July 14, 2015

Exemption No. 12027

Regulatory Docket No. FAA–2015–1381

Mr. Timothy A. Paris

Vice President of Operations

Mr. William M. Bogar, Esq.

Attorney/Superintendent

Alex E. Paris Contracting Company, Inc.

1595 Smith Township Road

Atlasburg, PA 15004-0369

Dear Messrs. Paris and Bogar:

This letter is to inform you that we have granted your request for exemption. It transmits our 

decision, explains its basis, and gives you the conditions and limitations of the exemption, 

including the date it ends.

By letter dated April 23, 2015, you petitioned the Federal Aviation Administration (FAA) on 

behalf of Alex E. Paris Contracting Company, Inc. (hereinafter petitioner or operator) for an 

exemption. The petitioner requested to operate an unmanned aircraft system (UAS) to 

conduct aerial imaging for monitoring of construction sites.

See Appendix A for the petition submitted to the FAA describing the proposed operations and 

the regulations that the petitioner seeks an exemption.

The FAA has determined that good cause exists for not publishing a summary of the petition 

in the Federal Register because the requested exemption would not set a precedent, and any 

delay in acting on this petition would be detrimental to the petitioner.

Airworthiness Certification

The UAS proposed by the petitioner is a Yuneec Q500 Typhoon.
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The petitioner requested relief from 14 CFR part 21, Certification procedures for products 

and parts, Subpart H—Airworthiness Certificates. In accordance with the statutory criteria 

provided in Section 333 of Public Law 112−95 in reference to 49 U.S.C. § 44704, and in 

consideration of the size, weight, speed, and limited operating area associated with the 

aircraft and its operation, the Secretary of Transportation has determined that this aircraft 

meets the conditions of Section 333. Therefore, the FAA finds that the requested relief from 

14 CFR part 21, Certification procedures for products and parts, Subpart H—Airworthiness 

Certificates, and any associated noise certification and testing requirements of part 36, is 

not necessary.

The Basis for Our Decision

You have requested to use a UAS for aerial data collection1. The FAA has issued grants of 

exemption in circumstances similar in all material respects to those presented in your petition. 

In Grants of Exemption Nos. 11062 to Astraeus Aerial (see Docket No. FAA−2014−0352), 

11109 to Clayco, Inc. (see Docket No. FAA−2014−0507), 11112 to VDOS Global, LLC (see

Docket No. FAA−2014−0382), and 11213 to Aeryon Labs, Inc. (see Docket No. 

FAA−2014−0642), the FAA found that the enhanced safety achieved using an unmanned 

aircraft (UA) with the specifications described by the petitioner and carrying no passengers or 

crew, rather than a manned aircraft of significantly greater proportions, carrying crew in 

addition to flammable fuel, gives the FAA good cause to find that the UAS operation enabled 

by this exemption is in the public interest.

Having reviewed your reasons for requesting an exemption, I find that—

• They are similar in all material respects to relief previously requested in Grant of 

Exemption Nos. 11062, 11109, 11112, and 11213;

• The reasons stated by the FAA for granting Exemption Nos. 11062, 11109, 11112, and 

11213 also apply to the situation you present; and 

• A grant of exemption is in the public interest.

Our Decision

In consideration of the foregoing, I find that a grant of exemption is in the public interest. 

Therefore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701, 

delegated to me by the Administrator, Alex E. Paris Contracting Company, Inc. is granted an 

exemption from 14 CFR §§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 

91.7(a), 91.119(c), 91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 

91.417(a) and (b), to the extent necessary to allow the petitioner to operate a UAS to perform 

 

1 Aerial data collection includes any remote sensing and measuring by an instrument(s) aboard the UA. 

Examples include imagery (photography, video, infrared, etc.), electronic measurement (precision surveying, RF 

analysis, etc.), chemical measurement (particulate measurement, etc.), or any other gathering of data by 

instruments aboard the UA.
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aerial data collection. This exemption is subject to the conditions and limitations listed 

below.

Conditions and Limitations

In this grant of exemption, Alex E. Paris Contracting Company, Inc. is hereafter referred to as 

the operator.

Failure to comply with any of the conditions and limitations of this grant of exemption will be 

grounds for the immediate suspension or rescission of this exemption.

1. Operations authorized by this grant of exemption are limited to the Yuneec Q500 

Typhoon when weighing less than 55 pounds including payload. Proposed operations 

of any other aircraft will require a new petition or a petition to amend this exemption.

2. Operations for the purpose of closed-set motion picture and television filming are 

not permitted. 

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The 

exemption holder may use either groundspeed or calibrated airspeed to determine 

compliance with the 87 knot speed restriction. In no case will the UA be operated at 

airspeeds greater than the maximum UA operating airspeed recommended by the 

aircraft manufacturer.

4. The UA must be operated at an altitude of no more than 400 feet above ground level 

(AGL). Altitude must be reported in feet AGL.

5. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. 

This requires the PIC to be able to use human vision unaided by any device other than 

corrective lenses, as specified on the PIC’s FAA-issued airman medical certificate or 

U.S. driver’s license.

6. All operations must utilize a visual observer (VO). The UA must be operated within 

the visual line of sight (VLOS) of the PIC and VO at all times. The VO may be used 

to satisfy the VLOS requirement as long as the PIC always maintains VLOS 

capability. The VO 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 VO can perform the duties 

required of the VO.

7. This exemption and all documents needed to operate the UAS and conduct its 

operations in accordance with the conditions and limitations stated in this grant of 

exemption, are hereinafter referred to as the operating documents. The operating 
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documents must be accessible during UAS operations and made available to the 

Administrator upon request. If a discrepancy exists between the conditions and 

limitations in this exemption and the procedures outlined in the operating documents, 

the conditions and limitations herein 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 or any law enforcement official upon request. The 

operator must also present updated and revised documents if it petitions for extension 

or amendment to this grant of exemption. If the operator determines that any update 

or revision would affect the basis upon which the FAA granted this exemption, then 

the operator must petition for an amendment to its grant of exemption. The FAA’s 

UAS Integration Office (AFS−80) may be contacted if questions arise regarding 

updates or revisions to the operating documents.

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

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

a functional test flight prior to conducting further operations under this exemption. 

Functional test flights may only be conducted by a PIC with a VO and must remain at 

least 500 feet from other people. The functional test flight must be conducted in such 

a manner so as to not pose an undue hazard to persons and property.

9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is 

in a condition for safe operation.

10. Prior to each flight, the PIC must conduct a pre-flight inspection and determine the 

UAS is in a condition for safe flight. The pre-flight inspection must account for all 

potential discrepancies, e.g., inoperable components, items, or equipment. 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.

11. The operator must follow the UAS manufacturer’s maintenance, overhaul, 

replacement, inspection, and life limit requirements for the aircraft and 

aircraft components.

12. Each UAS operated under this exemption must comply with all manufacturer 

safety bulletins.

13. Under this grant of exemption, a PIC must hold either an airline transport, 

commercial, private, recreational, or sport pilot certificate. The PIC must also hold a 

current FAA airman medical certificate or a valid U.S. driver’s license issued by a 

state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal 
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government. The PIC must also meet the flight review requirements specified in 

14 CFR § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

14. The operator may not permit any PIC to operate unless the PIC demonstrates the 

ability to safely operate the UAS in a manner consistent with how the UAS will be 

operated under this exemption, including evasive and emergency maneuvers and 

maintaining appropriate distances from persons, vessels, vehicles and structures. PIC 

qualification flight hours and currency must be logged in a manner consistent with 

14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs 

(training, proficiency, and experience-building) and determining the PIC’s ability to 

safely operate the UAS in a manner consistent with how the UAS will be operated 

under this exemption are permitted under the terms of this 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 operations are considered nonparticipants, and the PIC must operate the UA 

with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All 

operations must be conducted under visual meteorological conditions (VMC). Flights 

under special visual flight rules (SVFR) are not authorized.

16. The UA may not operate within 5 nautical miles of an airport reference point (ARP) as 

denoted in the current FAA Airport/Facility Directory (AFD) or for airports not 

denoted with an ARP, the center of the airport symbol as denoted on the current 

FAA-published aeronautical chart, unless a letter of agreement with that airport’s 

management is obtained or otherwise permitted by a COA issued to the exemption 

holder. The letter of agreement with the airport management must be made available 

to the Administrator or any law enforcement official upon request.

17. 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.

18. If the UAS loses communications or loses its GPS signal, the UA must return to a 

pre-determined location within the private or controlled-access property.

19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies.

20. The PIC is prohibited from beginning a flight unless (considering wind and forecast 

weather conditions) there is enough available power for the UA to conduct the 

intended operation and to operate after that for at least five minutes or with the reserve 

power recommended by the manufacturer if greater.

21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All 

operations shall be conducted in accordance with an ATO-issued COA. The 
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exemption holder may apply for a new or amended COA if it intends to conduct 

operations that cannot be conducted under the terms of the attached COA.

22. All aircraft operated in accordance with this exemption must be identified by serial 

number, registered in accordance with 14 CFR part 47, and have identification 

(N−Number) markings in accordance with 14 CFR part 45, Subpart C. Markings must 

be as large as practicable.

23. Documents used by the operator to ensure the safe operation and flight of the UAS and 

any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the 

PIC at the Ground Control Station of the UAS any time the aircraft is operating. 

These documents must be made available to the Administrator or any law enforcement 

official upon request.

24. The UA must remain clear and give way to all manned aviation operations and 

activities at all times. 

25. The UAS may not be operated by the PIC from any moving device or vehicle. 

26. All Flight operations must be conducted at least 500 feet from all nonparticipating 

persons, vessels, vehicles, and structures unless:

a. Barriers or structures are present that sufficiently protect nonparticipating persons 

from the UA and/or debris in the event of an accident. The 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 in a manner ensuring the safety 

of nonparticipating persons; and

b. The owner/controller of any vessels, vehicles or structures has granted permission 

for operating closer to those objects and the PIC has made a safety assessment of 

the risk of operating closer to those objects and determined that it does not 

present an undue hazard.

The PIC, VO, operator trainees or essential persons are not considered 

nonparticipating persons under this exemption.

27. All operations shall be conducted over private or controlled-access property with 

permission from the property owner/controller or authorized representative. 

Permission from property owner/controller or authorized representative will be 

obtained for each flight to be conducted.

28. 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 
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reported to the National Transportation Safety Board (NTSB) per instructions 

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

If this exemption permits operations for the purpose of closed-set motion picture and 

television filming and production, the following additional conditions and limitations apply.

29. The operator must have a motion picture and television operations manual (MPTOM) 

as documented in this grant of exemption.

30. At least 3 days before aerial filming, the operator of the UAS affected by this 

exemption must submit a written Plan of Activities to the local Flight Standards 

District Office (FSDO) with jurisdiction over the area of proposed filming. The 3-day 

notification may be waived with the concurrence of the FSDO. The plan of activities 

must include at least the following:

a. Dates and times for all flights;

b. Name and phone number of the operator for the UAS aerial filming conducted 

under this grant of exemption;

c. Name and phone number of the person responsible for the on-scene operation of 

the UAS;

d. Make, model, and serial or N−Number of UAS to be used;

e. Name and certificate number of UAS PICs involved in the aerial filming;

f. A statement that the operator has obtained permission from property owners 

and/or local officials to conduct the filming production event; the list of those 

who gave permission must be made available to the inspector upon request;

g. Signature of exemption holder or representative; and

h. A description of the flight activity, including maps or diagrams of any area, city, 

town, county, and/or state over which filming will be conducted and the altitudes 

essential to accomplish the operation.

31. Flight operations may be conducted closer than 500 feet from participating persons 

consenting to be involved and necessary for the filming production, as specified in the 

exemption holder’s MPTOM.

Unless otherwise specified in this grant of exemption, the UAS, the UAS PIC, and the UAS 

operations must comply with all applicable parts of 14 CFR including, but not limited to, 

parts 45, 47, 61, and 91.
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This exemption terminates on July 31, 2017 unless sooner superseded or rescinded.

Sincerely,

/s/

John S. Duncan

Director, Flight Standards Service

Enclosures
ALEX E. PARIS 

CONTRACTING COMPANY, INC. 

P.O. BOX 369 • 1595 SMITH TOWNSHIP STATE ROAD (RT. 18) 

ATLASBURG, PA 15004-0369 

Office Phone No. (724) 947-2235 

FAX No. (724) 947-3820 

April23, 2015 

U.S Department of Transportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington, DC 20590 

Our Greatest Assets 

Our Employees 

RE: Request for Exemption under Section 333 of the FAA Modernization and 

Reform Act of2012 and Part 11 of the Federal Aviation Regulations from Certain 

Sections of 14 C.F.R. 

Dear Sir or Madam, 

Please review the enclosed application requesting exemption from the Federal 

Aviation Regulations listed above and contained within this document. If we can provide 

any additional information to assist in your review of this document, please do not 

hesitate to contact us at (724) 947-2235 or via email at either tparis@alexparis.com or 

wbogar@alexparis.com. 

Thank you, 

d~a!?~ 

Timothy A. Paris 

Vice President of Operations 

Alex E. Paris Contracting Company, Inc. 

1595 Smith Township Road 

Atlasburg, PA 15004-0369 

Phone: (724) 947-2235 

Email: tparis@alexparis.com 

~ William M. Bogar, Esq. 

Attorney/Superintendent 

Alex E. Paris Contracting Company, Inc. 

1595 Smith Township Road 

Atlasburg, PA 15004-0369 

Phone: (724) 947-2235 

Email: bbogar@alexparis.com 
April23, 2015 

U.S Department of Transportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington, DC 20590 

Re: Request for Exemption under Section 333 of the FAA Modernization and Refonn Act of2012 and 

Part 11 of the Federal Aviation Regulations from Certain Sections of 14 C.P.R. 

Dear Sir or Madam: 

Pursuant to Section 333 of the FAA Modernization and Reform Act of2012 (the "Reform Act"), Alex E. 

Paris Contracting Company, a Pennsylvania Corporation (Petitioner) and planned operator of a Small 

Unmanned Aircraft System (sUAS) hereby applies for an exemption from the listed Federal Aviation 

Regulations (FAR's) to allow for commercial operation of its sUAS to provide aerial imaging for 

monitoring of secured and controlled construction sites, so long as these operations are conducted under 

the conditions outlined within this framework or as may be established by the FAA as required by Section 

333. A summary of this request suitable for publication in the Federal Register is provided within Part 

VIII of this application. 

The requested exemption would allow the Petitioner to safely, efficiently and economically use a 

commercial sUAS within the National Air System (NAS). As detailed in this document and the attached 

instruction manual (plus additional documentation) within the Appendix, the requested exemption would 

permit the Petitioner to operate the sUAS under controlled conditions in airspace that is limited and 

predetermined. In addition, access to the sites, themselves, will be tightly controlled. Accordingly, the 

approval ofthis exemption would enhance safety and fulfill the Secretary of Transportation's 

responsibilities under Section 333(c) of the Reform Act to "establish requirements for the safe operation 

of such aircraft systems in the National Airspace System (NAS)." 

