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~ , ATTORNEYS AND COUNSELORS AT LAW 

Writer's Direct Line: (312) 269-2807 

mstephens@stonejonnsonlaw.com 

111 WEST WASHINGTON STREET 

Sum 1800 

CHICAGO, ILLINOIS 60602 

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave, SE 

Washington, DC 20590 

October 8, 2015 

TEL: 312.332.5656 

FAx: 312.332.5858 

StoneJohnsonlaw:~~m '·-· l 

Re: Exemption Request Under Section 333 of the FAA Reform Act and 

Part 11 of the Federal Aviation Regulations 

Dear Sir or Madam: 

Pursuant to Section 333 of the FAA Modernization and Reform Act of2012 (the "Reform Act" 

or "Section 333"), Subsection (f) of 49 U.S.C. § 44701, and 14 C.P.R. Part 11, McShane 

Construction Company ("McShane Construction") seeks an exemption from the Federal 

Aviation Regulations ("F ARs") listed below and discussed in Appendix A to allow it to operate 

the Yuneec Typhoon Q500 4K small Unmanned Aircraft Systems ("sUAS"). 

McShane Construction is a general contractor and construction firm involved in a number of 

industries including healthcare, hospitality, industrial, office and corporate headquarters. 

McShane Construction plans to use the sUAS for aerial imagery, inspection and data collection 

services for its projects at construction sites in various locations across the United States. The 

information collected by the sUAS will help McShane Construction inspect, monitor and oversee 

its construction projects. This will in turn translate to improved and more real-time decisions in 

construction that will enhance overall safety and lead to economic efficiencies. 

The safety and public benefits of using the sUAS in commercial construction applications are 

significant. The sUAS reduce the need to operate manned aircraft in unconventional operations, 

provide more accurate data in a manner that is more safe, economical and efficient, and with a 

reduced impact on the environment. 

Use of the sUAS also allows McShane Construction to limit inspections and construction site 

monitoring that must otherwise be accomplished by using lifts, ladders, scaffolds and other 

equipment at heights above work surfaces. Use of the sUAS will result in increased safety for 

construction workers and inspectors. 

Operations pursuant to the exemption will be subject to strict operating requirements and 

conditions to ensure at least an equivalent level of safety to currently authorized operations using 

manned aircraft and under conditions as may be modified by the FAA as required by Section 

333. 

ADDITIONAL OFFICES IN MERRILLVILLE, INDIANA, LISLE AND SPRINGFIELD, ILLINOIS 

ATTORNEYS ADMITTED IN ILLINOIS, INDIANA, COLORADO, MISSISSIPPI AND LOUISIANA 
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The Yuneec Typhoon q500 4K weighs approximately 60.0 ozs (1,700 grams) with battery and 

payload, and is powered electrically via a lithium polymer battery that drives four electric 

propellers. It operates at a maximum flight speed of 8 meters per second. This sUAS was 

designed with extensive automated control features, redundant systems, and integrated failsafes. Its default maximum flying height is 400ft, and McShane will conduct all operations 

underneath the 400' limit. 

Flight operations performed pursuant to this exemption will consist of at least two people: a 

pilot-in-command (the "PIC") and visual observer. The PIC is responsible for the direct and safe 

operation of the sUAS, monitoring their status and flight dynamics while maintaining visual line 

of sight and keeping the flight within the manufacturer's specified limits in terms of wind, flight 

range, battery life, and other operating limitations. The observer will be responsible for 

monitoring the airspace for other aircraft and hazards, advising the PIC before and during flight 

of all such observed risks, and monitoring the controlled operating area. The PIC will be a 

certificated airman who holds 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, 

possession, or the federal government. 

Because the sUAS will be used in lieu of comparatively higher risk operations now conducted 

with either fixed wing and rotary manned aircraft or by individuals, McShane Construction's 

operations will achieve at least an equivalent level of 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." 

The FAA has already granted many 333 exemption requests for operation of the sUAS model 

requested here. [See, e.g, FAA Exemption Nos. 11734, 11618, and 11438] Accordingly, it 

should grant this exemption request without delay. 

Applicant Information 

The name ofthe applicant is: 

McShane Construction Company 

The primary contact for this application is: 

Dennis Rumshas 

McShane Construction Company 

9550 W. Higgins Road, Suite 200 

Rosemont Illinois 60018 

Email- drumshas@mcshane.com 

Office- (847) 692-8727 

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Exemptions Requested 

McShane Construction respectfully requests exemptions from the following regulations as 

detailed in Appendix B: 

14 C.F.R. Part 21, Subpart H; 

14 C.F.R. § 91.7; 

14 C.F.R. § 91.9(b)(2); 

14 C.F.R. § 91.113; 

14 C.F.R. § 61.113(a), (b); 

14 C.F.R. § 61.133(a); 

14 C.F.R. § 91.119(c); 

14 C.F.R. § 91.121; 

14 C.F.R. § 91.151; 

14 C.F.R. § 91.203; 

14 C.F.R. § 91.405(a) and (b); 

14 C.F.R. § 91.407(a)(1); 

14 C.F.R. § 91.409(a)(1)-(2); and 

14 C.F.R. § 91.417(a). 

THE APPLICABLE LEGAL STANDARD UNDER SECTION 333 

Grant of this exemption application for use of the sUAS in aerial photography, data collection 

and inspection and monitoring applications will advance the Congressional mandate in Section 

333 of the Reform Act to accelerate the introduction ofUAS into the national airspace system 

("NAS") if it can be accomplished safely. This law directs the Secretary of Transportation to 

consider whether certain UAS may operate safely in the NAS before completion ofthe 

rulemaking required under Section 332 of the Reform Act. In 

The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This 

statutory authority, by its terms, includes exempting civil aircraft, as the term is defined under 

§40101 ofthe Act, from the requirement that all civil aircraft must have a current 

airworthiness certificate and those regulations requiring commercial pilots to operate aircraft 

in commercial service: 

The Administrator may grant an exemption from a requirement 

of a regulation prescribed under subsection (a) or (b) of this 

section or any of sections 44 702-44 716 of this title if the 

Administrator finds the exemption is in the public interest. 

49 U.S.C. §44701(t). See also 49 USC §44711(a); 49 USC §44704. 

The grant of the requested exemption is in the public interest based on the clear direction in 

Section 333 of the Reform Act; the additional authority in the Federal Aviation Act, as 

amended; the strong equivalent level of safety surrounding the proposed operations; and the 

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significant public benefit, including enhanced safety and cost savings associated with 

transitioning to UAS for aerial imagery, data collection and inspection services. McShane 

Construction therefore respectfully requests that the FAA grant the requested exemption 

without delay. 

Airworthiness of the Yuneec 0500 4K 

One element ofthe exemption application involves evidence ofthe airworthiness of the sUAS. 

McShane Construction believes that the sUAS has been shown to be airworthy and compliant 

with a significant level of safety. The previous 333 Grants of Exemptions by the FAA further 

highlight that operations of the sUAS will not adversely affect safety when compared to similar 

operations conducted by aircraft that have been issued an airworthiness certificate under 14 

C.P.R. Part 21, Subpart H. [e.g.,FAA Exemption Nos. 11734, 11618, and 11438] 

To enhance safety, it is also important to note that the sUAS are equipped with automated 

features which enhance safe takeoff, flight, and landing in many conditions, further details of 

which are provided in the applicable YUNEEC Q500 4K User Manuals.3 

To maintain airworthiness, McShane Construction will follow the inspection and maintenance 

programs designed specifically for the sUAS by the manufacturer, YUNEEC. Those programs 

are enhanced by an inflight monitoring system for the sUAS that monitor current position, 

wind speed and direction, battery charge, flight time, and altitude, including both above the 

takeoff location and above sea level. If onboard sensors detect a critical situation at any time 

(low battery, close proximity to the ground, weak data link signal, etc.) the sUAS will 

automatically initiate a preprogrammed safety procedure. In the event of any malfunction, the 

sUAS will undergo all maintenance required by the manufacturer and undergo flight testing 

before recommencing commercial operations. 

Proposed Operations and Associated Conditions 

McShane Construction intends to use the YUNEEC Typhoon q500 4K, weighing about four 

pounds with battery and payload (significantly less than 55 pounds), for the purpose of 

collecting aerial photography and data, as well as aerial inspection and monitoring 

applications at commercial construction sites. 

All of the sUAS operations will occur under tightly controlled conditions on privately owned 

land with the landowner's request and consent, solely during daylight hours, and at altitudes 

well below that which would pose a risk to other aircraft. The operations will take place in 

areas away from people, crowds and airports. Moreover, due to the nature and purpose ofthe 

operations, McShane Construction anticipates that it will fly the sUAS at relatively low 

altitudes and speeds and always below 400 feet AGL. The risk of interference with another 

aircraft is therefore minimal. 

Grant of this exemption to McShane Construction will be subject to the conditions listed in 

Appendix B, which are based upon the operating conditions required by the FAA's previous 

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grants of exemptions. The sUAS are characterized by a high degree of pre-programmed control 

and various built-in technical capabilities that limit the potential for operation outside of the 

conditions set forth in Appendix B . They were also designed with internal functional and 

safety features to assist the operator in safe and reliable operation. With pre-programmed flights 

and manual control, operators can easily maintain separation from manned aircraft operations 

and avoid other hazards. In the controlled environment under the operations conditions in 

Appendix B, operations will remain within visual line-of-sight (VLOS) and below 400 feet 

AGL. 

Operator Requirements 

As a condition to the grant of the exemptions, McShane Construction will require that the PIC 

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, possession, or the federal 

government. The PIC will also be subject to the flight review requirements pursuant to the 

Federal Aviation Regulations ("FARs"). 

In addition, the PIC must complete a training program for each sUAS that he or she will operate 

for McShane Construction. This training familiarizes the PIC to the operations and limitations 

of the sUAS. Training will also include discussions on the basic fundamentals ofUAS 

aerodynamics and technical limitations, as well as the more general topics of weather, the 

National Airspace System, and the regulatory framework. 

Public Interest 

The use of the sUAS in lieu of comparatively hazardous operations currently conducted with 

manned aircraft offers a net safety benefit and will achieve an enhanced level of safety, as 

mandated under Section 333(c) of the Reform Act. Approval of this application will also benefit 

the public interest by allowing better, safer, and more cost efficient information for McShane 

Construction and the public. Moreover, it will lessen the need for inspections by individuals that 

must often use equipment to observe construction sites from heights above the surface. 

Conventional aerial photography, inspection and monitoring operations using manned aircraft 

involve heavy aerial aircraft that must transit from airports to the operational location, carrying 

significant amounts of combustible fuel, and a multi-person crew. Manned aircraft are also at 

risk of fuel spillage and fire in the event of an accident or incident. By contrast, use of the 

sUAS is safe, economical and efficient. 

No national security issue is raised by the grant of the requested exemptions. Given the size, 

load-carrying capacity, the speed at which the sUAS operates (less than 25 meters per second), 

and the fact that they do not carry explosives or other dangerous materials, the use of the sUAS 

pose no threat to national security. In fact, the threat of causing damage to property is 

significantly reduced with the extremely low weight of the sUAS and limited operating areas. 

