Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 1 of 20

July 24, 2015 

U.S. Department of Transportation 

Docket Operations 

West Building Ground Floor, Room w12-140 

1200 New Jersey Ave., SE 

Washington, DC 20590 

RE: Petition for Section 333 Exemption Under FAA Modernization and Reform Act of 2012 

Petitioner : Valmie Resources, Inc. 

Petitioner’s sUAS(s) Models : Vertitek V1-X8a; Vertitek V2-H6a

Petitioner’s sUAS(s) Operations : Aerial Based Agricultural Applications; 

Aerial Based Search and Rescue Operations; 

Aerial Based Power-line Inspection; 

Aerial Based Pipe-line Inspection; 

Aerial Based Infrastructure Surveying; 

Aerial Photographic and Video Imaging 

Regulations Requiring Exemption : 14 CFR §§ 61.23(a) and (c); 

14 C.F.R. §§ 61.101(e)(4) and (5)

14 C.F.R. § 61.113(a); 

14 C.F.R. §61.315(a)

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)(1)

14 C.F.R. §91.405(a); 

14 C.F.R. §91.407(a)(1)

14 C.F.R. §§ 91.409(a)(1) and (2); and 

14 C.F.R. 91.417(a) and (b)

To whom it may concern, 

On behalf of Valmie Resources, Inc. (hereinafter referred to as “Valmie”), a Houston, Texas, 

corporation specializing in the use of Small Unmanned Aircraft Systems (sUAS) for aerial based 

agricultural applications, search and rescue operations, power-line inspections, pipe-line 

inspections, infrastructure surveying, and imaging, the undersigned counsel for Valmie hereby 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 2 of 20

applies for Section 333 exemption pursuant to the FAA Modernization and Reform Act of 2012, 

Public Law 112-95 (P.L. 112-95), and 14 C.F.R. Part 11. 

The Chief Executive Officer (CEO) and owner of Valmie, Gerald Brett Hammack, holds a private 

pilot, single engine, airplane certificate and rating. Consequently, Mr. Hammack understands the 

importance of safe flight operations and is acutely aware of the importance of complying with all 

Federal Aviation Regulations (F.A.R.s). As such, Valmie, through the careful oversight and 

tutelage of Mr. Hammack, will ensure that all sUAS flight operations are conducted in the safest 

possible manner. To that end, Valmie will comply with any flight or atmospheric condition 

limitations imposed upon the commercial operation of Valmie’s Vertitek V1-X8a and Vertitek 

V2-H6a. 

This petition will address the following topics, as they relate to Valmie’s commercial sUAS flight 

operations: Valmie’s sUAS models for which Valmie seeks exemption – a proprietary built sUAS 

called the Vertitek V1-X8a and Vertitek V2-H6a; Valmie’s sUAS flight operations and conditions; 

privacy concerns; public interest and safety concerns; and, the above specified F.A.R.s requiring 

exemption. Under Section 333(b)(1), Valmie’s petition will give the FAA good cause to issue a 

Certificate Of Waiver or Authorization by showing that the size, weight, speed, operational 

capacity, proximity to airports and populated areas, and operations within the Visual Line of Sight 

of the Pilot in Command and Visual Observer of Valmie’s sUAS models neither create a hazard 

to users of the National Airspace System or public nor pose a threat to national security. 

Additionally, this petition will prove that Valmie’s flight operations for the commercial usage of 

the Vertitek V1-X8a and Vertitek V2-H6a provides an equivalent level of safety when compared 

to the F.A.R.s requiring exemption. To that end, while the FAA has not granted a petition for 

Section 333 exemption as to a Vertitek V1-X8a and Vertitek V2-H6a, the FAA has already granted 

exemptions for similar commercial flight operations for the 3D Robotics X8-M and Tarot 810, as 

well as for sUAS models utilizing the Tarot 650 Sport frame and the Tarot 960 frame - sUAS 

models and frames most similar to Valmie’s Vertitek V1-X8a and Vertitek V2-H6a in size, speed, 

weight, and operational capacity. 

For example, in Exemption Number 11824, Regulatory Docket Number FAA-2015-1078, as well 

as Exemption Number 11617, Regulatory Docket Number FAA-2015-0549, and Exemption 

Number 11446, Regulatory Docket Number FAA-2014-0890, the FAA granted exemptions for the 

use of the 3D Robotics X8-M – a sUAS that is similar to the Vertitek V1-X8a. To that end, the 

FAA has granted exemptions to commercial sUAS operators of the Tarot 650 Sport Frame – the 

skeleton/backbone of the Vertitek V1-X8a’s design. In Exemption Number 11675, Regulatory 

Docket Number FAA-2015-0713, the FAA granted a Section 333 petition for the commercial 

operation of a Tarot 650 for aerial photography and videography. 

Likewise, in Exemption Number 11528, Regulatory Docket Number FAA-2015-0342, the FAA 

granted an exemption for the use of the Tarot 810 - a sUAS that is similar to the Vertitek V2-H6a. 

Like the Tarot 650 Sport Frame for the Vertitek V1-X8a, the FAA has also granted an exemption 

to commercial sUAS operators of the Tarot 960 Frame – the skeleton/backbone of the Vertitek 

V2-H6a. In Exemption Number 11221, Regulatory Docket Number FAA-2014-0557, the FAA 

granted a Section 333 petition for a Tarot 960 to conduct commercially operated aerial filming and 

inspections. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 3 of 20

Please refer to the “Table of Contents” beginning on page four (4) to assist your review of Valmie’s 

petition for Section 333 exemption. If we may provide additional insight or information regarding 

Valmie’s petition, please do not hesitate to contact The Ison Law Group at 863-712-9475 or 

Christopher@thepilotlawyer.com. 

 Sincerely, 

THE ISON LAW GROUP 

 Christopher Ison, Esq. 

Enclosures 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 4 of 20

TABLE OF CONTENTS

I. Glossary of Terms ................................................................................6 

II. Publishable Summary ................................................................................7 

III. Petitioner’s Contact Information ..............................................................8 

IV. Valmie Resources, Inc. Petition For Section3 333 Exemption ..........................8 

a. Valmie Resources, Inc. Overview .....................................................8 

b. The Vertitek V1-X8a Overview .....................................................8 

c. Vertitek V1-X8a Specifications .....................................................9 

d. Vertitek V2-H6a Overview ...................................................10 

e. Vertitek V2-H6a Specifications ...................................................10 

f. Vertitek V1-X8a and Vertitek V2-H6a Shared Componentry Overview ......11 

g. Vertitek V1-X8a and Vertitek V2-H6a Shared Componentry Specifications .....12 

V. Flight Conditions and Operating Procedures.....................................................13

VI. Privacy .......................................................................................16 

VII. Public Interest and Safety .....................................................................17 

VIII. Regulations from Which Exemption is Requested ..........................................17 

a. 14 CFR §§ 61.23(a) and (c): Medical Certificates Requirement and Duration ...............17 

b. 14 C.F.R. §§ 61.101(e)(4) and (5): Recreational Pilot Privileges and Limitations ...............18

c. 14 C.F.R. § 61.113(a): Private Pilot Privileges and Limitations: Pilot in Command ......18

d. 14 C.F.R. §61.315(a): What Are The Privileges and 

Limits of My Sport Pilot Certificate? ..........................................18

e. 14 C.F.R. § 91.7(a): Civil Aircraft Airworthiness ...................................................19 

f. 14 C.F.R. § 91.119(c): Minimum Safe Altitude: General ..........................................19

g. 14 C.F.R. §91.121: Altimeter Settings ............................................................19

h. 14 C.F.R. §91.151(a)(1): Fuel Requirements For Flight In VFR Conditions ...............20

i. 14 C.F.R. §91.405(a): Maintenance Required ...................................................20

j. 14 C.F.R. §91.407(a)(1): Operation After Maintenance, 

Preventative Maintenance, Rebuilding, Or Alteration ..................................20

k. 14 C.F.R. §§ 91.409(a)(1) and (2): Inspections ...................................................20

l. 14 C.F.R. 91.417(a) and (b): Maintenance Records ..........................................20 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 5 of 20

EXHIBIT LIST

Exhibit 1: Vertitek V1-X8a Specification List (2 pages) ..........................................21 

Exhibit 2: Vertitek V2-H6a Specification List (2 pages) ...........................................23 

Exhibit 3: FrSky Taranis X9D+ Manual (2 pages) ...................................................25 

Exhibit 4: FrSky X8R Manual (1 page) ............................................................27 

Exhibit 5: 3DR Radio 915 MHz V2 Quick Start Guide (4 pages) .................................28

Exhibit 6: 3DR Radio 915 MHz V2 Manual (12 pages) ..........................................32 

Exhibit 7: Mission Planner Autopilot Manual (2 pages) ...........................................44

Exhibit 8: Pixhawk Autopilot Manual (13 pages) .....................................................46 
Petition for Section 333 Exemption

Valmie Resources, Inc.

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GLOSSARY OF TERMS 

Aircraft: any contrivance invented, used, or designed to navigate, or fly in, the air (Title 49, United 

States Code (49 USC) § 40102). 

National Airspace System (NAS): the common network of U.S. airspace; air navigation facilities, 

equipment and services, airports or landing areas; aeronautical charts, information and services; 

rules, regulations and procedures, technical information, and manpower and material. 

Operational Control: with respect to a flight, means the exercise of authority over initiating, 

conducting or terminating a flight (14 CFR § 1.1). 

Pilot in Command (PIC): the person who has final authority and responsibility for the operation 

and safety of the flight; has been designated as PIC before or during the flight; and holds the 

appropriate category class and type-rating, if appropriate, for the conduct of the flight (14 CFR § 

1.1). 

Small Unmanned Aircraft System (sUAS): an unmanned aircraft and associated elements, 

including communication links and the components that control the unmanned aircraft, that are 

required for the pilot in command to operate safely and efficiently in the national airspace system 

(P.L. 112-95, Section 331), weighing less than 55 pounds, including payload. 

UAS Certificate of Waiver or Authorization (COA): an authorization issued by the Air Traffic 

Organization to an operator for a specific unmanned aircraft activity. 

Visual Line of Sight (VLOS): unaided (corrective lenses and/or sunglasses excepted) visual

contact between a pilot in command and an unmanned aircraft sufficient to maintain safe 

operational control of the aircraft, know its location, and be able to scan the airspace in which it is 

operating to see and avoid other air traffic or objects aloft or on the ground. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

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PUBLISHABLE SUMMARY

Pursuant to 14 C.F.R §11.81(f), should the FAA require a publishable summary for the Federal 

Register, Valmie Resources, Inc. (Valmie), submits the following information: 

 

Valmie seeks exemption from the following Federal Aviation Regulations (F.A.R.s) for the 

commercial operation of Small Unmanned Aircraft Systems (sUAS): 

14 CFR §§ 61.23(a) and (c); 14 C.F.R. §§ 61.101(e)(4) and (5); 14 C.F.R. § 

61.113(a); 14 C.F.R. §61.315(a); 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)(1); 14 C.F.R. §91.405(a); 14 C.F.R. 

