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September 22, 2015 

U.S. Department ofTransportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington, DC 20590 

Re: Exemption Request Under Section 333 of the FAA Reform Act and Part 11 of the Federal 

Aviation Regulations 

Dear Sir or Madam: 

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

and 14 C.P.R. Part 11, Zephyr-UAS, Inc. ("ZEPHYR"), an operator of the eBee ("eBee) and eXom 

("eXom") both being Small Unmanned Aircraft Systems (sUAS) manufactured by SenseFly SA of 

Switzerland, seeks an exemption from the Federal Aviation Regulations ("F ARs") listed below: 

• 14 C.P.R. 21, Subpart H 

• 14 C.P.R. 45.23 

• 14 C.P.R. 45.29 

• 14 C.P.R. 61.3 

• 14 C.P.R. 61.113(a)&(b) 

• 14 C.P.R. 61.133(a) 

• 14 C.P.R. 91.7(a) 

• 14 C.P.R. 91.9 

• 14 C.P.R. 91.109(a) & 91.319 (a) (1) 

• 14 C.P.R. 91.119 

• 14 C.P.R. 91.121 

• 14 C.P.R. 91.151(a) 

• 14 C.F.R. 91.203(a) & (b) 

• 14 CFR Subpart E (91.401- 91.417) 

The requested exemption would authorize commercial operations using the eBee and eXom for 

mapping and survey support applications of railroad corridors and other infrastructure. These 

operations will be subject to strict operating requirements defined in the eBee and eXom user 

manual (ZEPHYR requests the FAA treat the eBee & eX om training program, user manual, 

maintenance manual & risk assessment as proprietary under 14 C.F.R. 11.35(b) and does not 

include this document in the public docket) and conditions defined by the Safety Code of the 

Academy of Model Aeronautics (see Annex B), in order to ensure at least an equivalent level of 

safety to currently authorized operations using manned aircrafts. The aircraft carries an onboard 

geo-referenced still camera that allows it to conduct precision photogrammetry at the resolution 

necessary for highly accurate topographic mapping and modeling. This high-resolution data can be 

used for determining locations for track construction and reconfigurations. This data can also 

improve efficiency in engineering efforts for more accurately planning for increases in track 

infrastructure for the railroads and rail transit agencies. 

The use of an airborne survey vehicle also prevents personnel from entering dangerous areas of an 

operating railroad which is subject to strict FRA rules under 49CFR, Part 49-Transportation-213 

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Track Safety Standards. By approving these exemptions, the FAA will create benefits to both public 

agencies and private railroads which are ultimately in the public interest. 

The eBee & eXom (UAV's) will be operated in the field with both a Pilot in Command (PIC) and 

a ground-based Visual Observer (VO) in accordance with FAA Policy N 8900.227 Section 14 

"Operational Requirements for UAS" with the following additional restrictions: 

• All operations will occur in Class G airspace at no more than 400 ft. above ground level 

(AGL). 

• Operations will occur over railroad properties with the permission ofthe owner. 

• All required permits will be obtained from state and local government prior to operation. 

• The aircraft will not be operated at air shows or over an open-air assembly of people. 

• Operations will be limited to daytime and visual meteorological conditions (VFR flight 

rules) by an individual who fulfill the following requirements: 

o Aircraft will remain within Visual Line of Sight (VLOS) at no greater than 1/2NM 

from the PIC at all times 

o While the aircraft is airborne, the VO will be positioned within voice and/or radio 

distance from the PIC. 

o Has successfully passed a manufacturer's training program, for the UAV's; 

ZEPHYR requests the FAA treat the UA V' s training program as proprietary under 

14 C.P.R. 11.35(b) and does not include this document in the public docket; 

\ o Has a Private Pilot license. 

) • The PIC and VO will meet the requirements outlined in FAA Policy N 8900.227 Section 16 

Personnel Qualifications. Additionally, the PIC and VO will perform maintenance on the 

system and will complete a course of maintenance instruction as part oftheir initial training 

from the manufacturer. Due to the simplicity of the system, we do not anticipate the need 

for a supplemental pilot. 

While performing sUAS mapping operations on active railroad rights-of-way, the PIC and VO will 

be under the jurisdiction of the Federal Railroad Administration (FRA). Any personnel working on 

an active railroad line must obtain an initial 40 hours of safety training and an 8 hour annual 

refresher course. The operator of the sUAS must carry evidence ofbeing able to work on an active 

railroad in the form on an ID detailing the time and date of the training. While FRA regulations do 

not apply to the National Airspace System (NAS), we feel these added safety regulations further 

enhance our awareness and intent to operate a sUAS with the utmost care, attention, and 

responsibility. Furthermore, the use of a sUAS will help eliminate the need for personnel to enter 

hazardous and dangerous operating railroad right-of-way to measure and collect topographic data. 

A sUAS can help prevent injury and the loss oflife while working on active railroad rights-of-way. 

1. CHARACTERISTICS OF THE AIRCRAFT 

sUAS Operating Overview: The sUAS utilized are either a fixed or rotary-wing aircraft 

constructed of foam or rugged polycarbonate materials. The aircraft are easy to assemble or come 

pre- assembled. The sUAS can be operated manually or in fully autonomous flight modes. Creating 

pre- planned flight paths in autonomous mode is as simple as clicking on reference points on a georeferenced maps. Pre-mission waypoints, landing zones, and flight area dimensions can be entered 

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during preflight planning ensuring the sUAS operates only within specified boundaries and predetermined flight parameters. 

The Sensefly eBee is a fixed wing drone while the Sensefly Exom is a quad copter. 

The eBee is a battery-powered drone allowing flight times up to 

50 minutes. Its wingspan is 38 inches. Takeoff weight is 1.7 

pounds. 

The eXom is a battery-powered drone allowing flight times up to 

22 minutes. It measures approximately 7.0 H x 22 L x 32 Winches. 

Rotor blade diameter measures 13 inches. Takeoff weight is 3.7 

pounds. 

) The eBee is made of flexible foam that performs pre-programmed precision aerial mapping 

missions due to the on-board GPS and the related flight management software (eMotion) that allows 

the operator to plan safely and efficiently a mission in 3D, and then monitor it in real-time. Due to 

the embedded camera, protected by a foam envelope, the eBee takes a collection of high-definition 

still images that are used later to generate maps and contour lines of the surveyed area. 

/ 

The four main characteristics of the eBee & eX om are: 

a. Very light weight 

The eBee is so light that the operator can launch it by hand and let it land on almost any surface 

without requiring a parachute or landing net (belly land). Its low impact energy (38 J in case of a 

controlled emergency landing) also significantly reduces the risk of hazardous situations. Finally, 

the wings of the eBee are detachable and made of flexible foam with no sharp or hard edges and 

almost no internal strengthening structure. The eXom is also light weight and because it is a 

quadcopter can land and take off from open or confined spaces alike. 

b. Electric-powered 

The eBee & eXom are electric powered. A brushless engine technology makes it silent and reliable. 

The eBee propeller is attached with a rubber band to the body of the plane so that it can easily flex 

away in case of contact with any object. 

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c. Semi-automatic flight 

PH~R UliS 

The artificial intelligence incorporated within the eBee & eXom autopilot system continuously 

analyzes data from the Inertial Measurement Unit and from the onboard GPS and takes care of all 

the aspects of the flight under the supervision of the operator. 

d. Option for Manual control 

Additionally, the eBee & eXom provides an override capability that allows the operator to take 

manual actions during the flight (Go to Home, Go Land, Hold and Resume the mission) and also 

suspend automated operations and take manual control of the aircraft should it become necessary 

to respond emergent circumstances, thanks to the remote controller provided with the system. 

2. APPLICATIONS 

The intended applications are specifically for aerial mapping of railroad corridors & infrastructure 

that are heavily industrial in nature and away from the general public. 

3. APPLICABLE LEGAL STANDARD UNDER SECTION 333 

a. Airworthiness assessment of the eBee & eX om 

ZEPHYR notes that the airworthiness of the eBee & eXom have already been demonstrated for 

different projects in the United States, involving state/federal agencies or universities (among others 

the New Mexico State University: https://newscenter.nmsu.edu/Articles/view/10208/nmsu-uasflight-test-center-conducts-ebee-airworthiness-assessment, and the USACE New Orleans, who 

coordinated with the Department of Army and the FAA to obtain all authorizations required in order 

to operate the eBee UAS). 