Any other security concerns are ameliorated by the fact that all individuals holding an FAA 

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airman certificate are subject to a security screening by the U.S. Department of Homeland 

Security. 49 U.S.C. § 44903G)(2)(D)(i). 

The grant of the requested exemption is in the public interest based on the clear direction in 

Section 333, the Federal Aviation Act, the high and equivalent level of safety ofthe proposed 

operations, and the significant public benefit, including enhanced safety and cost savings to be 

realized as a result of the use of the sUAS for aerial imagery, data collection and inspections. It 

is also in-line with the previous Grants of Exemption by the FAA for the same sUAS model. 

[FAA Exemption Nos. 11734, 11618, and 11438.] Accordingly, McShane Construction 

respectfully requests that the FAA grant an expedited exemption. 

MBS/sme 

Enclosures 

Let to USDT mbs 1 00815 

Respectfully submitted, 

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APPENDIX A 

EXEMPTION REQUEST AND EQUIVALENT LEVEL 0 FSAFETY SHOWINGS 

UNDER APPLICABLE RULES SUBJECT TO EXEMPTION 

14 C .F.R.Part21,SubpartH :Airworthiness 

Certificates 14 C FR § 91.203(a)(1) 

Section 91.203(a)(l) requires all civil aircraft to have a certificate of airworthiness. Part 21, 

Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements for the 

issuance of airworthiness certificates as required by FAR§ 91.203(a)(1). Given the very small 

size of the aircraft and the limited operating area associated with their utilization, it is 

unnecessary to go through the certificate of airworthiness process under Part 21 Subpart H to 

achieve or exceed current safety levels. 

Such an exemption meets the requirements of an equivalent level of safety under Part 11 and 

Section 333 of the Reform Act. The Federal Aviation Act and Section 333 of the Reform 

Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness 

certificate, upon consideration of the size, weight, speed, operational capability, and 

proximity to airports and populated areas of the UAS involved. 

In this case, an analysis of these criteria demonstrates 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 (fixed wing or rotorcraft) with an airworthiness certificate. 

The Yuneec Typhoon Q500 4K weights about 60 ounces with battery and payload. It does 

not carry a pilot or passenger and does not carry flammable fuel, and will operate exclusively 

within an area pre-disclosed and in compliance with conditions set forth herein. Operations 

under this exemption will be tightly controlled and monitored by the operator, pursuant to the 

conditions set forth in Appendix B, the applicable Yuneec manuals, and by local public 

safety requirements. 

Receipt of the prior permission of the land owner (or lessee), the size of the aircraft, the lack of 

flammable fuel, and the fact that the aircraft is carried to the location and not flown there all 

establish the equivalent level of safety. The sUAS provide at least an equivalent level of 

safety to that of such operations conducted with conventional manned aircraft that would be 

orders-of-magnitude larger and would be carrying passengers, cargo, and flammable fuel. The 

safety features including the Home feature, as described in the Yuneec Typhoon Q500 4K User 

Manuals, and throughout this document, underscore the importance placed on safety and 

reliability in the design and manufacture of the sUAS. 

14 C .F.R.§ 91.7 (a)-(b);Civil Aircraft Airworthiness 

Section 91.7(a) requires that a civil aircraft must be in airworthy condition to be operated. In 

previous grants of exemption for the sUAS, the FAA concluded that an exemption was 

required under 14 C.F.R. § 91.7(a). In each instance, the FAA granted relief under§ 91.7(a) 

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through a requirement that each petitioner ensure that the sUAS is in an airworthy conditionbased on compliance with the User Manual- prior to every flight. McShane Construction 

therefore requests that the FAA find similar relief under the same conditions here. 

Section 91.7(b) places responsibility on the PIC to ensure an aircraft is in a condition safe 

for flight. In prior grants of exemption to the sUAS, the FAA determined that exemption 

from this section was not necessary. [See, e.g., Exemption No. 11191; 11195; 11120.] To 

the extent that the FAA determines an exemption is required here, McShane Construction 

respectfully requests that the FAA find compliance with the manufacturer's manuals, and 

requirements of the grant of exemption, a sufficient means for ensuring that the sUAS are in 

a condition for safe flight. 

14 C .F.R.§ 91.113;Right-of-WayRules 

Section 91.113 requires that vigilance be maintained by each person operating an aircraft to 

see and avoid other aircraft. Unlike manned aircraft, the sUAS pilot is not on-board the 

aircraft to observe and avoid other aircraft, operating the sUAS from the ground. 

McShane Construction's proposed operating conditions will achieve an equivalent or greater 

level of safety. All operations will involve two individuals-one FAA certificated pilot as the 

PIC and one visual observer who will monitor the immediate and surrounding airspace of the 

operation for potential obstruction hazards and other possible intrusions. The sUAS will also be 

limited to designated areas below 400 feet AGL. 

14 C .F.R.§ 61.113(a)& (b);61.133(a):Private Pilot Privileges and Limitations; Pilot 

in Command; Commercial Pilot Privileges and Limitations 

Section 61.113(a) & (b) limit private pilots to non-commercial operations. Unlike a 

conventional aircraft that carries a pilot, passengers, and cargo, the sUAS are remotely 

controlled with no passengers or property of others on-board. Section 61.133(a) requires an 

individual with at least a commercial pilot's license to act as pilot in command of an aircraft for 

compensation or hire. 

McShane Construction respectfully proposes that operator requirements should take into 

account the characteristics of the particular UAS. Here, the sUAS have a high degree of preprogrammed control and various built-in technical capabilities that strictly limit the potential 

for operation outside of the operating conditions set forth in Appendix B and the exemption 

application. The small size, endurance, range and payload capacities ofthe sUAS mean that no 

passengers and/or cargo will ever be carried by the aircraft. Rather, commercial operations will 

be strictly limited to acquiring aerial imagery, data collection and inspections. 

Considering these conditions, operating limitations and restrictions, an equivalent level of 

safety will be provided by allowing operation of the sUAS by McShane Construction with 

individuals who possess a valid FAA airline transport, commercial, private, recreational or 

sport pilot certificate. The risks associated with the operation of the sUAS (given their small 

size, speed, operational capabilities and limitations, and lack of combustible fuel) are so 

diminished from the level of risk associated with commercial operations (and even operations 

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permitted with a private pilot certificate) contemplated by Part 61 with manned aircraft, that 

allowing operations of the sUAS as set forth in Appendix B meets and exceeds the present 

level of safety provided under 14 C.F .R. § 61.113(a)-(b ), and does not call for a commercial 

pilot certificate as set forth in§ 61.133. [FAA Exemption No. 11357 (requiring at least a 

recreational or sport pilot certificate, and a current FAA airman medical certificate or valid 

U.S. driver's license).] 

14 C FR § 91.119:Minimum Safe Altitudes 

Section 91.119 establishes safe altitudes for operation of civil aircraft. Specifically, 91.119( c) 

limits aircraft flying over areas other than congested areas to an altitude of 500 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. 

As set forth herein, the sUAS will not operate at higher than 400 feet AGL. The sUAS will, 

however, be operated to avoid congested or populated areas. Because aerial photography, 

data collection and inspection work must be accomplished at relatively low altitudes and at 

altitudes less than 500 feet AGL, an exemption from Section 91.119( c) is needed. 

The equivalent level of safety will be achieved given the size, weight, speed, and material with 

which the sUAS are built. Also, all flights will be conducted over private and/or controlledaccess property with the permission of the land owner or those who control the land. Because of 

the advance notice to the landowner, all affected individuals will be aware of the flights. 

Compared to operations conducted with aircraft or rotorcraft weighing far more than the 

sUAS, and carrying flammable fuel, any risk associated with these operations will be 

significantly less than those currently allowed with conventional aircraft operating at or below 

500 feet AGL. Indeed, the low-altitude operations of the sUAS will maintain separation from 

operations of conventional aircraft that must comply with Section 91.119. 

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

This regulation prohibits an individual from beginning "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 Yuneec Typhoon Q500 4K is powered by a removable, rechargeable, lithium-polymer 

battery that provides approximately 25 minutes of powered flight. Without an exemption from 

§ 14 CFR 91.151, flights by McShane Construction would not be possible. Given the 

limitations on the proposed operations and their locations, a less burdensome reserve 

requirement for flight in daylight VFR conditions is reasonable. Moreover, the Yuneec 

Typhoon Q500 4K provides low battery warnings that indicate the PIC must command the 

aircraft's return to the launch point when low battery capacity voltage is reached. A critical low 

battery warning is also provided. The aircraft will initiate an automatic descent and landing at 

the critical low battery warning. 

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An exemption from 14 CFR § 91.151(a) is safe and within the scope ofthe prior exemptions 

for the sUAS. [See, e.g., Exemption Nos. 11734, 11618, and 11438] In line with the previous 

grants of exemption, McShane Construction requests that the FAA grant relief under the 

condition that the PIC will not begin a flight unless (considering wind and forecast weather 

conditions) there is enough power to fly to the first point of intended landing and, assuming 

normal cruise speed, land the sUAS and to operate after that for at least 5 minutes. [See 

Exemption No. 11325.] 

14 C .F.R.§ § 91.9(b)(2);91.203(a)-(b);Carriage of Civil Aircraft Airworthiness 

Certificate and Registration 

Sections 91.9(b) and 91.203(a)-(b) require an aircraft operator to carry airworthiness 

documents and other aircraft manuals onboard the aircraft at all times. Because the sUAS 

are small in size and do not contain a cabin or flight deck, carriage of such documents and 

manuals is impossible. 

The intent of these regulations is to ensure that the PIC has access to important documents 

during flight. Here, an equivalent level of safety is achieved if the PIC has access to the 

applicable sUAS manual(s), registration certificate and other required documents from the 

Ground Control Station from which he or she is conducting operations. This is consistent with 

a prior opinion of the FAA Office of the Chief Counsel, and other grants of exemptions for 

commercial UAS operations. [See Memorandum from Mark Bury, FAA Assistant Chief 

Counsel for International Law, Legislation and Regulation, to John Duncan, FAA Flight 

Standards Service (Aug. 8, 2014).] 

14 C .F.R.§ 91.121:AltimeterSettings 

Section 91.121 requires that each individual operating an aircraft shall maintain the cruising 

altitude or flight level of that aircraft, as the case may be, by reference to an altimeter that is 

set, when operating below 18,000 feet MSL to: 

0 The current reported altimeter setting of a station along the route and within 100 

nautical miles of the aircraft; 

0 If there is no station within the area prescribed in paragraph (a)(l)(i) of this section, 

the current reported altimeter setting of an appropriate available station; 

0 In the case of an aircraft not equipped with a radio, the elevation of the departure 

airport or an appropriate altimeter setting available before departure. 

To provide an equivalent level of safety, the sUAS autopilot calculates the reference altitude 

(ground level) with on-board GPS. The altitude information generated from the GPS is 

transmitted to the PIC. The PIC shall confirm the altitude of the launch site shown on the GPS 

altitude indicator before flight. The FAA has granted relief from this section in prior grants of 

exemption under the condition that the operator set the altimeter to zero feet AGL rather than 

local barometric pressure or field altitude before each flight. [Exemption Nos. 11062 and 

11067.] A similar grant of exemption is thus warranted here. 