The name and address of the applicant are: 

Timothy A. Paris 

Vice President of Operations 

Alex E. Paris Contracting Company, Inc. 

1595 Smith Township Road 

Atlasburg, PA 15004-0369 

Phone: (724) 947-2235 

Email: tparis@alexparis.com 

William M. Bogar, Esq. 

Attorney/Superintendent 

Alex E. Paris Contracting Company, Inc. 

1595 Smith Township Road 

Atlasburg, PA 15004-0369 

Phone: (724) 947-2235 

Email: bbogar@alexparis.com 

The regulations from which the exemption is requested are as follows: 
14 C.P.R. Part 21(h) 

14 C.P.R.§ 91.203(a) (1) 

14 C.P.R.§ 45.23(b) 

14 C.P.R. § 45.27(a) 

14 C.P.R.§ 91.9(c) 

14 C.P.R.§ 61.113(a) & (b) 

14 C.P.R.§ 91.7(a) 

14 C.P.R.§ 91.9(b) (2) 

14 C.P.R.§ 91.203(a) & (b) 

14 C.P.R.§ 91.103 

14 C.P.R.§ 91.109(a) 

14 C.P.R.§ 91.119 

14 C.P.R.§ 91.121 

14 C.P.R.§ 91.151(a) 

14 C.P.R.§ 91.405(a) 

14 C.P.R.§ 91.407(a) (1) 

14 C.P.R. § 409(a) (2) 

14 C.P.R.§ 417(a) & (b) 

I. DESCRIPTION OF PETITIONER 

Alex E. Paris Contracting Company, Inc. (AEP) is a Pennsylvania Corporation specializing in heavy 

construction and a variety of industrial services related to it. Operating primarily in Pennsylvania, Ohio 

and the Mid-Atlantic region, we engage in a variety of construction services, both public and private, 

which include underground utility installation, site development, building foundation construction, site 

demolition and remediation, environmental mitigation & reclamation as well as const. management. 

Having been in existence for 67 years, we are members in, and actively involved in the National Utility 

Contractor's Association, Pennsylvania Utility Contractor's Association, West Virginia Utility 

Contractor's Association, American General Contractors Association and the Associated Builders and 

Contractors Association. 

II. RELEVANT STATUTORY AUTHORITY 

This petition for exemption is submitted in accordance with Section 333(a) through (c) ofthe FAA 

Modernization and Refonn Act of2012. The "Reform Act" gives authority to the Secretary of 

Transportation to consider whether certain unmanned aircraft systems (UAS) may operate safely 

within the National Airspace System (NAS) before completion of the rulemaking required under 

Section 332 of the "Reform Act". The Secretary has delegated this aviation authority to the 

Administrator of the FAA. In making this determination, the Administrator must determine which 

types of UAS's do not create a hazard to users of the NAS or the public or pose a threat to national 

security in light of the following considerations, stated under Section 333(b ): 

• The size, weight, speed and operational capability of the UAS. 

• Whether the UAS operates within the visual sight line ofthe operator. 

• Whether the UAS operates within close proximity to airports and populated areas. 

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Accordingly, under Section 3 3 3 (c), if the Administrator makes the determination that the U AS "may 

operate safely in the national airspace system (NAS), the Secretary shall establish requirements for the 

safe operation of such aircraft in the national airspace system (NAS). 

In addition, under 49 U.S.C. § 44701(£) the Administrator is expressly given the authority to grant 

exemptions from its safety regulations and standards if the Administrator finds the exemption is in the 

public interest. (49 U.S.C. § 44701(£) permits exemptions from§§ 44701(a) & (b) and§§ 44702 

through 44716). Furthermore, a party requesting such an exemption must explain the reasons why the 

exemption: (1). would be in the public interest or how it would benefit the public as a whole, and (2). 

that it would not adversely affect safety (or how it would provide a level of safety at least equal to the 

existing regulation from which exemption is sought) under 14 C.P.R.§ 11.81. 

The sUAS owned by Alex E. Paris Contracting Company, Inc. is a small multirotor vehicle and it 

weighs less than 5 pounds ( apx. 60oz.) at lift -off. Under normal conditions, it operates at a speed of no 

more than 25 knots. It has the capability of hovering and moving within both a horizontal and vertical 

plane simultaneously. The sUAS will operate only in the visual line of sight of its pilot in command 

(PIC) and a visual observer (VO) that will be present during actual flight operations. The sUAS will 

only operate under controlled conditions, in airspace that is both predetermined and limited. In 

addition, ground-access to these sites will be tightly controlled. Finally, the sUAS will operate at an 

altitude of no more than 400 feet, posing no risk to users of the national airspace system. Accordingly, 

these operations insure that the sUAS will "not create a hazard to users of the national airspace system 

or to the public" as mandated within Section 333(b) of the Reform Act. 

Given the small size of the sUAS involved and the restricted environment within which it will operate, 

this petition for exemption falls squarely within the "equivalent level of safety" under 14 C.F .R § 

11.81 in which Congress intended that the FAA, by exemption, permit commercial operation of the 

sUAS to commence, pending completion of formal rulemaking. Furthermore, due to its small size plus 

the low altitudes and restricted areas in which it will operate, approval of this petition presents no 

national security issue. 

Considering the clear direction in Section 333 of the Reform Act, the authority contained in the 

Federal Aviation Act as amended, the equivalent level of safety surrounding the proposed operations 

and the public benefit which it will incur, the grant of the requested exemptions are also in the public 

interest. 

Accordingly, Alex E. Paris Contracting Company, Inc. respectfully requests the FAA to grant the 

requested exemption without delay. 

III. PUBLIC INTEREST 

This exemption application is expressly submitted to fulfill Congress' goal in passing Section 

333(a) through (c) of the FAA Modernization and Reform Act of2012 (the "Reform Act"). The law 

allows the Secretary of Transportation to consider whether certain small unmanned aircraft systems 

(sUAS) can operate safely within the national airspace system (NAS) before completion of the 

rulemaking that is required under Section 332 of the "Reform Act". By granting an exemption, the 

FAA will fulfill Congress' intent of allowing a sUAS to operate with significant safety precautions in 

a restricted, low risk environment. 

The use of a sUAS on a construction site will significantly reduce the risk to our employees/workers 

with respect to slips and falls while inspecting, surveying and monitoring site progress. A sUAS is 

3 
capable of photographing and collecting data from many areas that normally require employee 

inspection, thus eliminating many of the risks associated with it. Accordingly, since slips and falls are 

a major source of construction site injuries and fatalities, the effect of reducing their probability 

through the use of a sUAS would squarely be within the public interest. 

In addition, the use of a sUAS on a construction site will allow for a more thorough site review, 

potentially revealing issues and concerns that might not be evident from an on-ground, visual 

inspection. Generally, the projects that we undertake are subject to stringent environmental controls. 

The primary objective of these controls is to regulate (or even eliminate) the discharge of potential 

pollutants from the site into the surrounding environment. Often the failure of these controls to do so 

may subject the contractor to substantial fines from the Environmental Protection Agency (EPA) or a 

similar state authority or both. As a contractor, we take both the construction and maintenance of 

environmental controls very seriously, conducting visual inspections on a daily basis. In addition to 

the risks posed by slips and falls, visual inspections can only provide a limited, view of the 

effectiveness of these controls. The use of a sUAS will provide a birds-eye, view of the controls. Any 

potential breaches will readily be evident as will be the extent of the discharge and potential damage 

done to the surrounding environment. The collection of such data will allow for faster, more focused 

and efficient repair and maintenance times. This too, is squarely within the public interest since a more 

sustainable and cleaner eco-system is beneficial to everyone. 

The sUAS can provide for quick and cost effective aerial monitoring of all or a significant portion of a 

construction site-something that is not possible without this technology. The sUAS can be used to 

monitor site progress on a daily basis, allowing site crews and project managers to examine and 

inspect completed work for flaws, more quickly. Similarly, aerial monitoring will allow for a more 

efficient allocation of equipment and manpower-as it will allow site crews and project managers to 

better identify areas of the project that require additional resources. These considerations are within 

the public interest because they enhance the ability to produce a safer product and work to assure both 

the cost-effectiveness and safety of the work performed. 

The sUAS that we propose to fly for operations under this application weighs less than 5 pounds (apx. 

60oz) and carries no on-board pilot, passengers or cargo. It also carries no combustible fuels or other 

flammable material-unlike larger conventional aircraft that could be used to provide the same services. 

Utilizing a sUAS, instead of a larger conventional aircraft, provides for a much greater degree of 

safety for both our employees and the general public. Lastly, it should also be noted that our sUAS 

will be powered by rechargeable lithium ion batteries-as opposed to the burning of fossil fuels. Hence, 

the environmental impact of utilizing the sUAS for aerial imaging is greatly reduced-especially when 

contrasted with the use of a larger conventional aircraft to provide the same thing. 

IV. DESCRIPTION OF OPERATIONS 

The grant of exemption to Alex E. Paris Contracting Company, Inc. for the Yuneec QSOO Typhoon 

sUAS will be subject to the following operating conditions. The main restrictions have been 

summarized below. 

1. Operations will be conducted over private, controlled-access, or public property where approved. 

2. Written and/or verbal permission from the land-owner/authority will be required before the 

commencement of any flight. 

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3. All operations conducted within 5 miles from an airport shall only be initiated after verbal 

coordination with the airport authority, or air traffic control when a control tower is present at the 

airport. 

4. All onsite personnel will consent to the sUAS flyover on site by written waiver and the pilot in 

command (PIC) will obtain additional written or verbal consent of anyone who is allowed within 100 

feet of the flight operation. 

5. All required permissions and pennits will be obtained from territorial, state, county or city 

jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies. 

6. A briefing will be conducted with regard to the planned sUAS operation prior to the start of each 

day's operations. This briefing will be mandatory for all personnel who are performing duties within 

the boundaries of the secured area of which the sUAS will be operating. 

7. The Yuneec Typhoon Q500 (sUAS) weighs less than 5 pounds (apx. 60oz.). 

8. All flights will be operated within the visual line of sight of both the pilot in command (PIC) and an 

additional visual observer (VO). 

9. Maximum total flight time for each operational flight will be limited to the amount of time that the 

second low battery warning indicator on the hand-held flight control box is achieved. This generally 

allows for a flight time of20-25 minutes, as per manufacturer's specifications. 

10. All flights will be operated at an altitude of no more than 400 feet above ground level (AGL) and 

will operate in the secured area within a confined geo-fence, defined by a maximum 300 foot radius. 

11. The minimum crew for each operation will consist of a pilot in command (PIC) and a visual 

observer (VO). 

12. The pilot in command (PIC) will be an FAA licensed airman with a private pilot's certificate (or a 

sUAS certificate, once the FAA establishes the criteria and procedures for obtaining a sUAS license) 

and a second class medical certificate. 

13. The sUAS will operate in accordance with all safety and operational requirements contained within 

the instruction manual attached in the Appendix to this application. 

14. Both the pilot in command (PIC) and visual observer (VO) will be trained in operation of the 

Yuneec Q500 Typhoon and will have received up-to-date maintenance information regarding the 

sUAS. 

15. The pilot in command (PIC) will conduct a pre-flight inspection, prior to each flight and determine 

that the sUAS is in a condition safe for flight. If the inspection reveals a condition that affects the safe 

operation ofthe sUAS, the aircraft will be prohibited from operating until the necessary maintenance 

is performed and the sUAS is made safe for flight. All maintenance performed on the sUAS will be 

denoted in a Maintenance Log kept specifically for the sUAS. 

16. The pilot in command (PIC) and visual observer (VO) will be able to communicate by voice at all 

times. 

17. The pilot in command (PIC) will be trained in advance for the safe operation of the sUAS to be 

5 
operated. This will include operation of the sUAS both in normal and in emergency modes of 

operation, and will include familiarization with the instruction manual published by the sUAS 

manufacturer and attached in the Appendix to this application. Training will also include types of 

maneuvers to be performed and the safe operation in relation to persons, property and applicable 

airspace. 

18. Contingency plans will be in place to safely tenninate flight if there is a loss of communication 

between the pilot in command (PIC) and visual observer (VO). 

19. Operations will only be conducted during daylight hours. 

V. REGULATIONS FROM WHICH EXEMPTION IS REQUESTED 

Alex E. Paris Contracting Company, Inc. ("Petitioner") requests an exemption from the following 

regulations as well as any additional regulations that may technically apply to the operation of 

sUAS's: 

14 C.F.R. Part 21(h): Airworthiness Certificates. 

14 C.F.R. § 91.203(a) (1) 

14 C.P.R.§ 91.203(a) (1) requires that no person may operate a civil aircraft unless it has within it a 

certificate of airworthiness. 14 C.P.R. Part 21(h) establishes the procedural requirements for the 

issuance of airworthiness certificates as required by 14 C.P.R.§ 91.203(a) (1). The Federal Aviation 

Act and Section 333 gives the FAA authorization to exempt aircraft from the requirement for an 

airworthiness certificate upon consideration of certain characteristics. These characteristics include the 

size, weight, speed, operational capability, and proximity to airports and populated areas of the 

particular UAS. Given the size of the aircraft, that we intend to operate (less than 5 lbs.) and the 

limited operating area associated with these operations, an exemption from 14 C.P.R. Part 21(h) meets 

the requirements of an equivalent level of safety under Part 11 and Section 333 of the Reform Act. 

Equivalent Level of Safety 

In this case, a further examination of these criteria demonstrate that the sUAS operated without an 

airworthiness certificate, under the conditions proposed herein, will be at least as safe, or safer, than a 

conventional aircraft (either fixed wing or rotorcraft) with an airworthiness certificate. The sUAS 

operated by Alex E. Paris Contracting Company, Inc. has a gross take-offweight of less than 5 pounds 

(apx. 60 oz.). It will not carry a pilot or a passenger. It will not carry explosive materials or flammable 

liquid fuels. It will operate exclusively in a secured area with receipt of permission from the landowner 

and consent obtained from all ground personnel, prior to flight. Unlike other civil aircraft, all proposed 

operations of the sUAS will be tightly controlled and monitored by its pilot in command (PIC) and an 

additional visual observer (VO). Furthennore, the aircraft will be carried to the area of operation, not 

flown. 

Taken together, these safety enhancements provide a greater degree of safety to the Petitioner's 

employees, members of the public and property owners than conventional operations of civil aircraft 

that require an airworthiness certificate under 14 C.P.R. Part 21(h). Such aircraft are considerably 

larger, carry passengers and cargo as well as flammable fuel and operate without the restrictions and 

conditions being proposed for our sUAS. In addition, application of these same criteria clearly 

demonstrate that the proposed operation of our sUAS poses no credible threat to national security due 

to its size, speed of operation, lack of explosive materials or flammable liquid fuels and inability to 

6 
carry a substantial external load. The FAA has issued several exemptions to 14 C.F.R. Part 2l(h) a 

sampling includes the following exemptions: 11062, 11080, Ill 09, 11153, and 1117 4. The FAA has 

issued several exemptions to 14 C.F.R. § 91.203(a) (1), a sampling includes the following exemptions: 

11062, 11080, 11109, 11153, and 11174. 