§91.407(a)(1); 14 C.F.R. §§ 91.409(a)(1) and (2); and 14 C.F.R. 91.417(a) and (b). 

Valmie seeks exemption from the above listed F.A.R.s for the purpose of commercially operating 

the Vertitek V1-X8a and Vertitek V2-H6a – sUAS models assembled from commercially 

available, “off-the-shelf” componentry. Valmie seeks to commercially operate these sUAS models 

for aerial based agricultural applications, search and rescue operations, power-line inspections, 

pipe-line inspections, infrastructure surveying, and imaging in an effort to increase the 

effectiveness of data collection, storage, and analysis. 

The Vertitek V1-X8a is comparable in size, weight, speed and operational capacity to the 3D 

Robotics X8-M sUAS and sUAS models that utilize the Tarot 650 Sport frame. The Vertitek V2-

H6a, likewise, is comparable in size, weight, speed and operational capacity to the Tarot 810 and 

sUAS models that utilize the Tarot 960 frame. To that end, while the FAA has not granted a petition 

for Section 333 exemption as to a Vertitek V1-X8a or a Vertitek V2-H6a, the FAA has already 

granted exemptions for commercial sUAS operators of the 3D Robotics X8-M and Tarot 810, as 

well as commercial operators of sUAS models utilizing the Tarot 650 Sport frame and Tarot 960 

frame. 

For example, in Exemption Number 11824, Regulatory Docket Number FAA-2015-1078, as well 

as Exemption Number 11617, Regulatory Docket Number FAA-2015-0549, and Exemption 

Number 11446, Regulatory Docket Number FAA-2014-0890, the FAA granted exemptions for the 

use of the 3D Robotics X8-M. To that end, the FAA has granted an exemption to commercial 

sUAS operators of the Tarot 650 Sport Frame – the skeleton/backbone of the Vertitek V1-X8a’s 

design. In Exemption Number 11675, Regulatory Docket Number FAA-2015-0713, the FAA 

granted a Section 333 petition to the commercial operator of a Tarot 650 for aerial photography 

and videography. 

Likewise, in Exemption Number 11528, Regulatory Docket Number FAA-2015-0342, the FAA 

granted an exemption for the use of the Tarot. Additionally, the FAA has also granted an exemption 

to commercial sUAS operators of the Tarot 960 Frame – the skeleton/backbone of the Vertitek 

V2-H6a. In Exemption Number 11221, Regulatory Docket Number FAA-2014-0557, the FAA 

granted a Section 333 petition to the commercial operator of a Tarot 960 for aerial filming and 

inspections. 

Under Section 333(b)(1) of the FAA Modernization and Reform Act of 2012, Valmie’s petition 

will give the FAA good cause to issue a Certificate Of Authorization by showing that the size, 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 8 of 20

weight, speed, operational capacity, proximity to airports and populated areas, and operations 

within the Visual Line of Sight of the Pilot in Command and Visual Observer of Valmie’s Vertitek 

V1-X8a and Vertitek V2-H6a do not create a hazard to users of the National Airspace System or 

public or pose a threat to national security. To that end, Valmie seeks exemption from the above 

specified F.A.R.s as Valmie’s proposed flight operations provide an equivalent level of safety 

when compared to the F.A.R.s to be exempted. Valmie will adhere to any flight or atmospheric 

condition limitation imposed by the FAA. 

PETITIONER’S CONTACT INFORMATION 

Petitioner: Counsel for Petitioner: 

Gerald Brett Hammack, CEO The Ison Law Group 

Valmie Resources, Inc. 2073 US Hwy 92 West, Suite 104 

1001 South Dairy Ashford, Suite 100 Winter Haven, FL 33881 

Houston, TX 77077 Phone: 863-712-9475 

Phone: 713-595-6675 Email: Christopher@thepilotlawyer.com 

VALMIE RESOURCES, INC., PETITION 

FOR SECTION 333 EXEMPTION 

Valmie Resources, Inc., (hereinafter “Valmie”) is a Houston, Texas, based corporation that is 

committed to pursuing opportunities for the commercialization of leading-edge products and 

services with a focus on making a significant impact within the four key technology “megasectors:” software, hardware, networking, and semi-conductors. Valmie identifies the utilization 

of sUAS models as an opportunity to provide customized solutions for aerial based agricultural 

applications, search and rescue operations, power-line inspections, pipe-line inspections, 

infrastructure surveying, and imagery while simplifying and increasing the effectiveness of data 

collection, storage, and analysis within these areas of operation. 

As such, Valmie would like an exemption from the following Federal Aviation Regulations 

(F.A.R.s) to commercially operate the Vertitek V1-X8a and Vertitek V2-H6a – sUAS models 

assembled from commercially available, “off-the-shelf” componentry: 14 CFR §§ 61.23(a) and 

(c); 14 C.F.R. §§ 61.101(e)(4) and (5); 14 C.F.R. § 61.113(a); 14 C.F.R. §61.315(a); 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)(1); 14 C.F.R. §91.405(a); 

14 C.F.R. §91.407(a)(1); 14 C.F.R. §§ 91.409(a)(1) and (2); and 14 C.F.R. 91.417(a) and (b). 

Vertitek V1-X8a 

Overview 

The Vertitek V1-X8a is a quad-boom, eight (8) motor sUAS, capable of providing hover flight in 

both the vertical and horizontal planes. The Vertitek V1-X8a consists of commercially available, 

“off the shelf” componentry, combined to create the Vertitek V1-X8a. In other words, the 

uniqueness of the Vertitek V1-X8a lies in the assembly of these common, commercially available, 

“off-the-shelf” components, not the components themselves. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 9 of 20

While Valmie’s Vertitek V1-X8a is a propriety built sUAS, the Vertitek V1-X8a is comparable in 

size, weight, speed, and operational capacity to the 3D Robotics X8-M and sUAS models utilizing 

a Tarot 650 Sport frame. To that end, while the FAA has not granted a petition for Section 333 

exemption as to a Vertitek V1-X8a, the FAA has already granted exemptions for similar 

commercial operators of the 3D Robotics X8-M in Exemption Number 11824, Regulatory Docket 

Number FAA-2015-1078, as well as Exemption Number 11617, Regulatory Docket Number FAA2015-0549, and Exemption Number 11446, Regulatory Docket Number FAA-2014-0890. 

Additionally, the FAA has also granted an exemption to the commercial sUAS operator of a 

Tarot 650 Sport frame – the skeleton/backbone of the Vertitek V1-X8a’s design. In Exemption 

Number 11675, Regulatory Docket Number FAA-2015-0713, the FAA granted a Section 333 

petition for the commercial operation of a sUAS with a Tarot 650 frame for aerial photography 

and videography. 

Vertitek V1-X8a 

Specifications 

The following minimum-equipment-list illustrates the bare-essential componentry necessary for 

the Vertitek V1-X8a to maintain stable and prolonged flight operations: 

 FR-Sky Taranis X9D Plus Transmitter;

 Fr-Sky X8R Receiver;

 Tarot 650 Sport Frame;

o Quad Main Plates;

o 16mm Clamp Style Motor Mounts (top/bottom motor plates);

o Carbon Fiber Arms 16mm x 330mm;

 Brushless 5010/14 360 KV Motors, or equivalent;

 Carbon Fiber 17 x 5.5. Propellers (4xCW, 4xCCW), or equivalent;

 LiPo 10,000 mAh Battery or LiPo 12,000 mAh Battery;

 3D Robotics Pixhawk Flight Controller;

 3D Robotics UBLOX GPS; and

 3D Robotics 915 MHz Telemetry Radio.

The following optional equipment may be used in connection with the operation of the Vertitek 

V1-X8a: 

 Thermal Imaging Camera;

 Multiple Spectrum Camera;

 Live High Definition Video Camera;

 Gimbals; and/or

 Sonar/Lidar instruments.
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 10 of 20

sUAS Performance: 

Empty Weight (no battery/camera/sensor payload): 4.0625 lbs 

Useful Payload: 5.9375 lbs 

Gross Weight: 10.0000 lbs 

Maximum Airspeed: 40 kts (battery only payload) 

15 kts (gross weight) 

Total Flight Time (gross weight): 26 minutes w/12,000mAh Battery 

Vertitek V2-H6a 

Overview 

The Vertitek V2-H6a is a hex-boom, six (6) motor sUAS, capable of providing hover flight in both 

the vertical and horizontal planes. The Vertitek V2-H6a consists of commercially available, “off 

the shelf” componentry, combined to create the Vertitek V2-H6a. In other words, just like the 

Vertitek V1-X8a, the uniqueness of the Vertitek V2-H6a lies in the assembly of these common, 

commercially available, “off-the-shelf” components, not the components themselves. 

While Valmie’s Vertitek V2-H6a is a propriety built sUAS, the Vertitek V2-H6a is comparable in 

size, weight, speed, and operational capacity to the Tarot 810 and sUAS models utilizing a Tarot 

960 frame. To that end, while the FAA has not granted a petition for Section 333 exemption as to 

a Vertitek V2-H6a, the FAA has already granted an exemption to a commercial operator of a Tarot 

810 in Exemption Number 11528, Regulatory Docket Number FAA-2015-0342. Likewise, the 

FAA has also granted an exemption to the commercial sUAS operator of a Tarot 960 Frame – the 

skeleton/backbone of the Vertitek V2-H6a’s design. In Exemption Number 11221, Regulatory 

Docket Number FAA-2014-0557, the FAA granted a Section 333 petition for a Tarot 960 to 

conduct aerial filming and inspections. 

Vertitek V2-H6a 

Specifications 

The following minimum-equipment-list illustrates the bare essential componentry necessary for 

the Vertitek V2-H6a to maintain stable and prolonged flight operations: 

 FR-Sky Taranis X9D Plus Transmitter; 

 Fr-Sky X8R Receiver; 

 Tarot 960 Frame; 

o Hex Frame Main Plates; 

o 25mm Clamp Style Motor Mounts; 

o Carbon Fiber Arms 25mm x 423.5mm; 

 Brushless 5008 330 KV Motors, or equivalent; 

 Carbon Fiber 17 x 5.5. Propellers (3xCW, 3CCW), or equivalent; 

 LiPo 10,000 mAh Battery or LiPo 12,000 mAh Battery; 

 3D Robotics Pixhawk Flight Controller; 

 3D Robotics UBLOX GPS; and 

 3D Robotics 915 MHz Telemetry Radio. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 11 of 20

The following optional equipment may be used in connection with the operation of the Vertitek 

V2-H6a: 

 Thermal Imaging Camera;

 Multiple Spectrum Camera;

 Live High Definition Video Camera;

 Gimbals; and/or

 Sonar/Lidar instruments.

sUAS Performance: 

Empty Weight (no battery/camera/sensor payload): 4.4000 lbs 

Useful Payload: 8.6000 lbs 

Gross Weight: 13.0000 lbs 

Maximum Airspeed: 38 kts (battery only payload) 

13 kts (gross weight) 

Total Flight Time (gross weight): 26 minutes w/12,000mAh Battery 

Vertitek V1-X8a and Vertitek V2-H6a 

Shared Componentry Overview 

Through the incorporation and use of the 3D Robotics Pixhawk Autopilot and uBlox GPS, the 

PIC of the Vertitek V1-X8a and Vertitek V2-H6a can operate these sUAS models with Mission 

Planner, an autopilot software suite designed for sUAS models. As such, Mission Planner allows 

a sUAS PIC to operate via a predetermined flight route while maintaining VLOS flight operations. 