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

Section 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) ofthis section, have discrepancies repaired as prescribed in part 43 of 

this chapter .... " Section 91.407 similarly makes reference to requirements in Part 43; Section 

91.409(a)(2) requires an annual inspection for the issuance of an airworthiness certificate. 

Section 91.417(a) requires the 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 for return to service. 

An equivalent level of safety will be achieved because the sUAS are small in size, will solely 

operate in limited and predetermined areas, and are not large, complex mechanical machines. 

McShane Construction will perform all maintenance and inspections in accordance with the 

manufacturers' manuals and any required manufacturer Safety or Service Bulletins. In 

addition, the PIC will conduct a pre-flight inspection of the sUAS and all associated 

equipment to account for all discrepancies and/or inoperable components. Maintenance will be 

performed and verified to address any conditions potentially affecting safe operation of the 

sUAS and no flights will occur unless and until all flight critical components of the sUAS have 

been found to be in a condition for safe operation. A functional flight test will be conducted 

following the replacement of any flight-critical components. 

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APPENDIXB 

MCSHANE CONSTRUCTION COMPANY OPERATING RESTRICTIONS AND 

LIMITATIONS 

1) Operations authorized by this grant of exemption are limited to the Yuneec Typhoon 

Q500 4K. Proposed operations of any other aircraft will require a new petition or a 

petition to amend this grant. 

2) The sUAS shall not be flown at a ground speed exceeding 87 knots (100 miles per hour). 

3) Above Ground Level ("AGL") altitude shall be restricted to 400 feet. All altitudes 

reported to Air Traffic Control ("ATC") shall be in feet AGL. 

4) The sUAS shall be operated within Visual Line-of-Sight ("VLOS") of the pilot-incommand ("PIC") and visual observer at all times. The PIC must use human vision 

unaided by any device other than corrective lenses, as specified on the PIC's FAAissued medical certificate. 

5) All operations must utilize a visual observer ("VO"). The VO may be used to satisfy the 

VLOS requirement as long as the PIC maintains VLOS capability. The VO and PIC must 

be able to communicate verbally at all times. The PIC must be designated before the flight 

and cannot transfer his or her designation for the duration of the flight. 

6) Any and all additional requirements identified in the exemption grant by the FAA shall 

be added to the sUAS Operations Documents ("OD"). The OD must be maintained and 

made available to the Administrator upon request. If a discrepancy exists between the 

conditions and limitations in the granted exemptions and the OD, the conditions and 

limitations in the granted exemptions shall take precedence and must be followed. 

Otherwise, the operator must follow the procedures outlined in the OD. 

The operator may update or revise its OD. It is the operator's responsibility to track such revisions 

and present updated and revised documents to the Administrator upon the request. The operator 

must also present updated and revised documents if it petitions for an extension or amendment of 

the granted exemptions. If the operator determines that any update or revision would affect the 

basis upon which the FAA granted the exemptions, then the operator must petition for 

amendment to its exemptions. The FAA's UAS Integration Office (AFS-80) may be contacted if 

questions arise regarding updates or revisions to the OD. 

7) Prior to each flight the PIC must inspect the sUAS to confirm that it is in a condition for 

safe flight. The preflight inspection shall account for all discrepancies (i.e., inoperable 

components, items, or equipment). The PIC shall not operate the aircraft if the inspection 

reveals a condition that affects the safe operation of the sUAS until the necessary 

maintenance has been performed and the sUAS is found to be in a condition for safe 

flight. The Ground Control Station ("GCS") shall be included in the preflight inspection. 
8) Any sUAS that has undergone maintenance or alterations that affect the sUAS operation 

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

functional test flight. The PIC who conducts the functional test flight must make an entry 

in the sUAS aircraft records. 

9) McShane Construction must follow the manufacturer's aircraft/component maintenance, 

overhaul, replacement, inspection, and life limit requirements. 

1 0) McShane Construction shall carry out its maintenance, inspections, and record keeping 

requirements, in accordance with the manufacturer's manuals and instructions. 

Maintenance, inspection, and alterations must be noted in the aircraft records, including 

total flight hours, description of work accomplished, and the signature of the authorized 

PIC or technician returning the sUAS to service. 

11) The PIC must make a record entry in the aircraft records of the corrective action taken 

against discrepancies discovered between inspections. 

12) The PIC must possess 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 government. The PIC must also meet the flight 

review requirements specified in 14 C.F .R. § 61.56 in an aircraft in which the PIC is 

rated on his or her pilot certificate. 

13) McShane Construction will not permit any PIC to operate the sUAS unless and until that 

PIC demonstrates the ability to safely operate the sUAS in a manner consistent with how 

the sUAS will be operated pursuant to this exemption, including evasive and emergency 

maneuvers and maintaining appropriate distances from people, vessels, vehicles and 

structures. PIC qualification flight hours and currency must be logged in a manner 

consistent with 14 C.F.R. § 61.51(b). 

14) The sUAS shall not be operated directly over any person, except authorized and 

consenting individuals, or below an altitude that is hazardous to persons or property on 

the surface in the event of an sUAS failure or emergency. 

15) Operating of the sUAS may be conducted at distances less than 500 feet from 

participating persons, vessels, vehicles or structures that perform an essential function 

in connection with these special purpose operations. Operations closer than 500 feet 

from the PIC, visual observer, operator trainees, and essential persons, are permitted 

when operationally necessary; but never so close as to present an undue hazard, per § 

91.119(a). 

16) Operation of the sUAS must be conducted at least 500 feet from all nonparticipating 

persons, vessels, vehicles, and structures unless: 

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

the land owner/controller has granted permission and the PIC has 
• . . 

made a safety assessment of the risk of operating closer to those 

objects and determined that it does not present an undue hazard. 

17) If the ·sUAS loses communications or loses its GPS signal, the sUAS must return to a 

pre-determined location within the operational area and land or be recovered in 

accordance with the manufacturer's user manuals. 

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

19) The PIC is prohibited from beginning a sUAS flight unless (considering wind and 

forecast weather conditions) there is enough power to fly to the intended point of 

landing and, assuming normal cruising speed, operate after that for at least 5 minutes. 

20) McShane Construction shall obtain an Air Traffic Organization (ATO) issued Certificate 

of Waiver of Authorization (COA) prior to conducting any operation. 

21) All aircraft operated in accordance with the requested exemption must be identified by 

serial number, registered in accordance with 14 C.F.R. Part 47, and have identification 

(N-Number) markings in accordance with 14 C.F.R. Part 45, Subpart C. Markings shall 

be as large as practicable. 

22) Each sUAS must comply with all manufacturer System and Safety Bulletins. 

23) The radio frequency spectrum used for operation and control of the sUAS must comply 

with Federal Communication (FCC) or other appropriate government oversight agency 

requirements. 

24) The documents required under 14 C.F.R. §§ 91.9 and 91.203 shall be available to the 

operator at the Ground Control Station of the sUAS any time the aircraft is operating. 

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

enforcement official upon request. 6 

25) The sUAS must remain clear and yield the right of way to all other manned 

operations and activities at all times (including, without limitation, ultralight vehicles, 

parachute activities, parasailing activities, hang gliders, etc.). 

26) Operations shall occur under Visual Meteorological Conditions (VMC); flights under 

special visual flight rules (SVFR) shall not be conducted. 

27) The sUAS shall not be operated from any moving device or vehicle. 

28) The sUAS shall not be operated closer than 500 feet below or 2,000 feet horizontally 

from a cloud or when visibility is less than 3 statute miles from the PIC. 

29) Operations will not be conducted within a 5 NM range ofthe geographic center of an 

airport as denoted on a current FAA-published aeronautical chart unless permission 

has been obtained from the local control tower or, in the case of a non-towered airport, 
written notice has been provided to the airport's management, and the operation is 

conducted in accordance with a NOT AM as required by the grant of this exemption. 

30) All operations shall be conducted over private and/or controlled-access property with 

permission from the landowner/controller or authorized representative. Permission from 

the landowner, controller, manager or authorized representative will be obtained for each 

flight to be conducted. 

31) Any incident, accident, or flight operation that transgresses the lateral or vertical 

boundaries of the operational area as defined by the applicable COA shall be reported to 

the FAA's UAS Integration Office (AFS-80) within 24 hours. Accidents shall be 

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

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

32) sUAS operations may not be conducted during night, as defined by 14 C.F.R. § 1.1. 
APPENDIXC 

FEDERAL REGISTRY SUMMARY 

Pursuant to 14 C.P.R. Part 11, McShane Construction offers the following summary for 

publication in the Federal Register, should publication be necessary: 

McShane Construction seeks an exemption from the following rules: 

14 C.P.R. Part 21, Subpart H; 14 C.P.R. § 91.7; 14 C.P.R. § 91.9(b)(2); 14 C.P.R. § 

91.113; 14 C.P.R.§ 61.113(a)-(b); 14 C.P.R.§ 61.133(a); 14 C.P.R.§ 91.119(c); 14 

C.P.R.§ 91.121; 14 C.P.R.§ 91.151; 14 C.P.R.§ 91.203; 14 C.P.R.§ 91.405(a)-(b); 

14 C.P.R.§ 91.407(a)(l); 14 C.P.R.§ 91.409(a)(1)-(2); and, 14 C.P.R.§ 91.417(a). 

Approval of these exemptions will permit McShane Construction to conduct commercial 

unmanned aircraft systems ("UAS") operations in commercial construction applications. The 

exemptions will enhance safety by reducing risk to the general public and property owners from 

the risk and hazards associated with performing equivalent work through individual construction 

workers and conventional manned air 

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TABLE OF CONTENTS 

ABLE OF CONTENTS 20 ·Installing The Flight Battery 

NTRODUCTION 21 · GPS Functionality 

ERIAL IMAGING SOLUTION 22 · Preparing to Fly 

Speciflctations 23 ·Flying 

Notices and Warnings 24 · Disabling GPS 

General Safety Precautions and Warnings 24 · Graphical User Interface (GUI) 

TYPHOON QSOO 4K RTF Contents 25 · Compass Calibration 

Battery Warnings and Usage Guidelines 27 · ST10+ and Receiver Binding 

Charging The Batteries 28 · ST10+ and CG03 Binding 

Preparing The CG03 29 GROUND IMAGING SOLUTION 

nstalling The Propellers 29 · Speciflctations 

TYPHOON QSOO 4K, CG03 and ST10+ Overview 29 · Battery Warnings and Usage Guidelines 

ST10+ Display 30 ·Installing The Steadygrip Batteries 

ST10+ Accessories 30 · Attaching The CG03 to The Steadygrip 

Flight Controls 31 · CG03APP 

Flight Controls - Smart Mode 31 ·Attaching A Mobile Device to The Steadygrip 

Follow Me Function 31 ·Using The Camera Pitch Control Wheel 

Watch Me Function 31 ·Taking Photos and Recording Video 

Flight Controls - Angle (Pilot) Mode 32 · Added Features for CG03 on Steadygrip Flight Controls - Home Mode 33 TROUBLESHOOTING 

Led Status Indications 35 WARRANTY INFORMATION 

aking Photos and Recording Video 35 CERTIFICATION INFORMATION 

1 
INTRODUCTION 

a superior modular, integrated aerial and ground imaging solution. The system arrives 100% factory-assembled and test flown, 

" Android touch screen personal ground station and a CG03 3-axis gimbal camera able to take 16 megapixel still photos and 

eos. The STEADYGRIP extends the use of the gimbal camera from the sky to the ground and, With the CGO APP, whatever is 

SmartPhone with the same control of video FPS, video start/stop and still photos as found on the ST10+. With the Q500 4K, 

ure amazing photographs and video footage for a wide variety of uses. 

dy to fly right out the box, please take the time to read through this entire instruction manual for more information on safety, 

ols and more before making your first flight. Please also visit www.yuneec.com for additional information including product 

d more. 

