JE Thompson, Inc. d/b/a All American Surveying 

301 W. Broadway Street 

Gainesville, Texas 76240 

(940)665-91 05 

www .allamericanenergyservices.net 

October 12, 2015 

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington, DC 20590 

; . ~. 

i. '- ~ .,) 

Re: Exemption Request Pursuant to Section 333 of the FAA Modernizationand Reform Act 

of 2012, 49 U.S.C. § 44701 (f), and Part 11 of the Federal Aviation Regulations 

Dear Sir or Madam: 

JE Thompson, Inc. d/b/a All American Surveying Services ("AA Surveying"), pursuant to Section 333 

ofthe FAA Modernization and Reform Act of2012 (the "Reform Act") ("Section 333"), Subsection (f) 

of 49 U.S.C.' § 44701, and 14 C.P.R. Part 11, is requesting an exemption from the Federal Aviation 

Regulations ("F ARs") listed below and discussed in Appendix A to allow AA Surveying to conduct 

commercial operations with Tuffwing UAV mapper Unmanned Aircraft System ("UAS") (the 

"Tuffwing") to provide surveying and energy development services, which are primarily located in 

remote unpopulated areas with minimal air traffic. These services include obtaining still photographs, 

real-time video, and other data taken by onboard sensors to monitor operations, environmental 

conditions, and forestland security. Performing these services with a UAS is in the public interest for 

several reasons, which are detailed further herein and include: (1) minimizing safety risks inherent in 

manned operations, both in the air and on the ground; (2) inspecting locations where humans are not 

able to go; (3) enhancing capabilities to utilize the UAS to assist first responders on safety or 

environmental incidents; (4) improving access control/security to sites; and (5) monitoring 

environmental conditions. 

The battery-powered Tuffwing weighs 54 ounces and has a flight time of 40-45 minutes depending on 

operating conditions. It employs a self-stabilizing aircraft configuration with stability augmentation 

avionics that provides ease-of-control and steady video imagery. Its high- performance design leverages 

advanced composite materials, innovative electronics, and cutting-edge sensor technology to increase 

mission capabilities and make Tuffwing a reliable and accurate solution to meet a variety of industry 

needs. 

Operations under the exemption will be conducted under the limitations and conditions set forth in 

Appendix Band as may be modified by the FAA as required by Section 333.2. Use ofthe Tuffwing in 

AA Surveying's operations as proposed herein, would provide significant public safety benefits over 

existing inspection and survey operations, while operating safely within the National Airspace System 

("NAS"). 

Use ofUAS offers numerous safety benefits for operations on the ground. First, the use ofUAS would 

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alleviate the need for personnel to perform difficult and dangerous manual inspections of remote, 

hazardous, or inaccessible locations along pipelines or facilities. Second, UAS will be able to more 

quickly and thoroughly assess safety conditions of roads used by vehicles following storm events. Third, 

use ofUAS would increase situational awareness of the surroundings and help prevent conflicts if 

wildlife or unauthorized personnel gain access to the property, or if a wildfire or other event threatened 

the facilities. Finally, the use ofUAS would improve visual access to areas that are offlimits to foot 

traffic and machinery due to risk of unstable, shifting earth or moving water. 

The use ofUAS would provide AA Surveying's clients with additional data it can use to conduct safer 

and more efficient operations. For inspections now conducted by manned aircraft, use of the UAS for 

these services will reduce the need to operate manned aircraft in a difficult environment and reduce the 

environmental impact of conventional aircraft operations. In addition, the small, lightweight, and easily 

controllable operating characteristics of the Tuffwing provide for safe operations over the remote or 

uninhabited locations of gas development and timberland. This feature would also be beneficial in 

surveying from above in detail features of facilities that it would be too dangerous to fly manned aircraft 

close to. Our clients also maintain strict control over access to their facilities, require all personnel to 

wear personal protective gear, including hard hats and safety glasses, and attend site-specific safety 

hazard briefings to be onsite, so these proposed operations would not endanger workers onsite. 

Although the Tuffwing can be operated by one person, AA Surveying's flight operations will always 

involve at least two people as required by the FAA: a vehicle operator ("VO") and a mission operator 

("MO"). The VO is responsible for flying the UAS, monitoring its status and flight dynamics, while 

keeping the flight within the manufacturer's specified operational limits to ensure safe operation of the 

vehicle. MOs will be responsible for monitoring the airspace for other aircraft and hazards and advising 

the VO before and during flight of all such observed risks. In addition to completing AA Surveying's 

training, the VO will hold at least a state-issued motor vehicle driver's license. 

While AA Surveying has modeled its request off of Part 3 3 3 Exemption grants as of the date of its 

application, AA Surveying requests that ,the FAA treat AA Surveying's application as requesting the 

most lenient relief granted to similar applicants at the time of adjudication. Additionally, should the 

FAA modify any of its UAS operating conditions through exemptions or otherwise after adjudicating 

AA Surveying's application, AA Surveying requests blanket approval to operate it's UAS in accordance 

with the more lenient operating conditions. AA Surveying reserves the right to supplement or amend its 

application. 

Applicant Information: 

The name of the applicant is: JE Thompson, Inc. d/b/a All American Surveying 

The primary contact for this application is: Shelley Head, 301 W. Broadway Street, Gainesville, TX 

76240;940-665-9105 

Email: Shead@Songratus.com 

Exemptions Requested: 

AA Surveying requests exemptions from the following regulations: 14 C.F.R. Part 21; 14 C.F.R. 

61.113(a) and (b); 14 C.F.R. 91.7(a); 14 C.F.R. 91.119(c); 14 C.F.R. 91.121; 14 C.F.R. 91.151(a); 14 

Page 2 
C.F.R. 91.405(a); 14 C.F.R. 91.407(a)(l); 14 C.F.R. 91.409(a)(l) and (2); 14 C.F.R. 91.417(a) and (b). 

Airworthiness of the UAS: 

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

airworthiness certificates as required by CFR §91.203 (a) (1). Given the size and limited operating area 

associated with the aircraft to be utilized by AA Surveying, an exemption from Part 21 Subpart H meets 

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

Section 44701 (f) of the Act and Section 333 ofthe 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 particular UAS. In all 

cases, an analysis of these criteria demonstrates that the UAS operated without an airworthiness 

certificate, in the restricted environment and under the conditions proposed herein will be at least as 

safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness 

certificate without the restrictions and conditions proposed. 

The Tuffwing is a more recently developed system. It does, however, utilize industry- standard sensors 

and controls, which provide numerous fail safes. The Tuffwing is equipped with automated features for 

safe takeoff, flight, and landings in varying conditions. The shorter flight times and very high 

maneuverability will dictate that this system will be used in close proximity to the operator and at lower 

altitudes, which will increase the safety of the system. Tuffwing Operator's Manual will be provided. 