14 C.F.R. § 45.23: Marking of the Aircraft. 

14 C.F.R. § 91.9(c) 

14 C.F.R. § 45.27(a) 

Applicant seeks an exemption from the aircraft marking and identification requirements contained in 14 

C.F.R. § 45.23, 14 C.F.R. § 91.9(c) and 14 C.F.R. § 45.27(a). 

• 14 C.F.R. § 45.23, Markings of the Aircraft, states: 

(a). Each operator of an aircraft must display on that aircraft marks consisting of the Roman capital 

letter "N'? (denoting United States registration) followed by the registration number of the 

Aircraft. Each suffix letter used in the marks displayed must also be a Roman capital letter. 

(b). When marks include only the Roman capital letter "N" and the registration number is displayed 

on limited, restricted or light-sport category aircraft or experimental or provisionally certificated 

aircraft, the operator must also display on that aircraft near the entrance to the cabin, cockpit or 

pilot station, in letters not less than 2 inches nor more than 6 inches high, the words "limited" 

"restricted", "light-sport", "experimental", or "provisional", as applicable. 

• 14 C.F.R. § 91.9(c), Civil Aircraft Flight Manual, Marking & Placard requirements, provides that: 

No person may operate a US-registered civil aircraft unless that aircraft is identified in 

Accordance with Part 45 of this chapter. 

• 14 C.F.R. § 45.27(a), Rotorcraft, states: 

Each operator of a rotorcraft must display on that rotorcraft horizontally on both surfaces of the 

Cabin, fuselage, boom, or tail the marks required by§ 45.23(b ). 

Exemption from 14 C.F.R. § 45.23(b) is warranted because the sUAS has no entrance to the cabin, 

cockpit or pilot station on which the markings can be placed. Given the size of the sUAS, 2 inch lettering 

will be impossible, as well. 

Equivalent Level of Safety 

Official marking systems for sUAS have yet to be established for operations inside the NAS. Petitioner is 

prepared to mark the sUAS with its name, location and origin. Petitioner will also fulfill any other request 

made by the FAA on this topic in accordance with 14 C.F.R. § 45 .29(f) where the pilot, observer and any 

others working with the sUAS will see the identification of the sUAS. 

The FAA has issued several exemptions to 14 C.F.R. § 45.23(b), a sampling includes the following 

exemptions: 8738, 10167, 10167A and 101700. 

The FAA has issued several exemptions to 14 C.F.R. § 91.9(c), a sampling includes the following 

exemptions: 11136, 11170,11171, 11174, and 11185. 

7 
14 C.F.R. § 61.113(a) & (b): Pilot in Command (P.I.C.) 

Petitioner seeks an exemption from the private pilot privileges and limitations, outlined in 14 C.F .R. § 

61.113(a) & (b). Accordingly, these regulations state: 

• (a). Except as provided in paragraphs (b) through (h) ofthis section, no person who holds a 

private pilot certificate may act as a pilot in command of an aircraft that is carrying passengers 

or property for compensation or hire: nor may that person, for compensation or hire, act as pilot 

in command of an aircraft. 

(b). A private pilot may, for compensation or hire, act as pilot in command 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. 

Accordingly, under paragraphs (b) through (h) of this section, no person who holds a private pilot 

certificate may act as pilot in command (PIC) of an aircraft which is carrying passengers or property for 

compensation or for hire; Similarly, nor may that person, for compensation or hire, act as pilot in 

command (PIC) of an aircraft. However, a private pilot may, for compensation or hire, act as pilot in 

command (PIC) of an aircraft in connection with any business or employment in certain circumstancesspecifically, if that flight is only incidental to that business or employment and the aircraft does not carry 

passengers or property for compensation or for hire. 

Equivalent Level of Safety 

Because the sUAS will not carry a pilot or passengers, the proposed operation can achieve the equivalent 

level of safety contemplated under these regulations by requiring the pilot in command (PIC) operating 

the aircraft to have a private pilot's license rather than a commercial pilot's license. Firstly, any flight 

conducted with the sUAS will only be incidental to that business or employment. Secondly, unlike a 

conventional aircraft carrying a pilot and living passengers, the sUAS is remotely controlled with no 

living thing or any cargo onboard. Additionally, the Yuneec Q500 Typhoon is equipped with numerous 

safety features that greatly reduce the risk of human error, contemplated by this regulation. 

• At start-up and prior to flight, the sUAS undergoes a self-initialization process. Flight is not 

possible unless this initialization process is successful. 

• The maximum altitude of the sUAS is limited to 400 feet and it has the capability to create 

a geo/virtual fence, restricting its horizontal movement. This will allow the pilot in command 

to create a pre-planned flight area-beyond from which the sUAS can't operate. 

• Battery strength is displayed on the hand-held, control box allowing for continuous 

monitoring by the pilot in command (PIC). In addition, the control box is equipped 

with low-level battery warning lights and is designed to vibrate and/or send an audible 

alert as the flight battery becomes diminished, thus warning the pilot in command (PIC) 

to land the sUAS. 

• The sUAS is equipped with a "Home Mode" function. Once activated, the sUAS will land 

automatically within 13-26 feet of the pilot in command (PIC). 

8 
Furthermore, the sUAS will only be operated within a secure and controlled area. Receipt of permission 

from the landowner will always be obtained prior to flight. In addition, any potential persons within 

this restricted area will not be exposed to these operations without their pre-obtained consent. Finally, we 

propose that a visual observer (VO) be utilized for each flight and be in verbal communication with the 

pilot in command (PIC) during its duration. 

Taken together, the sUAS to be operated hereunder weighs less than 5 pounds (apx. 60oz.) at lift-off. It 

carries no pilot or passengers. It carries no explosive materials, flammable fuels or other liquids. It will 

operate, exclusively, within a secured and restricted area. It is equipped with a number of features that 

greatly minimize the risks posed by human error and an additional party will be present to visually 

monitor the flight in addition to the pilot in command (PIC). For these reasons, the Petitioner believes that 

the risks associated with the operation ofthe sUAS are so diminished from the level of risk associated 

with commercial operations contemplated by Part 61, that allowing operations of the sUAS as requested 

with a private pilot as the pilot in command (PIC) exceeds the present level of safety as contemplated by 

14 C.F.R. § 61.113 (a) & (b). 

The FAA has issued several exemptions to 14 C.F.R. § 61.113, a sampling includes the following 

exemptions: 11062, 1106311109, 11215, 11227, 11229, 11239, 11241,11258, 11283, 11286, 11335. 

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

Petitioner seeks an exemption from 14 C.F.R. § 91.7(a). This regulation requires that a civil aircraft be in 

an airworthy condition in order to be operated. In the event that the exemption be granted allowing 

commercial operation of sUAS without an airworthiness certificate, no FAA regulatory standard will exist 

for determining airworthiness. 

Equivalent Level of Safety 

Petitioner proposes to operate a sUAS with a lift-off, gross weight of less than 5 pounds (apx. 60oz.) and 

it will not be flown unless it has been maintained and prepared in accordance with all specifications and 

requirements identified by the manufacturer. An equivalent level of safety will be achieved by ensuring 

compliance with the sUAS instruction manual and quick start guide, attached in the Appendix to this 

application. 

The FAA has issued several exemptions to 14 C.F.R. § 91. 7(a), a sampling includes the following 

exemptions: 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 11136, 11138,11150, 

11153, 11156, 11157, 1115811160, 11161, 11166, 11167, 11170, 11171, 11172, 11174, 11177, 11178, 

11184, 11185, 11188, 11189, 11191, 11192, 11193, 11195, 111204, 11215, 11227, 11229, 11335 0 

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

• Pursuant to 14 C.F.R. § 91.9(b) (2): 

(b). No person may operate a U.S.-registered civil aircraft ... 

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

Unless there is available in the aircraft a current approved airplane or Rotorcraft Flight Manual 

Approved manual material, markings, and placards, or any combination thereof. 

9 
Petitioner's sUAS has a take-off, gross weight ofless than 5 pounds (apx. 60oz.). Given the size of the 

sUAS, it has no ability to place or carry such a flight manual onboard the aircraft. Furthermore, there will 

be no pilot on board and no room or capacity to carry this item onboard the aircraft. 

Equivalent Level of Safety 

An equivalent level of safety will be achieved by keeping the sUAS instruction manual at the ground 

control point where the pilot in command (PIC) flying the sUAS will have immediate access to it. The 

FAA has issued several exemptions to 14 C.F.R. § 91.9(b)(2), a sampling includes the following 

exemptions: 8607, 8737, 8738, 9299, 9299A, 9565, 9565B, 1016710167A, 10602, 10700, 11062, 11063, 

11064, 11065, 11066, 11067, 11080, 11109, 11110, 11111, 11112, 11114, 11136, 11138, 11150, 11153, 

11156, 11157, 11062, 11063, 11080, 11109, 11153, 11174. 

14 C.F.R. § 91.203(a) and (b): Carrying Civil Aircraft Certification and Registration. 

• Pursuant to 14 C.F.R. § 91.203(a) and (b): 

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

the following: 

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

(b). No person may operate a civil aircraft unless the airworthiness certificate required by 

Paragraph (a) of this section or a special flight authorization issued under § 91.714 is 

Displayed at the cabin or cockpit entrance so that it is legible. 

Petitioner's sUAS has a take-off, gross weight ofless than 5 pounds (apx. 60oz.). Given its size, the 

sUAS has no ability to carry certification and/or registration documents, nor is there a place to display 

them. Furthermore, there is no pilot onboard, nor are there passengers or a crew. 

Equivalent Level of Safety 

An equivalent level of safety will be achieved by keeping these documents at the ground control point 

where the pilot in command (PIC) flying the sUAS will have immediate access to them. The FAA has 

issued several exemptions to 14 C.F.R. § 91.203 (a) & (b), a sampling includes the following exemptions: 

9565, 9665, 9789, 9789A, 9797, 9797A, 9816A, 10700, 11062, 11080, 11109, 11153, 11174. 

14 C.F.R § 91.103: Preflight Action. 

This regulation requires each pilot in command (PIC) to become familiar with specific information before 

each flight, including information contained in the FAA-approved flight manual on board the aircraft. As 

FAA approved rotorcraft flight manuals will not be provided for the aircraft an exemption will be needed. 

Equivalent Level of Safety 

An equivalent level of safety will be provided as set forth on pages 4-5 and 20-27 of the instruction 

manual as well as the quick start guide (both are attached within the Appendix to this application). The 

pilot in command (PIC) will take all required preflight actions-including reviewing weather, flight battery 

requirements, landing and takeoff distances and aircraft performance data before initiation of flight. 

Furthermore, the sUAS instruction manual will be kept at the ground control point where the pilot flying 

the sUAS will have immediate access to it. 

10 
14 C.F.R. § 91.109: Flight Instruction. 

Petitioner seeks an exemption from 14 C.P.R.§ 91.109(a), this regulation provides that "no person may 

operate a civil aircraft (except a manned free balloon) that is being used for flight instruction 

unless that aircraft has fully functional dual controls." sUAS and remotely piloted aircraft, by their design 

do not have fully functional dual controls. Flight control is accomplished through the use of a hand-held, 

control box that communicates with the aircraft via radio communications. 

Equivalent Level of Safety 

Given the size and speed of the Yuneec Q500 Typhoon sUAS, an equivalent level of safe training can be 

performed without dual controls because no pilot or passengers are aboard the Yuneec Q500 Typhoon 

sUAS. In addition, the system is equipped with an automatic "Home Mode" that can be activated at any 

time in response to unusual and unforeseen circumstances. Furthermore, all persons will remain a safe 

distance away should the sUAS experience any difficulties during flight instruction. Finally, the aircraft's 

light weight and slow speeds with no pilot or passengers on board will create less of a danger to the 

public than a conventional aircraft equipped with dual controls. The FAA has issued exemptions for flight 

training without fully functional dual controls for a number of aircraft and also for flight instruction in 

experimental aircraft. Exemptions include: 5778K, 9862A, 11062. 

14 C.F.R. § 91.119: Minimum Safe Altitude. 

Petitioner seeks an exemption from the minimum safe altitude requirements of 14 C.F .R. § 91.119. 

Specifically, § 91.119( c) limits aircraft flying over areas other than congested areas to an altitude of 5 00 

feet above the surface, except over open water or sparsely populated areas. In those cases, the aircraft may 

not be operated closer than 500 feet to any person, vessel, vehicle or structure. In addition, section 

91.119( d) will allow a helicopter to operate at less than those minimum altitudes when it can be operated 

"without hazard to persons or property on the surface", provided that "each person operating the 

helicopter complies with any routes or altitudes specifically prescribed for helicopters by the FAA." 

Because aerial monitoring and inspection work must be conducted at relatively low altitudes and 

sometimes at altitudes less than 500 feet, an exemption from 14 C.P.R.§ 91.119(c) is requested. 

Equivalent Level of Safety 

In comparison to flight operations conducted with rotorcraft weighing far more than the Yuneec Q500 

Typhoon sUAS and given the lack of flammable fuel, any risk associated with these operations is far less 

than those that are presently allowed with conventional aircraft. An equivalent level of safety will be 

achieved given the size, weight, speed, and material of which the sUAS is constructed as well as the 

location where it will be operated. As described in the instruction manual, the Yuneec Q500 Typhoon 

sUAS will always be operated within a "geo-fenced", restricted area and no flight will take place without 

the permission of the landowner or those who control the land. Additionally, any potential buildings and 

people within this restricted area will not be exposed to these operations without their pre-obtained 

consent. Furthermore, by operating at a lower altitude, the sUAS will effectively maintain separation with 

the operations of conventional aircraft that must comply with 14 C.P.R. § 91.119. The FAA has issued to 

several exemptions to 14 C.F.R. § 91.119(c,) a sampling includes the following: 11162, 11163, 11164, 

11165, 11166, 111080, 11109, 11110, 11111,11112, 11114, 11136, 11138, 11150, 11153, 11174, 11215, 

11227, 11229, 11239, 11258 and 11335. 

14 C.F.R. § 91.121 Altimeter Settings. 

11 
Petitioner seeks an exemption from 14 C.F.R. § 91.121, which requires the person operating an aircraft to 

maintain cruising altitude or flight level by reference to an altimeter that is set to the elevation of the 

departure airport or barometric pressure. An exemption is sought because the Yuneec Q500 Typhoon 

sUAS does not have a barometric altimeter, but rather a GPS altitude read-out. 