Moreover, SenseFly obtained flight approvals for the eBee (delivered by national civil aviation 

authorities) in many countries, among others: 

• Switzerland (flight approval for VLOS operations) 

• Canada (flight approval for VLOS operations) 

• Australia (flight approval for VLOS operations) 

• France (flight approval for Extended-VLOS operations) 

• Germany (flight approval for VLOS operations) 

• United Kingdom (flight approval for VLOS operations) 

• Norway (flight approval for VLOS operations) 

• Sweden (flight approval for VLOS operations) 

• Denmark (flight approval for VLOS operations) 

b. Operating requirements 

Grant of the exemption to ZEPHYR for the eBee & eXom will be subject to the following operating 

conditions, based on the operating conditions set forth by the Academy of Model Aeronautics (see 

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PH~RUIIS 

Annex B). The main restrictions are summarized below: 

• Operations to be conducted over private, controlled-access, or public property where 

approved; 

• Permission from the land owner/authority required before commencing any flight; 

• Operations over congested areas shall be avoided; 

• Operations must not interfere with manned aircraft operations, must yield the right of way 

to manned aircraft, and operators must See & A void other aircraft and obstacles at all times 

• Operations limited to Visual Flight Rules Meteorological Conditions (VMC) and daylight 

hours 

• Aircraft operations must remain within Visual Line of Sight (VLOS) and will be visually 

monitored at all times; 

• VLOS guaranteed with a GPS geo-fence around operator of0.5 miles 

• Flight ceiling pre-programed at 400 feet; 

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

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

at the airport; 

• All operations shall comply with required permissions and permits established by territorial, 

state, county or city jurisdictions; including local law enforcement, fire, or other appropriate 

governmental agencies. 

• The eBee & eXom operations will be compliant with existing safety procedures inherent 

to the activities of the related company. 

c. Operator Requirements 

The eBee & eXom operator will have a Private Pilot license and will successfully have passed a 

manufacturer's training program for Sense fly products. 

3. CONCLUSION 

We submit that the combination of the aircraft's light weight, historically demonstrated flight 

performance, qualified flight crew and strict operation under the guidelines established in 8900.227, 

the FAA can have confidence that the operation will have an equivalent or greater level of safety to 

manned aircraft performing the same mission. 

The name and contact information of the applicant are: 

Zephyr-UAS, Inc. 

Attn: Marc A. Canas, GIS Professional 

President 

Phone: (714) 420-7238 

Fax: (714) 480-1787 

Email: macanas@jlpatterson.com 

Or 

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PH~RUJIS 

Jacqueline L. Patterson, PE 

Vice President/Principal Engineer 

Phone: (714) 658-4298 

Fax: (714) 480-1789 

Email: j lpatterson@j lpatterson.com 

Kyle C. Patterson, PE 

Vice President/Visual Observer (VO) 

Phone: (714) 866-7211 

Fax: (714) 480-1789 

Email: kcpatterson@j lpatterson.com 

Janelle M. Patterson 

Vice President/Visual Observer (VO) 

Phone: (714) 866-7074 

Fax: (714) 480-1789 

Email: jmpatterson@j 1 patterson. com 

Sincerely, 

Zephyr-VAS, Inc. 

\. 

) '1'#~;1. ~ 

Marc A. Canas, GISP 

President 

Appendices: 

A. Exemption Request and Equivalent Level of Safety 

B. Academy of Model Aeronautics Safety Requirements 

C. Privacy Issues 

D. Safety Case 

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APPENDIX A: EXEMPTION REQUEST AND EQUIVALENT LEVEL OF SAFETY 

SHOWINGS UNDER APPLICABLE RULES SUBJECT TO EXEMPTION 

ZEPHYR requests an exemption from the following regulations as well as any additional 

regulations that may technically apply to the operation of the eBee & eXam: 

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

14 CFR § 91.203(a)(1) 

Section 91.203 requires all civil aircraft to have a certificate of airworthiness. Part 21, Subpart H, 

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

airworthiness certificates as required by FAR§ 91.203(a). Given the size of the eBee & eXom, its 

very light weight (the maximum take-off weight is 1. 7 pounds) (3 .1 pounds for the eXom) and the 

limited operating area associated with its utilization, it is unnecessary to go through the certificate 

of airworthiness process under Part 21 Subpart H in order to achieve or exceed current safety levels. 

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

3 3 3 of the Reform Act. The Federal Aviation Act and Section 3 3 3 of the Reform Act both authorize 

the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration 

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

the UAS involved. An analysis of these different criteria demonstrates that the eBee & eXom 

operated without an airworthiness certificate, under the conditions proposed in that exemption, will 

be at least as safe, or safer, than a conventional aircraft with an airworthiness certificate. A 

proprietary risk assessment for operations with the eBee & eXom, which demonstrates that 

assertion, is also being submitted to the FAA as part of this application. ZEPHYR requests the FAA 

treat the eBee & eXom risk assessment as proprietary under 14 C.F.R. 11.35(b) and not include this 

document in the public docket. 

14 C.F.R. § 45.23 & 14 C.F.R. § 45.29: Display of marks; size of marks 

These regulations provide that each aircraft must display "N" and the aircraft's registration number 

in letters at least 3 inches high. Additionally, the aircraft must display the word 

"EXPERIMENTAL" in letters at least 2 inches high near the entrance to the cabin, cockpit, or pilot 

station. 

Given the size ofthe eBee (wingspan of37.8 inches), this requirement is impossible to match. 

14 C.F.R. § 61.3: Requirements for certificates, ratings and authorizations 

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

Command; Commercial Pilot Privileges and Limitations 

The regulation provides that no person may serve as a required pilot flight crewmember of a civil 

aircraft of the United States, unless that person: 

(1) Has a pilot certificate or special purpose pilot authorization issued under this part in that person's 

physical possession or readily accessible in the aircraft when exercising the privileges of that pilot 

certificate or authorization. However, when the aircraft is operated within a foreign country, a pilot 

license issued by that country may be used. 

The regulation provides also that no person that holds a private pilot certificate may act as pilot in 
) 

command of an aircraft for compensation or hire. Subparagraph (b) allows a private pilot to act as 

pilot in command of an aircraft in connection with any business or employment if: 

(1) The flight is only incidental to that business or employment; 

(2) The aircraft does not carry passengers or property for compensation or hire. 

Given the safety features of the eBee & eXom and the fact that the missions are pre-programmed 

and monitored in real-time with a specific flight management software (eMotion), SenseFly 

proposes that operators of the eBee & eXom should not be required to hold a commercial pilot 

certification. Instead, operators should be required to: 

Have a private pilot license and have successfully passed a manufacturer's training program for the 

eBee. 

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

This regulation requires that no person may operate a civil aircraft unless it is in airworthy 

condition. Should the exemption be granted allowing commercial operation of the eBee & eX om 

without an airworthiness certificate, no standard will exist for airworthiness of the eBee & eX om. 

Given the size of the aircraft and the previous airworthiness assessments given to the eBee, eXom, 

among others: 

• New Mexico State University: https://newscenter.nmsu.edu/Articles/view/10208/nmsuuas-flight-test -center-conducts-ebee-airworthiness-assessment 

• USACE New Orleans, who coordinated with the Department of Army and the FAA to 

obtain all authorizations required in order to operate the eBee UAS for levee system 

monitoring, documentation of construction progress, and extensive oblique photography of 

USACE structures & activities 

An equivalent level of safety will be achieved by insuring compliance with the SenseFly manuals 

prior to each flight. 

14 C.F.R. § 91.9: Civil aircraft flight manual, marking, and placard requirements. 

This regulation provides that no person may operate an aircraft unless a current, approved flight 

manual is in the aircraft. ZEPHYR assumes that the intent of this requirement is to ensure that 

flight manual information is available to the aircrew while operating the aircraft. ZEPHYR requests 

an exemption to this requirement since the aircraft is not only too small to carry documentation, the 

documentation would not be available to the crew. 

The equivalent level of safety will be achieved by keeping a hard copy of the flight manual in the 

eBee & eXom transportation box. 

14 C.F.R. § 91.109(a) & 91.319(a)(1): Flight Instruction 

The regulation provides that "No person may operate a civil aircraft that is being used for flight 

instruction unless that aircraft has fully functioning dual controls." 

Flight instruction will be accomplished through an elaborated training program, using first the 

simulation mode of the flight management software eMotion. The equivalent level of safety during 
the training will be achieved by the manufacturer or authorized distributor providing the training 

\ and through the use of experienced and qualified operators familiar with the eBee & eX om. ) 

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14 CFR § 91.119: Minimum Safe Altitudes 

The regulation provides that over sparsely populated areas the aircraft cannot be operated closer 

than 500 feet to any person, vessel, vehicle, or structure. Since the aircraft will be operating at a 

maximum of 400 feet AGL, the eBee & eXom cannot comply with this requirement. 

The equivalent level of safety will be achieved because the eBee & eXom will only fly over private 

property with the permission of the landowner. The operator will define before every flight a 

working area radius and a flight area ceiling, preventing the eBee & eXom to go beyond the flight 

area. 

The landowner and the persons who may be on the ground in the flight area will be briefed of the 

expected route of flight and the associated risks to persons and property on the ground. Due to the 

small size of the eBee & eX om and the material with which the eBee & eXom is built, the hazard 

to persons, vessels, vehicles, and structures is not comparable to manned aircraft and should be 

considered in granting the exemption. 

Moreover, the aircraft will not be operated over congested areas nor over any open-air assembly of 

persons. The aircraft will be operated at an altitude allowing, if a power unit fails, an emergency 

landing without undue hazard to persons or property on the surface. 

14 CFR 91.121- Altimeter settings 

This section requires that each person operating an aircraft shall maintain the cruising altitude or 

flight level of that aircraft, as the case may be, by reference to an altimeter that is set, when operating 

below 18,000 feet MSL to: 

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

miles of the aircraft; 

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

current reported altimeter setting of an appropriate available station; 

• In the case of an aircraft not equipped with a radio, the elevation of the departure airport or 

an appropriate altimeter setting available before departure. 

