UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATIONFEDERAL 

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) CONCERNINGCOMMERCIAL

OPERATION OF CARBON CORE QUADCOPTER/YUNEEC Q500 4K

UNMANNEDAIRCRAFTSYSTEMS

PURSUANT TO SECTION 333 OF

THE FAA MODERNIZATION AND REFORM ACT OF 2012 (PUBLIC LAW 112-95)

December 10th, 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.com
2

TABLE OF CONTENTS

Page

GLOSSARY OF ABBREVIATIONS. ..................................................................................3

SUMMARY........................................................................................................................... 4

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

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

BASIS FOR PETITION....................................................................................................... 5

NAME AND ADDRESS 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. ...................................................................................................................38
3

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 Command

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 Landing
4

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 

photography 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 THEPETITIONER

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 Photography 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 customers. Steven Wilke will be specifically targeting:

Forest Service Lands

National Parks

Real-estate

Farm Irrigation Systems

Solar Panel Installations

Outdoor Activities including Hiking and Biking
5

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 

5300mAh Lithium Polymer batteries 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 Reform 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, Steven 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 equivalent 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 demonstrated, 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, Steven Wilke submits that he
7

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 Instruction 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 onboard. 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 path. 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 accordance with 14 C.F.R. § 11.81, Steven Wilke provides the following 

information in support of its petition for exemption:
8

A. Name and Address of 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 of 14 C.F.R. From Which Steven Wilke seeksExemption

1. Steven Wilke Seeks Exemption from the Requirements Of Section61.113(a) And

(b).

Section 61.113, entitled Private pilot privileges and limitations: Pilot in command, 

subsections (a) and (b) prescribe the following, in relevant part:

(a) No person who holds a private pilot certificate may act as a pilot in command (PIC) of an 

aircraft that is carrying passengers or property for compensation or hire; nor may that person, 

for compensation or hire, act as PIC of an aircraft.

(b) A private pilot may, for compensation or hire, act as PIC of an aircraft in 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 from the Requirements Of Section91.7(a)

Section 91.7, entitled civil 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 Section91.121.

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 of Section 91.151(b).

Section 91.151, entitled Fuel requirements for flight in VFR conditions, subsection (b), states 

the following:

(b) No person may begin a flight in a rotorcraft under VFR conditions unless (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 prescribed in subpart E of this part and shall between 

required inspections, except as provided in paragraph (c) of this section, have discrepancies 

repaired as prescribed in part 43 of this chapter[.]

6. Steven Wilke Seeks Exemption From The Requirements Of Section91.407(a)(1)

Section 91.407, entitled Operation after maintenance, preventivemaintenance,
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 OfSections 

91.409(a)(1) And 91.409(a)(2).

Section 91.409, entitled Inspections, subsection (a), states the following:

(a) Except as provided in paragraph (c) of this section, no person may operate an 

aircraft unless, within the preceding 12 calendar months, it has had --

(1) An annual inspection in accordance with part 43 of this chapter and has been approved for 

return to service by a person authorized by § 43.7 of this chapter or

(2) An inspection for the issuance of an airworthiness certificate in accordance with part 21 of 

this chapter.

8. Steven Wilke Seeks Exemption from The Requirements Of Sections 91.417(a) And

91.417(b).

Section 91.417, entitled Maintenance records, subsections (a) and (b), state the 

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 appropriate, for
11

each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an 

aircraft. The records must include--

(i) A description (or reference to data acceptable to the Administrator) of the work performed; 

and

(ii) The date of completion of the work performed; and

(iii) The signature, and certificate number of the person approving the 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 basis.

(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 prescribed 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 issold.

(3) A list of defects furnished to a registered owner or operator under § 43.11 of this chapter 

shall be retained until the defects are repaired and the aircraft is approved for return to service.

C. The Extent of Relief Steven Wilke Seeks And The Reason Steven Wilke Seeks The

Relief.