Equivalent Level of Safety 

An equivalent level of safety will be achieved by following the procedures set forth in the sUAS 

instruction manual. The pilot in command (PIC) will be able to confirm the altitude of the launch site, as 

it will be shown on the GPS altitude indicator (located on the hand-held, flight control box) before the 

flight takes place. Furthermore, the Yuneec Q500 Typhoon sUAS is pre-programmed for a maximum 

altitude limited to 400 feet AGL. In addition, the pilot in command (PIC) will be able to continuously 

monitor the altitude of the sUAS throughout the flight, as it is displayed on the hand-held, flight control 

box. Thus ensuring that the sUAS will only be operated at a safe altitude. 

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

Petitioner seeks an exemption from 14 C.F.R. § 91.151(a)'s fuel requirements for flight in VFR (Visual 

Flight Rule) conditions. Accordingly, § 91.151 states: 

• (a). No person may begin a flight in an airplane under VFR conditions unless (considering wind 

and forecast weather conditions) there is enough fuel to fly to the first point of intended landing 

and, assuming normal cruising speed -

(1) During the day, to fly after that for at least 30 minutes: or 

(2) At night, to fly after that for at least 45 minutes. 

The battery powering the Yuneec Q500 Typhoon sUAS provides for approximately 20-25 minutes of 

powered flight. Because of this, it is impossible to meet the 30 minute reserve requirement set forth in 14 

C.F.R. § 91.151(a). However, given the limitations on the sUAS's proposed flight area(s), the location of 

its operation within a predetermined area and the construction of the sUAS, an exemption from 14 C.F.R. 

§ 91.151( a) is required. 

Equivalent Level of Safety 

Petitioner believes that an exemption from 14 C.F.R. § 91.151(a) is warranted. Operating the 

Yuneec Q500 Typhoon sUAS, without 30 minutes of reserve fuel does not engender the type of risks that 

§ 91.151(a) was intended to prevent given the size (less than 5 lbs.), speed (top speed apx. 25 knots) and 

light-weight materials of which the sUAS is constructed. Furthermore, the fact that it carries no pilot, 

passengers or cargo also enhances its safety. Operation will be limited to a controlled area where only 

people that have signed waivers will be pennitted. The pilot in command (PIC) of the sUAS will able to 

continuously monitor the strength of the battery, as it is always displayed on the hand-held, flight control 

box. Once the battery strength is indicated as "low" on the flight control box, the pilot in command (PIC) 

will simply land the sUAS. As an additional safeguard, the "Home Mode" function of the sUAS can be 

programmed to operate in conjunction with low battery strength, so the sUAS can be programmed to 

automatically "land" once a predetermined amount of battery strength has been utilized. The FAA has 

issued similar exemptions to 14 C.F.R. § 91.151 (a) including exemption nos. 2689F, 5745, 10673 and 

10808. 

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

12 
14 C.F.R § 91.405(a) requires that an aircraft operator or owner "shall have that aircraft inspected as 

prescribed in subpart E of this part and shall between required inspections, except as provided in 

paragraph (c) of this section, have discrepancies repaired as prescribed in Part 4 3 of this chapter ... " 

§ 91.407(a) (1) also makes reference to requirements in Part 43. § 91.409(a) (2) requires an annual 

inspection for the issuance of an airworthiness certificate.§ 91.417(a) requires the aircraft owner or 

operator to keep records showing certain maintenance work that has been accomplished by certificated 

mechanics, under Part 43 or licensed pilots and records of approval of the aircraft to return to service. An 

exemption to these regulations is needed because Part 43 and these sections apply only to aircraft with an 

airworthiness certificate, which the sUAS will not have. 

Equivalent Level of Safety 

An equivalent level of safety will be achieved because the sUAS is nearly maintenance free. The sUAS 

will perform several automatic preflight checks, prior to take-off and a failure of any one of them will act 

to prevent flight. Visual pre-flight checks that cannot be performed by the system will also be perfonned 

prior to each flight. These pre-flight checks will include an inspection of the airframe, an inspection of the 

rotors and the inspection of all batteries (flight battery, control box battery). In the event that maintenance 

is required, it will be performed and noted in a maintenance log-specific to the sUAS, which will be kept. 

Both pre-flight checks and maintenance will be perfonned by the pilot in command (PIC) as this is the 

person most familiar with the aircraft and is best suited to maintain it in an airworthy condition. 

Furthermore, in the event that unforeseen mechanical issues arise, the sUAS can land immediately in its 

predetermined area of operation. It's small size, lack of pilot, passengers and significant cargo plus the 

fact that flight operations will only take place in restricted areas for a limited period of time, create less 

risk than the same factors associated with conventional fixed-wing aircraft and rotorcraft performing the 

same operation. 

VI. DRUG AND ALCOHOL PROGRAM 

Alex E. Paris Contracting Company, Inc. is committed to maintaining a safe, healthy and efficient 

workplace for the benefit of its employees, clients and the general public. Our Drug and Alcohol 

Abuse Prevention Policy has been developed to meet the requirements of the Drug-Free Workplace Act, 

Regulations of the US Department of Transportation (DOT) and the mandatory guidelines of the U.S. 

Department of Health and Human Services, (DHHS). 

VII. PRIVACY 

All flights will occur in accordance with any state or local laws regarding privacy. 

VIII. FEDRAL REGISTER SUMMARY 

Pursuant to 14 C.P.R. Part 11, the following summary is provided for publication in the Federal Register, 

should it be determined that publication is needed: 

Alex E. Paris Contracting Company, Inc. seeks an exemption from the following rules: 

14 C.P.R. Part 21, Subpart H; 14 C.P.R. § 91.203(a)(l); 14 C.P.R. § 45.23; 14 C.P.R. § 45.27(a), 14 

C.P.R.§ 61.113(a) & (b); 14 C.P.R.§ 91.9(c); 14 C.P.R.§ 91.9(b)(2); 14 C.P.R.§ 203(a) & (b); 14 

C.P.R.§ 91.7(a); 14 C.P.R.§ 91.103; 14 C.F.R § 91.109(a); 14 C.F.R § 91.119; 14 C.F.R § 91.121; 14 

13 
C.P.R.§ 121; 14 C.P.R.§ 91.151(a); 14 C.F.R § 91.405(a); 14 C.F.R § 91.407(a)(l); 14 C.F.R § 

91.409(a)(2); 14 C.F.R § 91.417(a) & (b). 

Approval of these exemptions allowing commercial operations of sUAS within the construction industry 

will enhance safety by reducing risk to the general public, property owners and on-site (construction), 

personnel. Manned aircraft monitoring and surveying creates a greater risk because the craft are much 

larger, carry on-board pilots, passengers and cargo and are also powered by combustible fuels. Similar 

monitoring and surveying conducted by on-site, personnel on the ground creates a greater risk due to the 

possibility of slips and falls. The operation of a small sUAS, weighing less than 5 pounds and powered by 

rechargeable lithium ion batteries will virtually eliminate the risk associated with a craft of larger mass 

powered by combustible fuels. Likewise, since the sUAS carries no pilot or passengers, these individuals 

will not be exposed to the risks associated with manned flights. Finally, the ability of the sUAS to 

monitor areas, difficult to access "on-foot" will reduce the risk of employee injuries due to slips & falls. 

All operations of this small sUAS will be conducted according to the strict conditions outlined within this 

petition. Accordingly, this will provide a level of safety equivalent to that envisioned by Congress when 

these regulations were originally enacted. In general, sUAS operations will be conducted only during 

daylight hours in predetermined and restricted areas. Property owners and onsite, personnel will have 

received advance notice of these operations and will have consented to them beforehand. The sUAS being 

operated weighs less than 5 pounds, will be flown no higher than 400 feet and will travel at slow speeds 

of no more than 25 knots. Accordingly, the risk to the property owners, on-site personnel and the general 

public is greatly reduced and the risk of interference with other aircraft is minimal. 

IX. CONCLUSION 

Satisfaction of the criteria provided in Section 33 of the Refonn Act of2012-size, weight, speed, 

operating capabilities, proximity to airports and populated areas, operation within a visual line of sight 

and national security-provide more than adequate justification for the grant of the requested exemptions 

allowing commercial operation of petitioner's sUAS in the construction industry. 

If you have any questions or require any additional information, please do not hesitate to contact either of 

the following parties. 

Respectfully Submitted, 

8ari;L 

Vice President of Operations 

Alex E. Paris Contracting Company, Inc . 

~~ 

. "~. z.:;._.-· 

William M. Bogar, Esq. 

Attorney/Superintendent 

Alex E. Paris Contracting Company, Inc. 

14 
APPENDIX 

(1). Yuneec QSOO Typhoon Instruction Manual.. .............................................. 16 

(2). Yuneec QSOO Typhoon Quick Start Guide ................................................. .47 

15 
G15CC 

TYPHOOn 

;,_ INSTRUCTION MANUAL __;_ 

16 

Version'2.1 

i 

I 

I 

l ' l 
y.u n c. c.~ ELECTRIC AVIATION 

17 
tABLE o-F CONTENTS 

1 TABLE OF CONTENTS 

2 INTRODUCTION 

2 SPECIFICATIONS 

3 NOTICES AND WARNINGS 

4 GENERAL SAFETY PRECAUTIONS AND WARNINGS 

5 FCC INFORMATION 

6 QSOO RTF CONTENTS 

7 BATTERY WARNINGS AND USAGE GUIDELINES 

lit CHARGING THE BATTERIES 

"9 PREPARING THE CG02•GB 

1).. INSTALLING THE PROPELLERS 

1.0 tlSOO, CGOZ~GB AND ST10 OVERVIEW 

11 STlODISPLAY . 

;i ~r~~~-~Cz6~;~~~; 13 FliGHT CONTROLS- SMART MODE 

i 

18 

15 FLIGHT CONTROLS- ANGLE (PILOT) MODE 

16 FLIGHT CONTROLS- HOME MODE 

17 LED STATUS INDICATIONS 

i9 TAKING PHOTOS AND RECORDING VIDEO 

20 INSTALLING THE FLIGHT BATTERY 

20 GPS FUNCTIONALITY 

21 PREPARING TO FLY 

22 FLYING 

23 DISABLING GPS 

23 GRAPHICALU~E~ INT~f{FACE 

24 COMPASS CALIBRATION 

26 STiO AND RECEIVER BINDING 

27 ST10 AND CG02-GB BINDING 

2~ TROUBLESHOOTING 

29 WARRANTYiNFdRMATION 
INTRODUCTION 

Change your perspective with the Yuneec QSOO Typhoon aerial photography and videography (APV) system. The system arrives 100% factory-assembled 

and test flown including the innovative 3-axis CG02-GB that records full HD 1080p (60, 50 or 48 fps) video and takes 12 mega pixel still photos. And the 

built-in digital video downlink delivers streaming video that can be viewed right on the screen of the included ST10 transmitter and Personal Ground 

Station. With the Q500 it's never been.easier to capture amazing photographs and video footage for a wide variety of uses. 

And although the Q500 is nearly 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 

QSOO 

Height: 210mm (8.3 in) 

Length (without rotor blades): 420mm (16.5 io) 

Width (without rotor blades): 420mm(16.5 in) 

Diameter (without rotor blades): 565mm.(22.2 in) 

Propeller/Rotor Blade Diameter: 33'0mm .(13.0 in) 

Weight (without batfely and payload): 1!:308 (40.0 oz) 

takeoff Weight (with battery and CG02·GB): 170dg 

(6Q.Ooz) · 

Battery; 5,400ri'lAh 3S 11.1VliPo (included] . . 

Charger: DC 35 11.1V LiPo balancing ami AC adapter 

(included) 

Ti'.insmllter: ST10 10·i:hailnel 2.4GHz With 5.8GHz vr~eo link (included) . . 

f![ght Time: 20-25 minutes 

CG02-GB 

Height: 115mm (4.5 in) 

Width: 75mm (2.91n) 

Depth: 135mm (1.4 in) 

Weight: 185g (6.5 oz) 

Video Resolution: 1080p 60, 50 or 48 fps 

Phd& ~<;lsolution: 12 mega pixels . 

Transl'l')lsslon Distance/Range: Up to 60bm (1970 ft) 

l;lepe~girig on receiving deviCe 

Transmission Band:.5.BGHz . . . 

Storage (memoJY); microSD Class 10 up to 128GB 

19 

ST10 

Number of Channels: 10 

.RC Band: 2.4GHz 

RC Modulation: Yuneec 

Video Downlink Band: 5.8GHz 

Telemetrv/OSD: Yes 

SD Card· Compatible: Yes 

LCD Screen Slze:4.5" 

TpLichscreen: Y_es 
NOriCES 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 ser.ious 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 resultln damage to the product, property and/or cause serious injury. 

WARNING: This is a sophisticated consumer product. It must be operated with caution and coml]lon 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:adultsupervision. 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. · 

Aqrr REcoMMENDATION: NoT FoR: cHILPREN uNDER 14 v£ARs.rHrs rs NorA. ToY. 

20 
GENERAL SAFETY PRECAUTIONS AND WARNINGS 

Gi\ 

CJ KEEP CLEAROFTHE DO NOTFLYNEARBYTALL THE.MAXIMUM FLYING 

SPINNING PROPELLERS! BUILDINGS/OBSTRUCTIONS ALTITUDE FOR THIS AIRCRAFT 

{100° MINIMUM CLEARANCE IS BOOOFT ABOVE SEA LEVEL! 

REQUIRED) 

® . . 

' 

DO.NOT FLY OVER 

CROWDS! 

DO NOTFLY·NEAR 

AIRPORTS! 

DO NOT FLY IN WINDS 

THA TEXCEED 8-12 MPH 

{13-19 KPH)! 

WARNING: Failure to use this product in th.e intended manner as de.scribed 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, dr.one, etc. is not a toy! If misused it can cause serious bodily harm and damage to property. 

WARNING: As the user of this productyou are solely and wholly .responsible for operating it: in. a manner that does not endanger yourself and others or result in damage to the product or the pr.operty of others. 

" l<eep your haf)ds, face and other parts of your body away from the spinflirig IJropeliers/rotor blades and other moving parts at an times. Keep itetilsthirt 

could impad or become entangled away from the prop!'!llers/rotor blades includitig 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 qr 

buifdings; 

• To ensure proper operation and safe flight performance never atl:ernpt to operate your aircraft nearby huildings or other obstructions that do bot offer 

a dear view of the sky and can restriCt GPS reception. . . · 

" Do pqt atttimjJt to operate your aircraft ln areas with potential magnetic arid/or radio Interference induding areas nearby broadcast towers, power 

transmission stations, higli voltage power lines, etc. 

o Always keep a safe distance in all directions around your atrcratt to avoid collisions and/or injury. This aircraft is control!sd by a radio slgrial subject to 

lnterfer~nce from ma.ny-sources outside your control. Jnterfe~ence can caL]se momentpry loss ofcontro1. 

