority for such UAS to operate without airworthiness certification. As discussed in detail above, David J. Tester will operate the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs safely in the NAS, without creating a hazard to users of the NAS, or the public, or otherwise pose a threat to national security.
CONCLUSION As set forth herein, David J. Tester seeks an exemption pursuant to 14 C.F.R. § 11.61 and Section 333 of the FAA Modernization and Reform Act of 2012 (FMRA), which will permit safe operation of the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs commer

cially, without an airworthiness certificate, for the limited purpose of conducting aerial video and photography over certain areas of the United States. By granting this Petition,

36the FAA Administrator will be fulfilling the Congressional mandate of the FAA Modern

ization and Reform Act of 2012, while also advancing the interests of the public, by allow

ing David J. Tester to safely, efficiently, and economically operate the DJI Phantom 2 Vi

sion+ and DJI Inspire 1 UASs commercially within the NAS.
WHEREFORE , in accordance with the Federal Aviation Regulations and the FAA Modernization and Reform Act of 2012, Section 333, David J. Tester respectfully requests that the Administrator grant this Petition for an exemption from the requirements of 14 C.F.R Sections 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), and permit Leading Edge to operate the DJI Phantom 2 Vision+ and DJI Inspire 1 UASs commercially for the purpose of conducting aerial video and photography over certain areas of the United States. Dated: August, 7 2015

Respectfully submitted, David J. Tester

_________________________ David J. Tester 12216 Chesterfield Ln. Oklahoma City, OK 73173 73078 Tel: (405) 315-0197

37Appendices : A – DJI Phantom 2 Vision+ Specifications Data Sheet B – DJI Inspire 1 Specifications Data Sheet C – DJI Phantom 2 Vision+ Manufacturer’s User Manual D – DJI Inspire 1 Manufacturer’s User Manual E – Monthly Maintenance Log

APPENDIX – A DJI PHANTOM 2 VISION+ TECHNICAL SPECIFICATIONS David J. Tester only utilizes safe and reliable UASs. DJI is an industry leader in small UAS production. DJI UASs are loaded with ground breaking software enabling the user to set parameters which will not allow flight into controlled airspace. Parameters can also be set to limit flight to no higher than a predetermined and set altitude as well as limit flight to a predetermined and set distance. In addition, DJI software provides real-time altitude and location information to the PIC via the linked monitor (smart phone/tablet devices) 1.1 DJI Phantom 2 Vision+ 1.1.1 Aircraft 1.1.1.1 Supported Battery – DJI 5200mAH LiPo Battery 1.1.1.2 Weight (Battery & Propellers Included) – 2lbs 11.810oz (1242g) 1.1.1.3 Hover Accuracy (Ready to Fly) – Vertical: .8m; Horizontal: 2.5m 1.1.1.4 Max Yaw Angular Velocity - 200 0 /s

381.1.1.5 Max Tilt Angel - 35 0 1.1.1.6 Max Ascent Speed – 6m/s 1.1.1.7 Max Descent Speed – 2m/s 1.1.1.8 Max Flight Speed – 15m/s (NOT RECOMMENDED) 1.1.2 Gimbal 1.1.2.1 Working Current – Static: 750mA; Dynamic: 900mA 1.1.2.2 Control Accuracy - ±0.03 0 1.1.2.3 Controllable Range – Pitch: -90 0 - 0 0 1.1.2.4 Maximum Angular Speed – Pitch: 90 0 /s
1.1.3 Camera 1.1.3.1 Operating Temperature Range - 32 0 F - 104 0 F (0 0 C - 40 0 C) 1.1.3.2 Sensor Size – 1/2.3” 1.1.3.3 Effective Pixels – 14M 1.1.3.4 Resolution – 4384x3288 4.1.3.5 HD Video Recording – 1080p30 & 720p 4.1.3.6 Recording Field of View - 110 0 /85 0
1.1.4 Transmitter 1.1.4.1 Operating Frequency – 5.728GHz – 5.85GHz 1.1.4.2 Communication Distance (unobstructed) – FCC Compliance: 800m 1.1.4.3 Receiver Sensitivity (1%PER) - -93dBm 1.1.4.4 Transmitter Power – FCC Compliance: 100mW 1.1.4.5 Working Voltage – 120mA@3.7V 1.1.5 Range Extender 1.1.5.1 Operating Frequency – 2412-2462MHz 1.1.5.2 Communication Distance (unobstructed) – 500-700m 1.1.5.3 Transmitter Power – 20dBm 1.1.5.4 Power Consumption – 2W