To provide an equivalent level of safety, the eBee & eXom autopilot calculates the reference altitude 

(ground level) with the on-board GPS during the pre-flight tests. The GPS and barometer data are 

merged with respect to their respective precisions. The GPS provides reliable information to correct 

potential barometric bias, while rapid variations in altitude are detected through the barometer. 

Hence, barometric bias induced by environmental factors is rejected. 

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

The regulation provides that no person may begin a flight in an airplane under day-VFR conditions 

unless there is enough fuel to fly to the first point of intended landing and to fly after that for at least 

30 minutes. 

Given the area of operation for the eBee & eXom, ZEPHYR believes that an equivalent level of 

safety is already achieved with the specific procedure preventing the eBee & eX om to accept a takeoff order is the battery level is below a given value. Moreover, SenseFly has integrated "low" and 
"critical" battery level warnings and implemented a "return to Home" (and "Go Land") actions in 

' these situations. 

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

This regulation provides as follows: 

• No person may operate a civil aircraft unless it has an appropriate and current 

airworthiness certificate. 

• No person may operate a civil aircraft unless the airworthiness certificate required by 

paragraph (a) of this section or a special flight authorization issued under §91.715 is 

displayed at the cabin or cockpit entrance so that it is legible to passengers or crew. 

The eBee weighs only 1.7 pounds (max take-offweight) & the eXom weighs 3.1 pounds. As such, 

there is no ability or place to carry certification and registration documents or to display them on 

the UAS. In addition, there is no pilot or passengers on board the aircraft. 

To obtain an equivalent level of safety and meet the intent of 91.203, ZEPHYR propose that 

documents deemed appropriate for this aircraft by the FAA will be co-located with the operator at 

the ground control station in the eBee & eXom box and available for inspection upon request 

14 CFR Subpart E (91.401- 91.417)- Maintenance, Preventive Maintenance, and 

Alterations 

The regulation provides that the operator is primarily responsible for maintaining the aircraft in an 

airworthy condition, including compliance with Parts 39 and 43. Paragraphs 91.407 and 91.409 

require that the aircraft be "approved for return to service by a person authorized under 43.7" after 

maintenance and inspection. 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. 

ZEPHYR proposes that the maintenance of the eBee & eXom will be accomplished by the 

owner/operator according to the maintenance manual, provided by SenseFly. ZEPHYR requests 

the FAA treat the eBee & eXom training program as proprietary under 14 C.F.R. 11.35(b) and not 

include this document in the public docket. 

An equivalent level of safety will be achieved because the eBee/eXom is small in size, it is not a 

complex mechanical device, it will carry no external payload, and it will operate only in restricted 

predetermined areas. 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. 

Finally, before every flight, the eBee/eXom runs automatically a sequence of pre-flight tests to 

make sure that every sensor and every critical part is running properly. If a problem is detected, the 

eBee/eXom will not be able to be switched-on and a message error is displayed on the main screen 

of 

the flight management software. The operator can then refer to the maintenance manual to 

troubleshoot this issue. Several parts of the eBee/eXom are easily interchangeable (propellers, 

wings), which allows the operator to make sure the wings and propulsion system are always 

airworthy when a mission is initiated. 
APPENDIX B: ACADEMY OF MODEL AERONAUTICS SAFETY REQUIREMENTS 

) 
Academy of Model Aeronautics National Model Aircraft Safety Code 

Effective January 1, 2014 

A. GENERAL: A model aircraft is a non-human-carrying aircraft capable of sustained flight in the atmosphere. It may not exceed limitations of this code and is 

intended exclusively for sport, recreation, education and/or competition. All model flights must be conducted in accordance with this safety code and any 

-~ditional rules specific to the flying site. 

;~odel aircraft will not be flown: 

(a) In a careless or reckless manner. 

(b) At a location where model aircraft activities are prohibited. 

2. Model aircraft pilots will: 

(a) Yield the right of way to all human-carrying aircraft. 

(b) See and avoid all aircraft and a spotter must be used when appropriate. (AMA Document #540-D.) 

(c) Not fly higher than approximately 400 feet above ground level within three (3} miles of an airport without notifying the airport operator. 

(d) Not interfere with operations and traffic patterns at any airport, heliport or seaplane base except where there is a mixed use agreement. 

(e) Not exceed a takeoff weight, including fuel, of 55 pounds unless in compliance with the AMA Large Model Airplane program. (AMA Document 520-A.) 

(0 Ensure the aircraft is identified with the name and address or AMA number of the owner on the inside or affixed to the outside of the model aircraft. (This 

does not apply to model aircraft flown indoors.) 

(g) Not operate aircraft with metal-blade propellers or with gaseous boosts except for helicopters operated under the provisions of AMA Document #555. 

(h) Not operate model aircraft while under the influence of alcohol or while using any drug that could adversely affect the pilot's ability to safely control the 

model. 

(i) Not operate model aircraft carrying pyrotechnic devices that explode or burn, or any device which propels a projectile or drops any object that creates a 

hazard to persons or property. 

Exceptions: 

• Free Flight fuses or devices that burn producing smoke and are securely attached to the model aircraft during flight. 

• Rocket motors (using solid propellant) up to a G-series size may be used provided they remain attached to the model during flight. Model rockets may 

be flown in accordance with the National Model Rocketry Safety Code but may not be launched from model aircraft. 

• Officially designated AMA Air Show Teams (AST) are authorized to use devices and practices as defined within the Team AMA Program Document. 

(AMA Document #718.) 

0) Not operate a turbine-powered aircraft, unless in compliance with the AMA turbine regulations. (AMA Document #51 0-A.) 

3. Model aircraft will not be flown in AMA sanctioned events, air shows or model demonstrations unless: 

(a) The aircraft, control system and pilot skills have successfully demonstrated all maneuvers intended or anticipated prior to the specific event. 

(b) An inexperienced pilot is assisted by an experienced pilot. 

4. When and where required by rule, helmets must be properly worn and fastened. They must be OSHA, DOT, ANSI, SNELL or NOCSAE approved or comply 

\with comparable standards. 

B. ) RADIO CONTROL (RC) 

1. All pilots shall avoid flying directly over unprotected people, vessels, vehicles or structures and shall avoid endangerment of life and property of others. 

2. A successful radio equipment ground-range check in accordance with manufacturer's recommendations will be completed before the first flight of a new or 

repaired model aircraft. 

3. At all flying sites a safety line(s) must be established in front of which all flying takes place. (AMA Document #706.) 

(a) Only personnel associated with flying the model aircraft are allowed at or in front of the safety line. 

(b) At air shows or demonstrations, a straight safety line must be established. 

(c) An area away from the safety line must be maintained for spectators. 

(d) Intentional flying behind the safety line is prohibited. 

4. RC model aircraft must use the radio-control frequencies currently allowed by the Federal Communications Commission (FCC). Only individuals properly 

licensed by the FCC are authorized to operate equipment on Amateur Band frequencies. 

5. RC model aircraft will not knowingly operate within three (3) miles of any pre-existing flying site without a frequency-management agreement. (AMA 

Documents #922 and #923.) 

6. With the exception of events flown under official AMA Competition Regulations, excluding takeoff and landing, no powered model may be flown outdoors 

closer than 25 feet to any individual, except for the pilot and the pilot's helper(s) located at the flightline. 

7. Under no circumstances may a pilot or other person touch an outdoor model aircraft in flight while it is still under power, except to divert it from striking an 

individual. 

8. RC night flying requires a lighting system providing the pilot with a clear view of the model's attitude and orientation at all times. Hand-held illumination 

systems are inadequate for night flying operations. 

9. The pilot of an RC model aircraft shall: 

(a) Maintain control during the entire flight, maintaining visual contact without enhancement other than by corrective lenses prescribed for the pilot. 

(b) Fly using the assistance of a camera or First-Person View (FPV) only in accordance with the procedures outlined in AMA Document #550. 

(c) Fly using the assistance of autopilot or stabilization system only in accordance with the procedures outlined in AMA Document #560. 

C. FREE FLIGHT 

1. Must be at least 100 feet downwind of spectators and automobile parking when the model aircraft is launched. 

2. Launch area must be clear of all individuals except mechanics, officials, and other fliers. 

'1 An effective device will be used to extinguish any fuse on the model aircraft after the fuse has completed its function. 

D. ) CONTROL LINE 

1. The complete control system (including the safety thong where applicable) must have an inspection and pull test prior to flying. 

2. The pull test will be in accordance with the current Competition Regulations for the applicable model aircraft category. 

3. Model aircraft not fitting a specific category shall use those pull-test requirements as indicated for Control Line Precision Aerobatics. 

4. The flying area must be clear of all utility wires or poles and a model aircraft will not be flown closer than 50 feet to any above-ground electric utility lines. 