A pre-programed flight route reduces the PIC’s work-load, allowing the PIC to focus on safe flight 

operations, such as remaining-battery levels, altitude, and obstructions, thereby reducing the risk 

of crashing, damaging property, or injuring people. 

Mission Planner provides excellent situational awareness for the sUAS PIC via similar flight data 

and information one would expect to find in the cockpit of a traditional fixed wing or rotorcraft 

aircraft, such as: artificial horizon, compass, altimeter, ground speed indicator, vertical speed 

indicators, yaw (degrees), and distance to waypoint (meters). Additionally, Mission Planner allows 

the PIC of a Vertitek V1-X8a or Vertitek V2-H6a the flexibility to operate via point-and-click 

waypoint entries on a laptop, working in tandem with Google Maps, Bing, open street maps, or a 

custom Web Map Service. These features allow a sUAS PIC the ability to access multiple 

command modes, further enhancing safe flight operations, such as: Acro, Stabilize, Loiter, Return 

to Launchpoint, Land, Simple, Guided, Position, Circle, and Auto (which runs fully scripted 

missions using GPS waypoints). Nevertheless, the Vertitek V1-X8a and Vertitek V2-H6a allow 

the PIC to resume manual control of the sUAS model during a pre-programmed flight, should the 

need arise. 

Since Valmie’s primary objective with each commercial sUAS flight is the safe return of the sUAS 

without injury to property or person, the Vertitek V1-X8a and Vertitek V2-H6a incorporate, 

through both the use of Mission Planner and the Fr-Sky Taranis X9D, failsafe programming 

options which, in the event of lost control signal or low battery, will either assist the PIC’s 

situational awareness or assist the PIC’s maneuverability of the sUAS. For example, the Fr-Sky 

Taranis X9D provides four failsafe modes: No Pulse; Hold; Custom; and Receiver. These failsafe 
Petition for Section 333 Exemption

Valmie Resources, Inc.

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modes enable the safe return and/or landing of the sUAS in the case of lost signal connectivity 

between the transmitter and the receiver or low batteries. As such, these systems will enable the 

PIC to make informed decisions, increasing the safety of each flight. 

Vertitek V1-X8a and Vertitek V2-H6a 

Shared Componentry Specifications 

LiPo 12000mah Battery 

Minimum Capacity: 1200mAh 

Configuration: 6S1P / 22.2V / 6cell 

Constant Discharge: 10C 

Peak Discharge (10 sec): 20C 

Approximate Dimensions: Length: 180 mm 

Width: 70 mm 

Height: 55 mm 

3DR U-Blox GPS+Compass (NEO-7 Series Module) 

Battery: Rechargeable 3V lithium backup battery 

Receiver Type: GPS L1 C/A, GLONASS L1 FDMA 

QZSS L1 C/A 

Galileo E1B/C 

SBAS: WASS, EGNOS, MSAS 

Navigation Update Rate: ≤ 10 Hz 

Accuracy GPS/GLONASS: Position 2.5 m CEP/4.0 m 

SBAS 2.0 m CEP/n.a. 

Acquisition GPS/GLONASS: Cold Starts: 29 s / 30 s 

Aided Starts: 5 s / n.a. 

Reacquisition: 1 s / 3 s 

Sensitivity GPS/GLONASS: Tracking: -162 dBm /-158 dBm 

Cold Starts: -148 dBm / -140 dBm 

Warm Starts: -148 dBm / -145 dBm 

Oscillator: TCXO (NEO-7N), crystal (NEO-7M) 

RTC Crystal: Built-in 

Anti-Jamming: Active CW detection and removal 

Approximate Dimensions: Width: 38 mm 

Height: 8.8 mm 

Length: 38 mm 

3DR Radio v2 915Mhz

Range: 500 meters 

Receiver Sensitivity: -121 dBm 

Transmit Power: ≤ 20 dBm (100mW) 

Air Data Rates: ≤ 250 kbps 

Features: MAVLink protocol framing and status reporting 

Frequency hopping spread spectrum (FHSS) 

Adaptive time division multiplexing (TDM) 

Built-in error correcting code 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 13 of 20

 AT commands for radio configuration 

 RT commands for remote radio configuration 

FR-Sky Taranis X9D Plus Transmitter

Operating Voltage Range: 6 ~ 15V (2S, 3S Lipos are acceptable) 

Operating Current: 260mA maximum 

Features: Quad Ball Bearing Gimbals 

 Receiver Match 

 Audio Speech Outputs 

 Real-time Flight Data Logging 

 Receiver Signal Strength Indicator Alerts 

 Super Low Latency 

 Vibration Alerts 

Failsafe Modes: No Pulse 

 Hold 

 Custom 

 Receiver 

 

3D Robotics Pixhawk Autopilot 

Processor: 32-bit ARM Cortex M4 core with FPU 

 168 Mhz/256 KB Ram/2 MB Flash 

 32-bit failsafe co-processor 

Sensors: ST Micro 16-bit gyroscope 

 ST Micro 14-bit accelerometer/magnetometer 

 MEAS barometer 

 MPU6000 accelerometer/magnetometer 

Power: Ideal diode controller with automatic failover 

 Servo rail high-power (7V) and high current ready 

 All peripheral outputs over-current protected 

 All inputs ESC protected 

Approximate Dimensions: Width: 50 mm (2.0”) 

 Height: 15.5 mm (.6”) 

 Length: 81.5 mm (3.2”) 

 

For further information regarding the components comprising the assembly of the Vertitek V1-

X8a and Vertitek V2-H6a, please refer to the attached exhibits.

FLIGHT CONDITIONS AND OPERATING PROCEDURES 

Valmie’s primary objective with every flight is the safe return of the Vertitek V1-X8a and Vertitek 

V2-H6a without injury to property or person. In order to obtain this desired objective, Valmie will 

abide by the following flight and atmospheric conditions limitations when performing flight 

operations with either the Vertitek V1-X8a or Vertitek V2-H6a: 

1. Valmie will not operate the sUAS models when weighing more than 55 pounds, 

including payload. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 14 of 20

2. Valmie will not operate the sUAS models at a speed exceeding 87 knots (100 miles 

per hour). Valmie will use either groundspeed or calibrated airspeed to determine 

compliance with the 87 knot speed restriction. 

3. Valmie will not operate the sUAS models at an altitude of more than 400 feet above 

ground level (AGL). Valmie will monitor altitude in feet AGL via GPS technology 

and monitoring. 

4. Valmie will only operate the sUAS models within VLOS of the PIC at all times. 

Valmie will require the PIC to be able to use human vision unaided by any device 

other than corrective lenses, as specified on the PIC’s FAA-issued airman medical 

certificate or U.S. driver’s license. 

5. Valmie requires the utilization of a visual observer (VO) on all commercial sUAS 

flights. The sUAS models will be operated within VLOS of the PIC and VO at all 

times. The VO may be used to satisfy the VLOS requirement as long as the PIC 

always maintains VLOS capability. Valmie requires that the VO and PIC be able 

to communicate verbally at all times. Valmie does not permit electronic messaging 

or texting during flight operations. Valmie requires the sUAS PIC to be designated 

before the flight and does not allow transfer of his or her designation during the 

flight. The PIC must ensure that the VO can perform the duties required of the VO. 

6. Valmie requires that all operating documents (defined as the granted exemption and 

all documents needed to operate the UAS model and conduct its operations in 

accordance with all grants conditions and limitations) must be accessible during 

sUAS operations and made available to the Administrator upon reasonable request. 

7. Valmie will require a functional test should any sUAS model undergo maintenance 

or alterations that affect that sUAS model’s operation or flight characteristics, e.g., 

replacement of a flight critical component, must undergo a functional test flight 

prior to conducting further operations under this exemption. Valmie requires that 

all function flights be conducted by a PIC with a VO and remain at least 500 feet 

from other people. Valmie further requires that the functional test flight be 

conducted in such a manner so as to not pose an undue hazard to persons and 

property. 

8. Valmie will be responsible for maintaining and inspecting the sUAS models to 

ensure that the sUAS model is in a condition for safe operation. 

9. Valmie requires that, prior to each flight, the PIC conduct a pre-flight inspection 

and determine whether the sUAS models are in a condition for safe flight. Valmie 

requires that the pre-flight inspection must account for all potential discrepancies, 

e.g., inoperable components, items, or equipment. Should the inspection reveal a 

condition that affects the safe operation of the sUAS model, Valmie prohibits the 

aircraft from operating until the necessary maintenance has been performed and the 

sUAS is found to be in a condition for safe flight. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 15 of 20

10. Valmie requires compliance with the component manufacturer’s maintenance, 

overhaul, replacement, inspection, and life limit requirements for the components 

that combine to assemble the sUAS models. 

11. Valmie requires compliance with all component manufacture’s safety bulletins for 

the components that combine to assemble the sUAS models. 

12. Valmie requires all sUAS model PICs to hold either an airline transport, 

commercial, private, recreational, or sport pilot certificate. Further, Valmie requires 

the PIC to 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 CFR § 61.56 in an aircraft in which the PIC is rated 

on his or her pilot certificate. 

13. Valmie prohibits any PIC to operate the sUAS models unless the PIC demonstrates 

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

sUAS will be operated under this petition for exemption, including evasive and 

emergency maneuvers and maintaining appropriate distances from persons, vessels, 

vehicles and structures. To that end, Valmie requires the PIC’s qualification flight 

hours and currency to be logged in a manner consistent with 14 CFR § 61.51(b). 

14. Valmie prohibits flight operations of the sUAS models during night, as defined in 

14 CFR § 1.1. All flight operations will be conducted under visual meteorological 

conditions (VMC). Valmie will not allow the sUAS models to be flown during 

special visual flight rules (SVFR). 

15. Valmie will not operate the sUAS models within 5 nautical miles of an airport 

reference point (ARP) as denoted in the current FAA Airport/Facility Directory 

(AFD) or for airports not denoted with an ARP, the center of the airport symbol as 

denoted on the current FAA-published aeronautical chart, unless a letter of 

agreement with that airport’s management is obtained or otherwise permitted by a 

COA issued to the exemption holder. Valmie will make the letter of agreement with 

the airport management available to the Administrator or any law enforcement 

official upon request. 

16. Valmie will operate the sUAS models at least 500 feet below and/or no more than 

2,000 feet horizontally from a cloud. Valmie will not operate the sUAS models 

when visibility is less than 3 statute miles. 