AERIAL IMAGING SOLUTION 

x 16.54 in (420mm) 

R DISTANCE: 20 in {510mm) 

METER: 13.0 in (330mm) 

ND PAYLOAD: 40.0 oz (1130g) 

WITH CG03: 60.0 oz (1700g) 

Po (included) 

ancing Smart Charger with AC Adapter (included) 

Hz with 5.8GHz video downlink (included) 

Default 400 Feet Above Ground Level 

5°/s 

BAND: 2.4GHz 

/s 

CG03 

Dimension: 4.2x5.0x3.1in (106x128x80mm) 

Weight: 6.9oz (195g) 

Sensor: 1/2.3" CMOS 

Effective Pixels: 12.4 Megapixels 

Camera lens: 14mm/F2.8 35mm 

FOV: 115 Degree 

Electronic Shutter: 1/30 -- 1/8000 

Working Temperature: 0-40 t 

Power Consumption: lOW 

Video Transmission Range: Up to 500m {1640ft) 

Transmission System: 5.2Ghz - 5.8Ghz 

Video UHD: 4K 30FPS 

2 

ST10+ 

Number of Channels: 10 

RC Band: 2.4GHz 

RC Modulation: Yuneec 

Video Downlink Band: 5.8GHz 

Telemetry/OSD: Yes 

SD Card Compatible: Yes 

LCD Screen Size: 5.5" 

Touchscreen: Yes 
ngs 

ety precautions and warnings, instructions, warranties and other collateral information is subject to change at the sole discre

 up-to-date information please visit the corresponding product page at www.Yuneec.com or contact the nearest Yuneec office 

ge terms are used throughout the product literature to indicate various levels of potential harm when operating this product: 

if not properly followed, create a possibility of property damage and/or little to no possibility of injury. 

h if not properly followed, create the probability of property damage and/or a possibility of serious injury. 

ch if not properly followed, create the probability of property damage, collateral damage and/or serious injury or create a high 

ry. 

E quick start guide and instruction manual to become familiar with the features of the product before operating. Failure to 

y can result in damage to the product, property and/or cause serious injury. 

icated consumer product. It must be operated with caution and common sense, and requires some basic mechanical ability. 

ct in a safe and responsible manner could result in damage to the product, property and/or cause serious injury. This product 

ildren without direct adult supervision. Do not use with incompatible components or alter this product in any way outside of 

Yuneec. The quick start guide and instruction manual contain instructions for safety, operation and maintenance. It is essential 

structions and warnings prior to assembly, setup and/or use in order to operate the product correctly and avoid damage or 

NOT FOR CHILDREN UNDER 14 YEARS. THIS IS NOT A TOY. 

3 
cautions And Warnings 

NOT FLY NEARBY TALL THE MAXIMUM FLYING 

LDINGS/OBSTRUCTIONS ALTITUDE FOR THIS AIRCRAFT 

° MINIMUM CLEARANCE IS SOOOFT ABOVE SEA LEVEL! 

QUIRED) 

DO NOT FLY OVER 

CROWDS! 

DO NOT FLY NEAR 

AIRPORTS! 

DO NOT FLY IN WINDS 

THAT EXCEED 8-12 MPH 

(13-19 KPH)! 

his product in the intended manner as described in the quick start guide and instruction manual can result in damage to the 

use serious injury. A Radio Controlled (RC) multirotor aircraft, APV platform, drone, etc. is not a toy! If misused it can cause 

age to property. 

his product you are solely and entirely responsible for operating it in a manner that does not endanger yourself and others or 

uct or the property of others. 

d other parts of your body away from the spinning propellers/rotor blades and other moving parts at all times. Keep items that 

angled away from the propellers/rotor blades including debris, parts, tools, loose clothing, etc. 

craft in open areas that are free from people, vehicles and other obstructions. Never fly near or above crowds, airports or 

on and safe flight performance never attempt to operate your aircraft nearby buildings or other obstructions that do not offer 

an restrict GPS reception. 

te your aircraft in areas with potential magnetic and/or radio interference including areas nearby broadcast towers, power 

oltage power lines, electrical storms, etc. 

ce in all directions around your aircraft to avoid collisions and/or injury. This aircraft is controlled by a radio signal subject to 

rces outside your control. Interference can cause momentary loss of control. 

e operation of the automatic landing function in Home Mode you must start the motors with the aircraft in a position that has 

ely 3 meters) of clear and open space around it and achieve a proper GPS lock. 

e your aircraft with any worn and/or damaged components, parts, etc. (including, but not limited to, damaged propellers/rotor 

aft in poor or severe weather conditions including heavy winds, precipitation, lightning, etc. 

4 
aft starting with a fully charged battery. Always land as soon as possible after the first level low voltage battery warning or land 

d level low voltage battery warning (as indicated by the vibrations and audible alerts from the transmitter/personal ground 

aft when the voltage of the battery in the transmitter/personal ground station is in a safe range (as indicated by the battery 

een of the transmitter/personal ground station). 

n clear line of sight and under control, and keep the transmitter/personal ground station powered on while the aircraft is 

control stick down fully and turn off the motors in the event the propellers/rotor blades come into contact with any objects. 

 and parts to cool after use before touching them and flying again. 

fter use and store/transport them per the corresponding guidelines. 

all electronic components, parts, etc. not specifically designed and protected for use in water. Moisture causes damage to 

arts. 

 the aircraft or any related accessories, components or parts in your mouth as doing so could cause serious injury or even death. 

mall parts and electronic components out of the reach of children. 

ctions and warnings included with this aircraft and any related accessories, components or parts (including, but not limited to, 

ies, etc.). 

eed controls (ESCs) installed in the TYPHOON are not compatible with any other product, and the TYPHOON is not compati

e of any other ESCs in the TYPHOON will cause a crash, which may result in damage to the product, property and/or cause 

5 
OO 4K RTF Contents 

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

1a f$G 

irframe w/lnstalled CG03 

d Personal Ground Station 

un Shade/Shield 

er/Charger 

6 USB to Micro USB Cable 

7 USB Interface/Programmer 

8 5400mAh 3S 11.1V LiPo Battery 

9 3S 11.1V LiPo Balance Connector Charge Lead 

10 DC 3S 11.1 V LiPo Balancing Charger 

6 

12 

11 DC Automobile Accessory Socket/ 

Cigarette Lighter Receptacle Adapter 

12 ACto DC Adapter/Power Supply 

13 16GB microSD Card w/ Adapter 

14 Motor Holder/Prop Installation Tool 

15 Propellers/Rotor Blades (2 sets) 

16 CGO STEADYGRlPTM 
and Usage Guidelines 

mer (LiPo) batteries are significantly more 

d or NiMH batteries. All instructions and 

exactly to prevent property damage and/ or 

ndling of LiPo batteries can result in fire. By 

he included liPo battery you assume all risks 

es. If you do not agree with these conditions 

product in new, unused condition to the place 

he LiPo battery in a safe, well-ventilated area 

als. 

ttery unattended at any time. When charging 

remain in constant observation to monitor the 

mmediately to any potential problems that may 

he LiPo battery you must allow it to cool to 

before recharging. 

y you must use only the included charger or a 

tery charger. Failure to do so may result in a 

e and/or serious injury. 

attery begins to balloon or swell, discontinue 

mediately. Quickly and safely disconnect the 

e, open area away from flammable materials to 

minutes. Continuing to charge or discharge a 

loon or swell can result in a fire. A battery that 

ven a small amount must be removed from 

 LiPo battery. Discharging the battery too low 

tery resulting in reduced power, flight duration 

irely. LiPo cells should not be discharged to 

 

room temperature and in a dry area for best 

7 

• When charging, transporting or temporarily storing the LiPo battery the 

temperature range should be from approximately 40-120° F (5-49° C). Do 

not store the battery or aircraft in a hot garage, car or direct sunlight. If 

stored in a hot garage or car the battery can be damaged or even catch fire. 

• Never leave batteries, chargers and power supplies unattended during 

use. 

• Never attempt to charge low voltage, ballooned/swollen, damaged or wet 

batteries. 

• Never allow children under 14 years of age to charge batteries. 

• Never charge a battery if any of the wire leads have been damaged or 

shorted. 

• Never attempt to disassemble the battery, charger or power supply. 

• Never drop batteries, chargers or power supplies. 

• Always inspect the battery, charger and power supply before charging. 

• Always ensure correct polarity before connecting batteries, chargers and 

power supplies. 

• Always disconnect the battery after charging. • Always terminate all processes if the battery, charger or power supply 

malfunctions. 

IMPORTANT NOTE: It's safer and better for the longevity of the battery to 

store it only partially charged for any length of time. Storing the battery 

approximately 50% charged (which is around 3.85V per cell) is typically 

best, however, it will take some careful management of the charge time and 

the use of a volt meter to achieve this voltage. If you have the equipment 

and skills to achieve the 50% charge level for storage it is recommended. If 

not, simply be sure to not store the battery fully charged whenever 

possible. In fact, as long as the battery will be stored at approximately room 

temperature and for no more than a few weeks before the next use, it may 

be best to store the battery in the discharged state after the last flight (as 

long as the battery was not over-discharged on the last flight). 
ries 

on) and Lithium Polymer (LiPo) batteries are 

than alkaline, NiCd or NiMH batteries. All 

must be followed exactly to prevent property 

ry as the mishandling of Lilon/LiPo batteries 

ng, charging or using the included Lilon/LiPo 

ks associated with them. If you do not agree 

e return the complete product in new, unused 

chase immediately. 

HT BATTERY 

3 charger from a 100-240V AC outlet using the 

or from a 12V DC accessory socket/cigarette 

icle using the corresponding adapter. Once 

 is powered on and ready to charge (green 

ce connector charge lead into the charger, then 

ery to the charge lead. The battery will begin 

nd it will take approximately 2 hours to charge 

ischarged) battery. 

10+ BATTERY 

ttery installed in the ST10+ from a 100-240V 

apter/charger, or from a suitable USB power 

the USB to micro USB cable. While the ST10+ 

cable to the USB adapter/charger, then plug it 

ging port on the right side. After approximate

dicator for the battery will blink blue while the 

l glow solid blue when the battery is fully 

mately 5.5 hours to charge a fully discharged 

y. 

ll vary depending on the region in which the 

ased (AU = Australian; EU = European; UK = 

d States). 