5. The flying area must be clear of all nonessential participants and spectators before the engine is started. 
Academy of Model Aeronautics 

5161 East Memorial Drive Muncie, Indiana 47302 

(800) 435-9262- Membership Services 

www.modelaircraft.org 

11SEE AND AVOID" GUIDANCE 

A. General: 

4• 

Aifl~ ACADEMY OF 

MODEL AERONAUTICS 

1. The primary means to avoid collisions between all aircraft flying within our National Airspace System 

(NAS) is "See and Avoid." 

2. Vigilance must be maintained by each person operating an aircraft (whether model or manned) so as to 

"see and avoid" other aircraft. 

3. Model aircraft must avoid manned aircraft. Our privilege to fly model aircraft in the NAS depends on our 

commitment to remain "well clear" of manned aircraft. 

4. Simply avoiding an actual collision is not enough. A "near miss" is not acceptable. 

5. Unless flying at a mixed-use site where manned and model aircraft routinely share airspace through 

their own site-specific rules, model aircraft must fly sufficiently far away from manned aircraft so as not to 

create a collision hazard. 

) Model aircraft flying must not only be safe, it must be perceived to be safe by the greater manned 

aviation community. Modelers must continually demonstrate their respect for the safety of manned 

aircraft by remaining vigilant and well clear. 

7. Whenever a potential conflict arises between model aircraft and manned aircraft, the pilot of the model 

aircraft must always give way to the manned aircraft. 

8. The pilot of a model aircraft must never assume the pilot of a manned aircraft can see the= model or will 

perform any maneuver to avoid the model's flight path. 

9. Visual Line of Sight is required by the Safety Code. It means that visual contact with the aircraft must be 

maintained without enhancement other than by corrective lenses prescribed for the model aircraft pilot. 

All RC flying must remain clear of clouds smoke or any other obstruction to the line of sight. 

10. "Blue Sky" is a term used to explain the method used to increase separation between a model and a 

manned aircraft in the same vicinity. The modeler should maneuver the aircraft in such a way as to 

increase the amount of blue sky perceived between the model and the manned aircraft. By increasing the 

blue sky separation, the question about depth perception is taken out of the equation and the modeler 

need not worry whether the model is closer to him than the manned aircraft or further away. Increasing 

the blue sky between the model and the manned aircraft automatically increases separation between 

them. 

>I 

Academy of Model Aeronautics 5161 East Memorial Drive Muncie, Indiana 47302 

(800) 435-9262 1 Membership Services 1 www.modelaircraft.org 
Academy of Model Aeronautics 

5161 East Memorial Drive Muncie, Indiana 47302 

(800) 435-9262 - Membership Services 

www.modelaircraft.org 

/ 

4• 

Aw.p;, ACADEMY OF 

MODEL AERONAUTICS 

11. A modeler should never place any consideration for the well-being of the model aircraft above the 

safety of manned aircraft. Maneuvering to avoid the conflict may require that the model aircraft be 

sacrificed. 

12. Free flight models should not be launched with relatively low altitude manned 

aircraft in sight and downwind or headed downwind from the launch site. 

B. Spotters: 

1. Before a flight, the pilot must insure that the spotter understands his/her duties 

and expectations. 

2. A spotter should be used to assist in monitoring the surrounding airspace for manned aircraft whenever 

a flight is expected td exceed 400 feet above the ground and that operation is expected to be in proximity 

to known manned aircraft traffic such as at a mixed-use facility or within three miles of an airport. The 

spotter must have sufficient visual acuity and be mature enough to take this responsibility very seriously. 

3. A spotter should also be prepared to assist his/her pilot in the event that another model aircraft or 

spectators become endangered or in turn are perceived to be a danger to the pilot or the pilot's model 

)rcraft. 

4. If a model aircraft pilot experiences what he or she considers a near miss with a manned aircraft, that 

model aircraft pilot should notify AMA Headquarters with a written report of the incident, including action 

taken by the model aircraft pilot to avoid the manned aircraft. This report is intended to help the modeler, 

the club, and the AMA capture as much detail as possible so that it may be used to assist all parties in 

recalling the particulars ofthe incident at a later time. Call1-800-435-9262 {1-800-IFLYAMA} extension 230 

or 251 for assistance with this report. 

Academy of Model Aeronautics 5161 East Memorial Drive Muncie, Indiana 47302 

(800) 435-9262 I Membership Services 1 www.modelaircraft.org 
AMA Document # 560 

, SINCE 1936 

\ 

Academy of Model Aeronautics 

AMA Advanced Flight Systems Committee 

amaflightsystems@gmail.com 

Radio Controlled Model Aircraft Operation 

Utilizing Failsafe, Stabilization and Autopilot Systems 

) 

1. DEFINITION OF TERMS: 

Please refer to Page 3, section 7 which contains an alphabetical listing of the definitions of the 

terms in italics that are used in this document. 

2. GENERAL: 

All model aircraft flights utilizing stabilization and autopilot control systems must be conducted 

in accordance with AMA's current National Model Aircraft Safety Code and any additional rules 

specific to a flying site/location. 

3. OPERATIONS- REQUIREMENTS- LIMITATIONS: 

a) AMA members flying radio controlled model aircraft equipped with flight stabilization and 

autopilot systems must maintain VLOS with the aircraft at all times including programmed 

autopilot waypoint flight. 

b) AMA Pilots must be able to instantaneously deactivate programmed flight of autopilot 

systems at any time during flight and resume manual control of the model aircraft. 

c) AMA Pilots must perform an RIC Test Flight of a model aircraft before activating a newly 

installed autopilot or stabilization system and/or after any repairs or replacement of model 

aircraft essential flight systems. 

d) Model aircraft exceeding 151bs and/or 70mph may only use an autopilot for a programmed 

"return to launch" (RTL) flight and not for programmed waypoint flying of a predetermined 

course. 

e) STABILIZATION & AUTOPILOT SYSTEMS MAY BE USED FOR/TO: 

• Stabilization/automatically stabilize aircraft to level flight when control sticks are centered. 

• Recovery/activate TRX switch to recover an out of control aircraft to level flight. 

• Heading/activate TRX switch to hold a model aircraft's heading for precision flight path. 

• Altitude/activate TRX switch to maintain fixed aircraft altitude while allowing directional control. 

• Return GPS/activate TRX switch to return aircraft via GPS to launch point. 

• Return FSS/failsafe activated from radio signal loss to return aircraft via GPS to launch point. 

• Fixed circle/activate TRX switch to circle aircraft at point of activation at fixed altitude. 

• Waypointlactivate TRX switch to initiate an autopilot programmed flight path via waypoints. 

• Fencing/autopilot programed to display site unique boundaries on video monitor/goggles. 

PAGE 1 OF 3 (Revision 01 /14/2013) 
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4. RANGE -ALTITUDE -WEIGHT- SPEED: 

a) One of the requirements in Federal Law (Public Law 112-95 Sec 336 (c) (2) February 14, 

2012) for model aircraft to be excluded from FAA regulations is that model aircraft be 

flown within VLOS of the operator. 

b) Model aircraft must be flown at or below 400 feet AGL when within 3 miles of an airport as 

stated in the AMA Safety Code. 

c) Model aircraft utilizing an autopilot for waypoint flying are limited to a maximum weight 

(including fuel, batteries, and onboard autopilot systems) of 151bs and a speed of 

70mph. 

5. RECOMMENDATIONS & INFORMATION: 

a) If your radio system lacks failsafe capability, consider using programmable digital servos or 

auxiliary failsafe modules. In the event of a radio signal failure these components will 

activate desired safe servo settings or an autopilot for return to base/launch (RTL). 

b) When using an autopilot system the "return to launch" (RTL) feature should be 

programmed to return the aircraft to a safe location and safely terminate the flight should 

manual control of the aircraft be lost. When using RTL, pay particular attention to the 

manufacturer's throttle recommendations to prevent stalling. 

c) The use of stabilization systems is recommended when flying FPV to improve flight 

stability and video quality. 

d) Pilots usually choose to incorporate stabilization and autopilot systems for model aircraft 

flying to enhance flight performance, correct bad tendencies of the model aircraft, 

maintain stability in windy weather, establish precision heading holds for 

takeoffs/landings, flight training for novice pilots, create a steady flight platform for 

cameras, and generally just to make an airplane easier and safer to fly. 

e) When purchasing stabilization and autopilot systems, always try to select quality equipment 

from reputable dealers, ensure for compatibility with other onboard systems, and install 

components according to manufacturers' instructions. 

6. PRIVACY PROTECTION SAFEGUARDS: 

The use of imaging technology for aerial surveillance with radio control model aircraft 

having the capability of obtaining high-resolution photographs and/or video, or using any 

types of sensors, for the collection, retention, or dissemination of surveillance data or 

information on individuals, homes, businesses, or property at locations where there is 

a reasonable expectation of privacy is strictly prohibited by the AMA unless written 

expressed permission is obtained from the individual property owners or managers. 

PAGE 2 OF 3 (Revision 01 /14/2013) 
7. DEFINITIONS OF TERMS: 

AMA Pilot is an AMA member who is capable of manually operating an R/C transmitter to 

control a model aircraft's flight path within its safe intended flight envelope without losing 

control or having a collision. 