17. Should the sUAS models lose communications or lose its GPS signal, Valmie 

requires the sUAS model to return to a pre-determined location within the private 

or controlled-access property. 

18. Valmie requires the PIC of any sUAS model to abort the flight in the event of 

unpredicted obstacles or emergencies. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 16 of 20

19. Valmie prohibits the PIC of any sUAS model from beginning a flight unless 

(considering wind and forecast weather conditions) there is enough available power 

for the sUAS model to conduct the intended operation and to operate after that for 

at least 5 minutes or with the reserve power recommended by component 

manufacturer if greater. 

20. Valmie requires that all documents used to ensure safe operation and flight of the 

sUAS models and any documents required under 14 CFR §§ 91.9 and 91.203 to be 

available to the PIC at the Ground Control Station of the sUAS model any time the 

aircraft are operating. Valmie will make these documents available to the 

Administrator or any law enforcement official upon reasonable request. 

21. Valmie requires that during all flights, the sUAS models PIC remain clear and give 

way to all manned aviation operations and activities at all times. 

22. Valmie prohibits the PIC of any sUAS models from operating the sUAS models 

from any moving device or vehicle. 

23. Valmie requires all flight operations of all sUAS models to be conducted at least 

500 feet from all nonparticipating persons, vessels, vehicles, and structures unless: 

a. Barriers or structures are present that sufficiently protect nonparticipating 

persons from the sUAS and/or debris in the event of an accident. Valmie 

will ensure that nonparticipating persons remain under such protection. If a 

situation arises where nonparticipating persons leave such protection and 

are within 500 feet of the sUAS, Valmie requires flight operations to cease 

immediately in a manner ensuring the safety of nonparticipating persons; 

and 

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

permission for operating closer to those objects and the PIC has made a 

safety assessment of the risk of operating closer to those objects and 

determined that it does not present an undue hazard. 

24. Valmie will operate all sUAS models flights over private or controlled-access 

property with permission from the property owner/controller or authorized 

representative. Valmie will obtain permission from the property owner/controller 

or authorized representative prior to each flight to be conducted. 

PRIVACY

Valmie’s use of the Vertitek V1-X8a and Vertitek V2-H6a for aerial based agricultural 

applications, as well as search and rescue operations, will not implicate any privacy concerns. 

Since Valmie will only commercially operate the sUAS models at the request of the property 

and/or business owner(s), Valmie will have the express consent and permission of the property 

and/or business owner(s) prior to flying over private property. The use of the Vertitek V1-X8a and 

Vertitek V2-H6a for aerial based agricultural applications, search and rescue operations, power-
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 17 of 20

line inspection, pipe-line inspection, infrastructure surveying, and imagery poses no greater 

privacy concerns than the use of traditional fixed wing or rotorcraft aircraft for similar commercial 

operations. Should Valmie’s commercial sUAS activity require aerial based photographic and 

video imagery, images taken will be of individuals who have consented to being 

photographed/filmed or otherwise have agreed to be in the area where aerial photographic or video 

imagery will take place. 

PUBLIC INTEREST AND SAFETY

Given the design, size, weight, speed, and operational capacity of the Vertitek V1-X8a and Vertitek 

V2-H6a, Valmie’s requested exemption from the above specified F.A.R.s will neither adversely 

affect the public’s safety nor create a hazard to users of the National Airspace System (NAS) or 

pose a threat to national security. Moreover, Valmie’s use of the Vertitek V1-X8a and Vertitek 

V2-H6a for aerial based agricultural applications, search and rescue operations, power-line 

inspections, pipe-line inspections, infrastructure surveying, and imagery will replace the need for 

fixed wing or rotorcraft aircraft within these areas of service. 

By replacing fixed wing or rotorcraft aircraft with sUAS models, the public will benefit in several 

ways. Most notably, the use of these sUAS models provides significant reductions in the risk of 

injury to property or person, should the sUAS require an emergency landing. The Vertitek V1-X8a 

and Vertitek V2-H6a are lightweight, powered by batteries, and carry no passengers. By 

comparison, fixed wing or rotorcraft aircraft, which weigh thousands of pounds, are powered by 

flammable fuels, and carry passengers, have been known to cause serious injury or death to 

passengers or bystanders. 

The use of Valmie’s Vertitek V1-X8a and Vertitek V2-H6a also benefits the public from an 

environmental and ecological perspective since these sUAS models do not run on fossil fuels. 

Since these sUAS models are battery powered, the use of the Vertitek V1-X8a and Vertitek V2-

H6a over the traditional fixed wing or rotorcraft aircraft will be more environmentally and 

ecologically friendly. In addition to the non-use of flammable fuels, given the extremely light 

weight of these sUAS models, should an emergency result in a forced landing, injury to property 

or persons would be negligible compared to the catastrophic injury to property or persons that 

would result in an emergency landing of a traditional fixed wing or rotorcraft aircraft. 

Apart from the added safety benefits of sUAS flight operations, the use of the Vertitek V1-X8a 

and Vertitek V2-H6a for the above noted aerial based applications creates new economic 

opportunities that could fuel the continued growth of aviation and aviation related interests. 

Consequently, the public will benefit from the use of sUAS models for commercial purposes as 

companies like Valmie will provide new jobs and economic opportunities, fueling innovation and 

creativity. 

REGULATIONS FROM WHICH EXEMPTION IS REQUESTED 

14 CFR §§ 61.23(a) and (c): Medical Certificates Requirement and Duration 

Valmie requests exemption from 14 CFR §§ 61.23(a) and (c) which provides for certain flight 

operations requiring medical certificates. Valmie’s petition for exemption provides an equivalent 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 18 of 20

level of safety in that Valmie would require a Vertitek V1-X8a or Vertitek V2-H6a PIC to hold 

either a current medical certificate, of any class, or a valid U.S. Driver’s License. Valmie’s petition 

for exemption provides an equivalent level of safety as provided in 14 C.F.R. §§61.23(a) and (c). 

14 C.F.R. §§ 61.101(e)(4) and (5): Recreational Pilot Privileges and Limitations; 14 C.F.R. § 

61.113(a): Private Pilot Privileges and Limitations: Pilot in Command; and 14 C.F.R. 

§61.315(a): What Are The Privileges and Limits of My Sport Pilot Certificate?

Valmie requests exemption from 14 C.F.R. §§ 61.101(e)(4) and (5) which prohibits recreational 

pilots from receiving compensation for hire or providing flight services in furtherance of a 

business, respectively. In addition, Valmie requests exemption from 14 C.F.R. §61.113(a), which 

prohibits a certificated private pilot from receiving compensation or flying for hire when acting as 

PIC; and from 14 C.F.R. §61.315(a), which provides the holder of a sport pilot certificate may 

only act as pilot in command of a light-sport aircraft. 

Valmie’s petition for exemption provides an equivalent level of safety in that Valmie requires the 

Vertitek V1-X8a or Vertitek V2-H6a PIC, at the bare minimum, to hold the privileges of a sport 

pilot certificate under 14 C.F.R. §61 Subpart J, hold either a medical certificate or valid U.S. 

Driver’s License, and to demonstrate proficiency in the PIC’s ability to safely operate the Vertitek 

V1-X8a in a manner consistent with how the sUAS will be operated under this petition for 

exemption.

Distinct comparisons between the commercial activities of Valmie and other businesses operating 

traditional fixed wing or rotorcraft aircraft expose the unnecessary limitations placed upon sport, 

recreational and private certificated pilots when considering PIC privileges of commercial sUAS 

flight operations. Whereas requiring pilots of traditional fixed wing and rotorcraft aircraft to hold 

commercial and Airline Transport Pilot (ATP) ratings ensures that the pilots possess the necessary 

skills, training and experience to safely transport persons and/or cargo from the point of departure 

to the intended point of destination, the same correlation for sUAS pilots and should not apply to 

the sUAS flight operations of Valmie. 

In the case of Valmie’s sUAS flight operations, no persons or third-party cargo will be carried by 

the Vertitek V1-X8a or Vertitek V2-H6a during Valmie’s aerial based commercial operations. 

Unlike traditional fixed wing or rotorcraft aircraft, which must traverse over a greater distance, 

greater amount of property, and a greater amount of people in order to get from the point of 

departure to the intended point of destination, Valmie’s sUAS will only fly over property 

authorized by Valmie’s clients. In other words, the Vertitek V1-X8a or Vertitek V2-H6a will not 

have to originate flight from a different location and traverse over the properties of disinterested 

parties in order to fulfill the purpose of Valmie’s flight operations. As such, the risk of injury to 

disinterested parties is substantially decreased by the use of a sUAS for aerial based commercial 

operations. 

Consequently, Valmie’s requirement that the Vertitek V1-X8a or Vertitek V2-H6a PIC hold, at 

least, a sport pilot certificate provides an equivalent level of safety to the requirement that a 

commercial or ATP rated pilot transport persons and/or cargo for hire in manned aircraft because 

the holder of a sport pilot certificate will have the necessary understanding of aeronautical 

principals, regulations and airspaces to effectuate a safe commercial sUAS flight. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 19 of 20

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

Valmie requests an exemption from 14 C.F.R. §91.7(a) which prohibits the operation of civil 

aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for 

Valmie’s Vertitek V1-X8a or Vertitek V2-H6a models, no standard will exist for determining 

airworthiness. In any event, Valmie’s proposed Flight Conditions and Operating Procedure will 

ensure an equivalent level of safety with 14 C.F.R. §91.7(a). 

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

Valmie requests an exemption from 14 C.F.R §91.119(c) which provides that except when 

necessary for takeoff or landing, no person may operate an aircraft below an altitude of 500 feet 

above the surface. Furthermore, this section provides that an aircraft may not be operated closer 

than 500 feet to any person, vessel, vehicle, or structure. Valmie’s petition requests that the 

Vertitek V1-X8a or Vertitek V2-H6a be flown at an altitude no higher than 400 feet AGL and, 

when complying with the conditions set forth in §23(b) of Valmie’s Flight Conditions and 

Operating Procedures, at distances closer than 500 feet from any person, vessel, vehicle, or 

structure. 

The requirement that the Vertitek V1-X8a or Vertitek V2-H6a maintain 400 feet or less AGL helps 

ensure that signal connectivity between the transmitter and receiver will not be lost. In addition, 

this height restriction ensures that the PIC will be able to maintain VLOS while simultaneously 

limiting the possibility of the sUAS models’ interference with other NAS traffic. 

Traditional principles requiring a 500 foot AGL minimum for fixed-wing or rotorcraft aircraft 

stemmed from a desire to protect the public should the need for a forced landing arise due to an 

unforeseen emergency situation or loss of power. These same concerns are not present with the 

Vertitek V1-X8a and Vertitek V2-H6a. Valmie’s sUAS models are extremely lightweight and 

small. Any injury to property or person would be negligible when compared to the catastrophic 

damage that a fixed wing or rotorcraft aircraft would inflict due to a forced landing. Consequently, 

Valmie’s Flight Conditions and Operating Procedures provide for an equivalent level of safety 

when compared to 14 C.F.R §91.119(c). 