8 
03 

g the flight battery and powering on the 

ve the cover/lock from the rear of the CG03 

rd. Failure to remove the cover/lock can result 

and the CG03! 

 to re-install the cover/lock after each flying 

ng/storing the TYPHOON Gust remember to 

e powering on the TYPHOON and CG03!). 

ock from the rear of the CG03 by carefully 

d into the corresponding slot on the bottom of 

cluded 16GB card or any name brand Class 10 

 protective material from the camera lens. 

9 

Installing The Propellers 

WARNING: We recommend wearing gloves and using extreme care when 

installing the propellers/rotor blades. 

!11 

Each motor and propeller are marked with an 'A' or 'B' to ensure easy 

installation in the correct positions (for example: install propellers marked 

with 'A' on motors marked with 'A'). 

IMPORTANT NOTE: It is NOT possible to install a propeller marked with 

'A' on a motor marked with 'B'. The threads go in different directions for 

the 'A' and 'B' motors/propellers. 

Step 1) Use the special tool (included) to hold the motor so it cannot spin. 

CAUTION: Do not over-tighten the propellers when using the tool. 

Step 2) Install the corresponding propeller by rotating it trialing edge first 

until it's secure against the a-ring located at the bottom of the motor shaft. 

You may want to add this: Continue to screw down the propeller 1-1.5 

turns more to ensure it is properly tighten and compressing the 0-rings 

slightly. 

Step 3) Repeat steps 1 and 2 to install the three remaining propellers 

securely. 
OO 4K, CG03 And ST10+ Overview 

15 16 17 

11 18 

12 19 

13 20 

14 21 

c\>c .. 

·- • 

23 

 an internal cooling fan and components that deliver vibrating and 

gh the ST10+ is equipped with digital 'trims' (located below the control 

nctional when controlling the TYPHOON. 

10 

The TYPHOON QSOO 4K I CG03 

1 CG03 Gimbal Camera 

2 Camera Microphone 

3 Camera LED Status Indicator 

4 Camera Lens 

5 5.8GHz Antenna 

6 Main LED Status Indicator 

7 Power Switch 

ST10+ 

8 Proportional Control Rate Slider 

9 USB Connector/Charging Port 

10 Audio/Earphone Jack 11 Take Still Photo Button 

12 Start/Stop Motors Button 

13 Rudder/Yaw Control (for Mode 2 and Mode 1) 

14 Throttle/Altitude Control (for Mode 2) 

Elevator/Pitch Control (for Mode 1) 

15 5.8GHz Antenna (located inside the case) 16 Status Indicators (for ST10+ battery, 5.8GHz 

WiFi and GPS) 

17 2.4GHz Antenna (located inside the handle) 

18 Start/Stop Video Recording Button 

19 Flight Mode Selection Switch 

20 Aileron/Roll Control (Mode 2 and Mode 1) 

21 Elevator/Pitch Control (Mode 2) 

Throttle/ Altitude Control (Mode 1) 

22 Power Switch 23 Volume and Navigation Touch-Activated Buttons Volume 

Down/VolumeUp/Menu/Home/Back) 

24 CG03 Pitch Angle/Position Control Slider 25 SD Card Slot (located under the battery) 
 touchscreen display that allows for changing various settings and viewing real-time telemetry data and streaming video during 

2 3 

I 

Welcon e,Pilot 

I 

I 

ngs Flight Settings 

 I 

14 

4 5 6 7 

I I I 

07:25 ). -=> 

'f VOLTS 1 

r ALT 1 

lfN/Aftl 

r G-SPD l If N/AmphH 

r DIS l 

••==o If N/Aft 1 

1r odel Select 1 

I 

13 12 

8 

9 

10 

11 

1 Model Name 

2 Status Information 

3 Direction to Home Point 

4 Clock/Current Time 

5 Watch Me/Follow Me Button 

6 GPS Status and Number of Satellites for ST10+ 

7 ST10+ Battery Charge Level Status Icon 

8 Aircraft Battery Voltage 9 Altitude of Aircraft (Above Ground Level) 

10 Ground Speed of Aircraft 

11 Distance of Aircraft from Home Point 

12 Model Select Menu Button 

13 In Flight Settings 

14 Flight Settings Menu Button 15 System Settings Menu Button 

16 Latitude/Longitude Position of Aircraft 

17 Number of Satellites for Aircraft 

18 GPS Status for Aircraft 

19 Flight Mode of Aircraft 

 the screen to increase the size of the video viewing area to full-screen and double tap again to return to the standard size. 

era settings, tap again to display camera settings. 

to fly the TYPHOON via First-Person View (FPV). There's a slight 'lag' in the CG03 streaming video downlink to the ST10+, 

video/FPV should only be used for aligning camera shots and not for flying! Attempting to fly via FPV can result in a crash that 

duct, property and/or cause serious injury. 

ming video from the CG03 to the ST10+ and to a separate phone/tablet (or another Yuneec transmitter/personal ground 

OT recommended as it will result in a very significant lag in the video downlink. 

11 
 

and optional-use Neck Strap to help hold and 

also install the included and optional-use LCD 

help improve viewing in sun light. 

l to apply suitable anti-glare screen protector 

 to further improve viewing in sun light. 

move around in excess as the strap can come 

and potentially fall and damage the sensitive 

his and the following sections refers to the 

iguration of the ST10+. The left-hand stick on 

le (climb/descend) and rudder (yaw left/right) 

d stick (also known as the throttle stick) is in 

ght the TYPHOON will maintain the current 

ick upward the TYPHOON will climb, and as 

ard the TYPHOON will descend. The farther 

n you move the stick the faster the TYPHOON 

12 

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 Feet I 122 Meters) -----,. 

Climb (Max. Altitude 

Maximum Climb Rate: · 

2m/s (6.6f/s) + 

Maintain Altitude 

Descend I Land 

Moving the left-hand stick to the left will turn (yaw) the nose of the 

TYPHOON to the left about the vertical axis. And moving the stick to the 

right will turn (yaw) the nose of the TYPHOON to the right. 

@\ 
L RATE SLIDER 

e Slider located on the right side of the ST10+ 

 climb/descend and directional control rates. 

e lowest control rates (best for first-time pilots 

tween 5000 feet and 8000 feet Above Mean 

 position for the highest control rates (best for 

nly be used when flying below 5000 feet MSL). 

 if you prefer. 

E 

med with three (3) flight modes that can be 

de Selection Switch located just above the 

13 

Flight Controls - Smart Mode 

When the Flight Mode Selection Switch is the top position the TYPHOON 

will be in Smart Mode. 

Although we recommend learning to fly the TYPHOON in Angle (Pilot) 

Mode as soon as possible, Smart Mode is typically the best mode for 

first-time pilots to fly in which also features 'Follow Me' and 'Watch Me' 

functions. 

In Smart Mode the TYPHOON will always move in the direction the 

right-hand control stick is pushed relative to the pilot and no matter which 

way the front/nose is pointed. So if you push the stick to the left the 

TYPHOON will always move to the left, regardless of the direction the nose 

is pointing and even if it's spinning. This mode can also be helpful for pilots 

that lose orientation while flying in Angle (Pilot) Mode . 

.. 

# 

SMART CIRCLE* 

+$ 

# 

..... 

*121 52 feet I 16 meters 
ws the TYPHOON to follow the pilot, adjusting 

of the ST10+. This function is enabled when 

pletes, and the TYPHOON is using shared GPS 

s time, you will see in orange, and j in 

, the TYPHOON will follow the movement of 

eration on the ST10+. The flight status is also 

te ST10+ and CG03. 

------+ 

----------+ 

e function, the aircraft will maintain a constant 

obstacles. Pilots who change their altitude by 

er ground, during flight should be mindful of 

14 

----

--------

---

---

------

---
e camera to keep tracking the remote control

t moves as the camera can automatically tilt its 

er. 

under Smart Mode is Follow Me. Watch Me 

y following steps: 

I \ 

I \ 

I \ 

,' \ -----iU: 

 ,'' \, ................... --... --· ,,'' 

 I /t\ \ \ \ \ ,' I I I / 

\ I 

/ 

r J 1 

L.f-r_j --o 

ot will always be kept in the frame wherever 

15 

Model: Typhoon 

-

Welcome, Pilot 

r J -, 

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10:48:28 pm 10)'. • .::> 

--o lEj) r o;··- System Settings - J r-M.--

Watch Me/Follow Me Button: When in Smart Mode, press to switch 

the TYPHOON between Watch Me and Follow me function. Follow Me 

function is the default setting, and the button is ORANGE. If it is GREY, 

it means ST10+ GPS isn't ready yet. Please wait. 

Model: Typhoon Welcome, Pilot 10:48:28 pm 10)'. 

-

r i -, L ...J 

0 [EJ • 

,. Ei Flight Settings I Model Select 

the button will change from ORANGE to GREEN. And now it is 

in Watch Me function. 

NOTE: Once the TYPHOON is above 2m and out of Smart Circle during 

flying, the TYPHOON yaw direction will take the control itself. Camera 

lens will always point to you as long as Flight Mode Selection Switch is in 

Smart Mode. Please put the CG03 Pitch Angle/Position Control Slider in 

the middle position. If you want to trim the camera angle up, then just 

move the Pitch Angle/Position Control Slider a bit up. If you want to trim 

the camera angle down, just move the slider down. 
Additional Smart Mode Features: 

*SMART CIRCLE 

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

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

least 26 feet/8 meters behind the TYPHOON. 

GEO-FENCE 

The geo-fence is a virtual 'barrier' that will keep the TYPHOON from traveling further than 300 feet (91 meters). Although this limit can be adjusted 

using the USB interface/programmer and software we strongly recommend 

using the default limit at all times. 

WARNING: Smart Mode only works when the TYPHOON has a suitable 

GPS signal/lock. If you take off in Smart Mode and the TYPHOON loses GPS signal/lock it will switch to Angle (Pilot) Mode automatically. This is 

why we strongly recommend learning to fly in Angle (Pilot) Mode as soon 

as possible. Otherwise, if you lose GPS signal/lock and are not able to 

properly control the TYPHOON in Angle (Pilot) Mode the aircraft may 

crash or even 'fly away'. 

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

warranty. 

16 

Flight Controls - Angle (Pilot) M

When the Flight Mode Selection Switch i

TYPHOON will be in Angle (also known as Pilo

+ 

•#• 

+ 

Angle (Pilot) 

by experience

the TYPHOO

the control st

front/nose of 

the right-han

TYPHOON w

and move to 

front/nose of 

away from yo

if the front/n

TYPHOON w

Additional Angle (Pilot) Mode Features: 

POSITION HOLD AND SELF-LEVELING 

the TYPHOON will automatically hold its po

signal/lock) and maintain a level attitude wh

centered. 

WARNING: If you do not properly control the 

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

IMPORTANT NOTE: Crash damage and 'fly aw

warranty. 
Flight Controls - Home Mode 

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

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

# 

+ 

LOCATION 0 • • ·r ••• 

- - - - - - 13-26 ft 

(4-Bm) 

---. PILOT LOCATION • • • 

a 

In Home Mode the GPS connectivity will fly back the TYPHOON, and 

automatically land within 13-26 ft 

(4-8m) of the pilot. This can be 

very helpful for first-time pilots 

who aren't quite ready to land the 

TYPHOON themselves. It can also 

be helpful for pilots that lose 

orientation during flight; simply 

activate Home Mode until the 

TYPHOON automatically moves 

toward the home position, and 

once you've confirmed orientation 

switch back to Angle (Pilot) Mode. 