" To ensure prQper ~ll~ safe opet·atioh pf the ?Utolll\ltlc landing fundi on in Horne Mode you must start the motors with the airCI·aft in a posjliarJ that has 

·at teast 10 feet {aJl!Jroxiniately 3 ineters) Of dear and open space around l t and achieve a proper GPS lock. . . . . o Do notattempt"to operate your aircraft with ;ohy worn and/qr damaged comlJoilenls, parts, etc. {including, but not limited to, damaged pr<Jpellers/rotor 

blades, old batteries, etc.). · · · 

~ Never operate yotir aircraft in poor or severe weather conditions inducliilg heavy winds, precipitation, lightning, etc. 

4 

21 
.. Always operate your aircraft starting with a fully charged battery. Always land as soon as possible after the first Ievell ow 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/persona! 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. 

s 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. 

e 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. 

e 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 QSOO are-not compatible with any other product, and the QSOO.is not compatible with any 

other E:SCs. Use-of any other ESCs in the QSOO will cause a crash, which may result in damage to the product,property and/or cause serious injury. 

FCC INFORMATION 

This device complies with part 15 of the FCc r(i!es .. Opercil:!on is subjecH6 thefoligVVlngtwo conditions: (1) This device maynofcaose harmful iri.terference, 

and-(2) this device.must accept any interference received, including interference that may cause undesired operation . 

. CAUTION.: Changes or rriodilication·s not .expressly apptoved by the party responsible for compliance could 'llold the user's authority to operate the 

equipment 

This product contains a t·adio transmii:l:er with wireless technology which has been tested and found lobe compliant with the applicable regulations governin,il ~radio transmitter in the. 2.400GI-Iz tci 2.4835GHz frequency range. . 

Ante11na SepaJ'i!tlon Distance: 

Malnl:aln '!. ~eJ:iaratiop 915t~nce of~t le{lst 2 in (50mm) between your boc,ly (not indud)n& Yol.lr fin,gers, hands and wrists} and the ,antenrii\s to meet the RF 

expos-ure ~afety requWerneii~ dii!~~imined by F<:;C regulations; · · · 

.5 

22 
Q$00 RTF CONTENTS 

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

& . 

. 

4 

:1 0500 RTF Airframe w/lnstalfed CGb2cGB 

2 STtO Transrt1ii:ter and Personal Ground Station 

3 ST10 LCD Sere eli Sun S11ade/Shield · 

4 s'rio NeckS~rap . . 

~ ACto DC l)SB AdapJer/Charger 

6 USB to Micro USB Cable 

.7 usa tnt.~rface/Programmer 

· a 540DmAh 3S 11.1\/ liPo Battery 

9 35 1:i.1V UPo Balance Connector Charge lead 

10 DC 35 11.1V UPo Balancing Charger 

6 

23 

13 t:!!l {jjj 

11· D.~ M\omo))iieA.;ce!i:sor-y.So:C~et/ 

tigt~re:H:a krgiltel' Receptacle Adapter 

1:? A(; tb De AdapteriPawer supply 

13 BGB microso .t"ardw/Ait'apter · 14 Motor Holder/Prop Installation Tool 

15 Pt-op~l!er:s/Rotor Blades (2 sets) 
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 tl]eccomplete 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. Q 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. a To charge the LiPo battery you must use only the included charger or a sultilbly compatible LiPo battery charger. Failure to do so may result in a fire causing property damage and/or serious injury. 

~ . .If 9t ;;JnY time the UPo qattery begins to balloon {jr sWell, disco(ltinue t;!1~rgh1g pi' discharging immediately. Qukkiy and s11fely disconnect the 

battery, then pliJc~ ~~ iiJ a safe, open a.rea away from flammable maler!a!s to 

observe it fqHt,}e~st::l.~ mlr:n:J,te!; c:;qptjni,llng to charge or discharge a batte1y that has bfiglin tp ballpon.orswell ¢im restil~ in a fire. A ba:ttery that 

has ballooned or :Sw0i1e!1 even a small ;;ur~ount rnust be removed from s~rvlc~ compt'"tl;lly; . . . 

$ Do not p\.i~r~cllscharge tl)e LiPo hattery, Dlschl;lrglng the battery too low can cause dar'riage to the battery resu)l:jrm in reduced power, night duration 

or fallur~ o.f the battery .t;:ntirely. LiPo cells should not bf! discharged t<1 

below 3:ov :e?C.h.tinder load. ·· · · · • Store the UPo bati:ery at room temperature and hi a dry area for best result~. 

24 

• 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.eharge batteries. o 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: Ws safer and better forthe longevity of the batter{ to 

;s~ore it onlyjJari:ially cbarg~d for a:oy l~ngth of time~ Storing ~he b<Jt:!:ery apprmdm,ot~ly 5()'%, charl:eq (wliich Is aro!Ji1d 3.85V IJ~· ct'!ll) is wiJi&lly 

best; however, it will tal(~ !;ome careful mimagemen·t ofthe charge'time and 

the·use of'·avoltrrletel' to.;:~~6t~ve this ilolt;lge. If Voi.l have the equipment and skms to ;;tlli~v~tti~ ~o% d).arge level tor storage it is re'<=omniended.lf 

not; siinply be stlfe 'to niit ~ore the battery fully duiri;:ed whenever 

posslb!e, frl fact, as loflg as the .battery will be stored at apprq><imately room teilipetarure ~rid fqt iJ!l mpre th'ali ~few weel~s ~~fore \lie next use, it m.ay 

be best to store the baftety In the discharged state alter the last flight (as 

lof},g as th('l bal:l:ery was not over-plsc.lw~ed qn the last flight): 

! 

I 
CHARGING THE BATTERIES 

WARNING: Lithium lon (Ulan) and lithium Polymer (UPo} batteries are 

significantly more volatile than alkaline, NiCd or NiMH batteries. Ail 

instructions and warnings must be followed exactly to prevent property 

damage and/or serious injury as the mishandling of Lilon/liPo batteries can result in fire. By handling, charging or using the included Ulon/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 theplace 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 lf.IQ!\1 ST1p .E!ATTERY 

Ypu qm tharge the lilon battery h'ls\alled in the ST10 from a 100·240V AC 

o~tlet using the USB <!dapter"chargel', or from a suitable USB power source (2.0 amps n1ax), with the USB to micro USB cable. While the ST10 Is 

pow~red off conne~:t the catile to the USB adapter/charger, then. plug it li'Jtt:i,th~ USB co~nectpr/charging port ari the ti~ht side, After appro)(ii{Jately 30"45 seconds the lED Indicator for th!l battery will blii1k blue whUe tl1.e 

~(lt[ery .is cl1~rgin& and wm glow solid blue when the (Jatter\• is fully 

,dJ.arged. It )Viii take ;:~pproximately 5.5 hours to charge a fully discharged 

{not over~dischprged) batlf;ry; 

NOTE: Th~ AC plug type will vary depending on the region in which the 

product was jropqrted/purchased (AU "Australian: EU = European: UK = 

United !(lngdom; US = United !";b3tes). 

8 

25 
PREPARING 'THE CG02~GB 

WARNING: Before installing the flight battery and powering on the QSOO 

you MUST remove the cover/lock from the rear of the CG02-GB by 

carefully sliding it backward. Failure to remove the cover /lock can result in 

damage to the QSOO and the CG02-GB! 

QUICK TIP: It's a good idea to re-install the cover/lock after each flying 

session and while transporting/sto!'ing the QSOO Oust remember to remove 

the cover/lock before powering on the QSOO and CG02-GB!). 

Step 1), Remove the cqver/locik {rom fhe real' of the tG02-GB by carefully sliding it backliJard. · · · 

Step2) Slide the microSD card into tht; corn:sponding slot.on the bottom of 

the 'CG02~GB. You t;an· us.e the Included 8G~ c~i-d or any Class 10 rnkroSD 

card Lip to 128GB. 

Ste:P 3) Cai'eful_!y remove the ):lrote~:;tive ma~erial from the camera lens. 

9 

26 

INSTALliNG THE PROPELl~RS 

WARNING: We recommend weadng gloves and using extreme care when 

instali[ng the propellers/rotor blades. · 

Eadi niotor aiid propeller are. marked with an: 'A' or 1B' to enstrre easy 

installation In th~ cmreGJ: positions. (for example: Install propellers marked 

with 'A' on motor~ hjal'k¢dwlto 'A'J, 

IMPORTANT NOT£: It is ,NOT pqssible to i~stall a propeller marked with 

'A' on a motorrnarkedwito ~~:~·. The threads go in diff¢rent diredions for 

the 'A' and 'B' niotors/propellers. · 

Step 1) Use the spedai tpol (!ndu~e~) tP hold the motor so it .cannot spiri. 

CAUTION.: Do not ~\fer-tighten the propellers when using the tool. 

Step~} IMtllll 'the cpi're5pondlng j:Jropellir by rqhii!ng iJ; triaJing tidg~ fi~st 

until it's secure against the a-ring located at the bottoin of the l)lotor ~haft. 

'$tep .3) Repeat sh?po: 1 and 2 to lnsf:;lll lh\i three remaining propellers sei:urely. . . 
(1500, CG02=GB AND ST10 OVERVIEW 

14 15 16 

11 

10-~~2E~JE~J!~~ 12 

'13 

17 

18 

19 

ZG 

21 

5 

6 

The ST10 is equipped with an internal cooling fan and components that deliver vibrating and 

a.vdible alert~. · 

IMPORTJ\NT NOTE: Altho,ugh the STiO is equipped with digltal'trims' (lo,ated below the control 

s~~ks} th¢y are not active/fin1dional when tonlrollilig th\'! Q500. 

io 

27 

Q500 I CG02·GB 

1 CG02-GB Gimbal Camera 

2 Camera LED Statu.s Indicator 

3 Camera Lens 

4 5.8GHz Alitenna 

5 Main lED Status Indicator 

6 Power Switch 

ST10 

7 Proportional Control Rate Slider . 

8 USB Connector/Charging Port 

9 Audio/Earphone Jack 

10 Take Still Photo Button 

11 Start/Stop Motors Button . · · 

12 Rudder/Yaw Control{tor.Mode 2 and Mode 1) 

13 Thrott!e/AititudeCohtr.ol(forMode.2) 

Elev<~tor/Pitch Conttol (for Mode 1) 

14 S.BGHz t.ntenlia '(located inside the case) 

15, Stahls lndkators{for ST10 baltely, 5.E;GHz WiFi . dndGPS) . . . 

i6 2AGHz Antenna {located inside the handle) 

-17 Stllrt/Stop Video Retordihg Button · M ~Jight!VIild.eserectiot1.swi}ch 

1? Aileron/Roll Control (Mode 2 and Mode 1} 

20 Elevat9r/Pit<;l1 Control (Mode 2) 

.· Throtile/A(fitude Ca.htriJI {Made 1) 

21 Power Switch 

:~2 Volume 9nd Navigation Touch~Activatet:l Buttons 

• {VD/ume D,own/Volt1111e Up/M_imu/Home/Back) 

23 CG02.;GB Pitch Angle/Position Control Slider 

24 SD Card Slot {located under t/w battery) 
ST10 DISPLAY 

The ST10is equipped with a touchscreen display that allow$ for changing various settings and viewing real-time telemetry data and streaming video during 

flight. 

2 3 4 5 7 8 1 Mode( Name 

2 Frames Per Second for Video Recording Button 

3 Status Information 

4 Direction to Home Point 

5 Clock/Current Time 19 6 GPS Status and Number o.f Satellites for ST10 

7 S.SGHz WiFi Video Link Status 

18 10 8 ST10 Battery Charge L,evel Status Icon 

9 Aircraft Battery Voltage 

10 Altitude of Aircraft (Above Ground Level) 17 1.1 11 GrouncrSpeed of Aircraft 

12 pistan~e df Airtraft from Home Point 

16 12 13 Model Select Menu Button 

14 Fli!# Settings Mehu Button ~5 System Se.ffings Menu Bvtt.on 

16 Latitude/Longitude Position of Aircraft 

17 Number of Satellites for Aircraft 

18 GPS Status f~r Air~raft . 

15 1~ 13 19 Right Mode of Aircraft 

QUICK TIP; Double tap on the scr¢ei1 to ind·eas~ fh~ S!Z.e of the \lideb viewing area ti? fuiH;(;'((ij:ln_and ~O:u.b!e tap again tq return to tl,le standard size). 

WARNING: NEVER i)~te(l:ip~ tp fl'{~he QSQQ via. First-Pei's~mView (FPV). There';; a slfght 'lag' iil the (:;G02~GB streamlrig-Vi,t;leo dowhlihkto the ST10, and 

as a result the sfreamhig v!deoiFPV should only be used for aligning camera shots and not for flying! 1,\ftempting to fly via FPV can result in a crash that will 

C-aUS!i;! damage to the product, property 911#/0l'. CaUse SE)tioUS inJUi)i. . 

IMPORTANT NOTE:_Streaming video from the.CG02~GB to the ST10 and. to·.a separate phone/tablet (o1; another Yuneec trimsmitter/pers,Jn;id ground 

sti3tlon) at the same Li]:i1e is NOT re(:ommended as ft will result in a veiy significant lag in the Video downlink 

11 

28 
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 Vi!=Wing in sun light, 

fliGHT CONTROLS 

NOJE: The information in thiS and the following sections refers to the 

d~fault 'Mode 2' control ttlhllguration of the ST10. The left-hand stick on 

tli<'l ST10 controls the i:htottl!'i (climb/descend) and rudder (yaw left/right) 

chan.neJ.s .. When t~e lef_t-h'ln.d sti.c!< (also k,nowr a_s tbe throttle stick) ls in 

the 1i1lddle poslticih during night the Q~OO Wlil J'naintali1 the cutren.t 

il.ftr~uck. As you move the ~tick upward Uie QSOb will climb, and as you 

inove the stick downward the Q5oo will descend. 11le farther 1J.Way from 

th~ middle position yeti move tf1e stick the faster the .QSOO will dimh or 

descend. 

29 

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. 

400 

Climb 

Feet 

(Max. 

I 122 

Altitude 

Meters) ~ ( ® \ ~. 

Maintain Altitude 

Descend I Land 

Mqving the !eft-hand ·stkk tq the !eftwUl turn (yaw) the nose·of the .QSOO 

to the left abou~ the verlical axis. And moving the stick to the right will turn 

(yaw) the nose of the QSOCi to the right 
PROPORTIONAL CONTROL RATE SUDER 

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 

SELECTING A FLIGHT MODE 

The QSOO is programmed with thre.e {3) flight modes that can be selected 

via the Flight Mode Selection Switch located just above the right-hand 

control stick. 

30 

FLIGHT CONTROLS"' SMART MODE 

When the Flight Mode Selection Switch is the top position the Q500 will be 

in Smart Mode. 

Although we recommend learning to fly the Q500 in.Angle (Pilot) Mode as 

soon as possible, Smart Mode is typically the best mode for first-time pilots 

to fly in and also features 'Follow Me'. 

In Smart Mode the QSOO 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 Q500 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. 