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

Valmie requests exemption from 14 C.F.R. §91.121 which provides guidelines for the use of 

altimeter settings while operating an aircraft. Valmie’s petition for exemption provides an 

equivalent level of safety such that the Vertitek V1-X8a or Vertitek V2-H6a PIC will be able to 

determine the AGL height of the sUAS model due to GPS technology. The AGL height of the 

sUAS will be displayed for the PIC during all flight operations. As such, the PIC will be able to 

maintain the requirement that the Vertitek V1-X8a or Vertitek V2-H6a fly no higher than 400 feet 

AGL during all flight operations. 
Petition for Section 333 Exemption

Valmie Resources, Inc.

Page 20 of 20

14 C.F.R. §91.151(a)(1): Fuel Requirements For Flight In VFR Conditions 

Valmie requests exemption from 14 C.F.R. §91.151(a)(1) which provides that no person may begin 

a flight in an airplane under VFR conditions with less than 30 minutes of reserve fuel. Valmie’s 

petition for exemption provides an equivalent level of safety due to Valmie’s prohibition against 

the PIC from beginning a flight unless (considering wind and forecast weather conditions) there is 

enough available power for the sUAS model to conduct the intended operation and to operate after 

that for at least 5 minutes or with the reserve power recommended by the manufacturer if greater. 

Given the design and technology of the Vertitek V1-X8a and Vertitek V2-H6a, Valmie’s PIC will 

have access to all relevant information concerning the sUAS model’s battery life. The PIC will be 

able to make an accurate determination as to whether the PIC can comply with Valmie’s “fuel” 

requirements for each flight. Consequently, Valmie’s Flight Conditions and Operating Procedures 

provide for an equivalent level of safety when compared to 14 C.F.R §91.151(a)(1). 

14 C.F.R. §91.405(a): Maintenance Required; 14 C.F.R. §91.407(a)(1): Operation After 

Maintenance, Preventative Maintenance, Rebuilding, Or Alteration; 14 C.F.R. §§ 

91.409(a)(1) and (2): Inspections; 14 C.F.R. 91.417(a) and (b): Maintenance Records

Valmie requests exemption from the following F.A.Rs: 14 C.F.R. §91.405(a), which provides the 

owner or operator of aircraft shall have the aircraft inspected pursuant to Subpart E of 14 C.F.R; 

14 C.F.R. §91.407(a)(1), which provides that no person may operate any aircraft having undergone 

preventive maintenance unless approved for return to service by a person authorized under §43.7; 

14 C.F.R. §§91.409(a)(1) and (2), which provides that no person may operate an aircraft within 

the preceding 12 calendar months unless an annual inspection has been performed; and 14 C.F.R. 

§§91.417(a) and (b), which provides for the recording of an aircraft’s maintenance if the aircraft 

holds an airworthiness certificate. 

Valmie’s petition for exemption provides an equivalent level of safety since Valmie requires 

compliance with the component manufacturer’s maintenance, overhaul, replacement, inspection, 

and life limit requirements for the components that comprise the minimum-equipment-list (see 

above) for the Vertitek V1-X8a and Vertitek V2-H6a. Due to the nature of a sUAS, compliance 

with certain maintenance requirements under Subpart E of 14 C.F.R. are either impossible or cost 

prohibitive to implement when applied to a sUAS. As such, Valmie should be exempt from these 

regulations as Valmie’s Flight Conditions and Operating Procedures provide for an equivalent 

level of safety when compared to these F.A.R.s. 
Vertitek V1-X8a

Unmanned Aerial Vehicle

The Vertitek V1-X8 is constructed using off the shelf components featuring a 

lightweight carbon fiber frame, multistage vibration dampening, and custom camera 

and sensor mounts, which are impact resistant and easily maintained.

Minimum Equipment List Configuration:

• 1 – Fr-Sky Taranis X9D Plus Transmitter (for manual control)

• 1 – Fr-Sky X8R Receiver (for manual control)

• 2 – 650 Quad Frame Main Plates (from Tarot 650 Sport Frame)

• 4 – 16mm Clamp Style Motor Mounts with top/bottom motor plates

• 4 – Carbon Fiber Arms (16mm x 330mm)

• 8 – Brushless Electric 5010/14 360KV Motors (from RCTimer) with 40a ESCs

• 8 – Carbon Fiber Propellors, 17x5.5 (4xCW, 4xCCW)

• 1 – Lithium Polymer (LiPo) Battery of 12000mah capacity

• 1 – Pixhawk Flight Controller (from 3DRobotics) offering:

◦ fully autonomous flight capability with “Return to Home” ability

◦ 32 bit STM32F427 Cortex M4 core with FPU

◦ 168 MHz/256 KB RAM/2 MB Flash

◦ 32 bit STM32F103 failsafe co-processor

◦ ST Micro L3GD20 3-axis 16-bit gyroscope

Version: 0.2 – Revised: July 17, 2015 1 of 2

Exhibit 1
Vertitek V1-X8a

Unmanned Aerial Vehicle

◦ ST Micro LSM303D 3-axis 14-bit accelerometer / magnetometer

◦ Invensense MPU 6000 3-axis accelerometer/gyroscope

◦ MEAS MS5611 barometer

◦ Real Time Current and Voltage Sensing

• 1 – UBLOX GPS

• 1 – 915 MHz Telemetry Radio

Mandatory Payload:

• Battery 12,000mah (recommended)

Optional Payloads include, but are not limited to:

• Thermal Imaging Camera(s)

• Multiple Spectrum Camera(s)

• Live High Definition Video Camera(s)

• Gimbals

• Sonar / Lidar Instruments

Characteristics:

• Empty Weight (no battery, camera/sensor payload) of 4.0625 pounds.

• Battery 12,000mah, weight of 4.0625 pounds

• Recommended Gross Weight (all up weight, max capacity) of 10.0000 pounds.

• Useful Payload of 5.9375 pounds at Recommended Gross Weight.

• Maximum Airspeed of 40 knots, with only the battery, and 15 knots at

Recommended Gross Weight.

Configuring the maximum recommend payload (battery plus camera/sensor package) 

for no more than 5.9375 pounds, where the Gross Weight will not exceed 10.0000 

pounds, will produce at least 26 minutes of flight time. Reserving 6 minutes for 

performing the “Return to Home” capability if necessary, gives the operator 20 minutes

for performance of mission objectives.

Version: 0.2 – Revised: July 17, 2015 2 of 2
Vertitek V2-H6a

Unmanned Aerial Vehicle

The Vertitek V2-H6a is constructed using off the shelf components featuring a 

lightweight carbon fiber frame, multistage vibration dampening, and custom camera 

and sensor mounts, which are impact resistant and easily maintained.

Minimum Equipment List Configuration:

• 1 – Fr-Sky Taranis X9D Plus Transmitter (for manual control)

• 1 – Fr-Sky X8R Receiver (for manual control)

• 2 – Hex Frame Main Plates (from Tarot 960 Frame)

• 6 – 25mm Clamp Style Motor Mounts

• 6 – Carbon Fiber Arms (25mm x 423.5mm)

• 6 – Brushless Electric 5008 330KV Motors (from Foxtech) with 40a ESCs

• 6 – Carbon Fiber Propellors 17x5.5, (3xCW, 3xCCW)

• 1 – Lithium Polymer (LiPo) Battery of 12000mah capacity

• 1 – Pixhawk Flight Controller (from 3DRobotics) offering:

◦ fully autonomous flight capability with “Return to Home” ability

◦ 32 bit STM32F427 Cortex M4 core with FPU

◦ 168 MHz/256 KB RAM/2 MB Flash

◦ 32 bit STM32F103 failsafe co-processor

Version: 0.2 – Revised: July 17, 2015 1 of 2

Exhibit 2
Vertitek V2-H6a

Unmanned Aerial Vehicle

◦ ST Micro L3GD20 3-axis 16-bit gyroscope

◦ ST Micro LSM303D 3-axis 14-bit accelerometer / magnetometer

◦ Invensense MPU 6000 3-axis accelerometer/gyroscope

◦ MEAS MS5611 barometer

◦ Real Time Current and Voltage Sensing

• 1 – UBLOX GPS

• 1 – 915 MHz Telemetry Radio

Mandatory Payload:

• Battery 12,000mah (recommended)

Optional Payloads include, but are not limited to:

• Thermal Imaging Camera(s)

• Multiple Spectrum Camera(s)

• Live High Definition Video Camera(s)

• Gimbals

• Sonar / Lidar Instruments

Characteristics:

• Empty Weight (no battery, camera/sensor payload) of 4.400 pounds.

• Battery 12,000mah, weight of 4.0625 pounds

• Recommended Gross Weight (all up weight, max capacity) of 13.0000 pounds.

• Useful Payload of 8.6000 pounds at Recommended Gross Weight.

• Maximum Airspeed of 38 knots, with only the battery, and 13 knots at

Recommended Gross Weight.

Configuring the maximum recommend payload (battery plus camera/sensor package) 

for no more than 8.6000 pounds, where the Gross Weight will not exceed 13.0000 

pounds, will produce at least 26 minutes of flight time. Reserving 6 minutes for 

performing the “Return to Home” capability if necessary, gives the operator 20 minutes

for performance of mission objectives.

Version: 0.2 – Revised: July 17, 2015 2 of 2
Exhibit 3

FrSky Electronic Co., Ltd

Website:www.frsky-rc.com E-mail:frsky@frsky-rc.com Technical Support: sales4tech@gmail.com 

FrSky Electronic Co., Ltd

Website:www.frsky-rc.com E-mail: frsky@frsky-rc.com Technical Support: sales4tech@gmail.com 

Introduction

www.frsky-rc.com www.frsky-rc.com

FrSky 2.4GHz ACCST X8R Manual

Range Check

A pre-flight range check should be done before each flying session. Reflections from nearby metal fences, 

concrete buildings or tress can cause loss of signal both during range check and during the flight. Follow the 

steps below to perform the range check.

1. Place the model at least 60cm (two feet) above non-metal contaminated ground (e.g. on a wooden bench).

2. The receiver antennas should be separated in the model, and do not touch the ground.

3. The module antenna should be in a vertical position.

4. Turn on the transmitter and the receiver, press the F/S button on the XJT module for 4 seconds to enter

range check mode, the RED LED will be off, GREEN LED will flash rapidly. The effective distance will be 

decreased to 1/30 (at least 30m).

5. Walk away from the model while simultaneously operating the controls on the transmitter to confirm all

controls’ normal operation.

6. Press the F/S button on the XJT module for 1~2 seconds to exit range check mode, RED LED will be back

on, indicating normal operation is back.

Failsafe

Failsafe is a useful feature in which all controls move to a preset position whenever the control signal is lost for 

a period of time. X8R supports failsafe function for all channels. Follow the steps below to set failsafe positions 

for each channel:

1. Bind the receiver first and turn on both the transmitter and the receiver;

2. Move the controls to the desired failsafe position for all channels;

3. Press briefly the F/S button on the receiver (less than 1 second). The Green LED will flash twice, indicating

the failsafe position has been set in the receiver.