Autopilot Systems incorporate programmable flight stabilization with an altitude sensor and 

a GPS receiver for accurate positioning and to navigate/control a radio controlled model 

aircraft's flight path. Advanced systems offer software for entering navigable waypoints. The 

flight data waypoints may be saved to autopilot's/GPS memory for programmed flight. 

Essential Flight Systems are any systems or components necessary to maintain 

stable flight within a model aircraft's flight envelope. (This includes primary R/C systems 

and any stabilization or gyros required to maintain stability and heading in certain 

types of model aircraft that would be uncontrollable/unstable without their use). 

Failsafe Systems are designed to minimize or prevent damage and safely terminate a 

flight when a radio controlled model aircraft loses radio signal. Modern radio systems can 

be programmed to position servos to a desired control setting in the event of radio signal 

failure. 

First Person View (FPV) refers to the operation of a radio controlled (R/C) model aircraft 

using an on board camera's cockpit view to orient and control the aircraft. (AMA Document 

#550). 

Flight Envelope is defined as the range of airspeeds, attitudes and flight maneuvers which 

a model aircraft can safely perform/operate for its intended use. 

Non-Essential Flight Systems are any systems or components that are not necessary to 

maintain stable flight within the model aircraft's intended flight envelope. (This includes 

autopilot or stabilization systems that can be activated and deactivated in flight by the pilot 

without affecting manually controlled stable flight). 

RIC Test Flight requires an AMA Pilot to manually operate an R/C transmitter to control 

a model aircraft's flight path and determine if the aircraft is capable of maintaining stable 

flight within its safe intended flight envelope. 

Stabilization Systems are designed to maintain intended model aircraft flight attitudes. 

The pilot can install, program and/or activate a system to stabilize yaw, pitch, or roll or any 

one attitude or combination of attitudes. Systems are often based on rate/heading hold 

gyros or inertial motion sensors utilizing multi-axis gyros and accelerometers for 

attitude stabilization. 

Visual Line of Sight (VLOS) is the distance at which the pilot is able to maintain visual 

contact with the aircraft and determine its orientation and attitude without enhancements 

other than corrective lenses. 

PAGE 3 OF 3 (Revision 07 /20/2013) 
) 

) 

APPENDIX C: PRIVACY ISSUES 

The eBee/eXom is proposed to be flown over sterile, unpopulated to lightly populated areas generally 

over private railroad property not open to the general public at the direction of the owner railroad. In 

addition, we propose to obtain landowner permission to fly over properties as part of our services and 

to notify non-landowners over which we will be flying. Finally, most of our flights will be 300 to 400 

feet above ground surface, making visual recognition of people on the ground impossible. Because of 

the sterile environment and the pre-notification of landowners and personnel on the ground, privacy 

compromises due to ZEPHYR activities are anticipated to be alleviated. Under no circumstances will 

ZEPHYR's aircraft be utilized to purposefully invade the privacy of peoples or properties in areas 

within our studies or outside of our study boundaries. 
\ 

) 

APPENDIX D: SAFETY CASE 

Safety of our flight crew, other aircraft, people on the ground, and public and private properties is of 

utmost importance to ZEPHYR. ZEPHYR's Pilot in Command (PIC) will be responsible for all 

safety procedures and protocols while on the ground. The Visual Observer (VO) will assist the PIC 

in maintaining safety procedures throughout the course of a project. Safety procedures to be utilized 

in the filed include the following: 

• A full diagnostic check of the aircraft by the PIC and VO using a pre-flight checklist will be 

performed on the ground prior to commencement of each project; 

• High visibility (day-glow orange or green) will be worn by the flight crew during each 

project. In addition, at the ground station, a high contrast flag or banner that contains the 

words "Unmanned Aircraft Ground Station" will be placed prior to any flights; 

• Operations to be conducted over private or public controlled-access property where 

approved; 

• Permission from the land owner/authority required before commencing any flight; 

• Operations over congested areas shall be avoided; 

• Operations will not interfere with manned aircraft operations, will yield the right of way to 

manned aircraft, and operators must See & A void other aircraft and obstacles at all times. 

Use of an ADS-B receiver by the VO will assist in monitoring the presence of other proximal 

aircraft; 

• Operations limited to Visual Flight Rules Meteorological Conditions (VMC) and daylight 

hours 

• Aircraft operations will remain within Visual Line of Sight (VLOS) and will be visually 

monitored at all times; 

• Use of a high-definition first-person view from the aircraft will assist the PIC and VO 

identify potential flight conflicts and terminate or alter the pre-programmed flight plan; 

• VLOS guaranteed with a GPS geo-fence around operator of 0.5 miles 

• Flight ceiling pre-programed at 400 feet; 

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

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

the airport; 

• All operations will comply with required permissions and permits established by territorial, 

state, county or city jurisdictions; including local law enforcement, fire, or other appropriate 

governmental agencies; 
\ 

) 

• Post-flight inspection of the aircraft will be performed by the PIC and VO utilizing a 

postflight checklist; 

• The eBee operations will be compliant with existing safety procedures inherent to the 

activities ofthe related company. 
', 

) 

\ 

) 

\ 

) 

--------sense Fly 

Extended User Manual 

eBee and eBee Ag 

Revision 14 I December 2014 

Copyright© 2010-2015 senseFiy Ltd 

"-'~ 

sense Fly 

a Parrot company 

\ 

) 

GENERAL INFORMATION 

READ THIS USER MANUAL CAREFULLY BEFORE USING A SENSEFLY LTD PRODUCT. 

sense Fly Ltd products are intended for professional use only. 

Applicable Regulations 

senseFiy Ltd products are subject to Civil Aviation regulations. Regulations may vary depending on the country 

where you intend to operate your product. 

ANY USE OF SENSEFLY LTD PRODUCTS IN BREACH OF THE LAW OF THE COUNTRYWHEREYOU OPERATE THE PRODUCT 

IS UNDER YOUR SOLE RESPONSIBILITY. 

INFORM YOURSELF BEFORE USING THE PRODUCT. SOME COUNTRIES MAY HAVE LAWS THAT LIMIT THE USE OF UNMANNED AIRCRAFT TO 'LINE-OF-SIGHT' OPERATIONS AND/OR PROHIBIT THE USE OF UNMANNED AIRCRAFT AT ALL 

OR IN SPECIFIC AREAS. 

Privacy 

Recording and circulating an image of an individual may constitute an infringement of their image and privacy for 

which you can be liable. Ask for authorization before taking pictures of an individual, particularly if you want to keep 

your recordings and/or circulate images on the Web or any other medium. Do not circulate degrading images or 

ones that could undermine the reputation or dignity of an individual. Check that your use of the cameras on board 

senseFiy Ltd products comply with the legal provision on privacy in the country where you operate your product. 

Limited Warranty 

SenseFiy Ltd warrants that the product will be free from defects in material and workmanship for a period of twelve 

(12) months from the date of delivery. Sense Fly Ltd further warrants that the product will perform substantially in 

accordance with its specification. During the warranty period senseFiy Ltd's sole liability shall be at senseFiy Ltd's 

sole option, either to repair or to replace the defective product with another product or a product with similar specifications, at no charge, or to reimburse the purchase price of the product, or if repair or replacement is not possible, 

issue a credit note; provided however, that the defect has been confirmed by senseFiy Ltd and that the defective 

product is returned to senseFiy Ltd in accordance with the support and repair form together with all required flight 

logfiles. 

Warranty does not apply, without limitation, in case: a) the products are not stored and used according to their 

specifications, b) the products are damaged due to carelessness, negligence, or wrong use by the user, and c) for 

defects due to normal wear and tear including, but not limited to, deterioration to the airframe after first flight, 

normal degradation, misuse, moisture or liquids, proximity or exposure to heat, accidents, excessive strain, abuse, 

neglect, misapplication, repairs or modifications made by third party other than senseFiy Ltd, damage due to manual 

operation, damage due to take-off or landing location with obstacles, damage due to low altitude flight, damage due 

to loss of data radio connection, damage due to strong wind, rain or humidity, or other causes for which senseFiy Ltd 

has no control. 
THE FOREGOING WARRANTIES ARE IN LIEU OF ALL WARRANTIES, EITHER EXPRESSED OR IMPLIED, INCLUDING WITHOUT LIMITATION ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, AND OF 

ANY OTHER OBLIGATION ON THE PART OF SENSE FLY LTD. 

Limitation of liability 

TO THE EXTENT PERMITTED BY APPLICABLE LAW, IN NO EVENT WILL SENSEFLY LTD BE LIABLE FOR ANY LOSS OF REVENUE, LOSS OF PROFIT, LOSS OF DATA, OR INDIRECT, SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES, EVEN IF 

SENSEFLY LTD HAS BEEN NOTIFIED OF THE POSSIBILITY OF SUCH DAMAGES, AND WHETHER THIS LIABILITY ARISES 

FROM A CLAIM BASED ON CONTRACT, WARRANTY, TORT OR OTHERWISE, WITH THE EXCEPTION OF GROSS NEGLIGENCE AND DEATH. 

YOU SHALL AT ALL TIMES OPERATE THE PRODUCT IN AREAS OR UNDER CIRCUMSTANCES SO AS TO GUARANTY SECURITY AND SAFETY OF PEOPLE, PROPERTY AND ANIMALS. 