'@52 t..:Ct/:26Jit~lcr$ 
The Follow Me feature the Q500 Typhoon to follow the pilot, adjusting its 

location to the location of the ST10. The Fo!!ow Me feature is enabled 

when the number of connected satellites is 6 or more. When Follow Me is 

active the QSOO's Main LED Status Indicator will blink white eve1y three 

seconds. If the Q500's Main LED Status Indicator remains solid green, the 

Follow Me feature is nat enabled. 

When using the FO~LOW ME fe~ture, keep hJ rilind th<Jt fhe <Jircraft: will 

maintal11 a ~ons@nt altitude and can not ~etect obqtacles.- Pilots Who 

change thelt~tfihide by for example, moving to higliergt'ound, during flight 

. should be mihclf~l of this. 

14 

31 

..-------~+X 

.. ·. ,.till .. 

.. 

... ,. .. .. 
Additional Smart Mode Features: 

*SMART CIRCLE 

In most cases the Smart Circle will keep the QSOO from coming within 

approximately 26 feet (8 meters) of you (as long as you position yourself at 

least 26 feet/8 meters behind the QSOO. 

GEO-FENCE 

The geo-fence is a virtual 'barrier' that will keep the QSOO from traveling 

farther than 300 feet (91 meters). And 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 Q500 has a suitable GPS 

signal/lock. If you take off in Smart Mode and the Q500 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 t~~ Q50~ in Angle (Pilot) Mode the aircraft may crash or ev!!it 'flY away'. . . 

IMPORTANT NOTE:Q'asl:i damage and 'fly awa~·s' are NOTcovered under 

warranty, 

'32 

FLIGHT CONTROLS -ANGlE (PILOT) MODE 

When the Flight Mode Selection Switch is the middle position the QSOO 

will. be in Angle {also known as Pilot) Mode. 

Angle (Pilot) Mode is the mode preferred 

by experienced RC/drone ·pilots because 

the Q500 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 QSOO 

will bank toward the left side and move to 

the left. This means if the front/nose of 

the QSOO is pointing away from you it will 

mqve to the'reft/bi.jtif the frqntfnose is 

pointing at you the QSOd will move to the 

right. · 

Additional Angle (Pilot) Mode Features: 

POSiTiON i-iOLD AND SELF-LEVEliNG 

Th.e :QSOO wiir alitQmilHcally hold jts po;;itjpn (with' a suitJble · GPS 

$ignalilock) and maintain a level attitude when the right•hand stid< is 

centered. 

WARNING: If you do not ~roperly control the Q~OO In Angle (Pilot) Mode 

the aircraft lltay'crash or eveh 'fly away'. 

IMPQRTANT NOTE: Cr<Jsh damage and 'fly a ways' are NOT i:o\lel'e'd UtKjer 

warrani:y. 
FLIGHT CONTROLS ~ BOME MODE 

When the Flight Mode Selection Switch is in the bottom position the Q500 

will be in Home (also known as Return to Home) Mode. 

LANDING . ... 

~O~A:l~N • .")(Ya a a r· ;, a ·~~ 13-26ft 

(4-Sm) 

~ ~ • • PILOT lOCATION ;..: is .• m 

~ 

~ 

In Home Mode the the Follow Me 

feature will fly back the QSOO in a 

straight line in the direction of the 

pilots' current location, and 

automatically land within 13-26 ft 

(4-Sm) of the pilot. This can be 

very helpful for first-time pilots 

who aren't quite ready to land the 

QSOO themselves. It can also be 

helpful fqr.pilots tliat lose orientation during flight; simply activate 

Ho111e Mode until the QSOO 

automatically moves toward the 

hpro~ position, and on~e yqlr've 

coi11'lrmed orientaiion·switch back 

to Angle (Piiot) tv1ode- And if the 

Q!ioo ever loses the link wmi the 

ST10 it will automatically enter Home. Mode. When 1-lome Mode is 

activated the QSOO will respond as follows: 

1:6 

33 

A) When flying higher than 33 feet {10 meters) the QSOO wlll maintain the 

current altitude, fly back to the home point, then descend vertically until it 

lands. 

.• ~ 10m 

B) When flying lower than 33 feet (10 meters) the QSOO will climb to 33 

feet (10 meters) while flying back to the home point, then will descend 

vertically until it lands. 

• 

.. 10m 
CAUTION: You must be certain there are no obstacles in the 'Return to 

Home' flight path otherwise the Q500 may come into contact with them 

and crash. And while the QSOO 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 QSOO has a suitable GPS 

signal/lock. If the Q500 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 QSOO in Angle. (Pilot) 

Mode the aircraft may crash or even 'fly away'. 

LED STATUS INDICAlfONS 

LED:$TATUS INDICATIONS DURING STARTUP 

Main lED Status Indicator 

Initialization In progress 

Initialization failed 

The aircraft is in 'bind' mode 

The aircraft is not connected/linked to the transmitter 

The aircraft is In a.no-fly zone• 

'Please see the instruction manuaUor mor.e infonnation 

regarding no-fly zones 

tEOSl'AtUS:lNDICAT!ONS 13EFQRE'/0Uf\ING FLIG~!T 

Main lED.Status.Jnclkator 

The ~trCI'aftls ln.Smart Mode wiih GPS lock 

The alrt~?ft is In Smart Mac]~ 1';'fthqut (:;PS (D<;l< 

Theafrr:Ji'lft isln An'gle Mqd.; with GPS lock 

Th\C ail·craitis in Angle M(Jde withol!t GPS lock 

l)le aircraft Is in l-lcm1a Mode 

Filitlevellowvoltage battery warning 

IMPORTANT NOTE: Crash damage and 'fly aways' are NOT covered under 

warranty. 

Flashes red, green and blue (2 times per second) 

Pulses red (3 times per second) 

Flashes orange very rapidly (10 times per second) 

Flashes blue rapidly (5 times per second) 

Flashes red and white rapidly.(S·timespersecond) 

Glows solid green 

· Fl~?h.6 gre~n (3 times per se~o.nd) then off 

(for :i. second) 

Gidi'IS sOlid purple 

Flashes !JUrp!e {3 times persec<;~nd) then off 

(for 1 second) 

Ffashesl'ed rnpidly ($times per second) 

Flashes rod, green and blue ev~ry 3 seconds 

17 

34 

---

• I I I I • ~ I I I I I • I J I I I 

---------- ·······•RtiMIIIIIIIliiiiiDI··· I I I I I I I I I I I I I I I 

'I I I I I I I I I I I I I I I 

---

II II Iii 

I • • I • 

••••••••••••••• I 91 I 
Second Ievell ow voltage battery warning 

GPS lost 

Compass calibration required 

Below Motor LED Status Indicators 

Low voltage battery warning 

GPS disabled/lost 

LED STATUS INDICATIONS FOR CAliBRATION MODES 

Main LED Status Indicator 

Compass calibration Mode entered 

Col"l)pass calibration started 

Accelerometer calibration started 

Accelerometer calibration Mode entered/data collection 

finished 

Calibr.ation Jailed 

.C-G02·G\3 CAMERAt!:MTAtUSJNDICftTIONS 

WiFi I cameraJnitialization in progress 

MicroSD card error or missing microSD card 

Ready 

Taking still photo 

Recording video 

Flashes red, green and blue continuously ~ 

Flashes purple (1 flash per second) ····- Flashes orange twice between any LED indication 

(when in the air) 

Flash rapidly (5 times per second) 

Flash 3 times per second then off 1 second second 

Flashes red and green slowly (2 times per second) 

Flashes.red and green rapidly (5 times per second) 

Flashes red, green and blue rapidly 

(3 times per second) 

Flashes red, green and blue slowly 

(1 time per second) 

Glows solid white 

Glows s.o\lci red 

Fhish~s yellow (1 time per second) 

Gl<JW& solid grt!en 

Gfo~s s~!fd b!ue (1 time for 2 seconds) 

H;ishes green. blUE! slowly {1 tlmi<' per 2 sei:pnde) 

18 

35 

---

I'III'IMIIIII:fll 

•••••••••••••••••••••••••••••• 

•••••••••••••••••••••••••••••• 

• • I 
TAKING PHOTOS AND RECORDING VIDEO 

The ST10 seamlessly integrates control of the CG02-GB so you can easily 

take still photos and start/stop video recording using the corresponding 

buttons located on top: 

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 CG02-GB will change from 

glowing solid green to glowing solid 

blue. 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-rec:ording video-in-orderto take still photos. 

TO· START/STOP RECORDING VIDEO 

Pre$;; .. tl)e button loc.ate9 near Jfl~ top 

right corner of ~he STiO: You'U hear an 

\tudible indication froi1] thE; S1:10 e<;1ch 

time the recording start~/stops; And 

while video js recording the LED jndicat{)r qn the front of tl)~ i:;GO~·GE! wilt 

flash blue af"ld green, and there Will be a red dot next tn the time length of the recording_ near the upper right-hand corner qn th'l screen of th~ ST~O. · 

IMPO!tfANT NOTF.: You can c~oose to record video iii 48, 50 (PAL) or 60 

(NTSC) fral'fies per second by tapping t.he c:;oxresponcling button near the 

ypper !eft·hancl.ci:lrner· Qri the sc:;re·en of the $T1b. And· keep in n1incl i:h~t 

the delay in the live vJdeo stream will be lowest at 48 ·and 50 as compared f~;;-60 frames per second. 

19 

36 

The slider located on the left side of the ST10 allows you to set the 

pitch/tilt position of the CG02-GB from approximately straight ahead 

(when the slider is in the uppermost position) to approximately straight 

down (when the slider is in the lowermost position). And you can easily set a position in between by adjusting the slider accordingly. 

QUICK TIP: There's an adjustable counterbalance located:on the rear .of 

the CG02-GB. This counterbalance has been adju~te·d ~t the factoiy to 

provide the best balance and performance overall sa typkally it should 

NOT need to be .. <>.djusted. However, if you find th?t th.e cqoi-GB is 

tnakirig any 'btiziing' sounds while powered Oh, tai·eful!y twist the COI,lnterbaiance in or out until ihe sound stops in order to achieve the best balance, 

p(!rformance and t:lhoto/video ·quality. 
JNSTALLING THE FLIGHT BATTERY 

Afterthe·flight battery has been fully charged it's ready to be installed in the 

QSOO: 

IMPORTANT NOTE: Keep the Q500 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. 

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. 

20 

37 

GPS FUNCTIONAUTY 

The QSOO 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 QSOO 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 QSOO 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 QSOO in Angle (Pilot) Mode 

without GPS assistance and accept ALL responsibility and liability for 

crashes or 'fly aways'. 

If the QSOO 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 Below Motor LED Status Indicators will flash three (3) times 

per second then will stay off for one (1) second when the QSOO 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), SmaJi: Mode and Home Mode will work again. 

WARNING: Loss of GPS signal/lock may result in a crash or even a 'fly 

away', 
IMPORTANT NOTE: Crash damage and 'flyaways' 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 QSOO in the 'No-Fly Zones' within a 4 mile (6.4 kilometer) 

radius of"most major airports. 

PREPARING TO FLY 

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 sei'ious injury. 

WARNING: Always operate the Q500 in open areas (approximately 10000 

square feet/930 square meters or more) that are free from people, vehicles, 

trees and othet .obstfuciior.s •. Never fly .near or above cr'o\>Jds, airports or buildings. · . . · · · .. ··- · ·· ·· . ·· . · · · . · · 

N~ver -~J;te.nliJt fQ opilrate the QSCO 

ne.;~r.by. Jiill _buifdj(lgS/9bstttn;Lions 

that do llot offei· a dear view of .tlie 

sky (i;t minlm!Jm cteara~nce of :ido•). 

A~~r selecting a. suitable flying area, 

please fonow these steps: 

step1) ALWAYS turn the:! ST1() on 

ahd. <~l{ow it to lioot up (ully BEFORE 

turning the· qsoo on. 

21 

38 

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 QSOO on a level and stable surface then slide the power 

switch to the 'ON' position. DO NOT TOUCH OR MOVE THE Q500 

UNTIL THE INITIALIZATION PROCESS IS COMPLETE. The Main LED 

Status Indicator on the bottom of the QSOOwill show one· of the following 

indications when initialization is complete: 

• • • ·-•· • • TAKEOFF ZONE • • • • • • • • 

~"~~, 

~ .. • ... • Ptl.OT 

;;~ LOCf,TION •• • • •· • • 

• The QSOO is in Smart Mode with 

GPS lock Glows solid green 

• The Q500 is in Smart Mode without 

.GPS lock Flashes green (3 times per 

second) then off (for 1 second) 

• The QSOO is in Angle (Pilot) Mode 

with GPS lock Glows solid _purple 

• l:he QSOO is fri Angie (Pilot) Mod!Ol 

withouU3Ps ·lpck Fla~h~.s PiJI'p!e (3 

timeS per second) 'then off (~or 1 

se_cond)' · 

Step 3) If. you do not have a G'P$lock move: the .Q500 to a different area, t~m ~~ off. then back an again. dr, if 

ypu have! a GPS lock, proc~ed to the 

nexfstep. . . 

*ep S) Step back approximately 26 feet(~ mete1:sl ~ehind the QSOD. 
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. 

FLYING 

TAKEOFF 

WARN!NG: Do not ai±empho operat~tlici Q$00 In winds 

that exeeed 8-12 miles per hour (13-19 kilometers per 

hour). 

to ~akeoff, slowly raise the left-hand stick to slightly above the center 

position. The QSOO wfll takeoff and climb slowly (or raise the stick further 

until it 'does). Allow the stick to return to the center position when the 

QSOO reaches the desireq .altitude. 

f-lVJNG 

Take yow· time le<Jming how the QSOO responds to various cqn[rol inputs 

while Oying.lnSn1art K1odethe QSOOwill always move in the direction the 

right-hand c~ntrol stick is pu~hed teiative to the pil~~ ~~d n~ m~l:l:er which 

\"'Jay the front/nose is pointed. Hi Angl!! (Pilot) Mode the Q500 will move in 

the dired.ion the control si:T~k 1~ p~shed r~l~tive to tli~ front/nos~ of the 

;lir<;raft {<1nd the 'angle' of movem~rit Is determined by how f'-lr you push the 

$tid< away from !he ~enter position}. And please see the corresponding 

39 

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 QSOO is 

drifting out of/beyond your control, simply release both control sticks. The 

Q500 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 QSOO automatically flies itself back to the 

home point and lands. 

LANDING 

There are two ways to land the QSOO: 

1) Pqsition the QSOO above the area where you would like to land. Slowly 

lower the left-hang stick t() below th\l,,~;enter po_sition;, Tl"je QSOO VVill 

descend slowly and !and. After the QSOO lands, press and hold the red 

START /STOP button for approximately two \2) seconds to stop the motors. 

2) Activate I-I orne Mode and tl)e QSOO wlllautomatically fly itself back to the 

home point and wii! land within a 10 foot (3 meter) diameter circfe around il 

WJ\RN!N.~:)lJWi!YSiand<is"sooli <js possib!e::;~fterthe flrst l(:ve!low voltage 

bi!~ecy warning, Qr land imme~lately after the second level low voltage 

battery warning (as lodicat¢d bY fhe vibrations _and audible alerts from the 

srio, and by the Below Motor U:p Statu~ hidicators rtashing rapidly}. At:Jd 

If at any time the Aircraft Balterv Volfage shown on the screen Is below 

:to.7v, land the Q590 lnimediately. 