Pre- and post-flight inspections and systems checks will precede and follow each flight following a 

prescribed protocol. Test flights are conducted following any upgrades to system software, firmware, or 

hardware to ensure safety of operations. 

Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by 

AA Surveying pursuant to the Safety Checklist's requirements, and under the requirements and in 

compliance with local public safety requirements, to provide security for the area of operation as is now 

done with conventional aerial mapping and surveying. These safety enhancements, which already apply 

to civil aircraft operated in connection with mapping and surveying operations, provide a greater degree 

of safety to the public and property owners than conventional operations conducted with airworthiness 

certificates issued under 14 C.F .R. Part 21, Subpart H. Application of these same criteria demonstrates 

that there is no credible threat to national security posed by the UAS, due to its size, speed of operations, 

location of operation, lack of explosive materials or flammable liquid fuels and inability to carry a 

substantial external load. 

Operating Conditions: 

AA Surveying requests an exemption subject to the conditions listed in Appendix B, which are 

substantially similar to the operating conditions required for the FAA's previous grants of exemptions 

under Section 333. In accordance with the conditions approved in previous exemption grants, AA 

Surveying is requesting authority to operate the Tuffwing within visual line of sight and below 200 feet 

AGL. The area of operations would include those lands owned or leased by AA Surveying's clients in 

the ranching, natural gas, oil, utilities, wildlife, or timberland management industries across the United 

States. Given that the operating sites are often not flat, AA Surveying will use the elevation of the 

highest predominant terrain within 1 mile of the launch point and within the visual line of sight as a 

Page 3 
ground reference point to establish the 200 feet ceiling. In other words, AA Surveying will not operate 

the Tuffwing any higher than 200 feet above the highest point within 1 mile from the launch point, and 

will only do so provided the UAS is within the line of sight. These operating conditions, along with 

those listed in Appendix B, would provide an equivalent level of safety for the reasons described below. 

First, AA Surveying's clients are generally located in remote areas that rarely see air traffic that they are 

not aware of in advance. 

Second, flight operations in many of AA Surveying's client locations are limited due to the terrain. In 

addition to the requirement that pilots must fly at least 500 feet AGL, the FAA recommends that pilots 

operating under Visual Flight Rules ("VFR") fly over ridges with at least 1,000 feet clearance. Pilots 

flying under instrument flight rules ("IFR") over mountainous areas must fly at "an altitude of2,000 feet 

above the highest obstacle within a horizontal distance of 4 nautical miles from the course to be flown. 1 

Given the locations of our projects and FAA minimum flight altitudes, the Tuffwing will be able to 

operate below altitudes in use by manned aircraft. 

Third, the VO will operate the Tuffwing from higher elevations in regard to project area when possible, 

allowing the MO to maintain full visibility of the airspace over the project to avoid conflict with any 

manned aircraft. AA Surveying will use a MO who will stay in radio contact with the VO if the terrain 

warrants it. 

Fourth, AA Surveying's operational procedures will require VOs to deconflict by suspending all UAS 

operations when a manned aircraft operates within airspace infringement boundaries, greatly reducing 

the risk to any manned aircraft. The VO will be able to immediately land the UAS when the VO or MO 

spot another manned aircraft within the planned area of operations or safety personnel direct 

cessation of UAS operations. 

Fifth, AA Surveying maintains contact with any personnel onsite, requiring all personnel to wear 

personal protective gear, including hard hats and safety glasses, and mandates site specific safety 

training as required by clients. Non-participant AA Surveying employees will carry radios and be alerted 

before UAS operations begin. These safeguards, along with the UAS's light weight, provide an 

equivalent level of safety for non-participants to be closer than 500 feet. 

Sixth, the Tuffwing is equipped with visible strobe lights that will alert any manned aircraft in the area 

to its position. 

Seventh, the Turffwing flight software, Pixhawk Mission Planner manufactured by 3D Robotics, 

provides many built-in functional and safety features to assist the VO in safe and reliable operation. 

Both systems can operate autonomously in "Navigation" mode. In Navigation mode, the VO selects 

waypoints, rally points, and a landing area before launching. The UAS then U:ses GPS navigation to 

follow the pre-selected flight path. The UAS also can be flown in a semi-autonomous mode in which the 

1 FAA Aviation Safety Program, Tips on Mountain Flying, available at 

https://www.faa.gov/regulations policies/handbooks manuals/aviation/media/tips on mountain flying.pdf. Pilots operating 

under VFR also must operate at an altitude that would allow them to make an "emergency landing without undue hazard to 

persons or property on the surface." 14 C.F.R. § 91.119(a). 6 FAR 91.177(a)(2)(i). 

Page 4 
UAS flight software maintains a preset altitude and airspeed and the VO controls heading. Additionally, 

the flight software allows the VO to set certain fail safes, i.e. actions the UAS will take in response to 

loss oflink, loss of GPS, and low battery regardless of the flight mode in which the UAS is currently 

operating. For example, the VO can configure the failsafe so that, in a loss of link situation, the UAS 

flies to a pre-set waypoint and loiters for a short time to give the UAS time to reconnect with the ground 

control station and lands at a pre-set landing spot if loss of link persists beyond a pre-determined length 

of time. The VO can do the same for low battery situations. Finally, any risk presented by possible 

helicopter medical evacuation flights would be mitigated by requiring the VO to terminate UAS 

operations at the command of safety personnel or the MO. The VO will maintain constant radio contact 

with safety personnel. AA Surveying requests authorization to operate the Tuffwing less than 500 feet 

from nonparticipating employees without barriers or structures to protect them, provided they wear 

customary safety gear (e.g. hard hats). An equivalent level of safety is provided because the UAS's 

weight, materials, and reliability, along with the required operator training and operating environment, 

prevent these systems from posing a serious risk to clients/employees wearing personal protective gear. 

Operator Requirements: 

Sections 61.113(a) and (b) limit private pilots to non-commercial operations. Because the UAS will not 

carry a pilot or passengers, the proposed operations can achieve the equivalent level of safety of current 

operations by requiring the PICs operating the UAS to have a private pilot's license rather than a 

commercial pilot's license to operate the UAS. Unlike a conventional aircraft that carries the pilot and 

passengers, the UAS is remotely-controlled with no living thing on board. The area of operation is 

controlled and restricted, and all flights are planned and coordinated in advance as set forth in the Safety 

Checklist. The level of safety provided by the requirements included in the Safety Checklist exceeds 

that provided by a single individual holding a commercial pilot's certificate operating a conventional 

aircraft. The risks associated with the operation of the UAS are so diminished from the level of risk 

associated with commercial operations contemplated by Part 61 when drafted, that allowing operations 

of the UAS as requested exceeds the present level of safety achieved by 14 C.F.R. §61.113(a) and (b). 