39APPENDIX – B DJI INSPIRE 1 TECHNICAL SPECIFICATIONS David J. Tester only utilizes safe and reliable UASs. DJI is an industry leader in small UAS production. DJI UASs are loaded with ground breaking software enabling the user to set parameters which will not allow flight into controlled airspace. Parameters can also be set to limit flight to no higher than a predetermined and set altitude as well as limit flight to a predetermined and set distance. In addition, DJI software provides real-time altitude and location information to the PIC via the linked monitor (smart phone/tablet devices) 2.2 DJI Inspire 1 2.2.1 Aircraft 2.2.1.1 Model – T600 2.2.1.2 Weight (Battery Included) – 6lbs 7.5291oz (2935g) 2.2.1.3 Hovering Accuracy (GPS Mode) – Vertical: 0.5m; Horizontal: 2.5m 2.2.1.4 Max Angular Velocity – Pitch: 300 0 /s; Yaw: 150 0 /s 2.2.1.5 Max Tilt Angle - 35 0 2.2.1.6 Max Ascent Speed – 5m/s 2.2.1.7 Max Descent Speed – 4m/s 2.2.1.8 Max Speed – 22m/s (ATTI mode, no wind – NOT RECOMMEND

ED) 2.2.1.9 Max Flight Altitude – 4500m 2.2.1.10 Max Wind Resistance – 10m/s 2.2.1.11 Max Flight Time – Approximately 18 minutes 2.2.1.12 Motor Model – DJI 3510 2.2.1.13 Propeller Model – DJI 1345 2.2.1.14 Operating Temperature Range – 14 0 F to 104 0 F (-10 0 C to 40 0 C) 2.2.1.15 Dimensions – 17 1⁄4 ” x 17 3⁄4 ” x 12” 2.2.2 Gimbal 2.2.2.1 Model – ZENMUSE X3 2.2.2.2 Output Power (with camera) – Static: 9W; In Motion: 11W

402.2.2.3 Operating Current – Static: 750mA; In Motion: 900mA 2.2.2.4 Angular Vibration Range - ±0.03 0 2.2.2.5 Mounting – Detachable 2.2.2.6 Controllable Range – Pitch: -90 0 to +30 0 ; Pan: ±320 0 2.2.2.7 Mechanical Range – Pitch: -125 0 to 45 0 ; Pan: ±330 0 2.2.2.8 Max Controllable Speed – Pitch: 120 0 /s; Pan: 180 0 /s 2.2.3 Camera 2.2.3.1 Name – X3 2.2.3.2 Model – FC350 2.2.3.3 Total Pixels – 12.76M 2.2.3.4 Effective Pixels – 12.4M 2.2.3.5 Image Max Size – 4000x3000 2.2.3.6 ISO Range – 100-3200 2.2.3.7 Field of View - 94 0 2.2.3.8 CMOS – Sony EXMOR 1/2.3” 2.2.3.9 HD Video Recording – UHD(4K): 4096x2160p24/25, 3840x2160p24/25/30; FHD: 1920x1080p24/25/30/48/50/60; HD: 1280x720p24/25/30/48/50/60 2.2.3.10 Operating Temperature Range - 32 0 F - 104 0 F (0 0 C - 40 0 C) 2.2.4 Transmitter 2.2.4.1 Name – C1 2.2.4.2 Operating Frequency – 5.728-5.850GHz; 2.400-2.483GHz 2.2.4.3 Communicating Distance (unobstructed) – 2000m 2.2.4.4 Output Power – 9W 2.2.4.5 Operating Temperature Range - 14 0 F to 104 0 F (-10 0 C to 40 0 C) 2.2.4.6 Battery – 600mAh LiPo 2S

41APPENDIX – C DJI Phantom 2 Vision+ Manufacturer’s User Manual

APPENDIX – D DJI Inspire 1 Manufacturer’s User Manual

42APPENDIX – E

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