1. Extent of Relief Steven Wilke Seeks and The Reason Steven WilkeSeeks 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 requirements, 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 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.

As set forth more fully below, Steven Wilke submits that an equivalent 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 PIC
13

is able to safely operate either the Yuneec 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 Wilke 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 of Relief Steven Wilke Seeks and the Reason Steven WilkeFrom 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 

airworthiness 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 WilkeSeeks 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

information
14

from the UA to the PIC at the ground control station (GCS). Since the FAA requires that any 

altitude information concerning UAS operations be reported to air traffic control (ATC) in 

feet above ground level (AGL), 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 safetywill

be maintained since the Yuneec Q500 4k is equipped with a barometric pressure sensor and 

GPS equipment, which automatically ensures that a ground level pressure setting will be 

established prior to each flight, and provides the PIC with altitude information of the UA on 

the heads-up display of the GCS.

4. Extent Of Relief Steven Wilke Seeks And The Reason Steven WilkeSeeks 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 battery 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 flight 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 

enough 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 WilkeSeeks Relief From 

Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), And 91.417(a) & (b).

Since Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) 

only apply to aircraft with an airworthiness certificate, 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 perform 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 significant 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 TheNAS.

The Yuneec Q500 4k is battery 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 

manned 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 internal
17

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 aircraft 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 efficient, 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 contribute 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 technology in order to remain competitive. Operating the battery powered Yuneec 

Q500 4k is one such technology that not only allows companies greater operational
18

flexibility compared to manned aircraft, but provides such flexibility without the 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. companies, 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 law enforcement notification, and in accordance with the Federal Aviation Regulations, 

including the minimum altitude requirements of 14 C.F. R. § 91.119.

E. The Reasons Why Granting The Exemption Would Not Adversely Affect Safety,Or 

How The Exemption Would Provide A Level Of Safety At Least Equal To That 

Provided By The Rule From Which Steven Wilke Seeks Exemption.

1. Reasons Why the Yuneec Q500 4k Meet’s The Conditions Of The FAA 

Modernization and Reform Act of 2012 (FMRA) Section 333.
19

In consideration 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 otherwise pose a threat to national security. Specifically, 

FMRA Section 333 states the following, in part:

(a) In General--Notwithstanding any other requirement of this subtitle, and not later than 180 

days after the date of enactment of this Act, the Secretary of Transportation shall determine if 

certain unmanned aircraft systems may 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 the 

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 of 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 of the 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 and Navigation Modes Enable the UAS's 

To Remain Within a Defined Operational Area.

The Yuneec Q500 4k may be operated in both manual and fully autonomous return to 

home flight 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 Q500 4k User Manual, attached hereto as Exhibit B.

Iii. 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 position 

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 and 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 of Yuneec Q500 4k Are Limited to 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 of 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 pounds
22

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 operating 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 vision 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 beyond assisting the PIC with seeing and 

avoiding other air traffic and other ground based obstacles/obstructions and is not 

permitted to operate the camera or other instruments.

9. The operating documents and the grant of exemption must be accessible during 
23

UAS 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 contained 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 determines 

that any update or revision would affect the basis upon which the FAA granted 

the exemption, then the operator must petition for amendment to its grant of 

exemption. The FAA’s UAS Integration Office (AFS-80) may be contacted if 

questions arise regarding 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 prohibited from operating until the necessary maintenance has been 

performed and the UAS is found to be in a condition for safe flight. The Ground 

Control Station must be included in the preflight inspection. All maintenance and 

alterations must be properly documented in the aircraft records.

11. Any UAS that has undergone maintenance or alterations that affect the UAS operation 

or flight characteristics, e.g. replacement of a flight critical component, must undergo 

a functional test flight. The PIC who conducts the 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 documents.