Public Interest: 

AA Surveying respectfully submits that its use ofthe UAS in lieu of manned operations, which are 

currently conducted with conventional fixed wing and rotary 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 also will benefit the public interest by allowing better, safer, and more cost efficient 

information gathering for the ecosystem services and energy development industries. Conventional 

aerial survey and inspection operations using manned aircraft involve very heavy aerial vehicles that 

must transit to the operational location and carry significant quantities of combustible fuels and a multiperson crew in piloting and observation roles. These operations become even more difficult in the, 

energy and forestry industries due to the terrain. By contrast, the Tuffwing weighs 3.375 lbs., including 

its payload, uses a battery for power, is carried to and from the area of activity, removes the need for 

airborne pilots and observers, and poses less risk to people and infrastructure on the ground, as well as 

other aircraft. Additionally, no national security issue is raised by the grant of the requested exemptions 

due to the UAS's small size and load-carrying capacity, as well as its operational limitations and absence 

of flammable fuel. On the other hand, the use of these systems is likely to enhance national security 

Page 5 
through better and more accurate monitoring of critical national infrastructure. The grant of the 

requested exemption is in the public interest based on the clear direction in Section 333 and 49 U.S.C. § 

44701(f),5 the equivalent and enhanced level of safety of the proposed operations, the significant public 

benefit, and cost savings to be realized as a result of the use ofUAS for aerial inspection and survey 

services.2 Moreover, the FAA has granted similar exemptions for UAS used to conduct high resolution 

aerial imaging and surveying operations.3 Accordingly, the applicant respectfully requests that the FAA 

grant the requested exemption without delay. 

Privacy Concerns: 

The proposed operations will take place only in largely unpopulated, remote areas that are owned or 

leased, and access controlled by AA Surveying's clients. Access to these areas is generally restricted to 

employees and authorized personnel only. No privacy issues are raised by this application. 

Federal Register Summary: 

Pursuant to 14 C.F.R. § 11.81(f), the following summary is provided for publication in the Federal 

Register, should the FAA determine that publication is needed: 

Docket No.: No. FAA-2015- Petitioner: JE Thompson, Inc. d/b/a All American Surveying 

Section of 14 C.F.R.: Part 21, § 61.113(a) and (b),§ 91.7(a), § 91.119(c), § 91.121, § 91.151(a), § 

91.405(a), § 91.407(a)(l), § 91.409(a)(2), § 91.41 ?(a) and (b). 

Description of Relief Sought: AA Surveying is seeking an exemption to conduct commercial operations 

using a small unmanned aircraft (55 pounds or less) in remote areas of the United States. 

AA Surveying requests that the FAA not request public comment on its application because it would not 

set a precedent and because the relief requested is identical to exemptions granted previously. 14 C.F.R. 

§ 11.87. 

2 Under 49 U.S.C. § 4470l(f), 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 44702-44716 of [Title 49] if the Administrator fmds the 

exemption is in the public interest." 

3 See Exemption Nos. 11109, 11110, 11136, 11172. 

Page 6 
APPENDIX A 

EXEMPTION REQUEST AND EQUIVALENT LEVEL OF SAFETY SHOWINGS UNDER 

APPLICABLE RULES SUBJECT TO EXEMPTION 

AA Surveying requests an exemption from the following regulations as well as any additional 

regulations that may technically apply to the operation of the Tuffwing UAS: 

14 C.F .R. Part 21, Subpart H: Airworthiness Certificates 

Part 21, Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements for the 

issuance of airworthiness certificates as required by§ 91.203(a)(1 ). Given the size and weight of the 

aircraft, the operating conditions, design safety features, and the proposed conditions and limitations, 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. Section 333 and 49 U.S.C. § 44701(f) 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 UAS 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 Tuffwing weighs 3.375 

pounds fully loaded. It will not carry a pilot, passenger or flammable fuel. These UASs operate 

exclusively within a controlled area pre- disclosed and in compliance with conditions set forth herein. 

Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored 

by the VO and observer(s), pursuant to the conditions set forth in Appendix B, the Operator's Manual, 

and local public safety requirements. 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 UAS provides at least 

an equivalent level of safety to that of such operations being conducted with conventional aircraft that 

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

14 C.F.R. §§ 61.113(a) & (b): Commercial Pilot Privileges 

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

aircraft that carries a pilot, passengers, and cargo, the Tuffwing is remotely controlled with no 

passengers or property of others on board. The area of operation is controlled and restricted, and all 

flights are planned and coordinated in advance as set forth in the Operator's Manual. In conjunction with 

the required training of the V 0 and observers, the level of safety provided by the requirements included 

in the Operator's Manual exceeds that provided by a single individual holding a commercial pilot 

certificate operating a conventional aircraft. The proposed operations will achieve at least an 

equivalent level of safety. 

Page 7 
14 C.F.R. § 91.7(a): Minimum Safe Altitudes 

Section 91.7(a) prohibits an individual from operating a civil aircraft unless it is in an airworthy 

condition. No FAA standard exists for determining an aircraft's airworthiness when an airworthiness 

certificate is not issued. As the FAA has done with previous exemption grants, airworthiness will be 

ensured and an equivalent level of safety will be achieved by compliance with the operating documents 

prior to every flight. 4 

14 C.F .R. § 91.119( c): Minimum Safe Altitudes 

Section 91.119 establishes safe altitudes for operation of civil aircraft. Specifically, Section 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. Because some of the aerial inspection 

and survey work must be accomplished at altitudes less than 500 feet AGL and nonparticipating 

employees will be working within 500 feet of the UAS, an exemption from Section 91.119(c) is needed. 

The equivalent level of safety will be achieved because AA Surveying's employees and the client's 

onsite employees are required to wear personal protective gear and because the UAS, given its size, 

weight, speed, and materials, does not pose a serious risk. Also, every flight will be conducted over land 

owned or controlled by AA Surveying's clients. Compared to aerial inspection operations conducted 

with aircraft or rotorcraft weighing far more than 3.375 pounds (for the Tuffwing) and carrying 

flammable fuel, any risk associated with these operations will be far less than those currently allowed 

with conventional aircraft operating at or below 500 feet AGL. 

14 C.F.R. § 121: Altimeter Setting 

Section 121 requires each person operating an aircraft to maintain cruising altitude by reference to an 

altimeter that is set "to the elevation of the departure airport or an appropriate altimeter setting available 

before departure." As the UAS may not have a barometric altimeter, but instead a GPS altitude read out, 

an exemption is required. An equivalent level of safety will be achieved by the operator, pursuant to the 

Operator's Manual, confirming the altitude of the launch site shown on the GPS altitude indicator before 

flight. 