FCC and iC Compliance statement: 

~ This device complies with part 15 of the FCC Rules and Industry Canada License-exempt RSS standard(s). 

Operation is subject to the following two conditions: 

1. This device may not cause harmful interference, and 

2. This device must accept any interference received, including interference that may cause undesired operation. Changes or modifications not expressly approved by the party responsible for compliance could void 

the user's authority to operate the equipment. 

This equipment has been tested and found to comply with the limits for a class B digital device, pursuant to part 

15 of the FCC Rules. These lim its are designed to provide a reasonable protection against harmful interference in a 

residential installation. This equipment generates, uses and can radiate radio frequency energy and, if not installed 

and uses in accordance with the instructions, may cause harmful interference to radio communications. However, 

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

interference to radio or television reception, wich can be determined by turning the equipment off and on, the user 

is encouraged to try to correct the interference by one or more of the following measures: 

1. Reorient or relocate the receiving antenna 

2. Increase the separation between the equipment and the receiver 

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

4. Consult the dealer or an experienced radio/TV technician for help. 
.. " 

) 

\ 

) 

This Class B digital apparatus complies with Canadian ICES-003. 

This equipment complies with FCC's radiation exposure limits set forth for an uncontrolled environment under the 

following conditions: 

1. This equipment should be installed and operated such that a minimum separation distance of 20cm is 

maintained between the radiator (antenna) and user's/nearby person's body at all times. 

2. This transmitter must not be co-located or operating in conjunction with any other antenna or transmitter. 

Disposal of this product at the end of its life 

~ At the end of this product's life, please do not dispose of this product in your general household waste. A Instead, in order to prevent possible harm to the environment or human health from uncontrolled waste 

disposal, please dispose of this product separately in accordance with your local laws and regulation. For 

- more information on the separate collection systems for waste electrical and electronic equipment that 

are available for consumers, near your home, free of charge, please contact your local municipal authority. 

You can also contact senseFiy Ltd or the reseller from which you purchased your drone who may provide recycling 

services or be part of a recycling scheme. 

Copyrights 

senseFiy Ltd reserves the right to make changes to specifications and product descriptions contained in this document at any time without notice. Please consult www.sensetly.com for the latest release. 

Copyright© 2015 sense Fly Ltd. All rights reserved. REPRODUCTION, USE OR DISCLOSURE OF ALL OR IN PART OF THIS 

MANUAL TO THIRD PARTIES WITHOUTTHE PRIOR WRITTEN PERMISSION OF SENSEFLY LTD IS STRICTLY PROHIBITED. 
) 

Address 

sense fly Ltd 

Route de Geneve 38 

1033 Cheseaux-Lausanne 

Switzerland 

Website: http:/ /www.sensefly.com 

Technical support 

If you have questions about any of your senseFiy products: 

• Try our Knowledge Base. You can find it within my.senseFiy (http://my.sensefly.com). 

• Send an email to support@sensefly.com. 
"· ) 

\. 

) 

Welcome to your eBee 

Congratulations on your purchase of the eBee, a complex and powerful yet intuitive autonomous mapping system. We take great care to develop and design the 

best possible hardware and software tools for quick, high-quality and easy-to-use 

20 and 30 aerial mapping. 

0 Note: This manual refers to the version 2.4 of eMotion and version 3.2 

of Postflight Terra 3D software. Check the software version included 

in your package and consult the Release Notes for potential changes 

included in more recent versions of the software. 
\ 

I 

I 

Package contents 

eBee 

battery 

packs 

spare 

propeller 

remote control, 

cables and 

propeller 

attachment 

bands 

ground 

modem 

EPP 

glue 

wing eBee 

central body 

wing 

User manual 

battery 

charger 

eBee 

battery 

charger 

cable 

camera 

charger 

camera 
\ 

) 

The standard eBee package contains the following items: 

• 1x carrying case with foam protection 

• 1 x eBee central body with built-in autopilot 

• 1xpairofdetachablewings 

• 1 x spare propeller 

• 1 Ox spare propeller attachment rubber bands 

• 2x Lithium-Polymer battery packs 

• 1x Lithium-Polymer battery charger (including cables) 

• 1x 2.4 GHz USB ground modem (FCC ID: 2AC2VGMEBEE) for radio data link 

(including USB cable) 

• 1x 2.4 GHz remote control (including including 3 AA batteries) 

• 1 x still camera (including memory card, battery and charger) 

• 1x USB cable for interfacing with camera and on-board autopilot 

• 1xEPPglue 

• 1x eBee User Manual 

• 1x camera User Manual 

Depending on your order, your package may also include other items, such as 

additional payloads. Please verify upon delivery that your package is complete. 

In case of a missing item, please contact your eBee reseller immediately. 

0 Note: Camera user manuals are also available to download from our 

Knowledge Base, part of my.senseFiy*. 

* http://my.sensefly.com 
\. 

' / 

Hardware features 

data link antenna----- ----=:s~-- battery compartment 

"'/'""'14"-- pitot probe, status LED 

Top face of the eBee 

ground 

sensor -------;;.-;---,;..~~ 

Bottom face of 

the central body =:::::==::l§:==--

~~";----- central body ~--"k- camera compartment 

servo connection 

mechanism 

~--->.,-------~--propeller 

--~---wing 

Detachable 

wing 

The eBee is an autonomous flying drone comprised of the following components: 

• Central body: This is the core of the eBee and includes all the electronics, 

actuators and communications hardware on-board the drone. 

• Wing: The two wings of the eBee are detachable for storage and replacement. Each wing has two wing struts and two clips to hold it in place within 

the central body. 
J 

/ 

• Winglets: These structures add aerodynamic stability to the drone while it 

is in flight. 

• Ailerons: Used to control the eBee while in flight. 

• Servo connection mechanism: The ailerons are connected to the servomotors within the central body oft he drone through this connection mechanism. 

• Propeller: Used to generate thrust while it is in flight. 

Caution: When attached to the motor the propeller spins at high 

speeds and can be potentially dangerous if it comes into contact with 

exposed skin. Be sure to always keep your hands clear oft he propeller 

when the battery is attached to the eBee. 

• Battery compartment: The eBee is powered by a LiPo (Lithium Polymer) 

battery stored within the battery compartment. 

Caution: Proper care of your battery is essential. Please read section 

'Proper battery care' on page 140 before using your drone for the first 

time. 

• Camera compartment: The eBeefeatures a built-in camera for taking aerial 

images stored within the camera compartment. 

• Data Link Antenna: Used by the drone to communicate with the eMotion 

software through the USB ground modem. 

• Pitot probe: This is the sensor used by the eBee to detect airspeed, wind 

and altitude. It must be kept clean and clear of obstructions to function 

properly. 

• Status LED: This coloured LED displays the current state of the eBee. It is 

housed underneath the pitot probe and thus illuminates the entire transparent probe in various colours depending on the drone's state. 
\ 

) 

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• Ground sensor: The ground sensor, composed of a high-speed optical 

sensor and lens assembly, is used to detect the proximity of the ground. 
\ 

Software features 

The eBee package allows you to download and use eMotion* and 

Postflight Terra 30 * t at no extra cost. 

eMotion 2 

sense Fly 

eMotion is the integrated software package that allows you to interact with your 

eBee. Its easy-to-use interface allows you to plan a mapping flight intuitively from 

the comfort of your office or directly in the field. Once the drone is launched, you 

can use eMotion's wireless connection with your eBee to track its position, monitor 

the progress of your mapping flight and send commands if desired. 

Postfli ht ,.1 1

' 

Terra .. Powered by Pix4D ~ 

Once your eBee returns after an aerial mapping flight it is the turn of Postflight 

Terra 30 to process the captured images fully automatically. Postflight Terra 30 is 

a full-featured mapping solution: with just a few mouse clicks it can create highquality gee-referenced 2D and 3D orthomosaics and digital elevation/surface models (DEM/DSM). While you are still in the field Postflight Terra 30 analyses the quality of the captured images and generates an easy to understand report, letting you 

know immediately if the data you captured meets your mapping requirements. 

* Software access terms and conditions apply 

t Postflight Terra 3D works with eBee images only 
\ 
Contents 

Quick start guide 19 

1 Planning and simulating a flight 20 

1.1 Installing eMotion, Postflight Terra 30, and the ground modem 

drivers . . . . . . . . 20 

1.2 

1.3 

1.4 

1.5 

1.6 

The eMotion interface .. 

Creating a new flight plan 

The mission phase of a flight . 

Simulating your flight ... 

Getting ready for a mission 

2 Executing a flight 

2.1 Weather check 

2.2 Preparing the eBee for flight 

2.3 The setup phase of a flight . 

2.4 Take-off .......... . 

2.5 In-flight monitoring and control . 

2.6 Landing ........ . 

2.7 Potential in-flight errors 

3 Processing image data 

3.1 Importing images and flight data 

3.2 In-field image quality check ... 

3.3 Creating advanced mapping products 

21 

23 

24 

26 

27 

29 

29 

30 

39 

43 

46 

48 

48 

50 

50 

53 

55 
II Advanced functionalities 

4 Understanding aerial mapping with the eBee 

4.1 Waypoints and their properties .. 

4.2 Advanced polygonal mission area . 

4.3 3D mission planning using elevation data .. 