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 authorized 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 thirdclass 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 during dedicated training sessions. During training, 

proficiency, and experience-building flights, all persons not essential for flight 
25

operations are considered nonparticipants, and the PIC must operate the UA with 

appropriate distance from nonparticipants in 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 aeronautical chart unless a letter of agreement 

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

accordance with a NOTAM as required by the operator’s COA. The letter of 

agreement with the airport management must be made available to the 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 must return to a predetermined 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 more than 72 hours in advance, but not less than 48 hours prior to the 

operation. All operations shall be conducted in accordance with airspace requirements 

in the ATO issued COA including class of airspace, altitude level and potential 

transponder requirements.

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 (NNumber) 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 request.

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 cease immediately and/or;

b. The aircraft is operated near vessels, vehicles or structures where the 

owner/controller of such vessels, vehicles or structures has granted 

permission and the PIC has made a safety assessment of the risk of operating 

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

hazard, 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 Transportation Safety Board (NTSB) per 

instructions contained on the NTSB Web site: www.ntsb.gov.

2. Reasons Why An Exemption From The Requirements Of Section 61.113(a) And (b) 

Would Not Adversely Affect Safety.

Steven Wilke submits that the equivalent level of safety established by Section 
28

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 Wilke's specific proposed flight 

operations.

The FAA has previously granted relief from Section 61.113(a) and (b) specific to 

UAS, in circumstances similar, in all material respects, to those presented herein (e.g.

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, vehicles 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 5
29

hours of those hours as a UAS pilot operating the same make and model of UAS to be used 

for operations under the exemption). In addition to the hour requirements, the PIC must 

accomplish 3 takeoffs and landings in the preceding 90 days (for currency purposes).

As in Exemption Nos. 11062, 11138, and 11153, 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 was obtained in compliance with applicable regulations 

would ensure safe operations, stating asfollows:

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 than 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 landings 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 proposed 

operations. The FAA also finds that prior documented flight experience that was obtained in 

compliance with applicable regulations would satisfy this requirement. Training, proficiency,
30

and experience-building flights can also be conducted 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 maintaining appropriate distances from people, vessels, vehicles and

structures.

3. Reasons Why an Exemption From The Requirements Of Section 91.7(a) WouldNot 

Adversely Affect Safety.

The equivalent level of safety established by Section 91.7(a) will be maintained 

because 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 previously 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 an Exemption From The Requirements Of Section 91.121 WouldNot 

Adversely Affect Safety.
31

The equivalent level of safety established by Section 91.121 will be maintained 

because the 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 

information, 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 installed 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 material respects, to those presented herein (e.g. Exemption 

Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11112, 11136, 11138,

11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161).

5. Reasons Why an Exemption From The Requirements Of Section 91.151(b) Would 

Not Adversely Affect Safety.

A grant of this exemption would ensure an equivalent level of safety established by 14

C.F.R. Section 91.151(b) as a result of (1) the technical specifications of the Yuneec Q500 4k

UAS's; (2) the limitations on 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 Yuneec Q500 4k

UAS's the limitations on the proposed flight operations and the location of the proposed 

operations, will ensure an equivalent level of safety established by 14 C.F.R. Section

91.151(b).

Furthermore, safety will be ensured as 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 critically 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 operating 

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, 11157, 11158, 11159,

11160, 11161).

6. Reasons Why An Exemption From The Requirements Of Sections 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), And 91.417(a) &(b) Would Not Adversely Affect 

Safety.

In seeking this exemption, 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 met
33

because 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 operating documents i.e., the Operations Manual, Monthly Maintenance 

Log, and Yuneec Q500 4k Instruction Manual. 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 safety 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 sought 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 maintained utilizing the monthly maintenance log.

Significantly, previous exemptions granted by the FAA concerning Sections 

91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) establish that safety is not 

adversely affected when the technical characteristics and operating limitations of the UAS are 

considered.
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 respects, to 

those presented herein (e.g. Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067,

11080, 11109, 11110, 11112, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159,

11160, 11161).