To disable the failsafe function, re-bind the receiver.

Failsafe is recommended to set when system is firstly used, or receiver has been re-bound. Follow steps below 

to set failsafe.

Option-1.How to set failsafe to a user-determined state on lost signal:

1) Bind the receiver to the transmitter module first and turn on both the transmitter and the receiver;

2) Move the controls to desired failsafe position for all channels;

3) Press briefly the F/S button on the receiver and you are done.

Option-2. How to set failsafe for no pulses on lost signal:

1) Turn off the transmitter, power on the receiver, and then press briefly the F/S button on the receiver.

Note: If failsafe is not set, failsafe default will hold last position before signal is lost. In this case, there 

 exists risk that your model will fly away or cause injury.

Specifications

Binding Procedure

Binding is the process of uniquely associating a particular receiver to a transmitter module. A transmitter module 

can be bound to multiple receivers (not to be used simultaneously). A receiver can only be bound to one 

transmitter module.

Follow the steps below to finish the binding procedure.

1. Turn on the transmitter while holding the F/S button on the module (please refer to the module instruction

manual for switch positions). Release the button. The RED LED on the XJT module will flash, indicating the 

transmitter is ready to bind to the receiver.

2. Set X8R receiver in bind mode (see below chart for details), The RED LED on the receiver will flash, 

indicating the binding process is completed.

3. Turn off both the transmitter and the receiver.

4. Turn on the transmitter and connect the battery. The GREEN LED on the receiver indicates the receiver is

receiving commands from the transmitter. The receiver/transmitter module binding will not have to be repeated, 

unless one of the two is replaced. 

What’s New!

 More number of channels: 1~8ch from conventional channel outputs, 1~16ch from SBUS port,

or combine two X8R to become a 16 channels receiver.

 Parallel two X8R to become a 16 channel receiver.

 With RSSI PWM output (0~3.3V)

 Smart Port enabled, realizing two-way full duplex transmission. 

Thank you for purchasing FrSky X8R 8/16ch full duplex telemetry receiver.In order to fully enjoy the benefits of 

this system, please read the instruction manual carefully and set up the device as described below.

Overview 

Green LED

ON

Flashing

OFF

Flash Twice

Red LED

Flashing

OFF

Flashing

OFF

Status

Binding

Normal

Signal Lost

Failsafe Set

Dimension: 46.47×26.78×14.12mm (L × W × H)

Weight: 16.6g

Number of Channels: 16CH (1~8ch from conventional channel outputs, 1~16ch from SBUS port

or combine two X8R to become a 16 channels receiver)

With RSSI PWM output (0~3.3V)

Operating Voltage Range: 4.0~10V

Operating Current: 100mA@5V

Operating Range: full range (>1.5km)

Firmware Upgradeable

Compatibility: FrSky DFT/DJT/DHT/DHT-U in D_mode

FrSky Taranis X9D Plus/XJT in D8 mode

FrSky Taranis X9D Plus/XJT in D16 mode

X8R-EU version only works with FrSky Taranis X9D Plus-EU version/XJT-EU version in D16-EU 

mode.

 Note: After binding procedure is completed, recycle the power and check if the receiver is really under 

control by linked transmitter.

Mode of X8R Telemetry Channel Output Jumped before Bind

(signal pins) F/S Button

Mode 2(D16)

Mode 3(D16)

Mode 4(D16)

Mode 5(D16)

√ 

√ 

√ 

×

×

CH1~CH8 CH7&CH8

CH3&CH4

CH1&CH2

CH1&CH2, CH3&CH4

CH1~CH8

CH9~CH16

CH9~CH16

CH1~CH8 No Jumper

connect the battery to any available

channel output (no need to hold the 

F/S button on X8R)

connect the battery to any available

channel output while holding the F/S

button on X8R

For more details, please check the complete manual for X8R from www.frsky-rc.com - Download -Manual.

Should you have other questions, please send e-mails to FrSky technical support sales4tech@gmail.com.

Receiver Mode and Binding Operation:

Mode 1(D8)

Receiver Mode select & Bind Operation

When combine two X8R to become a 16CH receiver, you need to disable telemetry on either one of the 

two X8R’s as above chart.

X8R-EU version only works with FrSky Taranis X9D Plus-EU version/XJT-EU version in D16-EU mode.

PORT Smart Port (S. Port) is a signal wire full duplex digital transmission interface developed by FrSky 

Electronic Co., Ltd. All products enabled with Smart Port (including XJT module, X8R receiver, 

new hub-less sensors, new Smart Dashboard,etc), serial port user data and other user input/ output devices 

can be connected without limitations for numbers or sequences at a high transmission speed.

Smart Port

SBUS Port

(CH1-CH16)

Conventional Channel

Outputs (CH1-CH8)

 RSSI Outport

F/S Button

LED

Please be attention that the Smart Port Protocol is only running in D16 mode.

Exhibit 4
3DR RADIOV2

QUICK START GUIDE

PARTS

GETTING STARTED

3DR Radios provide an air-to-ground data link between the autopilot and your ground station laptop or 

tablet. Follow this guide to install the radios on your plane, copter, or rover. 3DR Radios arrive ready to 

use. Just mount and connect to view real-time data from your drone.

Android adapter cable

6-wire Pixhawk connector cable

Micro-USB cable

Two 3DR Radios in 915 or 433 mHz

Attach the antennas, and use either radio as an air or ground module.

6-to-5-position APM and PX4 connector cable

Exhibit 5
MOUNT

CONNECT TO AUTOPILOT

Connect to the APM 2.5 or 2.6 telemetry port using 

2.6 the 6-to-5-position cable.

Connect to the PX4 I/O telemetry 

port using the 6-to-5-position cable.

Connect to the Pixhawk telemetry 

port using the 6-wire cable.

Mount the air module securely to your vehicle keeping the antenna clear of any propellers or moving 

components. Ensure that the antenna is oriented vertically for maximum range.

CONNECT TO MISSION PLANNER

Use the micro-USB cable to connect the ground module to your laptop. In Mission Planner and APM 

Planner ground station applications, select the communication option that shows COM, set the rate 

to 57600, and select Connect. The radio will not connect unless the vehicle is powered. Use the Flight 

Data screen to view your vehicle’s status and control missions in flight.

LEARN MORE 

about installing a mission planner application for your laptop or tablet and interacting with the 

autopilot using 3DR Radios (including retrieving flight data logs) at planner.ardupilot.com.

Mission Planner
TIPS

Orient the ground radio 

antenna vertically for 

maximum range.

CONNECT TO TABLET

Connect the ground module to your tablet using the Android adapter cable. Connect the colored end 

to the tablet and the black end to the radio. In DroidPlanner or Andropilot, select Connect.

DroidPlanner Flight Data screen

View the strength of the radio signal in the 

mission planner’s flight data screen.

SETTINGS

To change the radio settings in the mission planner, connect the radio to your computer, but do not 

select Connect. Radios can only be configured while unconnected to MAVLink. Select Initial Setup, 

3DR Radio, and Load Settings to configure the radios.

All settings should be the same for both modules. Ensure that the Net ID setting is identical on each 

radio to enable pairing. Select Save Settings to apply settings. For flying with friends, make sure your 

Net IDs do not conflict.

Use the configuration options on this screen to apply the correct airspace regulation requirements 

for your area. You are responsible for complying with all airspace regulations in your area, including 

frequency restrictions, power levels, and licenses. For more information on configuring 3DR Radios to 

comply with local regulations, visit the online documentation at goo.gl/Tsrksf.
SPECIFICATIONS

3DR Radio Guide V1 © 3D Robotics, Inc. 28 October 2013

SUPPORT

For more information about mission planner applications and APM firmware, visit ardupilot.com. For 

online documentation of 3DR Radios, visit goo.gl/Tsrksf. 

For customer support, contact us at help@3drobotics.com or call our support line at +1 (858) 225-1414.

Processing

100 mW maximum output power (adjustable)

-117 dBm receive sensitivity

Based on HopeRF’s HM-TRP module

RP-SMA connector

2-way full-duplex communication through adaptive TDM

UART interface

Transparent serial link

MAVLink protocol framing

Frequency Hopping Spread Spectrum (FHSS)

Configurable duty cycle

Error correction corrects up to 25% of bit errors

Open-source SIK firmware

Configurable through Mission Planner & APM Planner

Features

Interchangeable air and ground modules

915 or 433 mHz

Micro-USB port

6-position DF13 connector

Power

Supply voltage: 3.7-6 VDC (from USB or DF13)

Transmit current: 100 mA at 30 dBm

Receive current: 25 mA

Serial interface: 3.3 V UART

Dimensions

26.7 cm x 55.5 cm x 13.3 cm 

(without antenna)

3

4

5

1 Micro-USB port

2 6-wire cable connector

3 Antenna

4 Frequency

5 LED indicator

1

2

RADIO DESCRIPTION

LED MEANINGS

Solid green

Link established with paired radio

Blinking green

Searching for paired radio

Blinking red

Transmitting data

Solid red

Firmware update mode
Exhibit 6











! Safety - Read Before Flying !

Your first priority must absolutely be the safety of people!

Multicopters are essentially Flying Lawnmowers! 

• ArduCopter is an experimental aircraft running community-created code - Novel and unexpected results

are NOT uncommon!

• Crashes can happen, because of pilot error or hardware or software malfunction.

• Especially while you are learning, it is recommended that you avoid, stiff, ultra-sharp carbon fiber props.

o Get cheaper more flexible and more breakable plastic ones.

o Some carbon fiber props cut better than a Ginsu and while they are almost indestructible, you are not.

• If you are flying anywhere near other people, you are putting them at risk!

• Be sure to maintain safe distances between yourself, and spectators and your copter.

o Circumstances will require that you will need to make your own determination of what is a "safe distance"

from people and property.

o At a minimum, consider: at least 10ft (3m) but not further than 30ft (10m) from you.

o Keep all other people, property and obstacles considerably further away from your copter.

o Ensure that no one gets between you and your copter.

o Spectators should always be a safe distance behind the pilot.

o If people intrude beyond what you have determined to be the "safe" area, land immediately and do not

take off until they are clear.

o At full power, an average sized multi-copter can exceed 20 mph (32 km/h), can ascend to hundreds of feet

and easily travel more than a mile in distance before running out of battery.

• Always ensure that the battery cable is (NOT) connected to the power distribution board or harness until

you are ready to fly.

o After landing the first thing you should do is disconnect your battery cable.

o Always remove your props while you are testing motors.

o Your hands, arms and face and those of your friends will thank you.

o When the battery is connected, always assume the motors are armed.

o Check with a short throttle pulse.

o Don't pick up the model and the radio at the same time, you may bump the throttle.

o Do not attempt to fly longer than your batteries safe capacity.