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 Tuffwing batteries 

provide approximately 40-45 minutes of powered flight. Without an exemption from 14 C.F.R. § 

91.151, the Tuffwing flights would be limited to approximately 10 minutes in length because the VO 

would require the last 30 minutes to satisfy section 91.151(a). 

4 Exemption Nos. 11156, 11158, 11159. 

Page 8 
AA Surveying believes that an exemption from 14 C.F.R. § 91.151 (a) provides an equivalent level of 

safety and is consistent with prior exemptions. 8 Operating the UAS, without 30 minutes of reserve fuel 

does not engender the type of risks that Section 91.151 (a) was meant to prevent given the size and 

speed at which the UAS operates. In the unlikely event that the UAS' battery runs low, it would simply 

follow the pre-programmed command to land at a designated location. Given its weight and construction 

material, the risks are less than contemplated by the current regulation. 

AA Surveying believes that an equivalent or enhanced level of safety can be achieved by maintaining 10 

minutes of reserve power for the Tuffwing which, allowing at least 30 minutes of flight time, if not 

more, would be more than adequate to return the UAS to its planned landing zone from anywhere in its 

limited operating area. 5 

14 C.F.R. §§ 91.405(a), 91.407(a)(l ), 91.409(a)(2), and 91.417(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) of this 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. 

Pre-flight checks will be performed by a qualified person prior to each flight and at predefined intervals 

as part of the maintenance schedule. 

The pre-flight checklist includes: 

1. Visual inspection of the airframe; 

2. Visual inspections of propeller( s ); 

3. Verify GPS acquisition; 

4. Plan and upload mission; 

5. Camera and payload check; 

6. Controls check; 

7. Gyro/control surfaces check; 

8. Throttle check; 

9. Check sensors; and 

10. Verify failsafes are set correctly. 

An equivalent level of safety will be achieved because the UAS will operate only in restricted 

predetermined areas, and at low altitudes. In addition, the operator will ensure that the UAS is in 

working order prior to initiating flight, perform required maintenance, and keep a log of any 

maintenance that is performed. Test flights will be conducted prior to operations following adjustments 

5 Exemption 10673 (allowing Lockheed Martin Corporation to operate without compliance with 91.151 (a)); see also 

Exemptions 2689F, 5745, 10673 and 10808 

Page 9 
to UAS hardware, software, or firmware. Moreover, the operator is the person most familiar with the 

aircraft and is best suited to maintain the aircraft in an airworthy condition and to ensure an equivalent 

level of safety. Last, the Operator's Manual will have instructions to develop and document 

maintenance, overhaul, replacement, and inspection requirements. The UAS maintenance guidelines 

provide an equivalent level of safety to the maintenance requirements in Part 91. 

Page 10 
APPENDIX B 

AA SURVEYING OPERATING LIMITATIONS 

1) Operations authorized by the grant of exemption are limited to the following 

Tuffwing, weighing 3.375lbs. 

2) The UAS shall not be flown at a ground speed exceeding 60 kts. 

3) The UAS will not be operated at an altitude more than 200 feet above the highest 

predominant terrain except as may be provided by FAA Air Traffic Control (''ATC") 

via GOA. The highest predominant terrain is defined as terrain within 1 mile of the 

launch point and within the visual line of sight of the VO. All altitudes reported to 

ATC shall be in feet AGL. 

4) All operations must use a MO. The MO and VO must be able to communicate 

verbally at all times. The VO must be designated before the flight. The VO must 

ensure that the MO can perform the functions prescribed in the operating documents. 

5) The operating documents and this grant of exemption must be accessible during UAS 

operations and made available to the Administrator upon request. If a conflict exists 

between the conditions and limitations in the exemption and the procedures outlined 

in the operating documents, the conditions and limitations in the exemption take 

precedence and must be followed. Otherwise, AA Surveying must follow the 

procedures as outlined in its operating documents. AA Surveying may update or 

revise its operating documents. It is AA Surveying's responsibility to track such 

revisions and present updated and revised documents to the Administrator upon 

request. AA Surveying must also present updated and revised documents if it petitions 

for extension or amendment to this grant of exemption. 

6) Prior to each flight the VO must inspect the UAS to ensure that it is in a condition for 

safe flight. The VO shall not operate the aircraft if the inspection reveals a condition 

that affects the safe operation of the UAS until the necessary maintenance has been 

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

Control Station, if utilized, must be included in the preflight inspection. All 

maintenance and alterations must be properly documented in the aircraft records. 

7) Any UAS that has undergone maintenance or alterations that affect the UAS operation 

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

a functional test flight in accordance with the Operator's Manual. The VO who 

conducts the functional test flight must make an entry in the aircraft records of the 

flight. The requirements and procedures for a functional test flight and aircraft record 

entry shall be included in the Operator's ManuaL 

8) The pre-flight inspection must account for all discrepancies, e.g. inoperable 

components, items, or equipment, not already covered in the relevant sections of the 

Page 11 
operating documents. 

9) AA Surveying must follow Tufn~ing aircraft/component, maintenance, overhaul, 

replacement, inspection, and life limit requirements. 

1 0) AA Surveying must carry out its maintenance, inspections, and record keeping 

requirements, in accordance with the operating documents. Maintenance, inspection, 

alterations, and status of replacement/overhaul component parts must be noted in the 

aircraft records, including total time in service, description of work accomplished, and 

the signature of the person authorized to return the UAS to service. 

11) Each UAS operated under this exemption must comply with all manufacturer 

Safety Bulletins. 

12) The VO must possess at least valid state-issued motor vehicle driver's license. The 

VO must also meet the flight review requirements specified in 14 C.P.R.§ 61.56 in an 

aircraft in which the VO is rated on his or her pilot certificate. 

13) AA Surveying may not permit any VO to operate unless the VO meets the 

operator's qualification criteria and demonstrates the ability to safely operate the UAS 

in a manner consistent with how the UAS will be operated under this exemption, 

including evasive and emergency maneuvers and maintaining appropriate distances 

from persons, vessels, vehicles and structures.fi VO qualification flight hours and 

currency must be logged in a manner consistent with 14 C.F .R. § 61.51 (b). The VO 

must ensure that the MO is trained appropriately in order to fulfill his or her duties. A 

record of training and qualification must be documented and made available upon 

request by the Administrator. Flights for the purposes of training the operator's VOs 

and MOs (training, proficiency, and experience-building), are permitted under the 

terms of this exemption. However, training operations may only be conducted during 

dedicated training sessions. During training, proficiency, and experience-building 

flights, all persons not essential for flight operations are considered nonparticipants, 

and the VO must operate the UAS with appropriate distance from nonparticipants in 

accordance with these operating conditions. 

14) Operations may not be conducted during night, as defined in 14 C.P.R.§ 1.1. All 

operations must be conducted under visual meteorological conditions CVMC'). 

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

15) The UAS may not operate within 5 nautical miles of an airport reference point as 

denoted on a current FAA-published aeronautical chart. 