AFTER. lANDING 

ALWAYS turn off the Q500 BEFORE tunihig off the ST10. Then remove 

the.batbet:Y 'from. the QSOO and allow it to cool to ambient/room temperature 

before recha"rging. 
WARNING: Do NOT leave the ST10 and QSOO powered on and do NOT 

leave the flight battery installed in the QSOO 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 underwarranty. 

OISABLING GPS 

WARNING: Smart Mode and Home Mode, along with their corresponding 

features, only work when GPS is active and the QSOO has a suitable GPS 

signal/lock. If you disable/turn off GPS the QSOO can only be flown in 

Angle (Pilot) Mode. And if you cannot properly control the QSOO in Angle 

(Pilot) Mode the aircraft may crash or even 'fly away'. 

IMPORTANT NOTE: Crash damage and 'fly aways! are-NOT c;overed ·under 

warranty. 

We do nottypically recommend disabling GPS for any· reason, especially if 

you're a first-time or low-time piiot. 1-iowever, lfydu1r'e' an::exjjerienced 

pilot that's ~b!¢ to prbperly control the Q500 in Angle {Pilot) Mope, and you 

do not exc~ed any ~!ti{uc!e/distante limits or fly It~ aiiY:'no llyiilnes' in your 

area, ypu can. 4lsa.ble/turn off GPS; And do Ndt disab!e/t!Jrn of( GPS 

uhless you accept All responsibility and liability for eras tie~ ·ar •tiy aways'. 

IMPORtANt No'r£: EVerY tiri1e you turn the gsoo on if wlll default to 

(jaying GPS ad:i\te/on (G,ven if you dh;11ble.tJ GPs· the (ast tin~e .is wa·s. 

poW;;ited on). · 

Step 1) While the ST10. and QSOO are powered on ~nd linked (and tl1e 

n1o~ots .are NOT runnmgl, move tiie Proportioricil Control Rate Slider on the 

rlg~t side of lhe ST10 to the uppermost (ral:iblt) position. 

23 

40 

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 Sma1t mode 4 times in 3 seconds. 

When GPS has been disabled successfully the QSOO 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 Below Motor 

LED Status Indicators will flash three (3) times per second then will stay off 

for one (1) second. 

G.RAPHICAL USER INTERFACE (GUI) 

You can download the graphical user interface (GUI) software· on the QSOO 

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. 
COMPASS CALIBRATION 

Step 1) Do not calibrate the compass 

inside parking structures, near buildings or surfaces vyith 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. 

St~p 5) When the main LED status 

indicator tla$he~ red and green 

slowly (2 firnes per second] you 

h;!Ve en~ered compass· cillibration 

Inode. Pick up th_e aircraft al1d hold 

it flat with the nose pointed to the 

north. Afte1· 5 seconds the main 

LED status indicator. should flash 

l'e.d and green rapidly {5 limes per 

secottd). 

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. 

Step 6) Siowly rotate the aircraft . 360 degrees toward the north (as 

illustrated) until it's flat and upright in ya_ur hands-again. 

41 

Step 3) Move the Proportional 

Control Rate Slider on the right side 

of the STlO to the uppermost 

(rabbit} position. 

SteP. 1) Rotate the a!n:t:<Jft 45 

d¢grees to the left .. .Then slowly 

rotate th~ aircraft 360 degrees 

toW,;1rd the noi'th (as Illustrated) q~!;il It's flat and upright In your [12rid~ ag<Jin. · 

Step 4) Move the left-hand stick all 

the wa/to the left and hold it there. 

Then move the Flight Mode 

Selection Switch from Smart to 

Home and Home to Smart mode 4 

times. 

Step B) Rotate the aircraft 45 

.degree? to th.e left, Then slowly 

rotate lhe aircraft • 360 degrees 

tmvard the north (as illustrat~d> 

until it's flat and upright in Y!-lili' 

hanps again. 
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 ·fiat and upright in your 

hands again. 

IMPORTANT NOTE: Steps 6 to 9 

m"tjst b.e completed .in less than 30 

seconds in order to successfully 

complete compass calibration. 

2.5 

42 

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. 

Step 11) If you hear an audible 

indication after the main LED 

status indicator stops blinking 

rapidly you have successfully 

completed compass calibration. 

IMPORTANT NOTE: If compass 

qfibration fails the main LED 

status indicator will glow solid 

White and you must restart the 

calibration process. 
ST10 AND RECEIVER BINDING 

Step 1) Turn on the Q500, 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. 

Step 2) Turn on the ST10, 

~~d if : r(\:q6ired t?ri t!ie . sc~:een (outSide of the ppp' 

'lip . st<1tus \'lilndow) ·to · 

bypass ·tne RC aml WfF.i 

cormection process. 

step 3) lari th\'t 'Mod.;! 

Select' button, and If 

·required press 'OK' to 

bypass any pop up 

warnings/alerts. 

St~p 4) Select the ex!sting 

tnci.def (for example: 1QSOO') you would like to 

bind to (or cre~te a 'New 

Model'), and lf required 

press 'OK' to bypass any 

pop up warnirigsialer!s. 

43 

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 

'SR12S_XXXXX' receiver 

listed in the column Linder' 

'Model', then tap 'OK' after 

the connection· has been 

est?bltshed. . 

Step 7). Tap the 'Batk' 

button j:wo (2) times to 

retl!.rn to th~ main screen 

and the model/receiver 

sfJotild. ;JUtomatically 

ctiruied to the STlO. 
ST10 AND CG02"'GB BINDING 

Step 1) Turn on the ST10, and if reql!ired tap the screen (outside of the pop 

up status window) to bypass the RCand WiFi connection process. 

Step · 2) Tap the 'Model 

Seh~ct' button, and if 

required press 'OK' ·to 

bypass any pop up 

warnings/alerts. 

Step 3) Select the existing 

model (for example: 'QSOO') 

you· would like to bind to (or 

<;reate a 'New Moder). and if required press 'OK' to 

bypass ;my . pop . up 

. W?rninJil~l<!)erts. 

Step 4) "tUm qn .tli~ QSOO 

and erisili'e . that the 

CG02-GB is powered on. 

27 

44 

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. 

Step 6) Tap the 'Bind' 

button and select the 

'CG02_XXXXXX' camera 

listed in th.e column under 

'Camera', then enter the 

password '1234567890' 

when prompted an~ tap 

'OK' after. tb.e cpnm;cti9n · 

has heenestablisileC!. · 

step 7) Tap the 'Back' button tw6 (2) times to return to the main scree!:) and 

Jhe ti.m'Jera· should agfo~t~aiii:aiiY i:Qn~ec~ tci the ST10. 

IMPORTANT NOTE: S~realilltig Vl4eO. fr~n'l tli·e CGbi-GB to the ST10 and 

t~ ·"! . separate llhon~/tab!et (¢r ~!'loth~r Yuhe~t transmitter/pe!'scirial 

ground. station} at tpe same time .is NOT recomm~nded as it will•·esult in a 

very significant lag in the. vi(:leo qownlirk. 
TROUBLESHOOTING 

ISSUE POSSIBLE CAUSE SOLUTION 

QSOO will not initialize The QSOO was moved during initialization. Turn the Q500 off then back on again, and ensure it does 

not move during the Initialization process. 

Flight battery will not The QSOO flight battery needs to be replaced. Replace the QSOO flight battery. 

charge {red LED on charger glows solid red). 

QSOO GPS will not lock Overcast, thick clouds blocking GPS reception. Wait for lighter cloud covet or disable GPS*. 

(ST10 indicates GPS 

Disabled) Solar flares in progress. Wait for disturbance to subside or disable GPS*. 

QSOO is indoors. Move the·QSOO outside or disable GPS*. 

()bjects blocking 100 degrees of clear view of the sky. Disable GPS .. Flying indoors/disabling GPS NOT Recommended. 

(Possibly underneath a meta!llc or glass cover, inside a vehicle, near tall buildings, etc. .. ) Move QSOO to a dear and open area. 

Video transmitter nearby, such as an aftermarket video 

downlink system. 

Reposition-or remove the video transmitter. 

Rab~d threat level by the U,S. goyernme:nt. Wait f!ir the threat levello be reduced or disable bps•. 

. QSOO GPS has reduced 

precision 

The GPS mpdule is possibly damaged • Replace the GPS IT!odule. 

the compass has .lleen exposed to a magnet. Move the QSOO away from the magnetic source.lf problem persists, calibtate compass, 

QSOO GPS functions not The GPS m()du!e i.s possibiy ci~maged~ Replace the GPS 11iodule. 

oper<!tlng properly GPS lock has not been acquired. Ensure GPS anb;nna has dear View of sky and GPS lo.ck has 

been acquired. 

28 

45 

ISSUE POSSIBLE CAUSE SOLUTION 

QSOO Motors won't 'Compass error' is indicated by the LED. See below for troubleshooting 'compass error'. 

start QSOO is in No Fly Zone. Move at least 4 miles away from no fly zone. Most major airports are no fly z~me areas. 

QSOO is above 8,000 feet above MSL. Move QSOO below 8,000 feet above MSL. 

Incorrect motor start up procedure . Review Motor Starting/Stopping procedure in manual. .. 

QSOO is too close to a metal object or metal surface. Move QSOO away from large metal objects or surfaces. 

QSOO Flashes . orange 

twice between indications Compass needs to be calibrated . Calibrate compass. 

QSOO beeps constantly EMERGENCY Mode. Possibly due to obstructed propel- Check that nothing is obstructing any propeller/motor, and motors won't start fer during motor start up. turn the"QSOO off then back on again. 

QSOO Won't hold WeakGPS signal. Confirm. that 'the flying area has 100 degrees of clear 

position in hnver view·of the,sky. 

U.S. Government has raised threat level. Waitfor threat level to be reduced before flying. ·-··-

Vil:)ratjon lev~!s !:ligh, indicat<:ld by shaky !ancling \lear. C~e<;:k. to ensure propellers are not behf, nicked or . .• damaged In any Way. Replace damageq propellers . 

WARRANTY tNFORMATION 

Yuoeec produtts and accessar1es ai'e_guarimteed against t\'itihuf~ctqrlng defect~ f!)rsix(6} iiiohi;hs frortrfhe i:itiginal date of l:iurchast;; Yuneeds soiepbligation hi the event of such defects.during this period is to repair or replace the defective part ot· product wilh a comparable part or product at Yunee.c.'s sole 

d!~t:;l'~ti.9:t:J· Except fot· Sl!Ch repair or rej:i]acemet1i; the sale, processing or rithei' handling of this product Is without warranty, coridlLion or qther li~bility. 

Damage {including crash damage) resulting from u~e. accident, or normal wear and tear Is n9t_covered by this or any warranty. Yuneet ass.umes no liability 

for any accident, injury, death, l!'ls~. or other claim ~<;latlid to i>r resulting from the us~ of this prtiduct. 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 Whim using the 

proc!uds. Returns or repfacen'lenb• of parts andior products may be subject to shipping, handling, replacement and/or restocking fees. 

IMPORTANT NOTE: Crash damage is NOT covered under warranty. 

46 
10 

, 

12 

13 

QEiCC 

T....-PHOOn 

17 

1B 

19 

20 

21 

YUnc.c.C: 

ELECTRIC AVIATION 

1 CG02-GB Glrnbal Carnel71 

2 C:a.me~u L~O Status Indicator 

3 Cameral~ns 

4 5,6Gr-lz Antenna 

s Power Switch 

6 Mllln ~ED StaltJs Indicator 

7 Propo:Uonal Control Rate Slider 

s USB c0nncc.tor/Cha:grn!) Port 

9 Audlo(Ea:phone-Jark 

10 Take SIIIIPholo Bullon 

11 Slari/StopMotorsButton 

12. Rudd!!rNawcontrol[lorMode1andMode 1} 

13 Throttle/Altitude Contro!{forModt1J 

E!ev'!tor/PllcbConlrol{forModt 1) 

14 5.8GHzAnterlna (lo•atecl/ns/de the con} 

15 Status Indicators {for STIO baltery,S.SGH:tWIFi :.nd GPSJ 

16 2.4GHzAntenna (localed/nslde theltondfc} 

17 Slart!Stop Video Recording Button 

18 FllghiMadeSelect[onSwllch 

19 Aileron/Roll Conlroi(Mode2andMode 1} 

20 Elevator/Pitch Control (Mode:J} 

Throl'ti~/AIUtudc Conlrof {Mod! 1} 

21 PoWeJ Switch 

22 Volume and NavlgalfonTouch·Actlvated Buttons 

(Volum!DowJVVoT~meUp/MMU/Home!HockJ 

2~ CG02·GB PltchAngle/Posltion Control Slltll!t 

24 SO CcrdS!ot (/(Jcoto=dundt!rtflt:bal/1!1)') 

WWW.YUNEEC.(:OM · 

!Mf!oA:TANT NOTE: All safety precautions and war~lngs, lns~rucUonS, ~;ranlles and other coll~!eral . Always operat~ Your.arr~rart ~~~~~n lhe'voltag~ Or u,e bau~'ry In the transmitter/persona! ~iound ~!atlo.n . InfOrmation Is subject to change al the sole discrellon of Yuneec. For the most up-to-date lnforfliatfon ldn a safe ran fie (as Indicated by the b.attery charge~lalus Icon on !he screen ofthll-iransmltlerfpersonal please visit the corresponding product page at\W!'W.Yuneec,com or contact the nearest 'iuneec office or ground station) • . authorized di~trlbutor. · Always keep the aircraft In dear l!ne of sight and under control, and k!ep the tr.msmiUer/personal 

The following special language terms are used throughout the product literature to Indicate various ~~~~~~ ~t~~~~~h~ft?e c~~~~j stt~Z~J~~~V~fy a~d'~~r~~fftfle motors In the event the ptope.\lers{ 

. r~veJs of potential h<~rm when operating this product: ~~~:y~~:~~~ ~~~~~~~~~n;~dt:a':t :~~~~~!~!~ ose before touching them and before fJylng again. 

