IN THE MATTER OF THE PETITION FOR EXEMPTION OF: 

Jonathan Martin

FOR AN EXEMPTION SEEKING RELIEF FROM THE REQUIREMENTS OF

TITLE 14 OF THE CODE OF FEDERAL REGULATIONS

SECTIONS 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & 

(a)(2), AND 91.417(a) & (b) CONCERNING COMMERCIAL OPERATION OF 

TAROT 650 SPORT UNMANNED AIRCRAFT SYSTEMS

PURSUANT TO SECTION 333 OF

THE FAA MODERNIZATION AND REFORM ACT OF 2012 

(PUBLIC LAW 112-95)

Submitted on JUNE 3, 2015

Jonathan Martin 

582 Coatesville RD 

West Grove, PA 19390 

(610)476-1702 

FutureAviatorsUSA@gmail.com

UNITED STATES OF AMERICA 

DEPARTMENT OF TRANSPORTATION 

FEDERAL AVIATION ADMINISTRATION 

WASHINGTON, DC
TABLE OF CONTENTS

Page

GLOSSARY OF ABBREVIATIONS 3

SUMMARY 4

INTRODUCTION AND INTERESTS OF PETITIONER 4

BACKGROUND 5

BASIS FOR PETITION 5

NAME AND ADDRESS OF PETITIONER 7

THE SPECIFIC SECTIONS OF 14 C.F.R. FROM WHICH JONATHAN 

MARTIN SEEKS EXEMPTION 8

THE EXTENT OF RELIEF JONATHAN MARTIN SEEKS AND THE 

REASON JONATHAN MARTIN SEEKS THE RELIEF 11

THE REASONS WHY GRANTING JONATHAN MARTIN REQUEST

WOULD BE IN THE PUBLIC INTEREST 13

THE REASONS WHY GRANTING THE EXEMPTION WOULD NOT 

ADVERSELY AFFECT SAFETY 15

CONCLUSION 26 
GLOSSARY OF ABBREVIATIONS

AGL Above Ground Level

AOI Area of Interest

ATC Air Traffic Control

ATO Air Traffic Organization

AV Aerial Vehicle

CFR Code of Federal Regulations

COA Certificate of Authorization

FAA Federal Aviation Administration

FAR Federal Aviation Regulation

GCS Ground Control Station

GPS Global Positioning System

LOL Loss of Link

NAS National Airspace System

NOTAM Notice to Airman

PIC Pilot In Command

Section 333 FAA Modernization and Reform Act of 2012 (FMRA) 

Section 333

SO Safety Observer

SOP Standard Operating Procedures

UA Unmanned Aircraft

UAS Unmanned Aircraft System

VFR Visual Flight Rules

VLOS Visual Line of Site

VMC Visual Meteorological Conditions

VTOL Vertical Takeoff and Landing
SUMMARY

Jonathan Martin seeks exemption from the requirements of 14 C.F.R §§ 91.7(a), 

91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) &

(a)(2), and 91.417(a) & (b), to operate an Unmanned Aircraft System pursuant to Section 

333 of the FAA Modernization and Reform Act of 2012 (FMRA). This exemption will

permit Jonathan Martin to operate an Unmanned Aircraft System (UAS) for the

commercial purpose of conducting aerial video and photography for videography, real 

estate photography, special events, film sets, and landscape over certain areas of the 

United States. Jonathan Martin will increase public awareness and knowledge of UAS 

and promote safe operations. 

INTRODUCTION AND INTERESTS OF THE PETITIONER

Jonathan Martin provides its clients with expertise and knowledge in advanced 

technologies and solutions to increase efficiency, productivity and effectiveness. 

Jonathan Martin also provides its clients with the highest quality digital content for use 

in their commercial, personal, and non-profit multimedia projects. Jonathan Martin has 

over 10 years of professional experience in aviation, photography and graphic design 

and work with remotely piloted aircraft. Jonathan Martin has his Commercial Pilot’s 

license (2784208) and his Certified Instructor Rating (2784208CFI). The objective of 

Jonathan Martin’s operation is to provide high quality imaging for a variety of 

commercial, public, and residential uses, and promoting safe operations and airspace 

awareness while piloting UAS’s specifically targeting: 

 Aerial imaging for advertising and marketing brochures 

 Real Estate Photography 

 Land survey & appraisals 

 Equipment Inspections 

 Increase public knowledge of UAS and promote safe UAS operations. 
BACKGROUND

Unmanned Aircraft Systems: Tarot 650 Sport UAS 

Jonathan Martin, Commercial Pilot #2784208 seeks an exemption to operate Tarot 

systems for compensation or hire within the NAS. The 650 Sport is a vertical takeoff and 

landing (VTOL) Unmanned Aircraft (UA) with a Ground Control Station (GCS) utilizing 

a LED monitor display. The Tarot 650 Sport has a maximum gross weight of 

approximately 7 pounds, while having a length of 20 inches, width of 20 inches, height 

of 12 inches, and a maximum speed of approximately 29 knots. The Tarot 650 Sport is

equipped with four main rotors; driven by Lithium Polymer battery powered electric 

motors and utilizes the Eagle Tree Vector stabilization system.