16) The UAS may not be operated less than 500 feet below or less than 2,000 feet 

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

6 Prior documented flight experience that was obtained in compliance with applicable regulations may satisfy this 

requirement. 

Page 12 
17) If the UAS loses communications or loses its GPS signal, the UAS must return to 

a pre- determined location within the security perimeter and land or be recovered in 

accordance with the Operator's Manual. 

18) The VO must abort the flight in the event ofunpredicted obstacles or emergencies 

in accordance with the Operator's Manual. 

19) UAS operations must be completed within 30 minutes flight time. 

20) The radio frequency spectrum used for operation and control of the UAS must 

comply with Federal Communication (FCC) or other appropriate government 

oversight agency requirements. 

21) The documents required under 14 C.F.R. §§ 91.9 and 91.203 must be available to 

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

These documents shall be made available to the Administrator or any hiw enforcement 

official upon request. 

22) The UAS must remain clear and yield the right of way to all other manned 

operations and activities at all times. 

23) The UAS may not be operated from any moving device or vehicle. 

24) The UAS may not be operated over congested or densely populated areas. 

25) Flight operations must be conducted at least 500 feet from all nonparticipating 

persons, vessels, vehicles, structures, and public access roads unless: 

a. The nonparticipating persons are authorized to access the client's site and are 

wearing personal protective gear; 

b. For non-participants who do not qualify as client employees, barriers or 

structures are present that sufficiently protect them from the UAS and/or debris 

in the event of an accident. The operator must ensure that nonparticipating 

persons who are not client employees remain under such protection. If a 

situation arises where nonparticipating persons who are not client employees 

leave such protection and are within 500 feet of the UAS, flight operations 

must cease immediately; or 

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

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

and the VO has made a safety assessment of the risk of operating closer to 

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

26) Operations nearer than 500 feet to the VO, MO, operator trainees or essential 

persons as defined in the operating documents are permitted ifthose operations do not 

present an undue hazard to those persons per§ 91.119(a) as determined by the VO. 

Page 13 
27) All operations must be conducted over remote, private, or controlled-access 

property. 

28) 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 must be 

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

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

Page 14 
APPENDIX C 

SMALL UNMANNED AERIAL SYSTEM DESCRIPTION 

UAS SYSTEM DESCRIPTION 

UAS Operating Overview - Tuffwing: . 

The Tuffwing is a fixed-wing aircraft constructed of EPP foam and rugged carbon fiber composite. It 

has fully autonomous operation for takeoff, navigation, and landing. 

Parameter Wingspan 48in 

Length 18 in 

Weight fully loaded 54 oz (well below the 4.4 bl FAA proposed 

requirement for Micro U AS 

Weight, with EO side-look payload 3.375 lbs 

Payload Wireless Range 5- 15 km LOS 

Cruise Speed (Best) 26 kts (30 mph) 

Endurance (Dash speed) 52 kts (60 mph) 

Stall Speed 25 kts (29 mph) 

Max wind 20 kts sustained, 30 kts gusting 

Precipitation None 

Flight Rate 40-45 mins 

Climb Rate Launch 500 ft/min @ 2,000 AMSL 

Launch Hand launch, no catapult 

Landing Autonomous or manual 

Page 15 
The UAS can be operated in fully autonomous flight modes. Creating pre-planned flight paths to fly in 

autonomous mode is as simple as clicking on the map to create a pre-planned flight path. Pre-mission 

waypoints, landing zone points, and flight area dimensions can all be entered during preflight, ensuring 

the UAS operates only within specified parameters. 

The Tuffwing includes many advanced safety features that makes it the safest choice for areas like 

pipeline construction. Built-in intelligent fault handling allows the UAS to detect a system fault while in 

the air, and to automatically respond with a set command (one such option being to fly back to a 

preselected rally point and land). Faults that can be detected include: loss of communication, loss of 

GPS, and low battery levels. In addition, the operator can create no fly zones, and the system will 

visually and audibly warn the operator if the planned flight path would enter the no fly zorie. 

Operator's Manual- The Tuffwing Operator's Manual will be provided under separate cover with a 

request for confidential treatment. 

Power - The Tuffwing and its ground control station are both powered by a Lithium polymer 

rechargeable battery pack. A new battery has a fully charged voltage of approximately 12.4 V. A "fullpack" has a capacity of 4 Amp-hours. An additional "half-pack" can be installed for extended operation. 

A new "half-pack" has a fully charged voltage of 12.4V and a capacity of2 Amp-hours. The Tuffwing's 

battery charge is displayed in real-time on the ground control terminal, ensuring maximum flight 

duration and safety. 

Takeoff and Landing style/type - The Tuffwing is hand launched. The Tuffwing lands by returning to a 

pre-determined rally point and beginning a spiral descent. Once it reaches a preselected altitude, it heads 

toward the landing waypoint, descending until it lands and skids to a stop or it can manually landed. 

Navigation System- Specific maps can be downloaded to the display screen (such as air sectional and 

geographic maps) which are overlaid with GPS positional data. Waypoints can be created before and 

during flight operation creating specific locations and sequences for the aircraft. 

Defined "Keep Out" Areas - The navigation software allows for preplanning Keep Out Areas that allow 

the operator to designate airspace he or she does not want the Tuffwing to enter. If defined flight paths 

pass through an area designated as keep-out, the individual waypoints and waypoint connection 

segments tum red as a warning. Additionally, if a mission is uploaded and intersects with a keep out 

area, a warning is presented to the user. Also, if an aircraft in flight is navigated into a designated keep 

out area, an audible warning is sounded. 

Maintenance- The Tuffwing UAS needs very little maintenance, and operators may perform most 

required maintenance in the field with the field repair kit. 

Command and Control Systems - The UAS Ground Control Station (GCS) allows the operator 

simultaneous control over aircraft and payloads. The display screen provides all essential flight data to 

the operator. Telemetry data is transmitted to the command station at least once per second. 

Displayed on GCS: 

• Current position 

• Registered home position 

Page 16 
• Any autopilot flight plans 

• Registered emergency landing zone 

• Aircraft attitude 

• Altitude 

• Airspeed 

• Groundspeed 

• Compass reading/heading 

• Estimated wind heading 

• Communication strength 

• Range from home 

• Bearing from home 

• Duration of current mission 

• Rate of climb 

• Mode of the aircraft 

• Battery level 

Emergency Procedures and System Failures 

Loss of Link- The UAS does not need constant signal from the GCS to continue flying. 

Communications outages are detected by the system and are reported to the VO. During the 

communication outage, the UAS continues on its pre-determined flight path until a failsafe is triggered. 

Once a failsafe is triggered, the UAS will perform in accordance with the failsafe conditions uploaded 

before launch. This is accomplished without input from the operator. 