NOT!CE: Procedures, which if not properly followed, create a posslb!lityofproperty damage andtot little Always remove biltt~rlcs after use and storc/lransport them per the c;orrespondlng guidelines. to no posslblllty of InJury, · Avoid water cxpo.mte to all electronic compnnent~, parts, elc. not specifically de~lgned and protected CAUTION: Procedures, whrch if not properly followl!d, creat~ the probabl[[ty of property damage and/or for use ln water. Moisture causes damage to electronic components Elnd parts.. a possibility of serious injul}'. • ~ Never place any poxtlon of the aircraft or any related accessories, components or parts In your mouth ;s~ 

· : ~~:r~r~~J:r:~~:~di~~;~~.~~J[i~~ri~~~:!l?r!~l~~h~r~b~a~ 11~~f~~o~~~~\~fr~/u~operty damage, dftng skcou1ica~seferlouslnJu~ordv1ndeatlJ. f h 

WAliNIN6: Read the ENllnE quick start guide and Instruction manuarto become familiar with the ~a~:f'i!t/~fo'f!~Jfu~~:~::t l!:t::dn w:r~f~~n~~c~~d~J~i~sthYst~r~ra~:;~~h ::;~~~~~~~ accessoties, features of the product b~fore operating. Failure to operate the product correctly can result In damage compol).ents or parts (Including, but not limited to. chargers. rechargeable batteries, etc.). to the product, property anOfor cause serious InjuJY. CAUTION; The electronic speed controls (ESCs) lnstplfed In the QSOO are nat compatible with any other WARNING: lhls Is a sophlstrc<:~ted consumer prod.ud. It must b~ operated wllh coution and common producl, and the QSOO Is not compallble wlth any other ESCs. Use of any other ESCs In the QSOO wl!l . sense, and requires some baslc mech~ni(:al abHity. Failure to operate this product In a si'ife and cause a crash, which may result In damage to the product, ptopertyandfor cause serious Injury. · responsible manner could result In damage to the product, property andfor cause serious Injury. This product Js not Intended for use by chlldren wtthoutdlrecta:doltsupervisfon. Do not use wlth fncompati· DATTfnY WARNINGS AND USAGE GUIDiif.lNES 

ble . .:omponents or alter thls pto-dud In any way culslde of the InstrUctions p:ovided by Yuneec. The 

qukkst<srtgulde 01ndlnstructlpn manu<:~! contain lnstructlons·forsafety,operation andmalntenance.Jtls WAnNING: llt!Jfum Pcfym~r (l!Po) batteries areslgnlfkantly more volatne than alkallm~, N!Cd or NIMH essenUal to read and follow alllhe Instructions and warnings p1torto assembly, setup and!oruse in order battcrres. All Inslructions and warnings must be followed exactly ta prevent property damage and/or to operate the product correctly and avoid damvge or serious Injury, serlof!s Injury as I he mishand/lng of LIPo batteries c11n r~sult In fire.By handling, charging or using the Included UPo battel}'you ussume all risks associated with l!Po buUerles.Jfyou do not agrea with lhes~ 

AGE RECOMMEI'IDATIDN': NO"£ FOR CHILDREN UNDER 14 YEAn!>. "fHISISNOT A TOY, conditions please return the complete product in new, unused condition to the place of purchase Immediately. 

GENERAL SAFE1

Y PRECII.UTJOflS AHD WII.RNIHGS You must :always charge the UPo battery In a safe, well-ventl/ated area away rrom nammable materials. 

WARNING~ Failure to use this product In the Intended manner as described In !he quick start guide and Never charge the llPo battery unaltellded at .'lny time. When charging I he batlefY you must always Instruction manual can result In damage to the product, properly andforcause serious InJury. A Radio remain In constant observation to monitor the char!jlng procen and react immediately to any potential Controlled (RC) multlrator aircraft, APV platform, drone, etc.l:s-not a toy I lfrnlsused ll can caus!:! ser1ous problems that may occur. bodl!y harm and damage to property, After flying/discharging the UPo battery you must allow It to co or to ambient/room temp!!raLUre before 

~~r~~~;~~~ ~~~~~;~~~~~;s~ffadnuJ~1h~r~r~r sr~rs~fti~~~~~;~ ~~sfh en~~~~~~{gfth:~~~J~~yaoT~rh~%. ~~c~h~7~~~·he UPo battary you must us~ only I he Intruded charger or a sun ably compatible liP a battery Keep your hands, face and oth!:!r parts of your body away frotn I he spinning propellers/rOtor blades and charger. Failure to do so may resultJn a firll causing property damage ancl/orsedous Injury, other moVIng parts at ill! times. Keep Items that could Impact or b!!com~ ent~ngled aw;,y from the If at any time lhe UP.o battery l:iegl.ns to balloon or mreJJ, discontinue charging or dl!ochargfng propt!llers!rotor blade~ lndudlng debris, partsJ tool~, loose clothing, etc, Immediately. Quickly and s21fely disconnect the battery, then place It In a safe, open area away from Always operate your illrcraft In open areas that are free from people, vehicles and other obstructions, flummable materials to observe It for ~t least 15 mlnUtes.Contfnu1ng to d1arge otdlscharge abil!tery Never fly near or above crowds, airports or buildings, · that ha$ begun to baltoon or swell cail result In a lire .. A battery that has ballooned or swollen even ra To ensure proper operation and safe flight performance never attempt to operate your ilTrcraft nearby small amount must be removed fromservfce completely. 

g~~~~~nt !t~;~~te~~~s~~~~~~~~~~a~~~~:;1~~~~:sc~~ft\tv~~~e :t~~t~~g:ti~a~df~~~~~~~ t~ei~~~~~~Ce ~~~~~~~vf~~~~~~:S~~~i~;~,~h~d~;a~l~~h~~g~~fu~~eo~at~:h!rt~~~~i~e!y~t~P~a~~~~~~~~1d~~~:1~ Including nreas nearby broadcast towers, powertransmlsfion stations, high voltage I! ower lines, etc. dfscharsed to below 3.0Veach under load. Always keep a safe distance rn a!r drrecUons around your aircraft to avoid co!l/slons apd/or InJury, This Store the-L!Po battery at room temperature-and In adf)"ar~a (or best rcsul!s. aircraft Is controlled by 21 radio signal subject lo interference from many source$ outside your control. When charging, !ran!portlng ot temporarily ~taring the LiPo battery the temperature ronge-should be Interference can ca. use momentary Joss. of control. · from approxlmalefy 40-12:0~ F {5-49• q. Do not store fhe battery or aircraft in a hot garage, car or direct Do not attempt to operate your alrc101ft ~boVe 8000 feet [l43B meters) AMSl (Above Mean Sea Level). sunlight. If stored In a hot garage or car the battery can be dama!Jed or even catch fire. Do not attempt to operate your aircraft In winds that exceed 8-12 miles per hour (13-19 kilometers per Never leave batteries, Chi!rgers and powersuppl!es unattended during use. hour). . Never attempt to charge low voltage, ballooned/~wol!en, damaged or wet batteries, To ensure proper and safe operation of the automatic landing funcHOn In 'Home' rnode you musl turn Never allow children under J 4 years of age to charge batteries. yaur aircraft on In a posltlon with at least 10 feet {approximately 3 meters) of clear llnd open ~pace Never charge a battery if My ofihewire leads have been damaged or shorted. around "1t and achieve a proper GP 5 lock. Neverallempt lo dlsassemble the batt"ery, charger or powet supply. Do not l':!ltempt to operate your aircraft with. any worn and/or damaged components, part>, etc. ~lever drop balterle$,chargers or powersupplle>. 

ll~~~rd~~~r~ie1 ;~~:i~:~~~r:~~ ~ao~~;~~~~~fee~~:{h~~o~:~d?tf~~~ fn~l~~f~~~:!~·winds, precipitation, ~~~:~~ ~';:fu~~t~~r~~c~t;~&:rff~ab~1~r~n!~~~~~~~~Yt~ri!~,r~nc~r~rir~i~d power supplies. lightning, etc. Always di'iConnect the battery after charging. Always operate your alrcraft stprling with a fully charged battery. Always lahd a~ soon as possible after Always terminate all proces~es If the battery, charger or power supply malfunctions. the first level low voltage battel)'warnrng orland lmmcd!atelyaflerthe s!:!cand level low voltage battery warning (as indicated by the vibrations and audible alerts from the transmltter/per!ional ground station). 

48 

. \ 

' 
!>ower the 5~3500-3 charger frOm a 100-240V AC ouUet using the AC adapter/power supply, or frorn a 12V DC accessory sockctlclgarette.Ughterreceptacle in a vehicle using the indudeQ. adapter. 

A green blinking LED indicates the charger is powerad .on and re<~dy to charge, and a red.blink!ng l€D Indicates the battery is charging. It will take ilpproximate\y 2· hours to charge a fully 

discharged {not over-discharged) battery. 

wARNING: AI( in!>tructions and \Vl'l;roings must be foUowed e?~actly to prevent property damage aml/or.seriow; injury CIS the mishandling of li!on/UPo batteries can result in fire. 

At WAYS turn the 5110 on and al!ow.it to boot up BEFORE turning the QSOO on {and ALWAYS turn the'Q500 off BEFORE ·tumingoffthe ST10). 

Place the QSOO.on a !eve! and sl.,bl~ surface then slide the switch to the 'ON' position. DO NOT. TOUCH OR MOVE THE QSOO UNTIL THE INlT!AUZATION.PROCESS IS COMPlETE. The main lED status Jndkator will gl6w solid green {Smart Mode) or solid purple {Angle/Pilot Mode) when i~maHzatfon is comp!ele, 

Proportional ControrRate Slider 

Sets the overall climb/descend and direclfotlal control rates. Use the turtle pos!Hoh for the loNest control rates {best for firsl-fime pilots and when flying between 5000 feet and 8000.fest Above Mean Sea level). Use the rabbit position fnr the highest control rates (best for experienced pilots and onlv wh.en. flying below 5000 feet AMSL 

2.1 Remove !he cover/Jock from tll~ rear of the CG02cG8 by carefully sliding it 

backward. 

e . 

. 

2.2 Insert the Included BGB card or any Class '10 mlcroSD card from t,GB to 128GB. 

2.3 Carefully remove the protective material from the camera lens. ~ 

Starting/Stopping the 

Motors 

Step back approximately 26 fEet (8 meters) behind the Q500. Press and hold the red START/STOP button for approximately three (3) seconds to .start the motors. Press and hold the button for a.pproxlmately two (2).seconds to slop the motors. 

CAUTION: Do notover-H"ghten the propellers when using the tocL 

Install the Battery 

NOYE: If the door will nal dose !he battery Is noUnsQrled.far enough Ia engage the cmmedor properly, 

There are two ways to land the QSOO: 

1) Position tht! QSOO ahova the area when~.' you would "!Ike to land. Slowly lower the left-hand sh"ck to befow the center posltlort. The Q500wlll desc:endstowfvand rand;Aite.r the QSOO lands, ~ress .:md hold l.he red SfART/STOP button for approximately one (1) second Ia sto'p the motors. · !!!"-------------------.. 2)Aclivate Ko~e Mode and the Qsoowm Flight·Controls: stickto!hel~ft/rightwillturn(yaw)thenosc automatically Ily Itself back to the home of the Q500lcft/rlghtaboutthevcrti~;al a>:l~. point and willian~ wjthln a 10 foot (3·meter} 

NOTE: The information In this and the TAKEOfF following steps refers to the default 'Mode 2' cont10! ~;onf1gurat1of) of the ST10. WARNING: Do not attempt to operate the Q500 in winds that exceed 8-12 m!fes per When the lert·hand slick . .Js in the middle houd13-19kl!ometersperhour), position the Q500 will maintain the current altitude. The farther awaY from the middle To lal::coff, stow!yralse thefeft~hondsH"ckto 

position you move the stkk the faster the slightly above !he center position. 1he QSOO QSOO will climb or descend. Moving the will takeoff and .climb slowly {or raise the 

Cllmb(Max.Aititude 

400 Feet/ 122 Meiers) 

~ 

. {@' -

.. Ma!ntainAII:itude ~ 

~ !~ Descend/Land {~'\ :__Yj=-

Selecting a Flight Mode 

The Q500 is programmed with three (3) O!ght modes that can be selected via the Flight Mode Sclcdion Switch \ototcd just above the rlght·hand control stick. 

49 

1) When I he lllsht mode swllcllls In the top position the.Q500 will be Tn Smart Mode, 

2} When the ilight mode switch Is in the middle pDSition the QSOO will be In Ansle {al~o known as Pilot) Mode_ 

3) When the flight roodo switch Is tn the lowest posllfon the QSOO .wH!.be: in Home Mo_de. 

diameter c!rde around lt. 

WARNING: Always land as soon as possible after the first !eve\ low vol!ag!! b<'!tterY warfling, or [and Immediately pfter the second level low voltage boHel)l w~rning (~5 

fndlc~ted by thevlbr~tlons and audl~le alerts from the ST10). And· if at ~ny lime the Aircraft 13atteryVoltage shown on the screen Is below 10,7V, land tl1e QSOO immediately_ 

I 

I 

I 

I ; 

j 

I 

I 

l 

! 

i 

l 

I .1 

I 

I 

! 
. When the maln LED status indicator glows sOlid purple lheQSOO Is In Angle (Pilot} Mode which ls·fntendcd for intermediate/experi· • enced pUots. The QSOO wllf move fn the direction the right·hartd control stick Is pushed relative to the fronUnose of the aircraft {and the ':mg!e1 of movement .i~ 

determined by how far you move the stick away fr~:n the center position). 

~ 

~ 

A~· B ? . . . . . 

c ~ .. a.. 

~~.~ Take Still Photo= Button A SlarttStop Recording VIdeo= Button B 

Use !he slider {C} on \he left side of the sno to set the pitch/till position {D) of the CG02-.GB. 

CAUTJON~.You MUST stop recording video in order to fake sfilf photos. It will take approximately 5 seconds to capture a still photo and before you can lake another. 

CAUTJON:·ALWAYS slop recording video before turning off t!ie Q500/CG02·GB to.avoicl.data loss. If 

i~~o~~~f~~~~~~U:he ~s{~ ~::~~~~;i~:p:r~~:afcl~ 26°:c=d~~~tl ~heln=e~ ~~g~f:~~ ~~ gloW solid green fndicating-the lastvldco fire was recovered. 

50 

" 

WhenlhemalnlEDstatuslndfc.a!orl'!ashes 

red thll QSOO fs In Home Mode. fo this mode tfH! Q500 will automatically ny Itself back to the homo point and wllllmdwilhin a 10.foot {3metcrl dtamete(cirdearound it. 

WARNING: If the QSOO foses GPS s.!gnal/lock whlle flying the. lEDs. under \ho motors: w!U nash lhree {3) times per second then wilt go off for one (1) second, the GPS status on the ST:10 screen will be listed-;:.s 'Disabled' and the QSOO will switch to An&le (Pilot) Mode automatlca!ly. Smart Mocl~:nnd 

Home Mode VJill not work and you must be able to properly control the Q500 ln Angle (Pilot} Mode otherwise It may crash or even 'rlyaway'. 

(ZJ Double tap the Center of the screen lo Increase tllesizeof the videov!ewlng<~rea. 

WARNING: NEVER atl.empt to fly the Q500 via FJrst·P~rson View (FPV}. Attempting to fly via FPV can result In a crash that wm cause damage to the produd, property and/orcauseseriousln]ury. 

11 Flight Mode of Aircraft 2) GPS Statu~ for Aircraft 3) Aircraft: Battery Vol !age 

IMPO~IANT NOTE: