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

IN THE MATTER OF THE PETITION FOR EXEMPTION OF: Steven Wilke, DBA: High Wheel Productions 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

OPERATION OF CARBON CORE QUADCOPTER/ YUNEEC Q500 4K UNMANNEDAIRCRAFT SYSTEMS

PURSUANT TO SECTION 333 OF THE FAA MODERNIZATION AND REFORM ACT OF 2012 (PUBLIC LAW 112
- 95)

December 10 th , 2015 Steven Wilke 23029 Hisega Rd

. Rapid City, SD 57702 605

- 646

- 3331

High Wheel Productions http://www.thehighwheel.com steven411@gmail.com steven@thehighwheel.com2 TABLE OF CONTENTS Page GLOSSARY OF ABBREVIATIONS.

................................ ................................ .................. 3 SUMMARY

................................ ................................ ................................ ........................... 4 INTRODUCTION AND INTERESTS OF PETITIONER.

................................ ................... 4 BACKGROUND.

................................ ................................ ................................ .................. 4 BASIS FOR PETITION.

................................ ................................ ................................ ...... 5
NAME AND ADDRE SS OF PETITIONER.

................................ ................................ ....... 8 THE SPECIFIC SECTIONS OF 14 C.F.R. FROM WHICH Steven Wilke SEEKS EXEMPTION.

................................ ................................ ................................ ....................... 8 THE EXTENT OF RELIEF Steven Wilke SEEKS AND THE REASON Steven Wilke SEEKS THE RELIEF.

................................ ................................ ................................ ......... 12 THE REASONS WHY GRANTING Steven Wilke’s REQUEST WOULD BE IN THE PUBLIC INTEREST

................................ ................................ ........ 15
THE REASONS WHY GRANTING THE EXEMPTION WOULD NOT ADVERSELY AFFECT SAFETY.

................................ ................................ ................................ .............. 18
SUMMARY THAT CAN BE PUBLISHED IN THE FEDERAL REGISTER.

................ 36 ANY ADDITIONAL INFORMATION, VIEWS, OR ARGUMENTS AVAILABLE TO SUPPORT Steven Wilke’s REQUEST.

................................ ................................ .............. 36
CONCLUSION.

................................ ................................ ................................ .................. 37 APPENDICES.

................................ ................................ ................................ ................... 383 GLOSSARY 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 Com mand Section 333 FAA Modernization and Reform Act of 2012 (FMRA) Section 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 Landing4 SUMMARY Steven Wilke 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 to operate an Unmanned Aircraft System (UAS) for the commercial purpose of conducting aerial video and photograph y of forest service lands, National Parks, real estate, farms, ranches and outdoor activates over certain areas of the United States and mostly in Western South Dakota.

INTRODUCTION AND INTERESTS OF THE PETITIONER Steven Wilke has been a professional photographer and videographer since college at Texas A&M University in College Station, Texas. Steven Wilke even worked for the Texas A&M Athletic department as a Video Producer, working with the most state of the art equipment. Steven Wilke has 15 years’ experience with P hotography and Videography and three yeas flying remote control helicopters. The objective of Steven Wilke’s aerial video and Photography operations is to provide unique view of what we see every day and to provide an above average service for his customer s. Steven Wilke will be specifically targeting:
Forest Service Lands
National Parks
Real

- estate Farm Irrigation Systems
Solar Panel Installations Outdoor Activities including Hiking and Biking5 BACKGROUND Unmanned Aircraft Systems: Yuneec Q500 4k Quadcopter , Steven Wilke seeks an exemption to operate Yuneec Q500 4k for compensation or hire within the NAS. The Yuneec Q500 4k is a vertical take

- off and landing (VTOL) Unmanned Aircraft (UA) with a Ground Control Station (GCS) Utilizing a 10

- channel 2 .4GHz with 5.8GHz video downlink controller . The Yuneec Q500 4k has a maximum gross weight of approximately 3 pounds 7 ounces, while having a width of 16.54 inches and a height of 9.45 inches, and a maximum speed of approximately 19 knots.
The Yuneec Q500 4k has a maximum gross weight of 6 pounds 5 ounces, a length of 18.3 inches, width of 17.7 inches, height of 7.48 inches, and a maximum speed of Approximately 19 knots. Yuneec Q500 4k is equipped with four main rotors; utilizing
5300 mA h Lithium Polymer ba tteries to power the four electric motors. The Yuneec Q500 4k that will be operated by Steven Wilke 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, Steven Wilke, pursuant to the provisions of the Federal Aviation Regulations (14 C.F.R. § 11.61) and the FAA Modernization and Ref orm Act of 2012 (FMRA), Section 333, Special Rules for Certain Unmanned Aircraft Systems , hereby petitions the Administrator to commercially operate the Yuneec Q500 4k 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) &6 (b). In consideration of the speed, weight, size, and limited operating area associated with the unmanned aircraft and its operation, Stev en Wilke’s operation of the Yuneec Q500 4k 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, Steven Wilke 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. Steven Wilke submits that the requested relief is proper since an equival ent level of safety will be ensured. Steven Wilke will use experienced personnel or technicians to perform maintenance, alterations, or preventive maintenance on the UAS's using the methods, techniques, and practices prescribed in the operating documents ( i.e., Monthly Maintenance Log, and Yuneec Q500 4k Instruction Manual). Furthermore, Steven Wilke will document and maintain all maintenance records for the Yuneec Q500 4k

. Relief from certain requirements of Section 61.113(a) and (b), entitled Private pilot privileges and limitations: Pilot in command , is requested by Steven Wilke to the extent necessary to allow a Pilot in Command (PIC) holding a private pilot or higher level certificate, as well as an airman medical certificate, and who has demonstrat ed, by meeting minimum flight

- hour and current requirements, that the PIC is able to safely operate the Yuneec Q500
4k in a manner consistent with this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicles and structures. Steven Wilke seeks relief from Section 91.7(a), entitled Civil aircraft airworthiness , because the Yuneec Q500 4k do not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. As such, Steve n Wilke submits that he7 will ensure that the Yuneec Q500 4k is in an airworthy condition, prior to every flight, by determining that the UAS's are in compliance with the operating documents (i.e., Monthly Maintenance Log, and Yuneec Q500 4k I nstruction Manual), and that the aircraft are in a condition for safe flight. Steven Wilke also seeks an exemption from the requirements of Section 91.121, entitled Altimeter Settings , as the Yuneec Q500 4k will not have a typical barometric altimeter onbo ard. However, altitude information of the Yuneec Q500 4k will be provided to the PIC via Global Positioning System (GPS) equipment and radio communications telemetry data link, which downlinks from the UAS to the GCS for active monitoring of the flight pat h. This altitude information, combined with Steven Wilke’s operation of the Yuneec Q500 4k within visual line of sight, at or below 400 feet AGL, will ensure a level of safety equivalent to Section 91.121. Additionally, Steven Wilke seeks an exemption from the requirements of Section 91.151(b), entitled Fuel requirements for flight in VFR conditions . Steven Wilke submits that safety will not be affected by operation of the Yuneec Q500 4k 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 10 minutes for the intended photo shoot and, assuming normal cruising speed, to fly after that for at least 2.5 minutes for recovery and landing.
In accordan ce with 14 C.F.R. § 11.81, Steven Wilke provides the following information in support of its petition for exemption:8 A. Name a nd Address o f The Petitioner The name and address of the Petitioner and point of contact is: Steven Wilke 23029 Hisega Rd, Rapid City, SD 57702. 605

- 646

- 3331 Email: steven411@gmail.com , steven@thehighwheel.com
B. The Specific Sections o f 14 C.F.R. From Which St even Wilke seeks Exemption 1. Steven Wilke Seeks Exemption f rom t he 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 p ilot may, for compensation or hire, act as PIC of an aircraft in connection 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 compensation or hire. 2. Steven Wilke Seeks Exemption f rom t he Requirements Of Section 91.7(a) Section 91.7, entitled c ivil aircraft airworthiness , subsection (a), states the following: (a) No person may operate a civil aircraft unless it is in an airworthy condition. 3. Steven Wilke Seeks Exemption From The Requirements Of Section 91.121. Section 91.121, entitled Altimeter settings, subsection (a), states the following, in part:9 (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. Steven Wilke Seeks Exemption From The Requirements o f 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 (considering 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.
5. Steven Wilke 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 pres cribed 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[.]
6. Steven Wilke Seeks Exemption From The Requirements Of Sect ion 91.407(a)(1) Section 91.407, entitled Operation after maintenance, preventive maintenance,10 rebuilding, 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. Steven Wilke Seeks Exemption From The Requirements Of Sections 91.409(a)(1) And 91.409(a)(2). Section 91.409, e ntitled 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 4 3 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. Steven Wilke Seeks Exemption f rom T he Requirements Of Sections 91.417(a) And 91.417(b). Section 91.417, entitled Maintenance records , subsections (a) and (b), state the following: (a) Except for work performed in accordance with §§ 91.411 and 91.413, each registered owner or operator shall keep the following records for the periods specified in paragraph (b) of this section: (1) Records of the maintenance, preventive maintenance, and alteration and records of the
100

- hour, annual, progressive, and other required or approved inspections, as appropria te, for11 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 dat e of completion of the work performed; and (iii) The signature, and certificate number of the person approving the aircraft 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, propeller, 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 basi s. (iv) The current inspection status of the aircraft, including the time since the last inspection required by the inspection program under which the aircraft 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 required. (vi) Copies of the forms prescrib ed by § 43.9(d) of this chapter for each major 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 prescribed:12 (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. (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 o f Relief Steven Wilke Seeks And The Reason Steven Wilke Seeks The Relief.
1. Extent o f Relief Steven Wilke Seeks a nd The Reason Steven Wilke Seeks Relief From Section 61.113(a) And (b). Relief from Section 61.113(a) and (b) entitled Private pilot privileges and limitations: Pilot in command , is requested to the extent necessary to allow a PIC holding a private pilot or higher level certificate, as well as a current and valid airman medical certificate, and who has met certain flight

- hour and currency requirem ents, to conduct the proposed 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 conne ction 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 compensation or hire. As set forth more fully below, Steven Wilke submits that an equ ivalent level of safety will be maintained because no PIC will be allowed to operate the Yuneec Q500 4k unless that
PIC has met certain flight

- hour and current requirements, demonstrating that the PIC13 is able to safely operate either the Yune ec Q500 4k in a manner consistent with the operations specifications as described in this exemption, including evasive and emergency maneuvers, as well as maintaining appropriate distances from people, vessels, vehicles and structures. Further, Steven Wilk e submits that all flights of the Yuneec Q500 4k conducted by the PIC pursuant to the grant of this Petition: (1) will be incidental to Steven Wilke’s business; and (2) will not carry passengers or property for compensation or hire.
2. Extent o f Relief Steven Wilke Seeks a nd t he Reason Steven Wilke From Section 91.7(a). Relief from Section 91.7(a) entitled Civil aircraft airworthiness , is requested to the extent required to allow Steven Wilke to determine that the Yuneec Q500 4k are in airworthy condition prior to every flight by ensuring that the UAS is in compliance with the operating documents (i.e., the Monthly Maintenance Log and Yuneec Q500 4k manuals. Steven Wilke seeks the requested relief because the Yuneec Q500 4k does not require an ai rworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. Therefore, Steven Wilke will ensure that the Yuneec Q500 4k is in airworthy condition based upon its compliance with the operating documents (i.e., Monthly Maintenance Log, and Yuneec Q500 4k Instruction Manual) prior to every flight, and further, determine that the aircraft are in condition for safe flight, as stated in the conditions and limitations below.
3. Extent Of Relief Steven Wilke Seeks And The Reason Steven Wilke Seeks Relief From Section 91.121. Relief from Section 91.121, entitled Altimeter settings, may be required to allow flight operations of the Yuneec Q500 4k UAS's, which utilize a barometric pressure sensor, GPS equipment, and a radio communications telemetry data link to downlink altitude information14 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 (A GL), Steven Wilke seeks the requested relief because the Yuneec Q500 4k ’s altimeter may be set on the ground to zero feet AGL, rather than the local barometric pressure 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 limitations stated below. As more fully set forth herein, an equivalent level of safety will
be maintained since the Yuneec Q500 4k is equ ipped 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 altitude information of the UA on the heads

- up display of the GC S.
4. Extent Of Relief Steven Wilke Seeks And The Reason Steven Wilke Seeks Relief From Section 91.151(b). Relief from Section 91.151(b) entitled Fuel requirements for flight in VFR conditions, is requested to the extent required to allow flights of the batte ry powered Yuneec Q500 4k during daylight hours in visual meteorological conditions (VMC), under visual flight rules (VFR), for a total duration of 10 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 2.5 minutes. Steven Wilke seeks the requested relief because without an exemption from Section 91.151(b), the flight time duration of the battery powered Yuneec Q500 4k will severely constrain the practicality of any aerial video or still photo f light operations that Steven Wilke proposes to conduct pursuant to this Petition.15 Significantly, as set forth below, the technical specifications of the Yuneec Q500
4k operating documents and Steven Wilke’s proposed operating limitations, ensure that Steven Wilke will safely operate the battery powered Yuneec Q500 4k during daylight hours in visual meteorological conditions (VMC), under visual flight rules (VFR), with

e nough battery power to fly for a total duration of 12 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 2.5 minutes.
5. Extent Of Relief Steven Wilke Seeks And The Reason Steven Wilke Seeks Reli ef 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, Steven Wilke requests relief from these Sections because the Yuneec Q500 4k does not require airworthiness certificates. As set forth more fully below, the Yuneec Q500 4k meets the conditions of FMRA Section 333 for operation without an airworthiness certificate. Accordingly, Steven Wilke will use trained technicians to perform maintenance, alterations, or preventive maintenance on the UAS's using the methods, techniques, and practices prescribed in the UAS operating documents (i.e., the Aerial Operations Manual, Monthly Maintenance Log, and Yuneec Q500 4k Instruction Manual). Furthermore, Steven Wilke will document and maintain all maintenance records for Yuneec Q500 4k

.