Security 

The system and communication links are spread spectrum. 

Operational Characteristics 

Characteristic !Yes/No 

Lights Out Operation No 

VFR Operations Yes 

FR Operations No 

Day Operations Yes 

Night Operations No 

lA vionics Equipment 

!Equipment ~es/No 

GPS ~es 

!Moving Map Indicator ~es 

rrracking Capability No 

rrcA/MCAS Collision A voidance No 

IELT (Falcon Tracker) !Yes 

rrransponder No 

Page 17 
The UAS can be operated in fully autonomous flight modes. Creating pre-planned flight paths to fly in 

autonomous mode is as simple as clicking on the map to create a pre-planned flight path. Pre-mission 

waypoints, landing zone points, and flight area dimensions can all be entered during preflight, ensuring 

the UAS operates only within specified parameters. 

Built-in intelligent fault handling allows the UAS to detect a system fault while in the air, and to 

automatically respond with a set command (one such option being to fly back to a pre-selected rally 

point and land). Faults that can be detected include: loss of communication, loss of GPS, and low battery 

levels. 

Page 18 
.liAV~MAPPER Airframe Assembly Manual 

Got Questions? 830-446-1500 Talk or Text 

TuftWing LLC 

Boerne, Texas USA 

www. tuffwing.com 
Kit contents 

1. EPP wing set 

2. 1/8" ply motor mount set 

3. 1/8" ply servo mount plate 

4. 1/8" ply airspeed sensor mount with zip ties 

5. Control hams (2) 

6. Coroplast center wing panel wrap top and 

bottom pieces 

7. Coroplast hatch 

8. Coroplast winglets 

9. Coroplast servo covers for wing bottom 

10. Coroplast wing cut fillers (2) 

11. 4mm Coroplast center wing ribs 

12. Coroplast accessory mounts (2) 

13. 10mm x 30.75" carbon fiber tube- center 

wing spar (1) 

14. 10mm x 25.9" carbon fiber tube -leading 

edge wing spars (2) 

15. 4 mm x 19.5" carbon fiber tube- elevon 

spars (2) 

16. Control rod with Z bend (2) 

17. Control rod quick connect (2) 

18. Velcro set 

19. 3mm x 8mm motor mount screws (4) 

20. Servo extensions, 12" 

21. Assembly manual 

Building materials - Not included 

• Medium CA. Foam safe NOT required. 

• CA accelerator. 

Electronics- Not included 

• Brushless outrunner motor-Turnigy SK3-

3530-1340KV. 

• 40 plus amp brushless speed control with 

3.5mm female bullet connectors. (Turnigy 

Plush 40) 

• APC 9x4.5E electric propeller. 

• Servos (2) Spektrum A5040 or Corona 

DS329MG. 

• PixHawk autopilot with airspeed sensor and 

telemetry radios. (3DR or HKPilot). 

• Spektrum transmitter with Elevon/Detta 

mixing and satellite receiver. (Taranis or 

Futaba with S.Bus are fine) 

• 6000 mAh 3S LiPo battery 

• Male and female XT60 connectors. 

• UPo battery charger 

• Canon Powershot S 11 0 

• Pixhawk to Canon camera trigger cable. 

(tuffwing.com) 

Install the Spars 

1. Fit the black Coroplast center cut filler into the 

cut on the EPP center wing. 

2. Align the parts by sliding the 10mm x 30.75" 

carbon fiber spar through the parts. 

3. Apply CA to both sides of the coroplast center 

cut filler. Avoid getting CA on the center spar. It's 

just there for alignment Press the parts together 

and CA accelerator on 

4. Use sandpaper to scuff both sides of the 4mm 

Coroplast center wing ribs. 

5. Apply medium CA to coroplast center rib side 

facing the foam. Do not glue spars. 

6. Spray CA accelerator on the foam. 

7. Align rib using leading edge and center spars, 

then press pieces together. 

8. install both center wing ribs. Do not glue spars. 

Slide a wing half onto the center spar. Leave a 1" 

gap. 

10. Apply CA to foam. 

11. Spray CA accelerator on the Coroplast center 

rib. 

@ 2015. TuffWing LLC. All rights reserved. 
1. Slide in the 1 Omm x 25.9" leading edge spar 

flush with wing root, then push wing root 

flush with center rib. Align pieces by pushing 

leading edge spar all the way into the center 

section. 

2. Press pieces together tightly until CA cures. 

Do both wings. 

3. Liberally drip medium CA into leading edge 

and center spar grooves. Spray with CA 

accelerator. 

Glue Coroplast to center section 

'? \ 

0 

Note camera lens opening right of center while 

plane is upside down. 

1. Test fit the Coroplast main center section so the 

camera circle is offset right when looking at the 

bottom of the plane - see photo. 

2. Lay the wing upside down. 

3. Liberally apply medium CA to the foam center 

section. 

4. Spray Coroplast center wing panel wrap with CA 

accelerator. 

5. Carefully and quickly align Coroplast center 

wing panel wrap with motor mount opening and 

Coroplast center wing ribs. 

6. Press very firmly until the CA cures. 

~ > "' .. ··· ~;{ ~\ ·•., 

. . . 

7. Test fold the Coroplast center wing panel wrap. 

Carefully warming the Coroplast with a heat gun 

will make it more malleable. 

8. Liberally apply medium CA to the top foam 

center section. 

9. Spray Coroplast center wing panel wrap with CA 

accelerator. 

10. Carefully and quickly push over and align the 

Coroplast center wing panel wrap with motor 

mount opening and Coroplast center wing ribs. 

11. Press very firm until CA cures. 

12. Liberally apply medium CA to the rear top foam 

center section. 

13. Spray Coroplast top center wing panel wrap with 

CA accelerator. 

14. Carefully and quickly align the Coroplast top 

center wing panel with motor mount opening 

and Coroplast center wing ribs. Press very 

firmly until CA cures. 

15. Test fit accessory Coroplast panels on wing. 

Panel with hole goes on right wing. 

16. Line up V-notch on panel with V-notch cut on 

root end of wing. See red circle in photo above. 

17. Scuff bottom side of Coroplast with fine 

sandpaper. 

18. Liberally apply CA to bottom side of coroplast. 

Spray CA accelerator on foam. Align and firmly 

press Coroplast to wing. 

© 2015. TuffWing LLC. All rights reserved. 2 
' ' '\ 

'',.~ 

i\1 

1. Poke hole in foam through hole in right 

Coroplast panel. The hole lines up with the 

servo wire groove below. 

2. Feed Pixhawk arm switch wire through hole and 

into the main bay. 

Glue control horn 

I 

1. Drip medium CA into the control horn gap. 

2. Quickly press the control horn into the gap. 

3. Spray with CA accelerator. 

4. Do both sides. 

Glue servo base cover 

1. Apply medium CA on the foam wing 1/2" 

wide around the perimeter of the servo 

cutout hole. 