And if the TYPHOON ever loses 

the link with the ST10+ it will 

automatically enter Home Mode. 

When Home Mode is activated the TYPHOON will respond as follows: 

17 

A) When flying higher than 33 feet (10 meters) th

current altitude, fly back to the home point, , or a

has enough satellites for Follow Me, then descen

----------+ 

B) When flying lower than 33 feet (10 meters) 

33 feet (10 meters) while flying back to the 

position, then descend vertically until it lands. 
CAUTION: You must be certain there are no obstacles in the 'Return to 

Home' flight path otherwise the TYPHOON may come into contact with 

them and crash. And while the TYPHOON is in Home Mode you will have 

a limited amount of directional control to help avoid obstacles, however, 

we strongly recommend switching to Smart or Angle Mode to avoid the 

obstacle (then you can switch back to Home Mode). 

WARNING: Home Mode only works when th

GPS signal/lock. If the TYPHOON loses GPS 

Angle (Pilot) Mode automatically. This is w

learning to fly in Angle (Pilot) Mode as soon a

lose GPS signal/lock and are not able to prope

Angle (Pilot) Mode the aircraft may crash or ev

Led Status Indications 

LED STATUS INDICAnONS DURING STARTUP 

Main LED Status lnclkator 

-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• 

"PPease see rile Instruction mtiiiUQ/ for more Information no-fly zones 

LED STATUS INDICAnONS BEFORE/DURING FUGHT 

Main LED Status lnclkator 

-The aircraft Is In Smart Mode with GPS lock -The aircraft Is In Smart Mode without GPS lock -The aircraft Is In Angle Mode with GPS lock -The aircraft Is In Angle Mode without GPS lock -The aircraft Is In Home Mode 

-Active Home Mode Activated -Active Smart Mode, Follow Me I Watch Me Feature Activated 

- Rrst level low voltage battery warning 

- Second level low voltage battery warning 

-GPS lost 

IMPORTANT NOTE: Crash damage and 'fly aw

warranty. 

Flashes red, green and blue (2 times per second) Pulses red (3 times per second) Flashes orange very rapidly (JO times per second) Flashes blue rapidly (5 times per second} Flashes red and white rapidly (5 times per second) 

Glows solid green 

Flashes green (3 times per second} then off (for J second) 

Glows solid purple 

Flashes purple (3 times per second} then off (for J second) Flashes red rapidly (5 times per second} 

Flashes red rapidly (5 times per second} for 3 seconds and 

white for 1 second 

Solid green for 3 seconds and white for 1 second 

Flashes red, green and blue every 3 seconds Flashes red, green and blue continuously Flashes purple (1 trash per second} 

18 

1 second 1 second 

I I I I I I I I I I I 

------

111111111111111111

111111111

I I I I I I I I I 

1 second 1 second 

I I I I I I 

111111111

I I I I I I I I I 

I I I 

I I I I I 
Below Motor Led Stltus Indicators 

- Low voltage battery warning 

LED STATUS INDICAnONS FOR CAUIRATION MODES 

Main LED Stltuslncllcator 

- Compass calibration Mode entered 

-Compass calibration started 

- Accelerometer calibration started - Accelerometer calibration Mode entered/data collection finished 

-Calibration failed 

CG03 CAMERA LED STATUS INDICATIONS 

·Without T-card orT-card Memory Full ·WIRError 

• WIR lnltlallzecl 

• WIR Connected to Terminal 

- Recocllnc VIdeo orTaklnc StiH Photos 

Flashes rapidly (5 rtmes per second} Flashes red and green slowly (2 times per second) Flashes red and green rapidly (5 ttma per second} Flashes red, green and blue rapidly (J limes per second) Flashes red, green and blue slowly (J rtme per second} 

Glows solid white 

Flashes yellow 

Flashes reel Flashes peen 

Glows solid peen 

Flashes peen ,blue slowly 

19 

1 second 1 second 

I I I I I I I 

111111111111111111111111111111111111

I I I I I 

-
Taking Photos And Recording Video 

The ST10+ seamlessly integrates control of the CG03 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 CG03 will change from glowing solid green to glowing solid 

blue. It will take approximately 1-2 seconds to capture the photo and before you can take another still photo. 

TO START/STOP RECORDING VIDEO 

Press the button located near the top right corner of the ST10+. You'll hear 

an audible indication from the ST10+ each time the recording starts/stops. 

And while video is recording the LED indicator on the front of the CG03 

will flash blue and green, and there will be a red dot next to the time length 

of the recording near the upper right-hand corner on the screen of the 

ST10+. 

NOTE: CG03 camera is the default selection in ST10+. You can take still 

phtos while video recording. The resolution is set by the video resolution. In 

this mode, you will capture still photos from the video. 

CAUTION: Do not change settings when aircraft is further than 1,000 feet 

from ST10+. 20 

CHOOSING CG03 PRO FOR TAKING PHOTO

If users are professionals in photography an

reset related specifications, please follow the 

Step 1) Press Flight Settings, choose Camera SSelect, and press OK. Step 2) The second left column is available for 

like white balance, etc. 

Step 3) Press 0, and press Video Settings, differ

PressG)to enter Photo Capturing, and press 

in this mode, the photos taken are 12 megap

Press 0 to enter Video Recording, and pres

recording. 

CAUTION: ALWAYS stop recording vide

TYPHOON/CG03 to avoid data loss. If yoTYPHOON/CG03 before you stop recording

removed) and turn the system on again. Wait 

until the camera LED starts to glow solid gre

file was recovered. 

CAUTION: When enter Photo Capturing, v

You MUST switch to video recording to s

video recording, picture taking (Button A) is a

set by the video resolution. In this mode, y

from the video. 
Installing The Flight Battery 

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

TYPHOON: 

IMPORTANT NOTE: Keep the TYPHOON level relative to the ground 

when installing the battery. 

SIDE UP 

.a 

STEP 1) Push the area at the top of the battery door to release the 

latch/lock, and then open the door. 

STEP 2) With the side of the battery cartridge that has the 'UP' arrow 

marking oriented upward, hold the handle and slide the battery into the 

battery compartment until you feel the connector make a positive connection. 

NOTE: If you do not install the battery in the correct orientation it will not 

be possible to make a positive connection. 

WARNING: Do not force the battery in to make the connection. It should 

be smooth with little restriction. If it feels tight remove the battery check 

the connector pins for alignment, and try again. Forcing the battery in can 

damage the connector and potentially cause the TYPHOON to loose power 

in flight. 

STEP 3) Close the battery door by pushing the area at the top to engage the 

latch/lock. 

NOTE: If the door will not close because it's coming into contact with the 

handle on the battery cartridge, the battery is not inserted far enough to 

engage the connector properly. 

21 

GPS Functionality 

the TYPHOON requires a suitable GPS signa

motors and to be flown. This means it should o

open areas that are free from people, vehicles 

in order to acquire a suitable GPS signal/lock it'

na installed in the top of the TYPHOON always 

(100° minimum clearance required). 

WARNING: Do NOT attempt to fly 

near or between tall buildings/obstructions, near or under dense 

vegetation, structures or indoors. Do 

NOT attempt to fly the TYPHOON with GP

location known to have poor GPS coverage. A

GPS unless you're able to properly control the 

Mode without GPS assistance and accept ALL r

crashes or 'fly aways'. 

If the TYPHOON loses GPS signal/lock while f

Angle (Pilot) Mode. Smart Mode and Hom

corresponding features, will no longer work. 

Indicator will flash purple and the LED Status 

will flash three (3) times per second then will 

when the TYPHOON loses GPS signal/lo

disabled/turned off). 

If the GPS signal/lock is reacquired (after 

suitable GPS signal), Smart Mode and Home M

WARNING: Loss of GPS signal/lock may res

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

warranty. 

NO-FLY ZONES 

With a suitable GPS signal/lock it will not be possible to start the motors, 

takeoff or fly the TYPHOON in the 'No-Fly Zones' within a 4 mile (6.4 

kilometer) radius of most major airports. 

Preparing to Fly 

WARNING: Before flying you MUST review and understand all of the 

NOTICES AND WARNINGS and the GENERAL SAFETY PRECAUTIONS 

AND WARNINGS found near the beginning of this instruction manual. 

Failure to operate this product in a safe and responsible manner could 

result in damage to the product, property and/or cause serious injury. 

WARNING: Always operate the TYPHOON in open areas (approximately 

10000 square feet/930 square meters or more) that are free from people, 

vehicles, trees and other obstructions. Never fly near or above crowds, 

airports or buildings. 

hf/t.Y/.4,(( 1}· /' /' '1/ 

I '.// # I 

10000 ft2 (93om•) i 

,. . , I )... , I 

Never attempt to operate the 

TYPHOON nearby tall buildings/obstructions that do not offer a clear 

view of the sky (a minimum clearance 

of 100°). 

After selecting a suitable flying area, 

please follow these steps: 

Step 1) ALWAYS turn the ST10+ on 

and allow it to boot up fully BEFORE 

turning the TYPHOON on. 

22 

IMPORTANT NOTE: If you're a first-time pi

putting the Flight Mode Selection Switch (locat

control stick) in the top position to activate S

experienced RC/drone pilot we strongly recom

the middle position to activate Angle (Pilot) Mo

Step 2) Place the TYPHOON on a level and s

power switch to the 'ON' position. DO NO

TYPHOON UNTIL THE INITIALIZATION PR

Main LED Status Indicator on the bottom of th

of the following indications when initialization 

• the TY

with GPS 

flashes wh

ing it can 

TAKEOFF ZONE • •••• • •• //0 

• the TY

without G

times pe

second) 

• the TY

Mode wi

purple 

• the TY

•••••••• PILOT LOCATION 

8 

the next step. 

• • • • • • • • Mode w

purple (3 

(for 1 sec

Step 3) If 

move the 

area, turn 

Or, if you 

Step 5) Step back approximately 26 feet (8 me
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 

WARNING: Do not attempt to operate the TYPHOON in 

winds that exceed 8-12 miles per hour (13-19 kilometers 

per hour). 

To takeoff, raise the left-hand stick to above the center position. the 

TYPHOON will takeoff and climb slowly (or raise the stick further until it 

does). Allow the stick to return to the center position when the TYPHOON 

reaches the desired altitude. 

FLYING 

Take your time learning how the TYPHOON responds to various control 

inputs while flying. In Smart Mode the TYPHOON will always move in the 

direction the right-hand control stick is pushed relative to the pilot and no 

matter which way the front/nose is pointed. In Angle (Pilot) Mode the 

TYPHOON will move in the direction the control stick is pushed relative to 

the front/nose of the aircraft (and the 'angle' of movement is determined by 

how far you push the stick away from the center position). Please see the 

23 

corresponding sections of this instruction man

Smart Mode and Angle (Pilot) Mode. 