The Tarot 650 Sport UAS that will be operated by Jonathan Martin and will be 

registered in accordance with 49 U.S.C. 44103, Registration of Aircraft, as well as 14 

C.F.R Part 47, Aircraft Registration, and marked in accordance with 14 C.F.R. Part 45, 

Identification and Registration Marking.

BASIS FOR PETITION

Petitioner, Jonathan Martin, pursuant to the provisions of the Federal Aviation 

Regulations (14 C.F.R. § 11.61) and the FAA Modernization and Reform Act of 2012 

(FMRA), Section 333, Special Rules for Certain Unmanned Aircraft Systems, hereby 

petitions the Administrator to commercially operate the Tarot 650 Sport UAS in the 

National Airspace System (NAS), and for an exemption from the requirements of 14 

C.F.R §§ 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a),

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b).
In consideration of the speed, weight, size, and limited operating area associated 

with the unmanned aircraft and its operation, Jonathan Martin’s operation of 650 Sport 

UAS meets the conditions of FMRA Section 333 and therefore, will not require an 

airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H.

Accordingly, Jonathan Martin requests relief from Sections 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), as these sections set forth 

requirements for maintenance that only apply to aircraft with an airworthiness certificate.

Jonathan Martin submits that the requested relief is proper since an equivalent

level of safety will be ensured. Jonathan Martin will use experienced personnel or 

technicians to perform maintenance, alterations, or preventive maintenance on the UASs 

using the methods, techniques, and practices prescribed in the operating documents (i.e., 

Monthly Maintenance Log, and Tarot 650 Sport Instruction Manual). Furthermore, 

Jonathan Martin will document and maintain all maintenance records for the Tarot 650 

Sport UAS.

Jonathan Martin seeks relief from Section 91.7(a), entitled Civil aircraft

airworthiness, because the Tarot 650 Sport UAS does not require an airworthiness 

certificate in accordance with 14 C.F.R. Part 21, Subpart H. As such, Jonathan Martin 

submits that he will ensure that the Tarot 650 Sport UAS is in an airworthy condition, 

prior to every flight, by determining that the UAS is in compliance with the operating 

documents (i.e., Monthly Maintenance Log, and Tarot 650 Sport Instruction Manual), 

and that the aircraft are in a condition for safe flight.

Jonathan Martin also seeks an exemption from the requirements of Section 

91.121, entitled Altimeter Settings, as the Tarot 650 Sport UAS will not have a typical 

barometric altimeter onboard. However, altitude information of the Tarot 650 Sport UAS 

will be provided to the PIC via Eagle Tree Vector Global Positioning System (GPS) 

equipment and radio communications telemetry data link, which downlinks from the UA 

to the GCS for active monitoring of the flight path. This altitude information, combined 

with Jonathan Martin’s operation of the Tarot 650 Sport UAS within visual line of sight, 

at or below 200 feet AGL, will ensure a level of safety equivalent to Section 91.121.
Additionally, Jonathan Martin seeks an exemption from the requirements of 

Section 91.151(b), entitled Fuel requirements for flight in VFR conditions. Jonathan 

Martin submits that safety will not be affected by operation of the Tarot 650 Sport UAS 

during daylight hours in visual meteorological conditions (VMC) under visual flight rules 

(VFR), with enough battery power to fly for a total duration of approximately 13 minutes 

to the first point of intended landing and, assuming normal cruising speed, to fly after that 

for at least 4 minutes.

In accordance with 14 C.F.R. § 11.81, Jonathan Martin provides the following 

information in support of its petition for exemption:

A. Name And Address Of The Petitioner.

The name and address of the Petitioner and point of contact is:

Jonathan Martin

582 Coatesville RD 

West Grove PA 19390

Email:FutureAviatorsUSA@gmail.com

610-476-1702
B. The Specific Sections Of 14 C.F.R. From Which Jonathan Martin Seeks 

Exemption.

1. Jonathan Martin Seeks Exemption From The Requirements Of Section 

91.7(a).

Section 91.7, entitled Civil aircraft airworthiness, subsection (a), states the

following:

(a) No person may operate a civil aircraft unless it is in an airworthy condition. 

2. Jonathan Martin Seeks Exemption From The Requirements Of Section 

91.121.