2. Spray CA accelerator on the servo cover. 

3. Leave a 1/4" gap between the two cut outs 

to allow the servo lead to pass through. 

4. Do both sides 

Install the Servo Plate 

1. Apply medium CA to the bottom of the servo 

mount plate. 

2. Spray CA Accelerator on the wing top. 

3. Line up the servo mount plate and press firmly. 

4. Do both sides. 

Install the Quick Connect 

1. Insert the pushrod quick connect on the tip side 

of the wing as shown. Press the black nylon 

washer on with pliers. 

Install the Servos 

.... 

1. Install a Spektrum A5040 servo in each servo 

mount plate as shown. 

2. Install the pushrod into the second hole from the 

end. 

3. Important! Use thread lock on the servo arm 

screw after ~ou have centered it. 

© 2015. Tuf!Wing LLC. All rights reserved. 3 
4. Connect servo extension. 

5. Tuck servo extension into groove on wing 

bottom. 

6. Push wire through opening into electronics bay. 

7. Tack servo extension to servo groove with hot 

glue. Do not use CA as it will be too permanent. 

Glue the Winglets 

surface of winglet with fine sa 

will be glued to the wing tip. 

2. Apply medium CA to a wing tip. 

3. Spray winglet with CA accelerator. 

4. Align front and bottom edges, then firmly press 

together until CA cures. Do both sides. 

Build the motor mount 

1. Glue the sides on with medium CA 

2. Glue the top and bottom with medium CA 

Test fit the motor mount in the cut out the rear 

of the plane. 

4. Apply medium CA to the motor mount where it 

will contact the plane. Do not us CA accelerator. 

5. Quickly and firmly push the mount in place. Do 

not hesitate as the CA may grab before the 

mount is properly set. 

Install the motor 

1. Install the X mount and prop adapter. Included 

with the Turnigy SK3-3530-134DKV. 

2. Trim the shaft with a rotary tool from the back of 

the motor as seen in the photo. 

© 2015. TufiWing LLC. All rights reserved. 4 
3. Mount the motor to the motor mount with the 

four 3mmx8mm screws. 

Build the airspeed pitot mount 

je ,~, !] ·=j 

1. Strap the airspeed pitot to the 1/8" ply mount 

with zip ties. 

Install Velcro 

0 

Note: Install Velcro hooks on the plane and Velcro 

loops on the components. That way you can easily 

swap damaged components or airframe. 

1. Electronics hatch 

2. Airspeed pitot 

3. Camera 

4. Telemetry 

5. GPS/Compass 

6. Spektrum satellite 

7. Pixhawk 

8. Buzzer 

9. ESC 

10. Airspeed sensor 

11. 12C hub 

Install autopilot (Pixhawk) 

1. Stick loop Velcro to bottom of components. 

2. Stick components to as shown in previous 

drawing. 

3. Setup the Pixhawk as described at 

http://plane.ardupilot.com. 

Center of Gravity 

There is balance hole on the bottom of the Coroplast 

hatch. As long as the plane balances or falls forward 

you're good. Tail heavy will be nearly impossible to 

fly. Nose heavy is fine. Add nose weight for first 

flights without camera. 

Set the control throws 

• 5/8" up 

• 5/8" down 

• Move stick right: Right elevon up, left elevon 

down 

• Move stick left: Left elevon up, right elevon 

down 

• Move stick forward: Both elevons down 

• Move stick back: Both elevons up 

© 2015. TuffWing LLC. All rights reserved. 5 
Install Mission Planner and connect your UAV Mapper to your ground station using the telemetry radios/a> 

1. Download and install Mission Planner on your Windows PC. 

2. Connect your telemetry radio to a USB port on your PC 

3. Connect your battery to your UAV Mapper. Do not arm your UAV Mapper. 

4. Start Mission Planner and select the CONNECT button on the top right. 

Note: Complete instructions with trouble shooting. 

Calibrate your compass 

You must recalibrate the compass each time you move your UAV Mapper to a new flight location./p> 
1. Start Mission Planner, Connect your UAV Mapper to Mission Planner and select Initial Setup> Mandatory H; 

2. Select Pixhawk/PX4, then select Live Calibration. 
3. Select Rotate with each data point and Use Auto Accept. 

4. Rotate your UAV Mapper on all axes until the calibration completes. The final offsets will be displayed (3 nun 

below 250 then you can assume they are good. 

Note: Complete compass calibration documentation. 

Flight modes 

The UAV Mapper is preprogrammed with 3 flight modes- Stabilize, Auto, and Return to L~unch (RTL). Flight modes< 

other switches are disabled. 
;··' 

,J 

o Stabilize- Standard RC control with simple stabilization. If you let go of the sticks your UAV Mapper will auto 

o Auto- Your UAV Mapper will follow the waypoints in the mission you have setup and uploaded to the Pixhav 

o RTL (Return to launch)- Your UAV Mapper will return to the location and loiter at 100 meters above where c 

Always connect your UAV Mapper battery where you want it to return. 

:Transmitter control check 

_Place your UAV Mapper on a level surface, turn the transmitter on, select Stabilize on your transmitter flight mode s1 

press the Arm button. 

(eft stick back: Motor off. 
!~"·~·" ....... ··- · , ,_._,, ···-·u••••·m" •• v• '"" · =· ,.. . .., ...... "''"'UV''"'!P-O!J• •11¥ ··' 

 'MiiMHWWIII..,.,""'"rt"'"!'•'"•''W'""'dUPI "' ;arn< ··""-"Z'TE·••yq-zr'f ··y,ru 

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left stick forward: Motor on full. Have a helper hold your UAV Mapper. 

Right stick forward: Both elevons move 5/8" (16mm) down. UAV Mapper pitches down. 

Right stick back: Both efevons move 5/8" (16mm) up. UAV Mapper pitches up. 

Right stick right: Left elevon down 5/8" (16mm), right elevon up 5/8" (16mm). UAV Mapper rolls right. 

Right stick left: Left elevon up 5/8" (16mm), right elevon down 5/8" (16mm). UAV Mapper rolls left. 

Autopilot response check 
Always make sure the autopilot is behaving properly before you fly. As you pitch and roll your UAV Mapper, the elevt 

your transmitter to Stabilize, ensure your throttle stick is back, connect your UAV Mapper battery, and press the arrr 

·~ 

,Roll UAV Mapper left: left elevon down, right elevon up. 

'Roll UAV Mapper right: Left elevon up, right elevon down. 

Pitch UAV Mapper down: Both elevons up. 
Pitch UAV Mapper up: Both elevons down. 