IMPORTANT NOTE: If at any time durin

TYPHOON is drifting out of/beyond your c

control sticks. the TYPHOON will automatica

hold its position (with a suitable GPS signal/loc

are centered. You can also activate Home 

automatically flies itself back to the home poin

LANDING 

There are two ways to land the TYPHOON: 

1) Position the TYPHOON above the area wh

Slowly lower the left-hand stick to below 

TYPHOON will descend slowly and land. After 

and hold the red START /STOP button for appr

stop the motors. 

2) Activate Home Mode and the TYPHOON wil

to the home point and will land within a 10 fo

around it. 

NOTE: An alternate form to shut the rotors off i

is to land the TYPHOON and simply switch into 

shut off if the TYPHOON is on the ground. 

WARNING: Always land as soon as possible af

battery warning, or land immediately after thbattery warning (as indicated by the vibrations 

ST10+, and by the LED Status Indicators below 

If at any time the Aircraft Battery Voltage sh

10.7V, land the TYPHOON immediately. 
AFTER LANDING 

ALWAYS turn off the TYPHOON BEFORE turning off the ST10+. Then 

remove the battery from the TYPHOON and allow it to cool to ambient/room 

temperature before recharging. 

WARNING: Do NOT leave the ST10+ and the TYPHOON powered on and 

do NOT leave the flight battery installed inside the TYPHOON as doing so 

can over-discharge and damage the batteries. Over-discharging can cause 

damage to the batteries resulting in reduced performance or failure of the 

batteries entirely. 

IMPORTANT NOTE: Battery damage, crash damage and 'fly aways' are 

NOT covered under warranty. 

Disabling GPS 

WARNING: Smart Mode and Home Mode, along with their corresponding 

features, only work when GPS is active and the TYPHOON has a suitable 

GPS signal/lock. If you disable/turn off GPS the TYPHOON can only be 

flown in Angle (Pilot) Mode. And if you cannot properly control the 

TYPHOON in Angle (Pilot) Mode the aircraft may crash or even 'fly away'. 

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

warranty. 

We do not typically recommend disabling GPS for any reason, especially if 

you're a first-time or low-time pilot. However, if you're an experienced 

pilot that's able to properly control the TYPHOON in Angle (Pilot) Mode, 

and you do not exceed any altitude/distance limits or fly in any 'no fly 

zones' in your area, you can disable/turn off GPS. Do NOT disable/turn off 

GPS unless you accept ALL responsibility and liability for crashes or 'fly 

aways'. 

24 

IMPORTANT NOTE: Every time you turn the T

to having GPS active/on (even if you disable

powered on). 

There are two ways to disable the GPS: I -

When the CG03 and ST10+, the multi-copter 

and ST10+ are bound, press 0 on ST10+ 

interface, GPS switch can be found, and 

turned off. 

GPS can also be disabled manually: 

1

. 

--

·

Step 1) While the ST10+ and the TYPHOON 

(and the motors are NOT running), move the 

Slider on the right side of the ST10+ to the upp

Step 2) Move the right-hand stick all the way t

until step 3 is completed. 

Step 3) Move the Flight Mode Selection Switc

Home to Smart mode 4 times in 3 seconds. 

When GPS has been disabled successfully th

audible indication and the GPS status on th

'Disabled'. Also, the Main LED Status Indicat

LED Status Indicators below the Motors wil

second then will stay off for one (1) second. 

Graphical User Interface (GUI) 

You can download the graphical user interfa

TYPHOON product page at www.Yuneec.c

instructions to install and operate the software 

status of all sensors, to adjust various settings, 

firmware and more using the included USB Inte
Compass Calibration 

Step 1) Do not calibrate the compass 

inside parking structures, near 

buildings or surfaces with metal in 

them (like roads parking lots with 

rebar). Only calibrate the compass in 

open areas/fields far away from 

power lines and other metallic or 

concrete surfaces/structures. 

Step 5) When the main LED status 

indicator flashes red and green 

slowly (2 times per second) you 

have entered compass calibration mode. Pick up the aircraft and hold 

it flat with the nose pointed to the 

north. After 5 seconds the main 

LED status indicator should flash 

red and green rapidly (5 times per 

second). 

Step 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) Slowly rotate the aircraft 

360 degrees toward the north (as 

illustrated) until it's flat and upright in your hands again. 

25 

CAMERA 

II VideoSettinp 

t AudioSwitcl EZ:J 

MULTICOPTER I Accelerometer I 

GPS 

• CaNbratlon 

Step 3) Tap the Setting button on 

the ST10+ screen, then tap the 

Calibration button. Choose Compass 

option and tap it. 

Step 7) Rotate the aircraft 45 

degrees to the left. Then slowly 

rotate the aircraft 360 degrees 

toward the north (as illustrated) 

until it's flat and upright in your 

hands again. 

Step 4

will b

screen

in MO

Step 8

degree

rotate 

toward 

until it

hands a
Step 9) Rotate the aircraft 45 

degrees to the left. Then slowly 

rotate the aircraft 360 degrees 

toward the north (as illustrated) 

until it's flat and upright in your 

hands again. 

Q 

IMPORTANT NOTE: Steps 6 to 9 

must be completed in less than 30 

seconds in order to successfully 

complete compass calibration. 

Step 10) The main LED status 

indicator should be flashing red and 

green rapidly (5 times per second). 

Hold the aircraft as still as possible 

until it main LED status indicator 

stops blinking rapidly. 

Step 1

indicat

status 

rapidly 

comple

IMPORTANT NOTE: If compass calibration fails the main LED status indicator will glow solid white and you must restart the c

26 
ST10+ and Receiver Binding 

Step 1) Turn on the TYPHOON, and 

after the Main LED Status Indicator 

begins to flash blue rapidly, lift the 

back end upward approximately 45° 

then back down to 'level' two (2) 

times to put the aircraft/receiver into 

bind mode. The Main LED Status 

Indicator will begin to the flash 

orange very rapidly when the 

aircraft/receiver are in bind mode. 

Welcome,PIIot 10:48:28 pm 10. • .:Ji 

A 

-:-

r•M Ai&htSettlnas 

Modei:4K Welcome,PIIot 10:48:28 pm . ., 

Model Select 

h 

• 

Step 2) Turn on the ST10+, 

and if required tap the 

screen (outside of the pop 

up status window) to bypass the RC and WiFi 

connection process. 

Step 3) Tap the 'Model 

Select' button, and if 

required press 'OK' to 

bypass any pop up 

warnings/alerts. 

Step 4) Select the existing 

model (for example: 'the 

TYPHOON') you would like 

to bind to (or create a 'New 

Model'), and if required 

press 'OK' to bypass any 

pop up warnings/alerts. 

27 

Modei:4K 

Model 

SR24_16042 I SR24_16042 t5 

Welcome,Pllot 10:48:28 pm 

camera 

Not connected 

II 

•KI 

I 
ST10+ and CG03 Binding 

Step 1) Turn on the ST10+, and if required tap the screen (outside of the 

pop up status window) to bypass the RC and WiFi connection process. 

_,.._. 

- -

... . ., 

Model Select 

Step 2) Tap the 'Model Select' 

button, and if required press 'OK' 

to bypass any pop up 

warnings/alerts. 

Step 3) Select the existing model 

(for example: the' TYPHOON') 

you would like to bind to (or 

create a 'New Model'), and if 

required press 'OK' to bypass any 

pop up warnings/alerts. 

Step 4) Turn on the TYPHOON 

and ensure that the camera is 

powered on. 

Step 5) if required tap the screen 

(outside of the pop up status 

window) to bypass the RC and 

WiFi connection process, then tap 

the 'Flight Settings' button and 

press 'OK' to bypass any pop up 

warnings/alerts. 

28 

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

tP Bind 

8 Camera Select t) 

+ Mode Select 

t:j Hardware Monitor 

_,...... -

-

... 

Model Camera 

Model: Typhoon Wekome,Pilot 10:48:28 pm 10• 

tP Bind 

Ill Camera Select 

+ Mode Select ( \ 

t:j Hardware Monitor 

Model: Typhoon Welcome,PIIot 10:48:2Bpm 10.,. 

Choose a camera NAME: 

C-G01 C-G02 C-G03 

C-G03-Pro 

. ., 

. ., 

I 

. ., 

. ., 

Step 6

select 

camer

'Came'1234

and ta

has be

Step 

button 

mode

'Choo

after 

establ

Step 8

(2) tim

screen 

autom

ST10+

IMPO

video 

ST10+ 

phone

transm

station

recom

very s

downl
GROUND IMAGING SYSTEM 

Specifictations 

CGO STEADVGRJP1M 

Height: 223mm (8.78 in) 

Depth (front to back): 182mm (7.17 in) 

Width: 70mm (2.76 in) Weight (without gimbal/batteries): 200g (7.05 oz) 

Angle Control Range (Pitch): 30° to -85° 

Required Batteries: 2850mAh Energizer® 8x 1.5V AA Batteries 

(Sold Separately) 

Runtime: 48-64 minutes (depending on usage) 

Battery Warnings and Usage Guidelines 

WARNING: Alkaline Batteries May explode or leak, and cause burn injury if recharged, 

disposed of in fire, mixed with a different battery type, inserted backwards or disassembled. Replace all batteries at the same time. Do not carry batteries loose in your pocket 

or purse. Do not remove the battery label. 

WARNING: All instructions and precautions must be read and followed exactly and you 

must follow instructions of the battery manufacturer. 

WARNING: procedures, which if not properly followed, create the probability of property 

damage, collateral damage and serious injury or create a high probability of superficial injury. 

Failure to exercise care while using this product and comply with the following 

conditions and guidance could result in product malfunction, excessive heat, fire, 

property damage, and ultimately injury. 

Lithium lon batteries are not toys. For the purpose of the document Li-lon, Li-Po, Li-Fe, 

NiCd or NiMH batteries will be described as "Batteries". 

Handling and Storage: 

• Never alter, puncture or impact Batteries or related components. 

• Do not directly connect the terminals with metal objects. This will short-circuit Batteries, resulting in heat and electrical discharge. 

29 

• Never store loose Batteries together, the Batteri

another causing a short circuit. 

• Never expose Batteries to extreme temperatures o

• Always disconnect Batteries when not in use. 

Before the First Charge: 

• Ensure batteries are not damaged, as this may cause 

• Always refer to your charger's manual to ensure saf

• Always charge Batteries in an open area away from 

surfaces. 

• Never charge Batteries that are hot to the touch (ab

If at any time Batteries become damaged, hot, or begin 

charging (or discharging) immediately. Quickly and safe

place the Batteries and/or charger in a safe, open area 

in an approved Li-Po bag to observe. After one ho

service. DO NOT continue to handle, attempt to use, 

follow these procedures can cause damage to Batter

serious injury. 

Damaged or swollen Batteries can be unstable and ve

until they have cooled. Dispose of batteries in the 

county, state or country. Contact the appropriate Yu

speak to a service technician for more information. 