D. The Reasons Why Granting Steven Wilke Request Would Be In The Interest; That Is, How It Would Benefit The Public As A Whole. Granting the present Petition will further the public interest by allowing Steven Wilke to safely, efficiently, and economically pe rform aerial video and photography of construction sites, real estate, and landscape over certain areas of the United States.16 Additionally, use of the Yuneec Q500 4k will decrease congestion of the NAS, reduce pollution, and provide significa nt benefits to the economy. Notably, the benefits of Steven Wilke's proposed operation of the Yuneec Q500 4k will be realized without implicating any privacy issues.
1. The Public Will Benefit From Decreased Congestion Of The NAS. The Yuneec Q500 4k is batte ry powered and serves 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 the Yuneec Q500 4k 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 Yuneec Q500 4k does not require an airport to takeoff or land. Likewise, a reduction of

m anned aircraft conducting aerial video and photography missions 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 Yuneec Q500 4k . Conducting aerial acquisitions with the Yuneec Q500 4k 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 photography flight operations. By using battery power and electric motors, the Yuneec Q500 4k produces no air pollution, and is the most viable environmentally conscious alternative to the cabin class, six cylinder internal17 combustion engine aircraft that are typically utilized for aerial video and photography while burning approximately 20

- 30 gallons per hour of leaded aviation fuel. The Yuneec Q500 4k , while reducing the carbon footprint of aerial acquisitions, also eliminates noise pollution, as the UA's are propelled by battery powered electric motors, rather than an internal combustion engine. By using the Yuneec Q500 4k to perform aerial acquisitions, 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 onboard the aircraft, the Yuneec Q500 4k (weighing approximately 3 pounds 7 ounces and, at their maximum gross weights with respectively (and with no fuel on board) has less physical potential for collateral damage to life and property on the ground, and in the air, compared to the manned aircraf t that typically conduct similar operations (weighing approximately 6,000 pounds, and a fuel capacity of 180 gallons).
3. Performing Aerial Video and Photography Operations With The Yuneec Q500 4k Will Benefit The Economy. In addition to being safe and effici ent, the Yuneec Q500 4k is also an economical alternative to using manned aircraft to conduct similar aerial operations. As such, operation of the Yuneec Q500 4k will allow United States based companies, like Steven Wilke’s to remain competitive and contri bute 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 aviation fuels, U.S. owned and operated companies must adopt new and alternative t echnology in order to remain competitive. Operating the battery powered Yuneec Q500 4k is one such technology that not only allows companies greater operational18 flexibility compared to manned aircraft, but provides such flexibility without th e high operational cost of a traditional manned aircraft. By operating the Yuneec Q500 4k , companies such as Steven Wilke’s can remain competitive and profitable and therefore, provide greater job stability to employees and contractors, which will ultimately contribute to growth of the U.S. economy. Improved financial performance of U.S. compa nies, through commercial use of the Yuneec Q500 4k , provides a stable workforce that increases consumer spending, improves local, state, and federal tax revenues and allows 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, Steven Wilke’s proposed operation of the Yuneec Q500 4k will not implicate any privacy issues. Specifically, the Yuneec Q500 4k will be operated only in compliance with operating documents (i.e. Aerial Operations Manual, Monthly Maintenance Log, and the Yuneec Q500 4k Instruction Manual's) which requires property owner involvement as well as local l aw 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 Steven Wilke Seeks Exemption.
1. Reasons Why t he Yuneec Q500 4k Meet’s The Conditions Of The FAA Modernization and Reform Act of 2012 (FMRA) Section 333.19 In conside ration of the size, weight, speed, and limited operating area associated with the unmanned aircraft and its operation, Steven Wilke’s operation of the Yuneec Q500 4k 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 certification and sets forth requirements for considering whether a UAS will create a hazard to users of the NAS or the public, or o therwise 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 Secretar y of Transportation shall determine if certain unmanned aircraft systems may operate 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 section 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 airworthiness certification under section 44704 of title 49, United States Code, is required for the operation of unmanned aircraft systems identified under paragraph (1).20 (c) Requirements for Safe Operation.

-- If the Secretary determines under this section that certain unmanned aircraft systems may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft systems in t he national airspace system. In seeking this exemption, Steven Wilke submits that the Yuneec Q500 4k can operate safely in the NAS pursuant to FMRA Section 333, as demonstrated by: (a) the characteristics of the Yuneec Q500 4k ; (b) the pilot certification requirement; and (c) the specific operating limitations.

a. The Specifications o f The Yuneec Q500 4k Demonstrates Its Safe Characteristics. The Yuneec Q500 4k does 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 o f t he Yuneec Q500 4k The technical specifications of the Yuneec Q500 4k are set forth by the Yuneec Q500 4k Specifications and Data Sheet, attached hereto as Exhibit A. ii. The Yuneec Q500 4k Autonomous Flight a nd Navigation Modes Enable t he UAS's To Remain Within a Defined Operational Area.
The Yuneec Q500 4k may be operated in both manual and fully autonomous ret urn to home flig ht modes. The Yuneec Q500 4k may be operated in manual flight mode only. A complete description of the flight and navigational modes of the Yuneec Q500 4k is provided in the manual Yuneec Q 500 4k User Manual , attached hereto as Exhibit B

. I ii. The Yuneec Q500 4k Are Designed For Automatic Return To Home Point Or Hover In The Event Of Loss Of The Control Link Or Navigation.21 When the Control Link is lost, the Yuneec Q500 4k will remain stationary in flight, for 3 seconds or more. If, after 3 seconds, the Yuneec Q500 4k due 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 positio n and shutdown. A complete description of the Failsafe Functions of the Yuneec Q500 4k are set forth in the manual of the Yuneec Q500 4k User Manuals, attached hereto as Exhibit B

. iv. The Yuneec Q500 4k GCS a nd Its Operation. A complete description of the operation and specifications of the Yuneec Q500 4k GCS and flight control software is provided in the manual for the Yuneec Q500 4k . The Yuneec Q500
4k User Manuals are attached hereto as Exhibit B

. b. Flight Operations o f Yuneec Q500 4k Are Limited t o The Line Of Sight Of A Certificated Pilot in Command . Steven Wilke will only utilize certificated pilots who possess a current and valid airman medical certificate to act as a pilot in command (PIC) of the Yuneec Q500 4k

.
c. Flights o f Yuneec Q500 4k Will Be Conducted Pursuant To Specific Operating Limitations. In seeking this exemption, Steven Wilke proposes to commercially operate Yuneec Q500 4k for the special purpose of conducting aerial video and photography over certain areas of United States, pursuant to the following specific operating limitations:
1. Operations authorized by this grant of exemption will be limited to the following aircraft described in the operating documents, rotorcraft UAS's weighing less than
55 po unds22 maximum gross weight: Yuneec Q500 4k Unmanned Aircraft Systems. Proposed operations of any other aircraft will require 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 UA may not be flown at an indicated airspeed exceeding 20 knots.
4. The UA must be operated at an altitude of no more than 400 feet above ground level (AGL), as indicated by the procedures specified in the ope rating documents unless a special request is made and approved by ATC. All altitudes reported to ATC must be in feet AGL.
5. The UA's 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 vi sion unaided by any device 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 duration 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 be yond 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.
9. The operating documents and the grant of exemption must be accessible during23 UA S operations and made available to the Administrator upon request. If a discrepancy exists between the conditions and limitations contained in the grant of exemption and the procedures outlined in the operating documents, the conditions and limitations con tained in the grant of exemption take precedence and must be followed. Otherwise, the operator must follow the procedures as outlined in its operating documents. The operator may update or revise its operating documents. It is the operator’s responsibility to track such revisions and present updated and revised documents to the Administrator upon request. The operator must also present updated and revised documents if it petitions for extension or amendment to the grant of exemption. If the operator determi nes 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 regardin g 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 condition for safe flight. If the inspection reveals a condition that affects the safe operation of the UAS, the aircraft is proh ibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight. The Ground Control Station must be included in the preflight inspection. All maintenance and alterations must be properly do cumented 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 component, must undergo a functional test flight. The PIC who conducts th e functional test flight must make an entry in the aircraft records.24 12. The pre

- flight inspection must account for all potential discrepancies, e.g. inoperable components, items, or equipment, not already covered in the relevant sections of the operating docu ments. 13. The operator must follow the UAS manufacturer’s aircraft/component, maintenance, 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, inspection, alterations, and status of replacement/overhaul component parts must be noted in the aircraft records, including total time in service, description of work accomplished, and the signature of the autho rized person returning the UAS to service Each UAS's operated under this exemption must comply with all manufacturer Safety Bulletins.
15. The authorized person must make an entry in the aircraft record of the corrective action taken against discrepancies discovered between inspections.
16. The PIC must possess at least a private pilot certificate and at least a current third

class medical certificate.
17. The operator may not permit any PIC to operate unless the PIC meets the operator’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 exemption, including evasive and emergency maneuvers and maintaining appropriate 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 PIC's are permitted under the terms of the exemption. However, training operations may only be conducted dur ing dedicated training sessions. During training, proficiency, and experience

- building flights, all persons not essential for flight25 operations are considered nonparticipants, and the PIC must operate the UA with appropriate distance from nonparticipants i n accordance with 14 C.F.R. § 91.119.
18. 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.
19. The UA may not operate within 5 nautical miles of an airport reference point as denoted on a current FAA published aeronauti cal chart unless a letter of agreement with that airport’s management is obtained, and the operation is conducted in accordance with a NOTAM as required by the operator’s COA. The letter of agreement with the airport management must be made available to th e Administrator
upon request. 20. 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.
21. If the UA loses communications or loses its GPS signal, it mus t return to a pre

determined location within the planned operating area and land or be recovered in accordance with the operating documents.
22. The PIC must abort the flight in the event of unpredicted obstacles or emergencies in accordance with the operating documents.
23. 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 UAS with 25% battery power remaining.26 24. 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 mo re 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 requireme nts. 25. 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 identification (N

Number) markings in accordance with 14 C.F.R. part 45, Subpart C. Markings must be as large as practicable.
26. Before conducting operations, the radio frequency spectrum used for operation and control of the UAS must comply with the Federal Communications Commission (FCC) or other appropriate government oversight agency requirements.
27. The documents required fewer than 14 C.F.R. 91.9 and 91.203 must be available 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 re quest. 28. The UAS must remain clear and yield the right of way to all manned aviation operations and activities at all times.
29. The UAS may not be operated by the PIC from any moving device or vehicle.
30. 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:27 a. Barriers or structures are present that sufficiently protect nonparticipating persons from the UAS and/or debris in the event of an accident. The operator must ensure that nonparticipating persons remain under such protection. If a situation arises where nonparticipating persons leave such protection and are within 500 feet of the UA, flight operations must ce ase 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 permission and the PIC has made a safety assessment of the risk of operating closer to thos e objects and determined that it does not present an undue 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).
31. All operations shall be conducted over private or controlled

- access property with permission from the land owner/controller or authorized representative. Permission from land owner/controller or authorized representative will be obtained for each flight to be conducted.
32. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of the operational area as defined by the applicable COA must be reported to the FAA's UAS Integration Office (AFS

- 80) within 24 hours. Accidents must be reported to the National Transpo rtation 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.
Steven Wilke s ubmits that the equivalent level of safety established by Section28 61.113(a) and (b) will be maintained because no PIC will be allowed to operate the Yuneec Q500 4k unless that PIC has demonstrated, by meeting minimum flight

- hour and currency requirements, that the PIC is able to safely operate the Yuneec Q500 4k UAS in a manner consistent with the exemption, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicles and structures. Considering Steven Wilke ’s proposed area of operations, and the operating limitations set forth

- above; the parallel nature of private pilot aeronautical knowledge requirements to those of commercial pilot requirements (See Exemption No. 11062); and the airmanship skills
necessary to safely operate the Yuneec Q500 4k UAS, Steven Wilke submits that the additional manned airmanship experience of a commercially certificated pilot would not correlate to the airmanship skills necessary for Steven Wi lke 's specific proposed flight operati ons. 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. Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11112, 11136, 11138, 11150, 11153, 11156, 11158, 11159, 11160, 11161). Steven Wilke will not allow any PIC to operate the Yuneec Q500 4k UAS unless that PIC has demonstrated, by meeting minimum flight

- hour requirements of the Yuneec Q500 4k UAS training and currency requirements, that the PIC is able to safely operate the Yuneec Q500 4k UAS in a manner consistent with this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from people, vessels, vehicle s and
structures. 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 minimum of 529 hours of those hours as a UAS pilot operating th e same make and model of UAS to be used for operations under the exemption). In addition to the hour requirements, the PIC must accomplish 3 takeoffs and landings in the preceding 90 days (for currency purposes). As in Exemption Nos. 11062, 11138, and 1115 3, prior documented flight experience that was obtained in compliance with applicable regulations will ensure an equivalent level of safety during Steven Wilke’s proposed operations. The Administrator has held that prior documented flight experience that w as 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 pilot 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 t han additive; i.e. 5 hours make and model time may be included 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 l andings in the preceding 90 days (for currency purposes). The FAA finds that at a minimum, the flight

- hour requirements in Exemption No. 11062 are appropriate to practice and build proficiency in the skills necessary to safely conduct the petitioner’s prop osed operations. The FAA also finds that prior documented flight experience that was obtained in compliance with applicable regulations would satisfy this requirement. Training, proficiency,30 and experience

- building flights can also be conduct ed under the grant of exemption to accomplish the required flight time. During training, proficiency, and experience

- building 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, Steven Wilke will ensure safe operations by not allowing any PIC to operate the Yuneec Q500 4k UAS unless that PIC has demonstrated, by meeting minimum flight

- hour and currency requirements, that the PIC is able to safely operate the Yuneec Q500
4k UAS in a manner consistent with the exemption, including evasive and emergency maneuvers and maintain ing appropriate distances from people, vessels, vehicles and
structures. 3. Reasons Why a n 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 b ecause prior to every flight, Steven Wilke will ensure that the Yuneec Q500 4k 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 p reviously granted relief from Section 91.7(a) 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). 4. Reasons Why a n Exemption From The Requirements Of Section 91.121 Would Not Adversely Affect Safety.31 The equivalent level of safety established by Section 91.121 will be maintained because th e altitude information of the Yuneec Q500 4k UAS's 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 altitude. This altitude
inf ormation, combined with Steven Wilke’s operation of the Yuneec Q500 4k UA's within visual line of sight, at or below 400 feet AGL, will ensure a level of safety equivalent to Section 91.121. The altitude information will be generated by GPS equipment insta lled on board the aircraft. Prior to each flight, a zero altitude initiation point is automatically established by the UAS's at ground level. The FAA has previously granted relief from Section 91.121 specific to UAS, in circumstances similar, in all materi al 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 a n 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 Yuneec Q500 4k UAS's; (2) the limitations o n the proposed flight operations; and (3) the location of the proposed flight operations. Accordingly, Steven Wilke will ensure that he will safely operate the battery powered Yuneec Q500 4k UA's during daylight hours in VFR conditions, with enough battery power to fly for a total duration of 10 minutes to the first point of intended landing and, assuming normal cruising speed, to fly after that for at least 2.5 minutes.32 Here, as in Exemption No. 11109, the technical specifications of the Yune ec Q500 4k UAS's the limitations on the pro posed 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 Yuneec Q500 4k UAS's provide audible and visual warnings to the PIC at the GCS when the UA's experiences low battery voltage, the first warning occurring at approximately 33% remaining battery power, and again at approximately 10% remaining battery power. At the critica lly low battery level, the Yuneec Q500 4k UAS's 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 oper ating 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 presented herein (e.g. Exemption Nos. 8811, 10808, 10673, 11042, 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11136, 11138, 11150, 11153, 11156, 11 157, 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, Steven Wilke submits that the equivalent level of safety 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 met33 because Steven Wilke will use trained tec hnicians to perform maintenance, alterations, or preventive maintenance on the UAS's using the methods, techniques, and practices prescribed in the operating documents i.e., the Operations Manual, Monthly Maintenance Log, and Yuneec Q500 4k Instruction Man ual. Furthermore, Steven Wilke will document and maintain all maintenance records for the Yuneec Q500 4k UAS's.
Since the Yuneec Q500 4k UAS's will be inspected as prescribed by the operating documents, Steven Wilke will maintain the equivalent level of sa fety established by Sections 91.405(a), 91.409(a)(1), and 91.409(a)(2). A copy of the Yuneec Q500 4k User Manuals are attached hereto as Exhibit B; a copy of the Yuneec Q500 4k UAS Maintenance LOG is attached hereto as Exhibit C. Likewise, the exemption so ught will not adversely affect safety because Steven Wilke will use trained technicians to perform maintenance, alterations or preventive maintenance on the UAS using the methods, techniques, and practices prescribed by the operating 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 Yuneec Q500 4k UAS's will be performed by trained technicians. Maintenance will be documented and ma intained 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.34 In consideration of Steven Wilke’s proposed operating limitations, the operating documents, and the technical aspects of the Yuneec Q500 4k UAS's, Steven Wilke submits that safety will not be adversely affected by granting exemption 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 r espects, 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, Steven Wilke requests that the FAA prescribe special conditions for the intended operation of Yuneec Q500 4 k UAS's, 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), 91.4 07(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). Such special conditions will permit safe operation of the UA's for the limited purpose of conducting aerial video and photography over certain areas of the United States for compensation or hire. FMRA S ection 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 c ertification in accordance with any requirements that must be established for the safe operation of the UAS in the NAS.35 Likewise, the Administrator may prescribe special conditions pursuant to 14 C.F.R. §21.16, for operation of the Yuneec Q5 00 4k UAS's, since the airworthiness regulations of 14 C.F.R. Part 21 do not contain adequate or appropriate safety standards, due to the novel or unusual design features of the aircraft. Section 21.16, entitled Special Conditions, states the following:
I f 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 pr opeller, it may prescribe 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 fi nds 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 Steven Wilke’s intend ed operation of the Yuneec Q500
4k UAS's, 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 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).36 F. A Summary That Can Be Published i n t he Federal Register stating: The Rules From Which Steven Wilke Seeks Exemption: Steven Wilke 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 o f The Nature Of The Exemption Steven Wilke Seeks: This exemption will permit Steven Wilke 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 Steven Wilke’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, Steven Wilke 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 t o national security and further, provides the authority for such UAS to operate without airworthiness certification. As discussed in detail above, Steven Wilke will operate the Yuneec Q500 4k UAS's safely in the NAS, without creating a hazard to users of t he NAS, or the public, or otherwise pose a threat to national security.37 CONCLUSION As set forth herein, Steven Wilke 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 Yuneec Q500 4k UAS's commercially, 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, the FAA Administrator will be fulfilling the Congressional

man date of the FAA Modernization and Reform Act of 2012, while also advancing the interests of the public, by allowing Steven Wilke to safely, efficiently, and economically operate the Yuneec Q500 4k UAS's commercially within the NAS. WHEREFORE , in accordance with the Federal Aviation Regulations and the FAA Modernization and Reform Act of 2012, Section 333, Steven Wilke 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 Steven Wilke to operate the Yuneec Q500 4k UAS's commercially for the purpose of conducting aerial video and photography over certain areas of the United States.

December 10 th , 2015 Steven Wilke38 APPENDICES:
A

- Yuneec Q500 4k

- Specifications
B

– Yuneec Q500 4k

- User Manual
C

– Yuneec Q500 4k

- Monthly Maintenance Log

APPENDIX

– A Yuneec Q500 4k TECHNICAL SPECIFICATIONS Steven Wilke only utili zes safe and reliable UAS's. Yuneec is an industry leader in small UAS production with a recent investment from Intel, the leading CPU manufacturer, of $60 Million

. Yuneec UAS's are loaded with ground breaking software enabling the user to set parameters which will not allow flight into controlled airspace from GPS coordinates built into the flight software . 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 with a maximum height of 400 feet . In addition, Yuneec software provides real

- time altitude and location information to the PIC via the linked monitor via GPS , Yuneec Q500 4k Radio Control Transmitte r Aircraft. TYPHOON Q500 4 K FLIGHT TIME: Up to 25 Minutes DIMENSIONS: 9.45 in (210mm) x 16.54 in (420mm) DIAGONAL MOTOR TO MOTOR DISTANCE: 20 in (510mm) PROPELLER/MAIN ROTOR DIAMETER: 13.0 in (330mm) WEIGHT WITHOUT BATTERY AND PAYLOAD: 40.0 oz (1130g) MAXIMUM TAKEOFF WEIGHT WITH CG O3: 60.0 oz (1700g) BATTERY: 5400mAh 3S 11.1V LiPo CHARGER: 3S 11.1V LiPo DC Balancing Smart Charger with AC Adapter TRANSMITTER: 10

- channel 2.4GHz with 5.8GHz video downlink39 MAXIMUM FLYING ALTITUDE: Default 400 Feet Above Ground Level
MAXIMUM ROTATION RAT E: 65°/s MAXIMUM ROLL ANGLE: 35° RADIO CONTROL FREQUENCY BAND: 2.4GHz MAXIMUM CLIMB RATE: 2m/s MAXIMUM DESCENT RATE: 3m/s CGO3 (Attached Camera) Dimension: 4.2x5.0x3.1in (106x128x80mm) Weight: 6.9oz (195g)
Sensor: 1/2.3” CMOS Effective Pixels: 12.4 Megapixels Camera lens: 14mm/F2.8 35mm FOV: 115 Degree Electronic Shutter: 1/30

—— 1/8000 Working Temperature: 0

- 40 Power Consumption: 10W Video Transmis sion Range: Up to 500m (1640ft)
Trans mission System: 5.2Ghz

— 5.8Ghz Video UHD: 4K 30FPS ST10+ (Remote Controller) Number of Channels: 10 RC Band: 2.4GHz RC Modulation: Yun eec Video Downlink Band: 5.8GHz Telemetry/OSD: Yes40 SD Card Compatible: Yes
LC D Screen Size: 5.5” Touchscreen: Yes

APPENDIX

– B Yuneec Q500 4k

– Manufacturer's User ManualVersion 2.01 1 

### TABLE OF CONTENTS

TABLE OF CONTENTS INTRODUCTION AERIAL IMAGING SOLUTION · Specifictations · Notices and Warnings · General Safety Precautions and Warnings · TYPHOON Q500 4K RTF Contents · Battery Warnings and Usage Guidelines · Charging The Batteries · Preparing The CGO3 · Installing The Propellers · TYPHOON Q500 4K, CGO3 and ST10+ Overview

· ST10+ Display

· ST10+ Accessories · Flight Controls · Flight Controls - Smart Mode · Follow Me Function · Watch Me Function · Flight Controls - Angle (Pilot) Mode · Flight Controls - Home Mode · Led Status Indications · Taking Photos and Recording Video · Installing The Flight Battery

· GPS Functionality · Preparing to Fly · Flying · Disabling GPS · Graphical User Interface (GUI) · Compass Calibration

· ST10+ and Receiver Binding

· ST10+ and CGO3 Binding GROUND IMAGING SOLUTION · Specifictations · Battery Warnings and Usage Guidelines · Installing The Steadygrip Batteries · Attaching The CGO3 to The Steadygrip · CGO3 APP · Attaching A Mobile Device to The Steadygrip · Using The Camera Pitch Control Wheel · Taking Photos and Recording Video · Added Features for CGO3 on Steadygrip TROUBLESHOOTING WARRANTY INFORMATION CERTIFICATION INFORMATION 1 2 2 3 3 4 6 7 8 9 9 10 11 12 12 13 14 15 16 17 18 20 20 21 22 23 24 24 25 27 28 29 29 29 30 30 31 31 31 31 32 33 35 352 

### INTRODUCTION

AERIAL IMAGING SOLUTION The TYPHOON Q500 4K is a superior modular, integrated aerial and ground imaging solution. The system arrives 100% factory-assembled and test flown, including a larger ST10+ 5.5’’ Android touch screen personal ground station and a CGO3 3-axis gimbal camera able to take 16 megapixel still photos and excellent Full HD 60 FPS videos. The STEADYGRIP extends the use of the gimbal camera from the sky to the ground and, With the CGO APP, whatever is shot can be viewed on your SmartPhone with the same control of video FPS, video start/stop and still photos as found on the ST10+. With the Q500 4K, it’s never been easier to capture amazing photographs and video footage for a wide variety of uses. Although the Q500 4K is ready to fly right out the box, please take the time to read through this entire instruction manual for more information on safety, battery charging, flight controls and more before making your first flight. Please also visit www.yuneec.com for additional information including product updates, bulletins, videos and more.

Specifictations

TYPHOON Q500 4K FLIGHT TIME: Up to 25 Minutes DIMENSIONS: 9.45 in (210mm) x 16.54 in (420mm) DIAGONAL MOTOR TO MOTOR DISTANCE: 20 in (510mm) PROPELLER/MAIN ROTOR DIAMETER: 13.0 in (330mm) WEIGHT WITHOUT BATTERY AND PAYLOAD: 40.0 oz (1130g) MAXIMUM TAKEOFF WEIGHT WITH CGO3: 60.0 oz (1700g) BATTERY: 5400mAh 3S 11.1V LiPo (included) CHARGER: 3S 11.1V LiPo DC Balancing Smart Charger with AC Adapter (included) TRANSMITTER: 10-channel 2.4GHz with 5.8GHz video downlink (included) MAXIMUM FLYING ALTITUDE: Default 400 Feet Above Ground Level (Adjustable via the Q500 GUI) MAXIMUM ROTATION RATE: 65°/s MAXIMUM ROLL ANGLE: 35° RADIO CONTROL FREQUENCY BAND: 2.4GHz MAXIMUM CLIMB RATE: 2m/s MAXIMUM DESCENT RATE: 3m/s CGO3 Dimension: 4.2x5.0x3.1in (106x128x80mm) Weight: 6.9oz (195g) Sensor: 1/2.3” CMOS Effective Pixels: 12.4 Megapixels Camera lens: 14mm/F2.8 35mm FOV: 115 Degree Electronic Shutter: 1/30 —— 1/8000 Working Temperature: 0-40 °C Power Consumption: 10W Video Transmission Range: Up to 500m (1640ft) Transmission System: 5.2Ghz — 5.8Ghz Video UHD: 4K 30FPS ST10+ Number of Channels: 10 RC Band: 2.4GHz RC Modulation: Yuneec Video Downlink Band: 5.8GHz Telemetry/OSD: Yes SD Card Compatible: Yes LCD Screen Size: 5.5” Touchscreen: Yes3 Notices And Warnings
**IMPORTANT NOTE:** All safety precautions and warnings, instructions, warranties and other collateral information is subject to change at the sole discre

tion of Yuneec. For the most up-to-date information please visit the corresponding product page at www.Yuneec.com or contact the nearest Yuneec office or authorized distributor. The following special language terms are used throughout the product literature to indicate various levels of potential harm when operating this product: **NOTICE:** Procedures, which if not properly followed, create a possibility of property damage and/or little to no possibility of injury. **CAUTION:** Procedures, which if not properly followed, create the probability of property damage and/or a possibility of serious injury. **WARNING:** Procedures, which if not properly followed, create the probability of property damage, collateral damage and/or serious injury or create a high probability of superficial injury. **WARNING:** Read the ENTIRE quick start guide and instruction manual to become familiar with the features of the product before operating. Failure to operate the product correctly can result in damage to the product, property and/or cause serious injury. **WARNING:** This is a sophisticated consumer product. It must be operated with caution and common sense, and requires some basic mechanical ability. Failure to operate this product in a safe and responsible manner could result in damage to the product, property and/or cause serious injury. This product is not intended for use by children without direct adult supervision. Do not use with incompatible components or alter this product in any way outside of the instructions provided by Yuneec. The quick start guide and instruction manual contain instructions for safety, operation and maintenance. It is essential to read and follow all the instructions and warnings prior to assembly, setup and/or use in order to operate the product correctly and avoid damage or serious injury. **AGE RECOMMENDATION: NOT FOR CHILDREN UNDER 14 YEARS. THIS IS NOT A TOY.**4 General Safety Precautions And Warnings

**WARNING:** Failure to use this product in the intended manner as described in the quick start guide and instruction manual can result in damage to the product, property and/ or cause serious injury. A Radio Controlled (RC) multirotor aircraft, APV platform, drone, etc. is not a toy! If misused it can cause serious bodily harm and damage to property. **WARNING:** As the user of this product you are solely and entirely responsible for operating it in a manner that does not endanger yourself and others or result in damage to the product or the property of others. • Keep your hands, face and other parts of your body away from the spinning propellers/rotor blades and other moving parts at all times. Keep items that could impact or become entangled away from the propellers/rotor blades including debris, parts, tools, loose clothing, etc. • Always operate your aircraft in open areas that are free from people, vehicles and other obstructions. Never fly near or above crowds, airports or buildings. • To ensure proper operation and safe flight performance never attempt to operate your aircraft nearby buildings or other obstructions that do not offer a clear view of the sky and can restrict GPS reception. • Do not attempt to operate your aircraft in areas with potential magnetic and/or radio interference including areas nearby broadcast towers, power transmission stations, high voltage power lines, electrical storms, etc. • Always keep a safe distance in all directions around your aircraft to avoid collisions and/or injury. This aircraft is controlled by a radio signal subject to interference from many sources outside your control. Interference can cause momentary loss of control. • To ensure proper and safe operation of the automatic landing function in Home Mode you must start the motors with the aircraft in a position that has at least 10 feet (approximately 3 meters) of clear and open space around it and achieve a proper GPS lock. • Do not attempt to operate your aircraft with any worn and/or damaged components, parts, etc. (including, but not limited to, damaged propellers/rotor blades, old batteries, etc.). • Never operate your aircraft in poor or severe weather conditions including heavy winds, precipitation, lightning, etc. **DO NOT FLY OVER CROWDS!**  **DO NOT FLY NEAR AIRPORTS!**  **THE MAXIMUM FLYING ALTITUDE FOR THIS AIRCRAFT**  **IS 8000FT ABOVE SEA LEVEL! DO NOT FLY NEARBY TALL**  **BUILDINGS/OBSTRUCTIONS (100° MINIMUM CLEARANCE**  **REQUIRED) KEEP CLEAR OF THE**  **SPINNING PROPELLERS!** MAX 8000ft 100  ̊

**DO NOT FLY IN WINDS THAT EXCEED 8–12 MPH**  **(13–19 KPH)!**5 • Always operate your aircraft starting with a fully charged battery. Always land as soon as possible after the first level low voltage battery warning or land immediately after the second level low voltage battery warning (as indicated by the vibrations and audible alerts from the transmitter/personal ground station). • Always operate your aircraft when the voltage of the battery in the transmitter/personal ground station is in a safe range (as indicated by the battery charge status icon on the screen of the transmitter/personal ground station). • Always keep the aircraft in clear line of sight and under control, and keep the transmitter/personal ground station powered on while the aircraft is powered on. • Always move the throttle control stick down fully and turn off the motors in the event the propellers/rotor blades come into contact with any objects. • Always allow components and parts to cool after use before touching them and flying again. • Always remove batteries after use and store/transport them per the corresponding guidelines. • Avoid water exposure to all electronic components, parts, etc. not specifically designed and protected for use in water. Moisture causes damage to electronic components and parts. • Never place any portion of the aircraft or any related accessories, components or parts in your mouth as doing so could cause serious injury or even death. • Always keep chemicals, small parts and electronic components out of the reach of children. • Carefully follow the instructions and warnings included with this aircraft and any related accessories, components or parts (including, but not limited to, chargers, rechargeable batteries, etc.). **CAUTION:** The electronic speed controls (ESCs) installed in the TYPHOON are not compatible with any other product, and the TYPHOON is not compati

ble with any other ESCs. Use of any other ESCs in the TYPHOON will cause a crash, which may result in damage to the product, property and/or cause serious injury.The TYPHOON Q500 4K RTF Contents

6 The TYPHOON RTF includes everything needed to fly right out of the box. There’s nothing extra to buy or provide!

1 The TYPHOON RTF Airframe w/Installed CGO3 2 ST10+ Transmitter and Personal Ground Station 3 ST10+ LCD Screen Sun Shade/Shield 4 ST10+ Neck Strap 5 AC to DC USB Adapter/Charger 6 USB to Micro USB Cable 7 USB Interface/Programmer 8 5400mAh 3S 11.1V LiPo Battery 9 3S 11.1V LiPo Balance Connector Charge Lead 10 DC 3S 11.1V LiPo Balancing Charger 11 DC Automobile Accessory Socket/ Cigarette Lighter Receptacle Adapter 12 AC to DC Adapter/Power Supply 13 16GB microSD Card w/Adapter 14 Motor Holder/Prop Installation Tool 15 Propellers/Rotor Blades (2 sets) 16 CGO STEADYGRIPTM **1**

**6 9**  **10 13**  **11 16**  **14**

**8 7**  **3 15** 

**2 4** 

**5**

**12**7 Battery Warnings and Usage Guidelines
**WARNING: Lithium Polymer (LiPo) batteries are significantly more**  **volatile than alkaline, NiCd or NiMH batteries. All instructions and warnings must be followed exactly to prevent property damage and/or**  **serious injury as the mishandling of LiPo batteries can result in fire. By handling, charging or using the included LiPo battery you assume all risks**  **associated with LiPo batteries. If you do not agree with these conditions please return the complete product in new, unused condition to the place**  **of purchase immediately.**

• You must always charge the LiPo battery in a safe, well-ventilated area away from flammable materials.
• Never charge the LiPo battery unattended at any time. When charging the battery you must always remain in constant observation to monitor the charging process and react immediately to any potential problems that may occur. • After flying/discharging the LiPo battery you must allow it to cool to ambient/room temperature before recharging.
• To charge the LiPo battery you must use only the included charger or a suitably compatible LiPo battery charger. Failure to do so may result in a fire causing property damage and/or serious injury.
• If at any time the LiPo battery begins to balloon or swell, discontinue charging or discharging immediately. Quickly and safely disconnect the battery, then place it in a safe, open area away from flammable materials to observe it for at least 15 minutes. Continuing to charge or discharge a battery that has begun to balloon or swell can result in a fire. A battery that has ballooned or swollen even a small amount must be removed from service completely.
• Do not over-discharge the LiPo battery. Discharging the battery too low can cause damage to the battery resulting in reduced power, flight duration or failure of the battery entirely. LiPo cells should not be discharged to below 3.0V each under load.
• Store the LiPo battery at room temperature and in a dry area for best results. • When charging, transporting or temporarily storing the LiPo battery the temperature range should be from approximately 40–120° F (5–49° C). Do not store the battery or aircraft in a hot garage, car or direct sunlight. If stored in a hot garage or car the battery can be damaged or even catch fire.
• Never leave batteries, chargers and power supplies unattended during use. • Never attempt to charge low voltage, ballooned/swollen, damaged or wet batteries.
• Never allow children under 14 years of age to charge batteries.
• Never charge a battery if any of the wire leads have been damaged or shorted.
• Never attempt to disassemble the battery, charger or power supply.
• Never drop batteries, chargers or power supplies.
• Always inspect the battery, charger and power supply before charging.
• Always ensure correct polarity before connecting batteries, chargers and power supplies.
• Always disconnect the battery after charging.
• Always terminate all processes if the battery, charger or power supply malfunctions. **IMPORTANT NOTE:** It’s safer and better for the longevity of the battery to store it only partially charged for any length of time. Storing the battery approximately 50% charged (which is around 3.85V per cell) is typically best, however, it will take some careful management of the charge time and the use of a volt meter to achieve this voltage. If you have the equipment and skills to achieve the 50% charge level for storage it is re commended. If not, simply be sure to not store the battery fully charged whenever possible. In fact, as long as the battery will be stored at approximately room temperature and for no more than a few weeks before the next use, it may be best to store the battery in the discharged state after the last flight (as long as the battery was not over-discharged on the last flight).Charging The Batteries **WARNING: Lithium Ion (LiIon) and Lithium Polymer (LiPo) batteries are significantly more volatile than alkaline, NiCd or NiMH batteries. All**  **instructions and warnings must be followed exactly to prevent property damage and/or serious injury as the mishandling of LiIon/LiPo batteries**  **can result in fire. By handling, charging or using the included LiIon/LiPo batteries you assume all risks associated with them. If you do not agree**  **with these conditions please return the complete product in new, unused condition to the place of purchase immediately.**  **CHARGING THE LIPO FLIGHT BATTERY** You can power the SC3500-3 charger from a 100-240V AC outlet using the AC adapter/power supply, or from a 12V DC accessory socket/cigarette lighter receptacle in a vehicle using the corresponding adapter. Once you’ve verified the charger is powered on and ready to charge (green blinking LED), plug the balance connector charge lead into the charger, then connect the LiPo flight battery to the charge lead. The battery will begin charging (red blinking LED) and it will take approximately 2 hours to charge a fully discharged (not over-discharged) battery. **CHARGING THE LI-ION ST10+ BATTERY** You can charge the LiIon battery installed in the ST10+ from a 100-240V AC outlet using the USB adapter/charger, or from a suitable USB power source (2.0 amps max), with the USB to micro USB cable. While the ST10+ is powered off connect the cable to the USB adapter/charger, then plug it into the USB connector/charging port on the right side. After approximate

ly 30-45 seconds the LED indicator for the battery will blink blue while the battery is charging, and will glow solid blue when the battery is fully charged. It will take approximately 5.5 hours to charge a fully discharged (not over-discharged ) battery. **NOTE:** The AC plug type will vary depending on the region in which the product was imported/purchased (AU = Australian; EU = European; UK = United Kingdom; US = United States). 8Preparing The CGO3
**WARNING:** Before installing the flight battery and powering on the TYPHOON you MUST remove the cover/lock from the rear of the CGO3 by carefully sliding it backward. Failure to remove the cover/lock can result in damage to the TYPHOON and the CGO3! **QUICK TIP:** It’s a good idea to re-install the cover/lock after each flying session and while transporting/storing the TYPHOON (just remember to remove the cover/lock before powering on the TYPHOON and CGO3!).

**Step 1)** Remove the cover/lock from the rear of the CGO3 by carefully sliding it backward. **Step 2)** Slide the microSD card into the corresponding slot on the bottom of the CGO3. You can use the included 16GB card or any name brand Class 10 microSD card up to 128GB. **Step 3)** Carefully remove the protective material from the camera lens. Installing The Propellers
**WARNING:** We recommend wearing gloves and using extreme care when installing the propellers/rotor blades.

Each motor and propeller are marked with an ‘A’ or ‘B’ to ensure easy installation in the correct positions (for example: install propellers marked with ‘A’ on motors marked with ‘A’). **IMPORTANT NOTE:** It is NOT possible to install a propeller marked with ‘A’ on a motor marked with ‘B’. The threads go in different directions for the ‘A’ and ‘B’ motors/propellers. **Step 1)** Use the special tool (included) to hold the motor so it cannot spin. **CAUTION:** Do not over-tighten the propellers when using the tool. **Step 2)** Install the corresponding propeller by rotating it trialing edge first until it‘s secure against the o-ring located at the bottom of the motor shaft. You may want to add this: Continue to screw down the propeller 1-1.5 turns more to ensure it is properly tighten and compressing the O-rings slightly. **Step 3)** Repeat steps 1 and 2 to install the three remaining propellers securely.
9 B

B A

AThe TYPHOON Q500 4K, CGO3 And ST10+ Overview

The TYPHOON Q500 4K / CGO3
1 CGO3 Gimbal Camera 2 Camera Microphone 3 Camera LED Status Indicator 4 Camera Lens 5 5.8GHz Antenna 6 Main LED Status Indicator 7 Power Switch
ST10+ 8 Proportional Control Rate Slider 9 USB Connector/Charging Port 10 Audio/Earphone Jack 11 Take Still Photo Button 12 Start/Stop Motors Button 13 Rudder/Yaw Control (for Mode 2 and Mode 1) 14 Throttle/Altitude Control (for Mode 2) Elevator/Pitch Control (for Mode 1) 15 5.8GHz Antenna (located inside the case) 16 Status Indicators (for ST10+ battery, 5.8GHz WiFi and GPS) 17 2.4GHz Antenna (located inside the handle) 18 Start/Stop Video Recording Button 19 Flight Mode Selection Switch 20 Aileron/Roll Control (Mode 2 and Mode 1) 21 Elevator/Pitch Control (Mode 2) Throttle/Altitude Control (Mode 1) 22 Power Switch 23 Volume and Navigation Touch-Activated Buttons Volume Down/VolumeUp/Menu/Home/Back) 24 CGO3 Pitch Angle/Position Control Slider 25 SD Card Slot (located under the battery) The ST10+ is equipped with an internal cooling fan and components that deliver vibrating and audible alerts. **IMPORTANT NOTE:** Although the ST10+ is equipped with digital ‘trims’ (located below the control sticks) they are not active/functional when controlling the TYPHOON. 10 6

7

8

9

10 11 12 13 14 15 16 17

18 19 20 21 22

23 24

2511 ST10+ Display

1 Model Name 2 Status Information 3 Direction to Home Point 4 Clock/Current Time 5 Watch Me/Follow Me Button 6 GPS Status and Number of Satellites for ST10+ 7 ST10+ Battery Charge Level Status Icon 8 Aircraft Battery Voltage 9 Altitude of Aircraft (Above Ground Level) 10 Ground Speed of Aircraft 11 Distance of Aircraft from Home Point 12 Model Select Menu Button 13 In Flight Settings 14 Flight Settings Menu Button 15 System Settings Menu Button 16 Latitude/Longitude Position of Aircraft 17 Number of Satellites for Aircraft 18 GPS Status for Aircraft 19 Flight Mode of Aircraft The ST10+ is equipped with a touchscreen display that allows for changing various settings and viewing real-time telemetry data and streaming video during flight.

**QUICK TIP:** 1. Double tap on the screen to increase the size of the video viewing area to full-screen and double tap again to return to the standard size. 2. Single tap to hide the camera settings, tap again to display camera settings.
**WARNING:** NEVER attempt to fly the TYPHOON via First-Person View (FPV). There’s a slight ‘lag’ in the CGO3 streaming video downlink to the ST10+, and as a result the streaming video/FPV should only be used for aligning camera shots and not for flying! Attempting to fly via FPV can result in a crash that will cause damage to the product, property and/or cause serious injury.
**IMPORTANT NOTE:** Streaming video from the CGO3 to the ST10+ and to a separate phone/tablet (or another Yuneec transmitter/personal ground station) at the same time is NOT recommended as it will result in a very significant lag in the video downlink. **8 7**  **6 5**  **4**

**9**

**10**

**11 19** 

**18**

**17**

**16**

**14 15**  **12 13**  **2 1**  **3**

Model:Q500 Welcome,Pilot 07:25

GPS N/A

SAT N/A

POS N/A E N/A N MODE N/A

ALT N/A ft VOLTS N/A V

G-SPD N/A mph

DIS N/A ft

System Settings Flight Settings Model Select AWB

3840 x 2160 F3012 ST10+ Accessories You can install the included and optional-use Neck Strap to help hold and support the ST10+. You can also install the included and optional-use LCD Screen Sun Shade/Shield to help improve viewing in sun light.

**QUICK TIP:** It may be helpful to apply suitable anti-glare screen protector material over the LCD screen to further improve viewing in sun light. **CAUTION:** Do not bend, or move around in excess as the strap can come unhooked from the ST10+ and potentially fall and damage the sensitive electronic components. Moving the left-hand stick to the left will turn (yaw) the nose of the TYPHOON to the left about the vertical axis. And moving the stick to the right will turn (yaw) the nose of the TYPHOON to the right. Flight Controls
**NOTE:** The information in this and the following sections refers to the default ‘Mode 2’ control configuration of the ST10+. The left-hand stick on the ST10+ controls the throttle (climb/descend) and rudder (yaw left/right) channels.. When the left-hand stick (also known as the throttle stick) is in the middle position during flight the TYPHOON will maintain the current altitude. As you move the stick upward the TYPHOON will climb, and as you move the stick downward the TYPHOON will descend. The farther away from the middle position you move the stick the faster the TYPHOON will climb or descend. **IMPORTANT NOTE:** The maximum altitude is limited to 400 feet (122 meters) AGL (Above Ground Level) in both Smart and Angle (Pilot) Mode. And although this limit can be adjusted using the USB interface/program

mer and software we strongly recommend using the default limit at all times.

Maximum Climb Rate: 2m/s (6.6f/s)13 **SELECTING A FLIGHT MODE** the TYPHOON is programmed with three (3) flight modes that can be selected via the Flight Mode Selection Switch located just above the right-hand control stick. **PROPORTIONAL CONTROL RATE SLIDER** The Proportional Control Rate Slider located on the right side of the ST10+ allows you to set the overall climb/descend and directional control rates. Use the turtle position for the lowest control rates (best for first-time pilots and required when flying between 5000 feet and 8000 feet Above Mean Sea Level), and use the rabbit position for the highest control rates (best for experienced pilots and can only be used when flying below 5000 feet MSL). Or use a position in between if you prefer. When the Flight Mode Selection Switch is the top position the TYPHOON will be in Smart Mode. Although we recommend learning to fly the TYPHOON in Angle (Pilot) Mode as soon as possible, Smart Mode is typically the best mode for first-time pilots to fly in which also features ‘Follow Me’ and ‘Watch Me’ functions. In Smart Mode the TYPHOON will always move in the direction the right-hand control stick is pushed relative to the pilot and no matter which way the front/nose is pointed. So if you push the stick to the left the TYPHOON will always move to the left, regardless of the direction the nose is pointing and even if it’s spinning. This mode can also be helpful for pilots that lose orientation while flying in Angle (Pilot) Mode. Flight Controls - Smart Mode

SMART CIRCLE*

*Ø 52 feet / 16 meters14 **FOLLOW ME FUNCTION** The Follow Me function allows the TYPHOON to follow the pilot, adjusting its location to the location of the ST10+. This function is enabled when ST10+ GPS positioning completes, and the TYPHOON is using shared GPS signal with the ST10+. At this time, you will see in orange , and in green color. When in Follow Me function, the TYPHOON will follow the movement of ST10+ if there is no extra operation on the ST10+. The flight status is also controllable when you operate ST10+ and CGO3.

Important Note: In Follow Me function, the aircraft will maintain a constant altitude and cannot detect obstacles. Pilots who change their altitude by for example, moving to higher ground, during flight should be mindful of this. MODE FollowSystem Setting Flight Setting Model Select MODE Model: 4K WELCOMEPILOT 11:25:11am

Watch

GPS N/A

SAT N/A

POS N/A E N/A N VOLTS
N/A V

ALT N/A ft

G-SPD N/A mph

DIS
N/A ft 3840 x 2160 F30 **WATCH ME FUNCTION** Watch Me function enables the camera to keep tracking the remote contro l

ler no matter where and how it moves as the camera can automatically tilt its angle according to the controller. Usually, the default function under Smart Mode is Follow Me. Watch Me function can be switched to by following steps:

15 In Watch Me function, the pilot will always be kept in the frame wherever he moves. Welcome,Pilot 10:48:28 pm 10

GPS Ready

SAT 13

POS 00.0000E 00.0000N MODE Follow

ALT 21.4 ft VOLTS
12.3 V

G-SPD 0.0 mph

DIS 22.5 ft

System Settings Flight Settings Model Select 3840 x 2160 F30 Model: Typhoon

Model: Typhoon Welcome,Pilot 10:48:28 pm 10

GPS Ready

SAT 13

POS 00.0000E 00.0000N MODE Watch

ALT 21.4 ft VOLTS
12.3 V

G-SPD 0.0 mph

DIS 22.5 ft

System Settings Flight Settings Model Select 3840 x 2160 F30

Press , the button will change from ORANGE to GREEN. And now it is in Watch Me function. NOTE: Once the TYPHOON is above 2m and out of Smart Circle during flying, the TYPHOON yaw direction will take the control itself. Camera lens will always point to you as long as Flight Mode Selection Switch is in Smart Mode. Please put the CGO3 Pitch Angle/Position Control Slider in the middle position. If you want to trim the camera angle up, then just move the Pitch Angle/Position Control Slider a bit up. If you want to trim the camera angle down, just move the slider down. Watch Me/Follow Me Button: When in Smart Mode, press to switch the TYPHOON between Watch Me and Follow me function. Follow Me function is the default setting, and the button is ORANGE. If it is GREY, it means ST10+ GPS isn’t ready yet. Please wait.16 **Additional Angle (Pilot) Mode Features:**
**POSITION HOLD AND SELF-LEVELING** the TYPHOON will automatically hold its position (with a suitable GPS signal/lock) and maintain a level attitude when the right-hand stick is centered.
**WARNING:** If you do not properly control the TYPHOON in Angle (Pilot) Mode the aircraft may crash or even ‘fly away’.
**IMPORTANT NOTE:** Crash damage and ‘fly aways’ are NOT covered under warranty. Flight Controls - Angle (Pilot) Mode When the Flight Mode Selection Switch is the middle position the TYPHOON will be in Angle (also known as Pilot) Mode.
Angle (Pilot) Mode is the mode preferred by experienced RC/drone pilots because the TYPHOON will move in the direction the control stick is pushed relative to the front/nose of the aircraft. So if you push the right-hand stick to the left the TYPHOON will bank toward the left side and move to the left. This means if the front/nose of the TYPHOON is pointing away from you it will move to the left, but if the front/nose is pointing at you the TYPHOON will move to the right. **Additional Smart Mode Features:** ***SMART CIRCLE** In most cases the Smart Circle will keep the TYPHOON from coming within approximately 26 feet (8 meters) of you (as long as you position yourself at least 26 feet/8 meters behind the TYPHOON.
**GEO-FENCE** The geo-fence is a virtual ‘barrier’ that will keep the TYPHOON from travel

ing further than 300 feet (91 meters). Although this limit can be adjusted using the USB interface/programmer and software we strongly recommend using the default limit at all times. **WARNING: Smart Mode only works when the TYPHOON has a suitable GPS signal/lock. If you take off in Smart Mode and the TYPHOON loses**  **GPS signal/lock it will switch to Angle (Pilot) Mode automatically. This is why we strongly recommend learning to fly in Angle (Pilot) Mode as soon**  **as possible. Otherwise, if you lose GPS signal/lock and are not able to properly control the TYPHOON in Angle (Pilot) Mode the aircraft may**  **crash or even ‘fly away’.**
**IMPORTANT NOTE:** Crash damage and ‘fly aways’ are NOT covered under warranty.Flight Controls - Home Mode When the Flight Mode Selection Switch is in the bottom position the TYPHOON will be in Home (also known as Return to Home) Mode.

PILOT LOCATION 13-26 ft (4-8m) LANDING LOCATION In Home Mode the GPS connectiv

ity will fly back the TYPHOON , a nd automatically land within 13-26 ft (4-8m) of the pilot. This can be very helpful for first-time pilots who aren’t quite ready to land the TYPHOON themselves. It can also be helpful for pilots that lose orientation during flight; simply activate Home Mode until the TYPHOON automatically moves toward the home position, and once you’ve confirmed orientation switch back to Angle (Pilot) Mode. And if the TYPHOON ever loses the link with the ST10+ it will automatically enter Home Mode. **When Home Mode is activated the TYPHOON will respond as follows:** 10 m

10 m **B)** When flying lower than 33 feet (10 meters) the TYPHOON will climb to 33 feet (10 meters) while flying back to the home point, or active home position, then descend vertically until it lands. **A)** When flying higher than 33 feet (10 meters) the TYPHOON will maintain the current altitude, fly back to the home point, , or active home point if the ST10+ has enough satellites for Follow Me, then descend vertically until it lands.

17**B)** When flying lower than 33 feet (10 meters) the TYPHOON will climb to 33 feet (10 meters) while flying back to the home point, or active home position, then descend vertically until it lands.

**CAUTION:** You must be certain there are no obstacles in the ‘Return to Home’ flight path otherwise the TYPHOON may come into contact with them and crash. And while the TYPHOON is in Home Mode you will have a limited amount of directional control to help avoid obstacles, however, we strongly recommend switching to Smart or Angle Mode to avoid the obstacle (then you can switch back to Home Mode). **WARNING:** Home Mode only works when the TYPHOON has a suitable GPS signal/lock. If the TYPHOON loses GPS signal/lock it will switch to Angle (Pilot) Mode automatically. This is why we strongly recommend learning to fly in Angle (Pilot) Mode as soon as possible. Otherwise, if you lose GPS signal/lock and are not able to properly control the TYPHOON in Angle (Pilot) Mode the aircraft may crash or even ‘fly away’.
**IMPORTANT NOTE:** Crash damage and ‘fly aways’ are NOT covered under warranty. Led Status Indications

1819Press to enter Photo Capturing, and press Button A to take pictures. in this mode, the photos taken are 12 megapixels. Press to enter Video Recording, and press Button B to start or stop recording. **CAUTION:** ALWAYS stop recording video before turning off the TYPHOON/CGO3 to avoid data loss. If you accidentally turn off the TYPHOON/CGO3 before you stop recording, re-insert microSDcard (if removed) and turn the system on again. Wait approximately 20 seconds until the camera LED starts to glow solid green indicating the last video file was recovered. **CAUTION:** When enter Photo Capturing, video recording is disabled. You MUST switch to video recording to start record videos. During video recording, picture taking (Button A) is accessible. The resolution is set by the video resolution. In this mode, you will capture still phtos from the video. Taking Photos And Recording Video
The ST10+ seamlessly integrates control of the CGO3 so you can easily take still photos and start/stop video recording using the corresponding buttons located on top:

**TO START/STOP RECORDING VIDEO** Press the button located near the top right corner of the ST10+. You’ll hear an audible indication from the ST10+ each time the recording starts/stops. And while video is recording the LED indicator on the front of the CGO3 will flash blue and green, and there will be a red dot next to the time length of the recording near the upper right-hand corner on the screen of the ST10+. **CHOOSING CGO3 PRO FOR TAKING PHOTOS AND RECORDING VIDEOS** If users are professionals in photography and video graphy, and want to reset related specifications, please follow the steps below: Step 1) Press Flight Settings, choose Camera Select, press C-GO3-Pro, press Select, and press OK. Step 2) The second left column is available for adjusting the camera settings, like white balance, etc. Step 3) Press , and press Video Settings, different video resolutions are available.

**NOTE:** CGO3 camera is the default selection in ST10+. You can take still phtos while video recording. The resolution is set by the video resolution. In this mode, you will capture still photos from the video. **CAUTION:** Do not change settings when aircraft is further than 1,000 feet from ST10+. **TO TAKE A STILL PHOTO** Press the button located near the top left corner of the ST10+. You’ll hear an audible ‘shutter’ sound from the ST10+ and the LED indicator on the front of the CGO3 will change from glowing solid green to glowing solid blue. It will take approximately 1-2 seconds to capture the photo and before you can take another still photo.

20 Model:Typhoon Welcome,Pilot 07:25

GPS N/A

SAT N/A

POS N/A E N/A N MODE N/A

ALT N/A ft VOLTS N/A V

G-SPD N/A mph

DIS N/A ft

System Settings Flight Settings Model Select WB

ISO 32 1/250s Auto Auto

Lock

Sunny

Cloudy

Fluorescent

AWB

3840 x 2160 F30 A B

CInstalling The Flight Battery After the flight battery has been fully charged it’s ready to be installed in the TYPHOON: **IMPORTANT NOTE:** Keep the TYPHOON level relative to the ground when installing the battery.

**STEP 1)** Push the area at the top of the battery door to release the latch/lock, and then open the door. **STEP 2)** With the side of the battery cartridge that has the ‘UP’ arrow marking oriented upward, hold the handle and slide the battery into the battery compartment until you feel the connector make a positive connec

tion. **NOTE:** If you do not install the battery in the correct orienta tion it will not be possible to make a positive connection. **WARNING:** Do not force the battery in to make the connection. It should be smooth with little restriction. If it feels tight remove the battery check the connector pins for alignment, and try again. Forcing the battery in can damage the connector and potentially cause the TYPHOON to loose power in flight. **STEP 3)** Close the battery door by pushing the area at the top to engage the latch/lock. **NOTE:** If the door will not close because it’s coming into contact with the handle on the battery cartridge, the battery is not inserted far enough to engage the connector properly. GPS Functionality the TYPHOON requires a suitable GPS signal/lock in order to start the motors and to be flown. This means it should only be operated outdoors in open areas that are free from people, vehicles and other obstructions. And in order to acquire a suitable GPS signal/lock it’s critical that the GPS anten

na installed in the top of the TYPHOON always have a clear view of the sky (100° minimum clearance required). **WARNING:** Do NOT attempt to fly near or between tall buildings/ob

structions, near or under dense vegetation, structures or indoors. Do NOT attempt to fly the TYPHOON wit h GPS enabled indoors or in any location known to have poor GPS coverage. And do NOT disable/turn off GPS unless you’re able to properly control the TYPHOON in Angle (Pilot) Mode without GPS assistance and accept ALL responsibility and liability for crashes or ‘fly aways’. If the TYPHOON loses GPS signal/lock while flying it can only be flown in Angle (Pilot) Mode. Smart Mode and Home Mode, along with their corresponding features, will no longer work. And the Main LED Status Indicator will flash purple and the LED Status Indicators below the motors will flash three (3) times per second then will stay off for one (1) second when the TYPHOON loses GPS signal/lock (or if GPS has been disabled/turned off). If the GPS signal/lock is reacquired (after receiving 5–10 seconds of suitable GPS signal), Smart Mode and Home Mode will work again.
**WARNING:** Loss of GPS signal/lock may result in a crash or even a ‘fly away’. 100  ̊

21**IMPORTANT NOTE:** Crash damage and ‘fly aways’ are NOT covered under warranty. **NO-FLY ZONES** With a suitable GPS signal/lock it will not be possible to start the motors, takeoff or fly the TYPHOON in the ‘No-Fly Zones’ within a 4 mile (6.4 kilometer) radius of most major airports. Preparing to Fly

22 **WARNING:** Before flying you MUST review and understand all of the NOTICES AND WARNINGS and the GENERAL SAFETY PRECAUTIONS AND WARNINGS found near the beginning of this instruction manual. Failure to operate this product in a safe and responsible manner could result in damage to the product, property and/or cause serious injury.
**WARNING:** Always operate the TYPHOON in open areas (approximately 10000 square feet/930 square meters or more) that are free from people, vehicles, trees and other obstructions. Never fly near or above crowds, airports or buildings. **IMPORTANT NOTE:** If you’re a first-time pilot we strongly recommend putting the Flight Mode Selection Switch (located just above the right-hand control stick) in the top position to activate Smart Mode. Or, if you’re an experienced RC/drone pilot we strongly recommend putting the switch in the middle position to activate Angle (Pilot) Mode. **Step 2)** Place the TYPHOON on a level and stable surface then slide the power switch to the ‘ON’ position. **DO NOT TOUCH OR MOVE THE TYPHOON UNTIL THE INITIALIZATION PROCESS IS COMPLETE.**  The Main LED Status Indicator on the bottom of the TYPHOON will show one of the following indications when initialization is complete:

• the TYPHOON is in Smart Mode with GPS lock Glows solid green, or flashes white every 3 seconds indicat

ing it can operate in Follow Me.
• the TYPHOON is in Smart Mode without GPS lock Flashes green (3 times per second) then off (for 1 second)
• the TYPHOON is in Angle (Pilot) Mode with GPS lock Glows solid purple
• the TYPHOON is in Angle (Pilot) Mode without GPS lock Flashes purple (3 times per second) then off (for 1 second) **Step 3)** If you do not have a GPS lock move the TYPHOON to a different area, turn it off, then back on again. Or, if you have a GPS lock, proceed to 10000 ft2 (930m2) Never attempt to operate the TYPHOON nearby tall buildings/ob

structions that do not offer a clear view of the sky (a minimum clearance of 100°). **After selecting a suitable flying area, please follow these steps:**  **Step 1)** ALWAYS turn the ST10+ on and allow it to boot up fully BEFORE turning the TYPHOON on. the next step. **Step 5)** Step back approximately 26 feet (8 meters) behind the TYPHOON. PILOT LOCATION TAKEOFF ZONE

26 ft (8m)the next step. **Step 5)** Step back approximately 26 feet (8 meters) behind the TYPHOON.

Flying
**TAKEOFF**

To takeoff, raise the left-hand stick to above the center position. the TYPHOON will takeoff and climb slowly (or raise the stick further until it does). Allow the stick to return to the center position when the TYPHOON reaches the desired altitude.
FLYING Take your time learning how the TYPHOON responds to various control inputs while flying. In Smart Mode the TYPHOON will always move in the direction the right-hand control stick is pushed relative to the pilot and no matter which way the front/nose is pointed. In Angle (Pilot) Mode the TYPHOON will move in the direction the control stick is pushed relative to the front/nose of the aircraft (and the ‘angle’ of movement is determined by how far you push the stick away from the center position). Please see the corresponding sections of this instruction manual for more information on Smart Mode and Angle (Pilot) Mode.
**IMPORTANT NOTE:** If at any time during flight you feel like the TYPHOON is drifting out of/beyond your control, simply release both control sticks. the TYPHOON will automatically self-level and will even hold its position (with a suitable GPS signal/lock) when both control sticks are centered. You can also activate Home Mode so the TYPHOON automatically flies itself back to the home point and lands.
**LANDING** There are two ways to land the TYPHOON: **1)** Position the TYPHOON above the area where you would like to land. Slowly lower the left-hand stick to below the center position. the TYPHOON will descend slowly and land. After the TYPHOON lands, press and hold the red START/STOP button for approximately two (2) seconds to stop the motors. **2)** Activate Home Mode and the TYPHOON will automatically fly itself back to the home point and will land within a 10 foot (3 meter) diameter circle around it.
**NOTE:** An alternate form to shut the rotors off in the case of a button failure is to land the TYPHOON and simply switch into Home Mode. The rotors will shut off if the TYPHOON is on the ground.
**WARNING:** Always land as soon as possible after the first level low voltage battery warning, or land immediately after the second level low voltage battery warning (as indicated by the vibrations and audible alerts from the ST10+, and by the LED Status Indicators below the Motors flashing rapidly). If at any time the Aircraft Battery Voltage shown on the screen is below 10.7V, land the TYPHOON immediately. **WARNING:** Do not attempt to operate the TYPHOON in winds that exceed 8–12 miles per hour (13–19 kilometers per hour). **Step 6)** Press and hold the red START/STOP button for approxi

mately three (3) seconds to start the motors. Or you can lower the left-hand stick all the way, move it all the way to the left, then all the way to the right and back to the middle to start the motors.

23**IMPORTANT NOTE:** Every time you turn the TYPHOON on it will default to having GPS active/on (even if you disabled GPS the last time is was powered on). **There are two ways to disable the GPS:**

**GPS can also be disabled manually:** Step 1) While the ST10+ and the TYPHOON are powered on and linked (and the motors are NOT running), move the Proportional Control Rate Slider on the right side of the ST10+ to the uppermost (rabbit) position. Step 2) Move the right-hand stick all the way to the right and hold it there until step 3 is completed. Step 3) Move the Flight Mode Selection Switch from Smart to Home and Home to Smart mode 4 times in 3 seconds. When GPS has been disabled successfully the TYPHOON will emit an audible indication and the GPS status on the ST10+ screen will show ‘Disabled’. Also, the Main LED Status Indicator will flash purple and the LED Status Indicators below the Motors will flash three (3) times per second then will stay off for one (1) second. **AFTER LANDING** ALWAYS turn off the TYPHOON BEFORE turning off the ST10+. Then remove the battery from the TYPHOON and allow it to cool to ambient/room temperature before recharging.
**WARNING:** Do NOT leave the ST10+ and the TYPHOON powered on and do NOT leave the flight battery installed inside the TYPHOON as doing so can over-discharge and damage the batteries. Over-discharging can cause damage to the batteries resulting in reduced performance or failure of the batteries entirely.
**IMPORTANT NOTE:** Battery damage, crash damage and ‘fly aways’ are NOT covered under warranty. Disabling GPS
**WARNING:** Smart Mode and Home Mode, along with their corresponding features, only work when GPS is active and the TYPHOON has a suitable GPS signal/lock. If you disable/turn off GPS the TYPHOON can only be flown in Angle (Pilot) Mode. And if you cannot properly control the TYPHOON in Angle (Pilot) Mode the aircraft may crash or even ‘fly away’.
**IMPORTANT NOTE:** Crash damage and ‘fly aways’ are NOT covered under warranty. We do not typically recommend disabling GPS for any reason, especially if you’re a first-time or low-time pilot. However, if you’re an experienced pilot that’s able to properly control the TYPHOON in Angle (Pilot) Mode, and you do not exceed any altitude/distance limits or fly in any ‘no fly zones’ in your area, you can disable/turn off GPS. Do NOT disable/turn off GPS unless you accept ALL responsibility and liability for crashes or ‘fly aways’. Graphical User Interface (GUI) You can download the graphical user interface (GUI) software on the TYPHOON product page at www.Yuneec.com. Follow the on-screen instructions to install and operate the software which allows you to see the status of all sensors, to adjust various settings, check GPS accuracy, update firmware and more using the included USB Interface/Programmer.
24 When the CGO3 and ST10+, the multi-copter and ST10+ are bound, press on ST10+ interface, GPS switch can be found, and turned off.Compass Calibration

**Step 5)** When the main LED status indicator flashes red and green slowly (2 times per second) you have entered compass calibration mode. Pick up the aircraft and hold it flat with the nose pointed to the north. After 5 seconds the main LED status indicator should flash red and green rapidly (5 times per second). **Step 7)** Rotate the aircraft 45 degrees to the left. Then slowly rotate the aircraft 360 degrees toward the north (as illustrated) until it's flat and upright in your hands again. **Step 6)** Slowly rotate the aircraft 360 degrees toward the north (as illustrated) until it's flat and upright in your hands again. **Step 8)** Rotate the aircraft 45 degrees to the left. Then slowly rotate the aircraft 360 degrees toward the north (as illustrated) until it's flat and upright in your hands again. **Step 1)** Do not calibrate the compass inside parking structures, near buildings or surfaces with metal in them (like roads parking lots with rebar). Only calibrate the compass in open areas/fields far away from power lines and other metallic or concrete surfaces/structures

. **Step 2)** Turn on the transmitter and allow it to boot up fully before turning on the aircraft. And when the transmitter and aircraft are powered on and linked proceed to the next step.

25 **Step 4)** If successful, THPHOON will beep, Return to the main screen. 'Mag Cali' will be displayed in MODE area. CAMERA

MULTICOPTER Video Settings

Audio Switch

GPS

Calibration OFF

ON Compass
Accelerometer

**Step 3)** Tap the Setting button on the ST10+ screen, then tap the Calibration button. Choose Compass option and tap it. Model: Typhoon Welcome,Pilot 07:25

GPS N/A

SAT N/A

POS N/A E N/A N MODE Mag Cali

ALT N/A ft VOLTS N/A V

G-SPD N/A mph

DIS N/A ft

System Settings Flight Settings Model Select 3840 x 2160 F30**Step 9)** Rotate the aircraft 45 degrees to the left. Then slowly rotate the aircraft 360 degrees toward the north (as illustrated) until it's flat and upright in your hands again.

**IMPORTANT NOTE:** If compass calibration fails the main LED status indicator will glow solid white and you must restart the calibration process. **Step 11)** If you hear an audible indication after the main LED status indicator stops blinking rapidly you have successfully completed compass calibration. **Step 10)** The main LED status indicator should be flashing red and green rapidly (5 times per second). Hold the aircraft as still as possible until it main LED status indicator stops blinking rapidly. **IMPORTANT NOTE:** Steps 6 to 9 must be completed in less than 30 seconds in order to successfully complete compass calibration. 30

26ST10+ and Receiver Binding **Step 1)** Turn on the TYPHOON, and after the Main LED Status Indicator begins to flash blue rapidly, lift the back end upward approximately 45° then back down to ‘level’ two (2) times to put the aircraft/receiver into bind mode. The Main LED Status Indicator will begin to the flash orange very rapidly when the aircraft/receiver are in bind mode. 2 x 45+ °

**Step 2)** Turn on the ST10+, and if required tap the screen (outside of the pop up status window) to bypass the RC and WiFi connection process. **Step 3)** Tap the ‘Model Select’ button, and if required press ‘OK’ to bypass any pop up warnings/alerts. **Step 4)** Select the existing model (for example: ‘the TYPHOON’) you would like to bind to (or create a ‘New Model’), and if required press ‘OK’ to bypass any pop up warnings/alerts. Model: 4K Welcome,Pilot 10:48:28 pm 10

GPS Ready

SAT 13

POS 00.0000E 00.0000N MODE Angle

ALT 21.4 ft VOLTS
12.3 V

G-SPD 0.0 mph

DIS 22.5 ft

System Settings Flight Settings Model Select HOME

27 **Step 5)** Tap the ‘Flight Settings’ button, and if required press ‘OK’ to bypass any pop up warnings/alerts. **Step 6)** Tap the ‘Bind’ button and select the ‘SR24_XXXXX’ receiver listed in the column under ‘Model’, then tap ‘OK’ after the connection has been established. **Step 7)** Tap the ‘Back’ button two (2) times to return to the main screen and the model/receiver should automatically connect to the ST10+. Model: 4K Welcome,Pilot 10:48:28 pm 10

GPS Ready

SAT 13

POS 00.0000E 00.0000N MODE Angle

ALT 21.4 ft VOLTS
12.3 V

G-SPD 0.0 mph

DIS 22.5 ft

System Settings Flight Settings Model Select HOME

Model: 4K Welcome,Pilot 10:48:28 pm 10

SR24_16042

SR24_16042 Not connected

Model Camera

Model: 4K Welcome,Pilot 10:48:28 pm 10
Model Select

New Model ghST10+ and CGO3 Binding

28 **Step 1)** Turn on the ST10+, and if required tap the screen (outside of the pop up status window) to bypass the RC and WiFi connection process. **Step 6)** Tap the ‘Bind’ button and select the ‘CGO3_XXXXXX’ camera listed in the column under ‘Camera’, then enter the password ‘1234567890’ when prompted and tap ‘OK’ after the connection has been established. **Step 7)** Tap the ‘Camera Select’ button and select proper camera model listed int the column under ‘Choose a camera ’, then tap ‘OK’ after the connection has been established. **Step 8)** Tap the ‘Back’ button two (2) times to return to the main screen and the camera should automatically connect to the ST10+.
**IMPORTANT NOTE:** Streaming video from the camera to the ST10+ and to a separate phone/tablet (or another Yuneec transmitter/personal ground station) at the same time is NOT recommended as it will result in a very significant lag in the video downlink. **Step 2)** Tap the ‘Model Select’ button, and if required press ‘OK’ to bypass any pop up warnings/alerts. **Step 3)** Select the existing model (for example: the‘ TYPHOON’) you would like to bind to (or create a ‘New Model’), and if required press ‘OK’ to bypass any pop up warnings/alerts. **Step 4)** Turn on the TYPHOON and ensure that the camera is powered on.
**Step 5)** if required tap the screen (outside of the pop up status window) to bypass the RC and WiFi connection process, then tap the ‘Flight Settings’ button and press ‘OK’ to bypass any pop up warnings/alerts. Model: Typhoon Welcome,Pilot 10:48:28 pm 10

GPS Ready

SAT 13

POS 00.0000E 00.0000N MODE Angle

ALT 21.4 ft VOLTS
12.3 V

G-SPD 0.0 mph

DIS 22.5 ft

System Settings Flight Settings Model Select HOME

Model: Typhoon Welcome,Pilot 10:48:28 pm 10
Model Select

New Model Typhoon

Model: Typhoon Welcome,Pilot 10:48:28 pm 10

GPS Ready

SAT 13

POS 00.0000E 00.0000N MODE Angle

ALT 21.4 ft VOLTS
12.3 V

G-SPD 0.0 mph

DIS 22.5 ft

System Settings Flight Settings Model Select HOME Model: Typhoon Welcome,Pilot 10:48:28 pm 10

CGO3_XXXXXXX Model Camera

Choose a camera NAME: C-GO1 C-GO2 C-GO3 C-GO3-Pro Model: Typhoon Welcome,Pilot 10:48:28 pm 10 Model: Typhoon Welcome,Pilot 10:48:28 pm 10

Bind

Camera Select

Hardware Monitor Mode Select

Model: Typhoon Welcome,Pilot 10:48:28 pm 10

Bind

Camera Select

Hardware Monitor Mode Select Not connected29 

### GROUND IMAGING SYSTEM
Specifictations
CGO STEADYGRIPTM Height: 223mm (8.78 in) Depth (front to back): 182mm (7.17 in) Width: 70mm (2.76 in) Weight (without gimbal/batteries): 200g (7.05 oz) Angle Control Range (Pitch): 30° to -85° Required Batteries: 2850mAh Energizer® 8x 1.5V AA Batteries (Sold Separately) Runtime: 48-64 minutes (depending on usage) Battery Warnings and Usage Guidelines

**WARNING:** Alkaline Batteries May explode or leak, and cause burn injury if recharged, disposed of in fire, mixed with a different battery type, inserted backwards or disassem

bled. Replace all batteries at the same time. Do not carry batteries loose in your pocket or purse. Do not remove the battery label. **WARNING:** All instructions and precautions must be read and followed exactly and you must follow instructions of the battery manufacturer. **WARNING:** procedures, which if not properly followed, create the probability of property damage, collateral damage and serious injury or create a high probability of superficial injury. Failure to exercise care while using this product and comply with the following conditions and guidance could result in product malfunction, excessive heat, fire, property damage, and ultimately injury. Lithium lon batteries are not toys. For the purpose of the document Li-lon, Li-Po, Li-Fe, NiCd or NiMH batteries will be described as "Batteries". **Handling and Storage:** ● Never alter, puncture or impact Batteries or related components. ● Do not directly connect the terminals with metal objects. This will short-circuit Batteries, resulting in heat and electrical discharge. ● Never store loose Batteries together, the Batteries' terminals may contact one another causing a short circuit. ● Never expose Batteries to extreme temperatures or direct sunlight. ● Always disconnect Batteries when not in use. **Before the First Charge :**  ● Ensure batteries are not damaged, as this may cause a short circuit of fire. ● Always refer to your charger's manual to ensure safe operation. ● Always charge Batteries in an open area away from flammable materials, liquids and surfaces. ● Never charge Batteries that are hot to the touch (above 120°F) If at any time Batteries become damaged, hot, or begin to balloon or swell, discontinue charging (or discharging) immediately. Quickly and safely disconnect the charger. Then place the Batteries and/or charger in a safe, open area away from flammable materials in an approved Li-Po bag to observe. After one hour, remove the Batteries from service. DO NOT continue to handle, attempt to use, or ship the Batteries. Failure to follow these procedures can cause damage to Batteries, personal property or cause serious injury. Damaged or swollen Batteries can be unstable and very hot. DO NOT touch batteries until they have cooled. Dispose of batteries in the manner required by your city, county, state or country. Contact the appropriate Yuneec Product Support Office to speak to a service technician for more information. In the event of fire, a Class D, dry chemical fire extinguisher must be used then batteries must be placed inside of an approved Li-Po bag. **Additional Guidelines and Warnings:** ● In the event of a crash, always quickly and safely disconnect and remove Batteries from the model. Then follow the previously listed safety procedures. ● If the internal contents of Batteries come into contact with your skin, wash the affected area(s) with soap and water immediately. If it comes into contact with your eye(s), flush them with generous amounts of water for 15 minutes and seek immedi

ately medical attention.30 **WARNING:** Alkaline Batteries May explode or leak, and cause burn injury if recharged, disposed of in fire, mixed with a different battery type, inserted backwards or disassembled. Replace all batteries at the same time. Do not carry batteries loose in your pocket or purse. Do not remove the battery label.
**STEP 1) Remove the Battery Cover / Door from**  **the bottom of the Steady**
**- GripTM**  Hold the bottom of the SteadyGripTM toward yourself with the front part facing downward. Installing The SteadygripTM Batteries

**WARNING:** Before switching on the SteadyGripTM it is highly recommended to first securely attach the CGO3 to your SteadyGripTM. **QUICK TIP:** It’s a good idea to ensure you have your microSD card with lots of space for photos and videos handy. **STEP 1)** Carefully slide the top part of the CGO3 (that also attaches below the nose of the Q500 the TYPHOON) onto the mount below the front part of the SteadyGripTM. A corresponding ‘click’ will be noticed once the CGO3 has securely been installed into the slide-in mount on the SteadyGripTM.