4.4 Flight visualization in Google EarthTM . . .. 

4.5 Autonomous controller and modes of flight . 

4.6 Linear landing . . . . . . . . . . . ..... 

4.7 Flying multiple drones at the same time .. 

4.8 Individual photo targets and oblique imagery 

4.9 Emergency Manoeuvres 

5 eMotion in-depth guide 

5.1 Toolbar ... 

5.2 Simulator . 

5.3 Control Bar 

5.4 Flight Monitoring tab 

5.5 Setup Phase tab . . . 

5.6 Mission Planning tab . 

5.7 Mission Waypoints tab . 

5.8 Camera tab . . . . . . 

5.9 Flight Parameters tab 

6 Manual control of the eBee 

6.1 

6.2 

Enabling manual control . 

Pre-flight testing of the remote control 

57 

58 

58 

62 

63 

66 

68 

72 

77 

83 

85 

89 

90 

93 

95 

98 

102 

106 

115 

117 

122 

126 

126 

128 
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6.3 Full Manual mode ... 

6.4 Assisted Manual mode . 

129 

130 
Situational awareness & assistance 

Multidirectional video feed 

Source Navcams (visual sensor) 

Number 5 

Video VGA (640 x 480 pixels) 

Horizontal field of view 100 degrees 

Availability One navcam at a time 

Object & range detection 

Sensor Ultrasonic 

Number 5 

Range Up to 6 m (20ft) 

Feedback Audio and visual object warning 

Operational safety 

Shrouding 

Material I Carbon fibre 

Function Defines propeller rotation area 

Protects from damage at low speed 

Signalisation lights 

Navigation lights I 2 green on the right, 2 red on the left 

Anti-collision lights 1 top strobe, 1 bottom strobe 

Ground proximity detection 

Avoidance procedure I Automatic stop (can be deactivated) 

Warning signals . Audio & visual 

Flight assistance features (Interactive mode) 

Cruise control Maintains (low) constant speed in a 

given direction 

Distance lock Keeps distance to frontal objects 

3 - 5 m (9.8- 16ft) 

Obstacle avoidance Depending on flight phase 

Safety procedures 

Automated failsafe behaviours 

Operator triggered 

Geofencing, return home, 

emergency stop, emergency landing 

Hold position, return home, go land, 

land now, emergency motor cut-off 

Autopilot fallback 

Type . 

Manual RC control I 

Independent low-level autopilot 

(backup for main autopilot) 

Independent RC controller 

(take manual control at any time) 

--- -~-"--'-----'--'----

Ground statl6n software 

Software application sense Fly eMotion X (supplied) 

Mission planning Intuitive 3D user interface 

Click and drag to set mission blocks 

Automatic 3D flight planning 

Edit mission plans during flight 

Flying Automated system checks 

Automated take-off & landing 

Real-time flight status 

Main camera video feed integration 

Thermal video feed integration 

Navcam video feed integration 

Fully automatic flight 

Interactive Screen Fly 

Manual flight (with assistance 

functions) 

In-flight switch between flight modes 

Black-box recording of all flight & 

' mission parameters 

After your flight Project & data management 

Seamless interface to Postflight 

Terra 3D 

DNG to JPEG conversion 

Image processing 

Software application PostflightTerra 3D (supplied) 

Processing Rapid Check processing 

Quality Report 

Automatic Aerial Triangulation (AAT) 

and Bundle Block Adjustment (BBA) 

Automatic point cloud classification 

and DTM extraction 

Point cloud filtering and smoothing 

Automatic brightness and colour 

correction 

rayCioud Editor [ Point cloud viewing & editing 

Polyline, surface & stockpile 

measurement 

Digitisation tools/vector object 

editing 

Fly-through animation 

Mosaic Editor I Seam line editing 

Planar/ortho projection selection 

Mosaic colour/brightness editing 

Output results 2D and 3D (orthoimage, point 

cloud, vector data, etc.) 

Optimised camera position, 

external orientation and internal 

parameters, undistorted images 

nical specifications 

--------sense Fly 
\,,~ 

Flight system ------··-

Type V-shaped quadcopter 

Dimensions (ind shrouding) 56 x 80 x 17 em (22 x 32 x 7 in) 

Engines 4 electric brush less motors 

Propellers 4 

Take-off weight 1.8 kg (3.91b) incl. battery, payload & 

shrouding 

Flight time (full system) Up to 22 min 

Max. climb rate 7 m/s (15 mph) 

MaK airspeed Automatic flight: 8 m/s (18 mph) 

Manual flight:12 m/s (27 mph) 

Wind resistance Automatic: up to 8 m/s (18 mph) 

Manual: up to 10 m/s (22 mph) 

Autopilot & control IMU, magnetometer, barometer 

&GPS 

Materials Composite body, moulded carbon 

·, fibre arms and legs, precisionmolded magnesium frame, 

precision-molded injected plastic 

Operating temperature -10 to 40° C (14°-1 04° F) 

Wireless communication 

Main communication link 

Type Digital, dual omnidirectional 

antennas, dual band, encrypted 

Frequency 2.4 GHz & 5 GHz ISM bands 

(country dependent) 

Data transmitted Commands, main camera stream, 

navcam stream, sensor data, etc. 

Range Up to 2 km (1 .2 mi) 

RC (Remote control) 

Type Digital 

Frequency I 2.4 GHz 

Range Up to 800 m (0.5 mi) 

System power 

Technology 

Type 

Power level display 

Charging time 

Smart battery 

LiPo, 3 cell, 8500 mAh 

LED display on battery, on-screen 

information 

1 - 1.5 h 

Integrate(( payloads 

Main camera 

Still images 38 MP, mechanical shutter 

DNG (RAW image with correction 

metadata) 

Ground sampling distance (GSD): 

- 1 mm/pixel at 6 m 

- 1 em/pixel at 60 m 

Recorded on board 

Gee-referenced (position & 

orientation) 

Video HD (1280 x 720 pixels) 

Recorded on board or streamed 

Horizontal field of view 63 degrees 

Digital zoom 6x 

Thermal camera 

Still images/video Thermal (80 x 60 pixels) overlaid on 

main camera stream 

Horizontal field of view 50 degrees 

Edge enhancement Yes 

Head navcam (visual sensor) 

Video 

Video live streaming range 

Horizontal field of view 

VGA (640 x 480 pixels) 

Up to 2 km (124 miles) 

100 degrees 

Lights 

Headlamp · Yes, used for video 

Flash I Yes (not active upon release) 

Number 4 navcams 

Positions Left, right, rear, bottom 

Video , VGA (640 x 480 pixels) 

Horizontal field of view 1100 degrees 

Availability One navcam at a time 

Operational use Side views (w/o turning main 

camera) & parallel flight along 

objects 

Back-up safely & control in 

tight environments 

Landing & ground proximity 

Flight modesTypes Automatic 

'llllteractive ScreenFiy 

Manual (RC) 

Availability Switch between modes at any time 

Automatic 

Control interface 

Mission planning 

Types of mission blocks 

In-flight mission changes 

Mouse, keyboard or touchscreen 

Drag,and-drop mission blocks 

Horizontal mapping 

Around point of interest 

User,defined route 

Yes: manual waypoint changes and 

updates possible at any time 

Interactive Screen Fly 

Primary control interface 

Flight assistance 

(depending on the flight phase) 

Screen-based actions & USB joypad 

Cruise control 

Distance lock 

Obstacle avoidance 

Manual (RC) 

Primary control interface 1 RC (remote control) 

On-board computing 

Type 4 on-board CPUs 

Quad-core processor ;, Pr'1nc·1pal autopilot & artificial 

intelligence 

Dual-core processor Video co-processing 

Single-core processor Low-level autopilot (safety fallback) 

and motor control 

Single-core processor Communication link management 

The information contained in this brochure is for promotional purpo>es only and does not 

constitute an offer, warranty or contract. 
-------- senseFiy 

Extended User Manual 

Revision 1.1 I August 2015 

Copyright© 2015 senseFiy Ltd 

"-'v- senseFiy 

a Parrot company 
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GENERAL INFORMATION 

READ THIS USER MANUAL CAREFULLY BEFORE USING A SENSEFLY LTD PRODUCT. 

sense Fly Ltd products are intended for professional use only. 

Always comply with Civil Aviation regulations, act responsibly and follow the instructions in this User Manual 

Applicable Regulations 

senseFiy Ltd products are subject to Civil Aviation regulations. Regulations may vary depending on the country 

where you intend to operate your product. 

ANY USE OF SENSEFLY LTD PRODUCTS IN BREACH OF THE LAW OF THE COUNTRY WHERE YOU OPERATE THE PRODUCT 

IS UNDER YOUR SOLE RESPONSIBILITY. 

INFORM YOURSELF BEFORE USING THE PRODUCT. SOME COUNTRIES MAY HAVE LAWS THAT LIMIT THE USE OF UNMANNED AIRCRAFT TO 'LINE-OF-SIGHT OPERATIONS AND/OR PROHIBITTHE USE OF UNMANNED AIRCRAFT IN ALL 

OR IN SPECIFIC LOCATIONS. 