7. The FAA May Prescribe Any Other Conditions For Safe Operation.

In accordance with Section 333 of the FAA Modernization and Reform Act of 2012 

(FMRA) and 14 C.F.R. § 21.16 entitled Special Conditions, Steven Wilke requests that the 

FAA prescribe special conditions for the intended operation of 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 §§ 

61.113(a) & (b), 91.7 (a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2),

and 91.417(a) & (b). Such special conditions will permit safe operation of the UA's for the 

limited purpose of conducting aerial video and photography over certain areas of the United 

States for compensation or hire. FMRA Section 333 sets forth the requirements for 

considering whether a UAS will create a hazard to users of the NAS or the public, or 

otherwise pose a threat to national security and further, provides the authority for such UAS to 

operate without airworthiness certification 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 14C.F.R.

§21.16, for operation of the Yuneec Q500 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:

If the FAA finds that the airworthiness regulations of this subchapter do not contain 

adequate or appropriate safety standards for an aircraft, aircraft engine, or propeller because of 

a novel or unusual design feature of the aircraft, aircraft engine or propeller, 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 finds necessary to establish a level of safety equivalent 

to that established in the regulations.

See 14 C.F.R. § 21.16.

Therefore, in accordance with FMRA Section 333 and 14 C.F.R. § 21.16, the FAA 

may prescribe special conditions for Steven Wilke’s intended 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 in the 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 of 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 to 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 the 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 

mandate 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 10th, 2015

Steven Wilke
38

APPENDICES:

A - Yuneec Q500 4k - Specifications

B – Yuneec Q500 4k - User Manual

C – Yuneec Q500 4k - Monthly Maintenance Log

APPENDIX –A

Yuneec Q500 4k TECHNICALSPECIFICATIONS

Steven Wilke only utilizes 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 Transmitter Aircraft.

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

CHARGER: 3S 11.1V LiPo DC Balancing Smart Charger with AC Adapter

TRANSMITTER: 10-channel 2.4GHz with 5.8GHz video downlink
39

MAXIMUM FLYING ALTITUDE: Default 400 Feet Above Ground Level

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 (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 Transmission Range: Up to 500m (1640ft)

Transmission System: 5.2Ghz — 5.8Ghz

Video UHD: 4K 30FPS

ST10+ (Remote Controller)

Number of Channels: 10

RC Band: 2.4GHz

RC Modulation: Yuneec Video Downlink Band: 5.8GHz

Telemetry/OSD: Yes
40

SD Card Compatible: Yes

LCD Screen Size: 5.5”

Touchscreen: Yes

APPENDIX – B

Yuneec Q500 4k – Manufacturer's User Manual 
Version 2.0
1

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

35
2

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: Yes
3

Notices And Warnings

IMPORTANT NOTE: All safety precautions and warnings, instructions, warranties and other collateral information is subject to change at the sole discretion 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!

100 ̊ MAX 8000ft

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 compatible 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

14 16

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 recommended. 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 approximately 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).

8
Preparing 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

A
The 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

25
11

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

4 5 6 7

9

10

11

19

18

17

16

15 14 13 12

1 2 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 F30
12

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/programmer 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 meters
14

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

Follow
System 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

3840 x 2160 F30 N/A ft

WATCH ME FUNCTION

Watch Me function enables the camera to keep tracking the remote controller 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 traveling 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 connectivity will fly back the TYPHOON, and 

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
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

18
19
Press 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

C
Installing 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 connection.

NOTE: If you do not install the battery in the correct orientation 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 antenna 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/obstructions, near or under dense 

vegetation, structures or indoors. Do 

NOT attempt to fly the TYPHOON with 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 indicating 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/obstructions 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)
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 approximately 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

26
ST10+ 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 gh
ST10+ 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 connected
29

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 disassembled. 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 immediately 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 SteadyGripTM 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 SteadyGripTM 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 quickly 
Taking 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 instructions along with the illustrations 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.Install 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 assembly.

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/A
32

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

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

36
APPENDIX – C

Steven Wilke Monthly 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