Attaching The CGO3 to The SteadygripTM

Slide the battery cover / door upward with slight force and inspect the AA battery compartment. **STEP 2) Install 8x AA Batteries** The use of rechargeable batteries is strongly recommended. Alkaline batteries only support the device to work 15 minutes. **STEP 3) Re-installing the Battery Cover / Door on the bottom of the SteadyGripTM**  Once you’ve installed 8 fresh AA batteries, Hold the bottom of the Steady

GripTM toward yourself with the front part facing downward. Slide the battery cover / door downward with slight force and ensure you hear and feel a noticeable ‘click’ indicating the battery cover / door has been closed securely. **STEP 2)** Carefully connect the CGO3’s power/control connector to the power/control port of the CGO SteadyGripTM and then insert a microSD card into the corresponding slot on the bottom of the CGO3. You can use the included 16GB card (from your RTF package) or any Class 10 microSD card up to 128GB. **STEP 3)** Powering on and initialization. Place your CGO SteadyGripTM on a flat and stable surface, then switch on the Steady

GripTM and it will initialize after 4-8 seconds of no movement or vibration. **SteadyGripTM Main LED Status:** Upon Powering on: Green LED blinking for twice and then solid GREEN for READY TO USE! Pitch Follow Function: GREEN LED blinking Low Voltage Warning: RED LED blinking slowly Power Cut-off: RED LED blinking quicklyTaking Photos and Recording Videos
1) To take a still photo, slide the Mode button to Photo Taking, press the red Photo Taking/Video Recording button. You’ll hear an audible shutter sound from the APP and the LED indicator on CGO3 front will flash in blue and green. It will take approximately 5 seconds to capture the photo and before you can take another still photo. IMPORTANT NOTE: You cannot take still photos while recording video. You MUST stop recording video, and switch to Photo Taking mode in order to take still photos. 2) To start recording videos, slide the Mode button to Video Recording, then press the red button to start. You’ll hear an audible indication from the APP each time the recording starts/stops. During recording, the LED indicator on CGO3 front will flash in blue and green. There will be recording time length display on the APP Screen. 3) To stop recording video simply press the red button located on the APP. You’ll hear an audible indication from the APP each time the recording starts/stops. And while video is recording, the LED indicator on the front of GCO3 will flash blue and green, and there will be an indicator showing time length of the recording on the APP screen. 31 Attaching A Mobile Device to The SteadygripTM
**Step 1)** Press the Curved Lip at the top front of the SteadyGripTM as illustrated and fit your Mobile Device with the screen facing toward the Main LED and Pitch Control Wheel. **Step 2)** Connect your Mobile Device to the CGO3’s WiFi by selecting CGO3’s SSID in your WiFi settings and entering the WiFi Key / Password: 1234567890. The SteadyGripTM features a camera pitch controller that allows precise camera angle control on the go. Simply roll the pitch control wheel forward to move the camera pitch/angle downward and roll the pitch control wheel backward to move the camera pitch/angle upward. Please review these instruc

tions along with the illustra

tions to familiarize yourself on how to control the CGO3 with your SteadyGripTM. Using The Camera Pitch Control Wheel

Download the free APP named as CGO3 to smart device at the APP Store or Google Play Store.In

stall the APP to your 5.8GHz WiFi capable device. Make a note of the network name and password located on the top of the gimbal assem

bly. CGO3 APP

CGO3 APP COMPATIBLE DEVICES Apple iOS: iphone 5/5c/5s/6/6+ ipad mini/mini+/3/4 Android: Mobile Devices with 5.8GHz Suport WB

ISO 32 1/250s 17:24:12

N/A32 Pitch Follow Function for CGO3 on SteadyGrip

Pitch Follow function allows the gimbal camera to track SteadyGrip in pitch direction. To Enter Pitch Follow: Press Pitch Follow Button on the top of the SteadyGrip to enter Pitch Follow Function. The green STEADYGRIP LED Status Indicator on top will start blinking instead of being solid when enter Pitch Follow. NOTE: 1) The default status of SteadyGrip is normal status without Pitch Follow. 2) When SteadyGrip is in Pitch Follow status, the gimbal camera tracks SteadyGrip in pitch direction, and the gimbal pitch control roller wheel on SteadyGrip is disabled. To Exit Pitch Follow: Press Pitch Follow Button to exit this function. Pitch Follow Button

### TROUBLESHOOTING

**ISSUE** the TYPHOON will not initialize Flight battery will not charge (red LED on charger glows solid red). the TYPHOON GPS will not lock (ST10+ indicates GPS Disabled)

the TYPHOON GPS has reduced precision

the TYPHOON GPS functions not operating properly **POSSIBLE CAUSE** the TYPHOON was moved during initialization. Poor connection between the Smart Charger and the flight battery. Overcast, thick clouds blocking GPS reception. Solar flares in progress. the TYPHOON is indoors. Objects blocking 100 degrees of clear view of the sky. (Possibly underneath a metallic or glass cover, inside a vehicle, near tall buildings, etc...) Video transmitter nearby, such as an aftermarket video downlink system. Raised threat level by the U.S. government. The GPS module is possibly damaged. The compass has been exposed to a magnet. The GPS module is possibly damaged. GPS lock has not been acquired. **SOLUTION** Turn the TYPHOON off then back on again, and ensure it does not move during the initialization process. Check your connections on both the Smart Charger, and the flight battery. Check the fuse on the Smart Charger Wait for the lighter cloud cover or disable GPS*. Wait for disturbance to subside or disable GPS*. Move the TYPHOON outside or disable GPS*. Disable GPS. Flying indoors/disabling GPS NOT Recommended. Move the TYPHOON to a clear and open area. Reposition or remove the video transmitter.

Wait for the threat level to be reduced or disable GPS*. Call Technical Support for replacement Move the TYPHOON away from the magnetic source. If problem persists, calibrate compass. Call Technical Support for replacement Ensure GPS antenna has clear view of sky and GPS lock has been acquired. 33**POSSIBLE CAUSE** ‘Compass error’ is indicated by the LED. TYPHOON is in No Fly Zone. TYPHOON is above 8,000 feet above MSL. Incorrect motor start up procedure. TYPHOON is too close to a metal object or metal surface . Failed Component Compass needs to be calibrated . EMERGENCY Mode. Possibly due to obstructed propeller during motor start up. Weak GPS signal. Component Disconnected, failed, or not assigned properly U.S. Government has raised threat level. Vibration levels high, indicated by shaky landing gear. **SOLUTION** Refer to page 25 for Compass Calibration Move at least 4 miles away from no fly zone. Most major airports are no fly zone areas. Move the TYPHOON below 8,000 feet above MSL. Review Motor Starting/Stopping procedure in manual. Move the TYPHOON away from large metal objects or surfaces. Connect your TYPHOON to the GUI to check the system. Refer to page 25 for Compass Calibration procedures. Check that nothing is obstructing any propeller/motor, turn the TYPHOON off then back on again. Confirm that the flying area has 100 degrees of clear view of the sky. Connect to the GUI to locate the problem. Wait for threat level to be reduced before flying. Check to ensure propellers are not bent, nicked or damaged in any way. Replace damaged propellers. **ISSUE** TYPHOON Motors won’t start

TYPHOON Flashes orange twice between indications TYPHOON beeps constantly and motors won't start TYPHOON Won’t hold position in hover TYPHOON pulses Red and won't start

34**FCC STATEMENT:** This equipment has been tested and found to comply with the limits for Part 15 of the FCC rules. These limits are designed to provide reasonable protection against harmful interference in a residential installation. This equipment generates, uses and can radiate radio frequency energy and, if not installed and used in accordance with the instructions, may cause harmful interference to radio communications. However, there is no guarantee that interference will not occur in a particular installation. If this equipment does cause harmful interference to radio or television reception, which can be determined by turning the equipment off and on, the user is encouraged to try to correct the interference by one or more of the following measures: Reorient or relocate the receiving antenna. Increase the separation between the equipment and receiver. Connect the equipment to an outlet on a circuit different from that to which the receiver is connected. This device complies with part 15 of the FCC rules. Operation is subject to the following two conditions: (1) This device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. 

### CERTIFICATION INFORMATION WARRANTY INFORMATION
Yuneec products and accessories are guaranteed against manufacturing defects for six (6) months from the original date of purchase. Yuneec’s sole obliga

tion in the event of such defects during this period is to repair or replace the defective part or product with a comparable part or product at Yuneec’s sole discretion. Except for such repair or replacement, the sale, processing or other handling of this product is without warranty, condition or other liability. Damage (including crash damage) resulting from use, accident, or normal wear and tear is not covered by this or any warranty. Yuneec assumes no liability for any accident, injury, death, loss, or other claim related to or resulting from the use of this product. In no event shall Yuneec be liable for incidental or consequential damages relating to or resulting from the use of this product or any of its parts. Please review the instructions carefully when using the products. Returns or replacements of parts and/or products may be subject to shipping, handling, replacement and/or restocking fees.
**IMPORTANT NOTE:** Crash damage is NOT covered under warranty.

35**NOTE:** This equipment has been tested and found to comply with the limits for a Class B digital device, pursuant to part 15 of the FCC Rules. These limits are designed to provide reasonable protection against harmful interference in a residential installation. This equipment generates, uses and can radiate radio frequency energy and, if not installed and used in accordance with the instructions, may cause harmful interference to radio communications. However, there is no guarantee that interference will not occur in a particular installation. If this equipment does cause harmful interference to radio or television reception, which can be determined by turning the equipment off and on, the user is encouraged to try to correct the interference by one or more of the following measures: —Reorient or relocate the receiving antenna. —Increase the separation between the equipment and receiver. —Connect the equipment into an outlet on a circuit different from that to which the receiver is connected. —Consult the dealer or an experienced radio/TV technician for help.
**RF EXPOSURE WARNING** This equipment must be installed and operated in accordance with provided instructions and the antenna(s) used for this transmitter must be installed to provide a separation distance of at least 20 cm from all persons and must not be co-located or operating in conjunction with any other antenna or transmit

ter. End-users and installers must be provide with antenna installation instructions and transmitter operating conditions for satisfying RF exposure compli

ance. **IC RADIATION EXPOSURE STATEMENT FOR CANADA** This device complies with Industry Canada licence-exempt RSS standard(s). Operation is subject to the following two conditions: (1) this device may not cause interference, and (2) this device must accept any interference, including interference that may cause undesired operation of the device. Le présent appareil est conforme aux CNR d'Industrie Canada applicables aux appareils radio exempts de licence. L'exploitation est autorisée aux deux conditions suivantes : (1) l'appareil ne doit pas produire de brouillage, et (2) l'utilisateur de l'appareil doit accepter tout brouillage radioélectrique subi, même si le brouillage est susceptible d'en compromettre le fonctionnement. This equipment complies with IC RSS-102 radiation exposure limit set forth for an uncontrolled environment. Cet équipement respecte les limites d'exposition aux rayonnements IC définies pour un environnement non contrôlé

36APPENDIX

– C Steven Wilke Mon thly Maintenance and Repair Log
Aircraft: Hours: Date: Date Issue Discovered Date Issue Resolved Issue Description/Maintenance Conducted Repair/Maintenance Performed By Airframe Motors Propellers Flight Control Update Gimbal Misc