 At a minimum it is very hard on the battery and at worst you will crash destructively.

• The APM and PX4 flight controllers we use incorporate a motor arming safety feature.

o Immediately prior to flight after the battery has been connected, the RC transmitters throttle stick needs to

be held down and to the right for several seconds to arm the motors.

o After landing your first response should be to hold the throttle down and to the left for several seconds to

"Disarm" the motors.

o Disarm condition can be tested by moving the throttle stick up, if the motors do not move it is dis armed.

o Even when disarmed, the throttle stick should always be kept in the full down position except when flying.

• Get used to switching back to Stabilize mode from other modes and reassuming full manual control.

o This is the single most important recovery technique (practice it).

o Stabilize mode can have Simple mode added to it, but if you do, practice with it till you are proficient.

o Do not use any modes other than Stabilize or Stabilize plus Simple until you are VERY comfortable flying.

• Important primary response to a crash, inadequate landing or unknown flight controller state.

o The first thing to do is throw a towel over your copters propellers (Propellers may start spinning

unexpectedly).

o Then immediately disconnect the battery.

o A large towel is your most important piece of safety equipment followed by a fire extinguisher and a first

aid kit. - - Generally better to use the first one than the last one.

• When testing or flying any of the navigation modes (using GPS):

o Ensure that your GPS has "Lock" before arming and takeoff.

o Check that your home position on the Mission Planner is in fact correct.

o Sometimes GPS's do not report the home position accurately, reboot if not accurate and wait for 8 or more

satellites (not just 3D lock) and check again.

Exhibit 7
Keep a safe distance between your Copter and People!

These tips can also help protect your multicopter from damage. 

• Avoid sudden or extreme transmitter control stick deflections

o Move the control sticks in small measured increments and don't "yank" on them.

o If the copter is properly calibrated and balanced it should require only small stick inputs to control altitude,

direction and speed.

o Your copter should be more or less stable on the horizontal plane without any control inputs.

o If you are "fighting" the copter, land and fix it - something is not right - Hardware adjustment or software

calibration may be required.

o Be especially careful of large throttle inputs, as a copter can gain (or lose) altitude very rapidly.

• Because MultiCopters are symmetrical it is especially easy to lose Visual Orientation.

o For manual flight modes, maintaining a clear vision of the Copters Orientation (direction it is facing) is the

most critical part of successful flight.

o Especially while learning it is very important to keep your copter appropriately close to you to aid in

maintaining visual orientation.

o Generally: more than 10ft (3m) but not further than 30ft (10m) from you.

o If the copter gets further than about 100ft (30m) it starts getting difficult to be able to

maintain orientation and can easily crash.

o If you lose Yaw orientation while flying in Stabilize mode, try only flying forward and using yaw to steer like

a car.

o It is much better to simply descend and land rather than have an orientation-induced crash or fly away.

 Fly-Aways often happen when the copter is commanded to tilt back towards the pilot but has

rotated in the meantime and is so far away that orientation is lost.

 Result: the copter flies further away and crashes or is lost.

• Always have Stabilize mode as the (Go To) one of your 3 options.

• High or unexpected winds or gusts can make flight considerably more difficult.

o High winds can prevent forward progress or spin the copter around causing you to become disoriented.

o The higher you are, the more likely high winds will be a problem.

o Switching to Stabilize mode and landing before you reach your skill limits can help you save your copter.

• Avoid flying at high speed or high altitude until you have gained considerable confidence in both manual

and automatic modes.

• When flying around trees or buildings it is very easy to lose visual orientation or even to lose sight of the

copter completely.

o Gusting winds around objects can also worsen the problem and radio signal loss can also occur.

o If your copter is approaching a potentially interfering object, immediately switch to stabilize mode and land

or retrieve the copter to your location.

• ArduPilot specific safety modes: RTL, FailSafe and GeoFence.

o RTL can provide a safe Return to Launch if it starts to get away from you.

o FailSafe and GeoFence can assist you with keeping the copter in a safe proximity.

o Do not rely on the above safety modes, always be ready to take control in stabilize and land the copter.

o Especially do not rely on the above safety modes to perform maneuvers or training that you would

otherwise consider dangerous.

o These modes are a supplement to, not a replacement for sound safety practices.

• On your first takeoff after tuning or hardware setup

o In stabilize mode advance the throttle very slowly until the copter is almost hovering.

o If the copter is trying to flip over turn it off and correct the problem, a motor could be turning the wrong

direction, or a wrong direction prop could be installed.

o If the copter tries to rotate on it's axis or fly off in some direction the transmitter or RC setup may be

incorrect, a motor or ESC may not be performing properly or the props may be installed incorrectly.

o When all problems are fixed it should be fairly easy to get the copter to hover a foot or 2 above the ground.

o If a stable and stationary hover a foot or 2 above the ground cannot be achieved, land and fix the problem

• When flying FPV "First Person View" (with a video camera), Set modes to: STABILIZE, SIMPLE, and RTL.

o Ensure RTL is working properly before using FPV,

o Use Stabilize mode to fly FPV and If you lose FPV video switch to Simple or RTL to get back.

• Make sure your battery can't fall out, use a Velcro Strap to hold it in place.
AUTOPILOT

QUICK START GUIDE

Exhibit 8
PARTS

1 Pixhawk

2 Buzzer

3 Safety switch 

4 Micro-SD card and adapter

5 Micro-USB cable

6 Six-wire cable x2 

 7 Power module

 8 I2

C splitter module

 9 Four-position I2

C splitter cable

10 Three-wire servo cable

11 Mounting foam

1 2 3 4 5 7

8 11

 MOUNT

Use the provided foam to mount Pixhawk as close as possible to your vehicle’s center of gravity. 

Make sure to orient the board with the arrow pointing forward.

Vehicle front

Attach the foam squares to the 

corners of the board.

GETTING STARTED

With the help of APM firmware, Pixhawk turns any 

RC plane, copter, or rover into a full-featured personal 

drone. Once you have a fully-assembled frame, follow 

this guide to install Pixhawk.

6

9 10

1 Mount

2 Connect

3 Load firmware

4 Calibrate

1
 CONNECT

(Required) Connect the buzzer 

and safety switch.

(Optional) Connect a 3DR 

Radio to Pixhawk’s Telem 

port using the 6-wire cable 

provided with your 3DR Radio 

Kit to receive data and 

communicate with 

the autopilot in flight. 

(GPS or GPS+Compass required)

Connect a 3DR GPS+Compass to 

provide the autopilot with positioning 

data during flight. This kit includes a 

6-wire cable to connect the GPS ports. 

Connect the MAG to the I2C port using 

the 4-wire cable provided with the 3DR 

GPS+Compass.

(Required) Connect the 3DR 

Power Module to the Power port 

using the 6-wire cable to direct 

power from your lithium polymer 

(LiPo) battery to the autopilot.

(Optional) The I2C splitter expands the I2C port to allow up 

to four additional peripherals to connect to Pixhawk. Use the 

4-wire cable to connect the I2C splitter and add a compass 

module, external LED, digital airspeed sensor, or other 

peripherals to your vehicle.

2
Connect the ground (-), power (+), and signal (S) wires to the RC 

pins using the provided 3-wire servo cable.

For a Spektrum DSM, DSM2, or DSM-X Satellite RC receiver, connect to 

the SPKT/DSM port.

CONNECT RADIO CONTROL

FOR PPM RC RECEIVERS AND FUTABA S.BUS RECEIVERS

FOR SPEKTRUM SATELLITE RECEIVERS

FOR PWM RECEIVERS

Purchase a PPM Encoder module to connect a PWM 

RC receiver to Pixhawk at store.3dr.com.

LOAD SD CARD INTO PIXHAWK

If the SD card is not preloaded into Pixhawk, insert the micro-SD card into the slot at the 

bottom end of the board.

For a complete list of RC systems compatible with Pixhawk, visit the APM wiki page here.
 LOAD FIRMWARE 

APM firmware is the brains of your autopilot operation and must be installed before using Pixhawk. 

To load firmware onto Pixhawk, install a mission planner application on your ground station computer. Choose 

either Mission Planner (Windows) or APM Planner for (Windows, OS X, and Linux). 

Both applications are available for free download from ardupilot.com.

For rovers, connect the throttle and steering 

wires to the main output signal pins.

Pin 3 = Throttle

Pin 4 = Steering

Mission planner

firmware

FOR COPTERS

FOR PLANES

FOR ROVERS

Connect each signal wire from the PDB to 

the main output signal (S) pins by motor 

number. Connect one wire for each motor 

to the corresponding pin.

Pin 1 = Motor 1 Pin 5 = Motor 5

Pin 2 = Motor 2 Pin 6 = Motor 6

Pin 3 = Motor 3 Pin 7 = Motor 7

Pin 4 = Motor 4 Pin 8 = Motor 8

For planes, connect the control channel 

wires to the main output signal pins.

Pin 1 = Aileron

Pin 2 = Elevator

Pin 3 = Throttle

Pin 4 = Rudder

CONNECT OUTPUTS

3
Download Mission Planner (Windows)

Mission Planner « Downloads

Sort by: Title | Hits | Date

■ MissionPlanner - Installer Select the installer 

package to download.

Ardupilot.com Downloads Mission Planner

After selecting the correct file, read the safety information and select Download.

Open the file to run the setup wizard. Proceed through any security warnings, and install all 

suggested drivers. When the installation is complete, open the application, and connect Pixhawk to your 

computer using the micro-USB cable. 

Your computer will automatically install the correct drivers. Do not select Connect at this time; Pixhawk can only 

load firmware while unconnected to Mavlink. 

Download APM Planner (Windows, OS X, and Linux)

APM Planner 2.0 « Downloads

Sort by: Title | Hits | Date

■ APM Planner 2.0 Mac

■ APM Planner 2.0 Windows

■ APM Planner 2.0 Linux

Select your platform to 

download.

Ardupilot.com Downloads APM Planner 2.0

INSTALL PLANNER
When prompted, follow the directions to load the firmware. Once the status bar shows that the download is 

complete, power cycle the board by disconnecting and reconnecting the USB.

If you hear a musical tone, your firmware installation is complete. If you hear a series of tones followed by three 

beeps, disconnect the USB and reconnect while holding down the safety button. Upon restart, listen for a series 

of tones followed by two beeps indicating that your firmware has loaded successfully.

beep BEEP beep... 

BEEP BEEP  Pixhawk needs your attention:

beep BEEP beep... BEEP BEEP BEEP

Everything is OK:

musical tone 

Select Initial Setup, Install Firmware, and select your vehicle.

 CALIBRATE

With Pixhawk connected to your computer, select the communication option from the drop-down menu for 

PX4 FMU, set the rate to 115200, and select the Connect icon. Select Initial Setup and Mandatory Hardware to 

access the calibration wizards. 

Remove propellers before performing calibration. !

4
SELECT FRAME TYPE (COPTERS ONLY)

CALIBRATE COMPASS

Select the options to enable the compass; to allow automatic declination 

calculation; and to specify Pixhawk. Select Live Calibration to launch the wizard, 

and follow the prompts.