Landing site requirements 

The most challenging part about flying a UAV Mapper, or any fixed wing UAV is getting it down. Unlike Pixhawk guide 

fixed wing. A copter can descend straight down, while a fixed wing must approach on a clear glide slope. If you are m 

landing pattern using Mission Planner and upload it to your UAV Mapper. First, make sure your flying site meets the 

create the takeoff and land shown mission below. 

Minimum Size Landing Site 

600ft (180m) between approach waypoinl and land1ng waypolnt OVer $hoot 200ft (60 m) 

Create a take off and land mission 

1. Start Mission Planner and select Flight Plan. 
2. Click on the map to create WAYPOINT 1. 
3. Click on the map again to create WAVPOINT 2. 

4. Right-click on the map and select Takeoff. Enter lOO(m) for takeoff altitude. Enter 30 (degrees) for takeoff p 

5. Use the Up button to move the TAKEOFF waypoint to the top. Verify Pitch Angle is 30 and Alt is 100. 

6. Set WAVPOINT 2 Altitude to 35m. This is your approach waypoint. 
7. Set WAVPOINT 3 to LAND and Alt to 0. 

8. Select WriteWPs to copy the mission to your UAV Mapper 

~IMPORTANT: Any mistake in this mission will result in a crash. You must understand every step of this process. This i! 

:the air and safely back to the ground. 

'Power up and check LED status. 

Turn on your transmitter and set your flight mode switch to Stabilize. Connect your UAV Mapper battery. The UAV IV 

:hole so you can see the Pixhawk status during boot up. Be sure to power up where you want your UAV Mapper to loi 

(-,,~r-tr·\ 

.''- _ .. \ 7,_ ,\"'_;Pixhawk i_s booting l.lP· 

C;QC·()Error. Most likely the Pixhawk Micro SD was removed to retrieve the flight log and not replaced. 

OC1

C1

0Pixhawk is waiting on GPS lock. Do not fly until green. 

Failsafe error. Do not fly. 

C1

C:C1

Q Pixhawk has GPS lock and is ready to fly . 

. Fly your UAV Mapper 

' 

1. Move to a spot in your flying field with 400ft. (120m) of clear space ahead, into the wind. 

2. Set your transmitter to Stabilize mode, make sure the throttle is down, and press the arm button until its sol 

3. Hold your UAV Mapper like the photo below. Be prepared for the motor to start full throttle. 

4. Have a helper switch the flight mode switch to Auto. This will execute the waypoint mission you have upload 

~The propeller will spin immediately. Be prepared. There is no delay. The motor will remain full throttle until take c 

'changed to Stabilize. 
I 

t>~ ~.~ ' 

,~ _, . . :'. {: .• .. 

. . "" . , • •I ' • "' ... :• : 

- • ... ~f 

l - • • .. ,... ..... ,.. /«. ·.~ ·"· 

....... . " . . ... .. ,.... .,.. : . ---·· --·~- -- _;2 __ • • "--~-=---------·:~_:j 

5. Pitch and roll your UAV Mapper to make sure control surfaces are properly moving. 

6. Face into the wind and hand launch your UAV Mapper as shown above. The toss should be a few degrees ab1 

Note: You can stop the motor and abort the takeoff by switching the flight mode switch to Stabilize. 

Creating aerial photography missions 

Aerial photography missions are trivial once you've mastered takeoff and landing missions. Here's a typical UAV Map 

1. Start Mission Planner, select Flight Plan, right-dick on the map and select Draw Polygon> Add Polygon Poin 

4. Select the Simple tab and set the following: 

o Camera: Canon SllO 

o Altitude: lOOm 

o Angle: This rotates the flight line. You want to fly cross wind. This site typically has a south wind, sot 

o Camera top facing forward: Check. 

o Flying Speed & Use flying speed: Leave unchecked. If checked it will override the default flying spee< 

o Add Takeoff and Land WP's: Check 

o Use RTL: If you need to Auto-land, then leave unchecked. If you prefer to have your UAV Mapper Ret 

complete and land manually, then check. 

5. Select the Grid Options tab and set the following 

o Overshoot [m]: to 80 on both ends. Your UAV Mapper can't turn tight enough to get back on the line 

o Start From: Set this to the furthest downwind corner of your survey area. You want your UAV Mappe 

while flying cross wind. This keeps the ground speed low and turns tighter. 

o Overlap[%] 80. This sets how frequently the shutter is triggered. 

o Side lap[%] 80. This sets how close the flight lines are. 

6. Select the Simple tab and then Accept. 
· 7 .. Modify takeoff and landing 

. . . ' 

o · Update TAKEOFF= parameters. Pitch angle should be 30 andAit must be.at least 100. 

: . . . . . ' . 

o You must have. an approach WAYPOINT1 35m Altitade, ~QO ft. (120m), down wind, from your I.AND 11. 

way points and_ use the Up Down arrows ,to move the w<:~ypoints. 

j>• 

1 

j 

o Note th:e waypoint command DO_SET_CAM...;.TRIGG_DIST. It is set to 21.9 in the image above. The Pi . . . 

every 21.9 meters. : 

8. 5~lect Write WPs to copy the mission t6 :your UAV Mapper~ 

I 

1 _..;-,;..,;--.-..•-·-~-.,..;,.,.;-.~~ ... -,.. aw"""*""''~--.··.,-·----~ ...... _.....;....;...._ . ..,~ '",· l 

tra~ing pictures I 

.i : . : . ' . ~ . . - . . : . . . . " . . . . ' . . ' 

\The UAV Mapper includes a Canon 5110 loaded with CHDK and KAP UAV Exposure Control Script on it's 50 card. The 

jtrigger the Canon 5110 through a special trigger cable. Do the following to take pictures with your .UAV Mapper: · .•. 

I 
1. Lock your SO card and insert it into the camera. 

2. Insert the camera trigger cable into the Mini USB port on the side of your camera. 

3. Turn your camera on. 

4. Press the blue Play button to load the KAP UAV Exposure Control Script. 

5. Half press the shutter to start the KAP UAV Exposure Control Script. 
6. Your camera is now waiting on a USB signal from your Pixhawk. It will send a signal while it's flying after the [ 

~ .·. -. - ~ :.. 'r. , ~ •; 

Q 

r-··· 

7. Always check your camera trigger system before you fly. Go to the FLIGHT DATA screen in Mission Planner. F 

NOW. If everything is setup correctly your Pixhawk will trigger the Canon camera to take a picture and is cap 
This product contains copyrighted software licensed under GNU General Public License v3 (GPLv3). Please see http:/11 

and o copy of the license. 

This product contains copyrighted software licensed under the BSD License. Please see !:11lns:Uqithub.com/PX4/FirmVI 

license. 

This product contains copyrighted Open Source Hardware licensed under the Creative Commons Attribution-Shore Ali, 

see https://qithub.com/PX4/Hardware for further information and o copy of the license.