In the event of fire, a Class D, dry chemical fire ex

batteries must be placed inside of an approved Li-Po 

Additional Guidelines and Warnings: 

• In the event of a crash, always quickly and safely d

from the model. Then follow the previously listed safe

• If the internal contents of Batteries come into co

affected area(s) with soap and water immediately. If eye(s), flush them with generous amounts of water fo

ately medical attention. 
Installing The Steadygrip TM Batteries 

WARNING: Alkaline Batteries May explode or leak, and cause burn injury if 

recharged, disposed of in fire, mixed with a different battery type, inserted 

backwards or disassembled. Replace all batteries at the same time. Do not 

carry batteries loose in your pocket or purse. Do not remove the battery 

label. 

STEP 1) Remove the 

Battery Cover I Door from 

the bottom of the SteadyHold the bottom of the 

SteadyGripTM toward 

yourself with the front 

part facing downward. • 

Slide the battery cover I door upward with slight force and inspect the AA 

battery compartment. 

STEP 2) lnstall8xAA Batteries 

The use of rechargeable batteries is strongly recommended. Alkaline 

batteries only support the device to work 15 minutes. 

STEP 3) Re-installing the Battery Cover I Door on the bottom of the SteadyGripTM 

Once you've installed 8 fresh AA batteries, Hold the bottom of the SteadyGripTM toward yourself with the front part facing downward. Slide the 

battery cover I door downward with slight force and ensure you hear and 

feel a noticeable 'click' indicating the battery cover I door has been closed 

securely. 

30 

Attaching The CG03 to The Stea

WARNING: Before switching on the SteadyGrip

to first securely attach the CG03 to your Stead

QUICK TIP: It's a good idea to ensure you have 

of space for photos and videos handy. 

STEP 1) Carefully slide the top part of the CG03 {tha

the QSOO the TYPHOON) onto the mount below the 

corresponding 'click' will be noticed once the CG03 

the slide-in mount on the SteadyGripTM. 

STEP 2) Carefully connect the CG03's power/contro

port of the CGO SteadyGripTM and then insert a microS

on the bottom of the CG03. You can use the inc

package) or any Class 10 microSD card up to 128GB. 

STEP 3) Powering on and initialization. Place your CG

s

G

s

v

S

Upon Powering on: Green LED blinking for twice and thPitch Follow Function: GREEN LED blinking 

Low Voltage Warning: RED LED blinking slowly 

Power Cut-off: RED LED blinking quickly 
CG03APP 

Download the free APP 

named as CG03 to smart 

device at the APP Store 

or Google Play Store.lnstall the APP to your 

5.8GHz WiFi capable 

device. Make a note of 

the network name and 

password located on the 

top of the gimbal assembly. [ --ON ---- •t Google· 0 Available on the AppStore 

CG03 APP COMPATIBLE DEVICES 

Apple iOS: iphone 5/5c/5s/6/6+ ipad mini/mini+/3/4 

Android: Mobile Devices with 5.8GHz Suport 

Attaching A Mobile Device to The Steadygripn" 

Step 1) Press the Curved Lip at the 

top front of the SteadyGrip•"' as 

illustrated and fit your Mobile 

Device with the screen facing 

toward the Main LED and Pitch 

Control Wheel. 

Step 2) Connect your Mobile Device 

to the CG03's WiFi by selecting 

CG03's SSID in your WiFi settings 

and entering the WiFi Key I 

Password: 1234567890. 

31 

Using The Camera Pitch Control W

The SteadyGrip'M features a camera pitch con

angle control on the go. Simply roll the pitch con

camera pitch/angle downward 

and roll the pitch control 

wheel backward to move the 

camera pitch/angle upward. 

Please review these instructions along with the illustrations to familiarize yourself on 

how to control the CG03 with 

your SteadyGrip•"'. 

Taking Photos and Recording Vid1) To take a still photo, slide the Mode butto

Photo Taking/Video Recording button. You

from the APP and the LED indicator on C

green. It will take approximately 5 seconds 

you can take another still photo. 

IMPORTANT NOTE: You cannot take stil

You MUST stop recording video, and switc

to take still photos. 

2) To start recording videos, slide the Mo

then press the red button to start. You'll he

APP each time the recording starts/stop

indicator on CG03 front will flash in blue an

time length display on the APP Screen. 

3) To stop recording video simply press the 

You'll hear an audible indication from the 

starts/stops. And while video is recording, t

GC03 will flash blue and green, and there w

length of the recording on the APP screen. 
Pitch Follow Function for CG03 on SteadyGrip 

Pitch Follow Button 

Pitch Follow function allows the gimbal camera to track SteadyGrip in pitch 

direction. 

To Enter Pitch Follow: 

Press Pitch Follow Button on the top of the SteadyGrip to enter Pitch 

Follow Function. The green STEADYGRIP LED Status Indicator on top will 

start blinking instead of being solid when enter Pitch Follow. 

NOTE: 

1) The default status of SteadyGrip is normal status without Pitch Follow. 

2) When SteadyGrip is in Pitch Follow status, the gimbal camera tracks 

SteadyGrip in pitch direction, and the gimbal pitch control roller wheel on 

SteadyGrip is disabled. 

To Exit Pitch Follow: 

Press Pitch Follow Button to exit this function. 

32 
TROUBLESHOOTING 

ISSUE POSSIBLE CAUSE SOLUTION 

the lYPHOON will not the lYPHOON was moved during initialization. Turn the TYPHOON off then ba

initialize does not move during the initial

Flight battery will not Poor connection between the Smart Charger and the Check your connections on bo

charge (red LED on 

charger glows solid red). 

flight battery. the flight battery. Check the fuse 

the TYPHOON GPS will Overcast, thick clouds blocking GPS reception. Wait for the lighter cloud cover 

not lock (ST10+ Solar flares in progress. Wait for disturbance to subside 

indicates GPS Disabled) 

the TYPHOON is indoors. Move the TYPHOON outside or 

Objects blocking 100 degrees of clear view of the sky. Disable GPS. Flying indoors/disabli

(Possibly underneath a metallic or glass cover, inside a 

vehicle, near tall buildings, etc ... ) 

Move the TYPHOON to a clear 

Video transmitter nearby, such as an aftermarket video Reposition or remove the video 

downlink system. 

Raised threat level by the U.S. government. Wait for the threat level to be re

the lYPHOON GPS has The GPS module is possibly damaged. Call Technical Support for replac

reduced precision 

The compass has been exposed to a magnet. Move the TYPHOON away from 

If problem persists, calibrate com

the TYPHOON GPS The GPS module is possibly damaged. Call Technical Support for replac

functions not operating 

properly GPS lock has not been acquired. Ensure GPS antenna has clear vi

been acquired. 

33 
. 

. 

ISSUE 

TYPHOON Motors won't 

start 

TYPHOON Flashes orange 

twice between indications 

lYPHOON beeps constantly 

and rnotorswon'tstart 

TYPHOON Won't hold 

position in hover 

TYPHOON pulses Red 

and won't start 

POSSIBLE CAUSE 

'Compass error' is indicated by the LED. 

TYPHOON is in No Fly Zone. 

TYPHOON is above 8,000 feet above MSL. 

Incorrect motor start up procedure. 

TYPHOON is too close to a metal object or metal surface . 

Failed Component 

Compass needs to be calibrated . 

EMERGENCY Mode. Possibly due to obstructed propeller 

during motor start up. 

Weak GPS signal. 

Component Disconnected, failed, or not assigned properly 

U.S. Government has raised threat level. 

Vibration levels high, indicated by shaky landing gear. 

34 

SOLUTION 

Refer to page 25 for Compass Ca

Move at least 4 miles away from 

airports are no fly zone areas. 

Move the TYPHOON below 8,00

Review Motor Starting/Stopping 

Move the TYPHOON away from la

Connect your TYPHOON to the GU

Refer to page 25 for Compass Ca

Check that nothing is obstructing 

the TYPHOON off then back on 

Confirm that the flying area has 1

the sky. 

Connect to the GUI to locate the 

Wait for threat level to be reduce

Check to ensure propellers are n

in any way. Replace damaged pro
l 

WARRANTY INFORMATION 

Yuneec products and accessories are guaranteed against manufacturing defects for six (6) months from the original date of pu

tion in the event of such defects during this period is to repair or replace the defective part or product with a comparable par

discretion. Except for such repair or replacement, the sale, processing or other handling of this product is without warranty

Damage (including crash damage) resulting from use, accident, or normal wear and tear is not covered by this or any warranty

for any accident, injury, death, loss, or other claim related to or resulting from the use of this product. In no event shall Yune

consequential damages relating to or resulting from the use of this product or any of its parts. Please review the instructio

products. Returns or replacements of parts and/or products may be subject to shipping, handling, replacement and/or restock

IMPORTANT NOTE: Crash damage is NOT covered under warranty. 

CERTIFICATION INFORMATION 

FCC STATEMENT: 

This equipment has been tested and found to comply with the limits for Part 15 of the FCC rules. These limits are designed to p

against harmful interference in a residential installation. This equipment generates, uses and can radiate radio frequency en

used in accordance with the instructions, may cause harmful interference to radio communications. 

However, there is no guarantee that interference will not occur in a particular installation. If this equipment does cause har

television reception, which can be determined by turning the equipment off and on, the user is encouraged to try to correct the 

of the following measures: 

Reorient or relocate the receiving antenna. 

Increase the separation between the equipment and receiver. 

Connect the equipment to an outlet on a circuit different from that to which the receiver is connected. 

This device complies with part 15 of the FCC rules. Operation is subject to the following two conditions: 

(1) This device may not cause harmful interference, and (2) this device must accept any interference received, including 

undesired operation. 

35 
i ... 

NOTE: This equipment has been tested and found to comply with the limits for a Class B digital device, pursuant to part 15 o

are designed to provide reasonable protection against harmful interference in a residential installation. This equipment generat

frequency energy and, if not installed and used in accordance with the instructions, may cause harmful interference to radio 

there is no guarantee that interference will not occur in a particular installation. If this equipment does cause harmful interf

reception, which can be determined by turning the equipment off and on, the user is encouraged to try to correct the interfe

following measures: 

-Reorient or relocate the receiving antenna. -Increase the separation between the equipment and receiver. -Connect the equipment into an outlet on a circuit different from that to which the receiver is connected. -Consult the dealer or an experienced radio/TV technician for help. 

RF EXPOSURE WARNING 

This equipment must be installed and operated in accordance with provided instructions and the antenna(s) used for this tra

provide a separation distance of at least 20 em from all persons and must not be co-located or operating in conjunction with a

ter. End-users and installers must be provide with antenna installation instructions and transmitter operating conditions for sa

ance. 

IC RADIATION EXPOSURE STATEMENT FOR CANADA 

This device complies with Industry Canada licence-exempt RSS standard(s). 

Operation is subject to the following two conditions: (1) this device may not cause interference, and (2) this device must acce

interference that may cause undesired operation of the device. 

Le present appareil est conforme aux CNR d'lndustrie Canada applicables aux appareils radio exempts de licence. L'exploit

conditions suivantes : (1) l'appareil ne doit pas produire de brouillage, et (2) l'utilisateur de l'appareil doit accepter tout brouillag

si le brouillage est susceptible d'en compromettre le fonctionnement. 

This equipment complies with IC RSS-102 radiation exposure limit set forth for an uncontrolled environment. 

Cet equipement respecte les limites d'exposition aux rayonnements IC definies pour un environnement non contr61e 

36