Show Me

videos demonstrating live calibration techniques at 3dr.com/learn.

For copter, select your frame orientation. 
CALIBRATE ACCELEROMETER

SELECT FLIGHT MODES

4

5

6

RC CALIBRATION

left stick

right stick

Select Accel Calibration, check the box for AC 3.0+, select Calibrate, and 

follow the prompts to calibrate Pixhawk’s accelerometer. Make sure to wait a 

couple of seconds before and after changing the positions of the vehicle.

Select Radio Calibration to teach Pixhawk to work with your RC 

transmitter. Turn on your transmitter, select Calibrate Radio, and move 

all sticks and switches to their extreme positions. Select Click when Done

once the red bars are set for all available channels.

Move each switch on your transmitter to its available positions. The mission 

planner will indicate the currently selected position with green highlighting. Select 

a mode for each switch position, and select Save Modes to assign.
LED MEANINGS

Flashing red and blue: initializing. Please wait.

Double flashing yellow: error. System refuses to arm.

Flashing blue: disarmed, searching for GPS. Autonomous, loiter, and return-to-launch 

modes require GPS lock.

Flashing green: disarmed, GPS lock acquired. Ready to arm. Quick double tone when 

disarming from the armed state.

Solid green plus single long tone: armed and ready to fly!

Flashing yellow: RC failsafe activated.

Flashing yellow plus quick repeating tone: battery failsafe activated.

Flashing yellow and blue plus high-high-high-low tone: GPS glitch or GPS failsafe 

activated.

Quick, constant blinking: performing system check. Please wait.

Solid: ready to arm. Proceed to the arming procedure.

Intermittent blinking: system ready. Press the safety button to activate.

SAFETY SWITCH MEANINGS

Learn more

about LED meanings and buzzer tones at 3dr.com/learn.
1

2

3

4

5

6

7

8

9

10

11

12

13

14

15

1 Spektrum DSM receiver

2 Telemetry (radio telemetry)

3 Telemetry (on-screen display)

4 USB

5 SPI (serial peripheral interface) bus

6 Power module

7 Safety switch button

8 Buzzer

 9 Serial

10 GPS module

11 CAN (controller area network) bus

12 I

2

C splitter or compass module

13 Analog to digital converter 6.6 V

14 Analog to digital converter 3.3 V 

15 LED indicator

PORTS

1 2

3 4

1 Input/output reset button

2 SD card

3 Flight management reset button 

4 Micro-USB port

1 2

ground

power

signal

1 Radio control receiver input

2 S.Bus output

3 Main outputs

4 Auxiliary outputs

3 4
Processor

32-bit ARM Cortex M4 core with FPU

168 Mhz/256 KB RAM/2 MB Flash

32-bit failsafe co-processor

Sensors

ST Micro 16-bit gyroscope

ST Micro 14-bit accelerometer/magnetometer

MEAS barometer

MPU6000 accelerometer/magnetometer

Power

Ideal diode controller with automatic failover

Servo rail high-power (7 V) and high-current ready

All peripheral outputs over-current protected, all 

inputs ESC protected

Interfaces

5x UART serial ports, 1 high-power capable, 2x with 

HW flow control

Spektrum DSM/DSM2/DSM-X Satellite input

Futaba S.BUS input and output

PPM sum signal

RSSI (PWM or voltage) input

I

2

C, SPI, 2x CAN, USB

3.3 and 6.6 ADC inputs

Dimensions

Weight 38 g (1.3 oz)

Width 50 mm (2.0”)

Height 15.5 mm (.6”)

Length 81.5 mm (3.2”)

SPECIFICATIONS

IMPORTANT NOTE

SUPPORT

For more information about Pixhawk and other documentation, visit 

3dr.com/learn. For more instruction on using APM firmware and 

planner software, visit ardupilot.com.

For customer support, contact us at help@3dr.com or call our 

support line at +1 (858) 225-1414 Monday through Friday, 8 am to 5 pm, PST.

Please note that these instructions describe basic setup for Pixhawk and do not represent the 

complete set of configuration procedures required to build a copter, plane, or rover. 

For more information on ESC calibration, battery monitoring, failsafes, mode descriptions, 

and more, visit ardupilot.com. Do not operate your vehicle without a complete understanding 

of the online instructions.
Operating a powered vehicle of any kind can be a lot of fun, but it carries certain inherent risks. Regulations 

governing the use of powered vehicles, including aircraft, vary from locale to locale, even within the same country 

or district. It is your responsibility to ensure that you understand and comply with all local laws and regulations.

Safety basics:

•	 Never operate the vehicle or software in a way that could be dangerous to you, other people, or property.

•	 Always keep propeller arcs free of objects and body parts while the vehicle is live.

•	 Keep in mind that software and hardware failures happen. Although we design our products to minimize 

such issues, you should always operate with the understanding that a failure could occur at any time and 

without warning. Accordingly, you should take the appropriate precautions to minimize danger in case of 

product failure.

•	 Never use the software or hardware for manned vehicles.

•	 Always operate within local laws and regulations.

•	 Do not operate the aircraft if you are under the age of 18. 

Additional safety information:

•	 Be sure to maintain safe distances between people and your aircraft. 

•	 Never operate your aircraft if your ability to do so with the utmost attention to safety is impaired in any 

way. Do not operate your aircraft while tired, under the influence of drugs or alcohol, or otherwise unable to 

operate it with the highest attention to safety. 

•	 Environment conditions can change rapidly and can make operation difficult. If this occurs, land your aircraft 

and discontinue use immediately. Do not operate your aircraft if operating conditions are not ideal. This 

includes, but is not limited to, rain, snow or excessive wind.

•	 Always ensure the battery cable is disconnected from the aircraft until you are ready to fly, and ensure that 

your batteries are fully charged prior to use.

•	 Always turn on the transmitter and ensure the throttle stick is all the way down before connecting the 

battery.

•	 After landing, disarm your vehicle immediately and disconnect the battery cable.

•	 Do not turn off the transmitter until after you have disconnected the battery.

•	 Always remove the propellers while testing the motors.

•	 When the battery is connected, always assume the vehicle is live and the motors are armed.

•	 Do not attempt to fly longer than the battery’s safe capacity.

•	 Do not operate the vehicle with excess weight attached.

•	 Ensure that all vehicle components are well maintained before each flight. Ensure that components are 

firmly attached and operating properly. 

•	 Replace any worn or damaged components before each flight. Never operate with any damaged or worn 

components.

•	 SAFETY IS THE FIRST PRIORITY. Take all precautions necessary to ensure your own safety as well as the 

safety of other people and property.

SAFETY
DISCLAIMER

THE LIMITED WARRANTIES APPLICABLE TO 3D ROBOTICS-BRANDED HARDWARE CAN BE FOUND AT 

WWW.3DROBOTICS.COM/TERMS/ AND CAN BE REFERENCED IN FULL AT THAT URL. 3D ROBOTICS 

RESERVES THE RIGHT TO UPDATE THE WARRANTIES AT ANY TIME WITHOUT EXPRESS NOTICE. 3D 

ROBOTICS MAKES NO OTHER WARRANTIES FOR 3D ROBOTICS-BRANDED PRODUCTS, AND MAKES 

NO WARRANTIES WHATSOEVER FOR SERVICE, SOFTWARE, MAINTENANCE OR SUPPORT FOR NON-3D 

ROBOTICS-BRANDED PRODUCTS. SUCH PRODUCTS, SOFTWARE, SERVICES, MAINTENANCE OR SUPPORT 

IS PROVIDED BY 3D ROBOTICS “AS IS” AND ANY THIRD-PARTY WARRANTIES, PRODUCTS, SOFTWARE, 

SERVICES, MAINTENANCE OR SUPPORT ARE PROVIDED BY THE ORIGINAL MANUFACTURER OR 

SUPPLIER, NOT BY 3D ROBOTICS. 3D ROBOTICS MAKES NO EXPRESS WARRANTIES EXCEPT THOSE STATED 

IN 3D ROBOTICS’ APPLICABLE WARRANTY IN EFFECT ON THE DATE OF THE INVOICE, PACKING SLIP OR 

ACKNOWLEDGEMENT.

3D ROBOTICS OFFERS THE HARDWARE AS-IS AND MAKES NO REPRESENTATIONS OR WARRANTIES OF 

ANY KIND CONCERNING THE HARDWARE, EXPRESS, IMPLIED, STATUTORY OR OTHERWISE, 

INCLUDING, WITHOUT LIMITATION, WARRANTIES OF TITLE, MERCHANTABILITY, FITNESS FOR A 

PARTICULAR PURPOSE, NON-INFRINGEMENT, OR THE ABSENCE OF LATENT OR OTHER DEFECTS, 

ACCURACY, OR THE PRESENCE OF ABSENCE OF ERRORS, WHETHER OR NOT DISCOVERABLE. SOME 

JURISDICTIONS DO NOT ALLOW THE EXCLUSION OF IMPLIED WARRANTIES, SO SUCH EXCLUSION MAY 

NOT APPLY TO YOU.

EXCEPT TO THE EXTENT REQUIRED BY APPLICABLE LAW, IN NO EVENT WILL 3D ROBOTICS BE LIABLE TO 

YOU ON ANY LEGAL THEORY FOR ANY SPECIAL, INCIDENTAL, CONSEQUENTIAL, PUNITIVE OR 

EXEMPLARY DAMAGES ARISING OUT OF THE USE OF THE HARDWARE.

3D ROBOTICS ACCEPTS NO LIABILITY FOR DAMAGE(S) OR INJURIES INCURRED DIRECTLY OR INDIRECTLY 

FROM THE USE OF THIS PRODUCT.

SOFTWARE IS SUBJECT TO THE SEPARATE SOFTWARE LICENSE AGREEMENT ACCOMPANYING OR MADE 

AVAILABLE TO YOU IN CONNECTION WITH THE SOFTWARE. A PORTION OF THE SOFTWARE MAY 

CONTAIN OR CONSIST OF OPEN-SOURCE SOFTWARE, WHICH YOU MAY USE UNDER THE TERMS AND 

CONDITIONS OF THE SPECIFIC LICENSE UNDER WHICH THE OPEN-SOURCE SOFTWARE IS DISTRIBUTED. 

YOU AGREE THAT YOU WILL BE BOUND BY ANY AND ALL SUCH LICENSE AGREEMENTS, AND THAT YOUR 

USAGE OF THIS PRODUCT INDICATES YOUR ACCEPTANCE OF THOSE AGREEMENTS. TITLE TO SOFTWARE 

REMAINS WITH THE APPLICABLE LICENSOR(S). IN NO EVENT WILL 3D ROBOTICS BE LIABLE TO YOU FOR 

DAMAGES, INCLUDING ANY GENERAL, SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES ARISING 

OUT OF THE USE OR INABILITY TO USE THE SOFTWARE.

Pixhawk Kit User Guide V8 © 3D Robotics, Inc. 20 March 2014