Privacy 

Recording and circulating an image of an individual may constitute an infringement of their image and privacy for 

which you can be liable. Ask for authorisation before taking pictures of an individual, particularly if you want to keep 

your recordings and/or circulate images on the internet or any other medium. Do not circulate degrading images or 

ones that could undermine the reputation or dignity of an individual. Check that your use of the cameras on board 

sense Fly Ltd products complies with the legal provision on privacy in the country where you operate your product. 

Limited Warranty 

Sense Fly Ltd warrants that the product will be free from defects in material and workmanship for a period of twelve 

(12) months from the date of delivery. senseFiy Ltd further warrants that the product will perform substantially in 

accordance with its specification. During the warranty period senseFiy Ltd's sole liability shall be at senseFiy Ltd's 

sole option, either to repair or to replace the defective product with another product or a product with similar specifications, at no charge, or to reimburse the purchase price of the product, or if repair or replacement is not possible, 

issue a credit note; provided however, that the defect has been confirmed by senseFly Ltd and that the defective 

product is returned to senseFly Ltd in accordance with the support and repair form together with all required flight 

log files. 

Warranty does not apply, without limitation, in case: a) the products are not stored, maintained or used according to 

their specifications, b) the products are damaged due to carelessness, negligence, or wrong use by the user, and c) for 

defects due to normal wear and tear including, but not limited to, normal degradation, misuse, moisture or liquids, 

proximity or exposure to heat, accidents, excessive strain, abuse, neglect, misapplication, repairs or modifications 

made by third party other than sense Fly Ltd, damage due to manual piloting in RC (remote controlled) or interactive 

flight, damage due to take-off or landing location with obstacles, damage due to low altitude or close-object flight, 
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damage due to relying on visual or/and ultrasonic feedback and in more general terms on any kind of situational 

awareness assista nee, damage due to using any kind of flight assistance features including but not limited to cruise 

control, distance lock and obstacle avoidance, damage due to loss of data radio connection, damage due to strong 

wind, rain, water or humidity, or other causes for which senseFiy Ltd has no control. 

Battery cells are excluded from warranty after first use. 

THE FOREGOING WARRANTIES ARE IN LIEU OF ALL WARRANTIES, EITHER EXPRESSED OR IMPLIED, INCLUDING WITHOUT LIMITATION ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, AND OF 

ANY OTHER OBLIGATION ON THE PART OF SENSEFLY LTD. 

Limitation of liability 

TO THE EXTENT PERMITTED BY APPLICABLE LAW, IN NO EVENT WILL SENSEFLY LTD BE LIABLE FOR ANY LOSS OF REVENUE, LOSS OF PROFIT, LOSS OF DATA, OR INDIRECT, SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES, EVEN IF 

SENSEFLY LTD HAS BEEN NOTIFIED OF THE POSSIBILITY OF SUCH DAMAGES, AND WHETHER THIS LIABILITY ARISES 

FROM A CLAIM BASED ON CONTRACT, WARRANTY, TORT OR OTHERWISE, WITH THE EXCEPTION OF GROSS NEGLIGENCE AND DEATH. 

YOU SHALL AT ALL TIMES OPERATE THE PRODUCT IN AREAS OR UNDER CIRCUMSTANCES SO AS TO GUARANTY SECURITY AND SAFETY OF PEOPLE, PROPERTY AND ANIMALS. IN THAT CONTEXT YOU MUST UNDERSTAND THAT PRODUCT 

FEATURES SUCH AS, BUT NOT LIMITED TO, AUTOPILOT, GPS, WIRELESS COMMUNICATION LINK, MULTIDIRECTIONAL 

VIDEO FEED, ULTRASONIC SENSORS, SITUATIONAL AWARENESS, FLIGHT ASSISTANCE, CRUISE CONTROL, DISTANCE 

LOCK, OBSTACLE AVOIDANCE AND GROUND DETECTION CAN FAIL AND THAT YOU SHOULD AT NO MOMENT RELY 

SOLELY ON THEM. 

Disposal of this product at the end of its life 

"Q/ At the end of this product's life, please do not dispose of this product in your general household waste. A Instead, in order to prevent possible harm to the environment or human health from uncontrolled waste 

disposal, please dispose of this product separately in accordance with your local laws and regulation. For 

- more information on the separate collection systems for waste electrical and electronic equipment that 

are available for consumers, near your home, free of charge, please contact your local municipal authority. 

You can also contact senseFiy Ltd or the reseller from which you purchased your drone who may provide recycling 

services or be part of a recycling scheme. 

Copyrights 

senseFiy Ltd reserves the right to make changes to specifications and product descriptions contained in this document at any time without notice. Please consult www.sensefly.com for the latest release. 

Copyright© 2015 senseFiy Ltd. All rights reserved. REPRODUCTION, USE OR DISCLOSURE OF ALL OR IN PART OF THIS 

MANUAL TO THIRD PARTIES WITHOUT THE PRIOR WRITTEN PERMISSION OF SENSEFLY LTD IS STRICTLY PROHIBITED. 
Address 

senseFiy Ltd 

Route de Geneve 38 

1033 Cheseaux-Lausanne 

Switzerland 

Website: http://www.sensefly.com 

Technical support 

senseFiy and our distributors are dedicated to providing you with full professional product support. 

To submit a support ticket and/or view your outstanding tickets, please use our customer portal at 

my.senseFiy.com. Log in with the same account details you used to download your drone's software 

(see the separate software information document in your eXom 's case). 

In addition to support access, my.senseFiy includes: 

• Details of all your senseFiy drones, including their serial numbers. 

• The Knowledge Base- packed full of helpful articles, tips, tutorials and webinars. 

• Download links for the latest versions of eMotion X and Postflight Terra 3D software. 
Welcome to your eXom 

Congratulations on your purchase of the eXom. This intelligent mapping and 

inspection drone (UAV, RPAS or UAS) offers TripleView imaging, advanced situational awareness, and a choice of flight modes: Autonomous mapping mode, 

Interactive Screen Fly mode, plus a Manual RC mode for experienced pilots. 

At senseFiy we build our products to the very highest standards. Inspired by the 

aeronautical backgrounds of our founders, we test both individual components 

and finished drones extensively in order to achieve the highest possible level of 

safety and reliability. 

We hope you enjoy using your eXom. 
\, 

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About this user manual 

A complete guide to your eXom comprises: 

• A user manual 

All you need to get you into the air safely and effectively. 

• An extended guide to the eXom 

Completes and complements the user manual, giving you a full guide to 

using the eXom. 

This document contains both. The user manual is also supplied on paper with 

youreXom. 

0 Note: This user manual refers to eMotion X version 1.0.0 and Postflight Terra 3D version 4. You can always find the latest versions of 

these on my.senseFiy*. The eXom requires eMotion X to operate. 

* http://my.sensefly.com 
Package contents 

The standard eXom package contains the following items: 

• 1x eXom drone 

• 1x Interactive Screen Fly Controller 

• 1x 2.4 GHz Remote Control (for safety pilots) 

• 1x 2.4 GHz I 5 GHz dual band USB radio modem 

• 2x SD memory cards (32GB) 

• 2x batteries 

• 2x single battery chargers w/power supplies 

• 1 x wheeled carry case 

• 1x User Manual 

• 1xUSBcableset 

• 1 x spare leg set 

• 1 x spare propeller set 

• eMotion X & Postflight Terra 30 software* 

Depending on your order, your package may also include other items. Please verify upon delivery that your package is complete. In case of a missing item, please 

contact senseFiy or your eXom reseller immediately. 

* download from my.senseFiy at no extra cost 
Hardware features 

TripleView head 

Left sensor module 

Left 

\ 

j 

Leg~---~-

Top 

Right sensor module 

Power button/ 

status LED & top strobe 

Right 

.__j ·~':··o:- .. --Leg clip ::-_:::~:-·-

Rear sensor module 

Ultrasonic transmitter 

Left navcam 

Ultrasonic receiver ~-_j 

Port access cover 

Navigation light 

Motor 
/ 

Triple View Head 

Flash* 

Main camera Thermal camera 

) 

Head sensor -----...:.~+--++--+----, 

module 

Ultrasonic receiver----------~ 

Head navcam _____ __. 

Ultrasonic transmitter ---------l 

*will be activated in a future firmware update 
Bottom 

Bottom sensor module ---------, 

TripleView head ------, Maintenance cover 

) 

,Q· 

!---Jl 

· _>/- 1,'~' '"' 'i! •

1

? ---,--+cc-r:__:.:__,--"'--:--__,. Batt om strobe 

q 

:! :i: 1 I " i!' 

Battery--· --,--.:------_,'_,1 -'=';---, '/• I 1: 

,, r·,, -- J I li'l 

, ! :~df~ator ,~€~}}"' , '-::~~~~~- 'l 

·Battery 

Battery release tabs-----' 
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Ports 

SD card slot ------------,r':::___--=="'-----== 

Autopilot port ------+--==2----=r---==:":." 

Maintenance port* ~--------,£-,"---+--------===-

Battery 

:I i/ 

*Do not use 

Battery release tabs