Section 91.121, entitled Altimeter settings, subsection (a), states the following, in 

part:

(a) 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--

(1) Below 18,000 feet MSL, to--

(i) The current reported altimeter setting of a station along the route and 

within 100 nautical miles of the aircraft;

(ii) there is no station within the area prescribed in paragraph (a)(1)(i) of

this section, the current reported altimeter setting of an appropriate

available station; or

(iii) the case of an aircraft not equipped with a radio, the elevation of 

the departure airport or an appropriate altimeter setting available

before departure.

3. Jonathan Martin Seeks Exemption From The Requirements Of Section

91.151(b).

Section 91.151, entitled Fuel requirements for flight in VFR conditions, subsection

(b), states the following:

(b) No person may begin a flight in a rotorcraft under VFR conditions unless 

(considering wind and forecast weather conditions) there is enough fuel to fly

to the first point of intended landing and, assuming normal cruising speed, to 

fly after that for at least 20 minutes.

4. Jonathan Martin Seeks Exemption From The Requirement Of Section 

91.405(a).

Section 91.405, entitled Maintenance required, subsection (a), states the

following: Each owner or operator of an aircraft—

(a) Shall have that aircraft inspected as prescribed in subpart E of this part and 

shall between required inspections, except as provided in paragraph (c) of this 

section, have discrepancies repaired as prescribed in part 43 of this chapter[.] 
5. Jonathan Martin Seeks Exemption From The Requirements Of Section 

91.407(a)(1)

Section 91.407, entitled Operation after maintenance, preventive maintenance, 

rebuilding, or alteration, subsection (a)(1), states the following:

(a) No person may operate any aircraft that has undergone maintenance, 

preventive maintenance, rebuilding, or alteration unless--

(1) It has been approved for return to service by a person authorized under §

43.7 of this chapter[.]

6. Jonathan Martin Seeks Exemption From The Requirements Of Sections 

91.409(a)(1) And 91.409(a)(2).

Section 91.409, entitled Inspections, subsection (a), states the following:

(a) Except as provided in paragraph (c) of this section, no person may operate an 

aircraft unless, within the preceding 12 calendar months, it has had --

(1) An annual inspection in accordance with part 43 of this chapter and has 

been approved for return to service by a person authorized by § 43.7 of 

this chapter; or

(2) An inspection for the issuance of an airworthiness certificate in accordance

with part 21 of this chapter.

7. Jonathan Martin Seeks Exemption From The Requirements Of Sections 

91.417(a) And 91.417(b).

Section 91.417, entitled Maintenance records, subsections (a) and (b), state the

following:

(a) Except for work performed in accordance with §§ 91.411 and 91.413, each 

registered owner or operator shall keep the following records for the periods 

specified in paragraph (b) of this section:

(1) Records of the maintenance, preventive maintenance, and alteration 

and records of the 100-hour, annual, progressive, and other required or 

approved inspections, as appropriate, for each aircraft (including the

airframe) and each engine, propeller, rotor, and appliance of an 

aircraft. The records must include--

(i) A description (or reference to data acceptable to the Administrator) of 

the work performed; and

(ii) The date of completion of the work performed; and

(iii) The signature, and certificate number of the person approving the

aircraft for return to service.

(2) Records containing the following information:

(i) The total time in service of the airframe, each engine, each propeller, 

and each rotor.

(ii) The current status of life-limited parts of each airframe, engine, 

propeller, rotor, and appliance.

(iii) The time since last overhaul of all items installed on the aircraft which 

are required to be overhauled on a specified time basis.

(iv) The current inspection status of the aircraft, including the time since

the last inspection required by the inspection program under which 
the aircraft and its appliances are maintained.

(v) The current status of applicable airworthiness directives (AD) and 

safety directives including, for each, the method of compliance, the

AD or safety directive number and revision date. If the AD or safety 

directive involves recurring action, the time and date when the next

action is required.

(vi) Copies of the forms prescribed by § 43.9(d) of this chapter for each 

major alteration to the airframe and currently installed engines, rotors, 

propellers, and appliances.

(b) The owner or operator shall retain the following records for the periods 

prescribed:

(1) The records specified in paragraph (a)(1) of this section shall be 

retained until the work is repeated or superseded by other work or for 1 

year after the work is performed.

(2) The records specified in paragraph (a)(2) of this section shall be 

retained and transferred with the aircraft at the time the aircraft is sold.

(3) A list of defects furnished to a registered owner or operator under § 

43.11 of this chapter shall be retained until the defects are repaired and 

the aircraft is approved for return to service.

C.The Extent Of Relief Jonathan Martin Seeks And The Reason Jonathan Martin 

Seeks The Relief.

1. Extent Of Relief Jonathan Martin Seeks And The Reason Jonathan 

Martin Seeks Relief From Section 91.7(a).

Relief from Section 91.7(a) entitled Civil aircraft airworthiness, is requested to 

the extent required to allow Jonathan Martin to determine that the Tarot 650 Sport UAS 

are in airworthy condition prior to every flight by ensuring that the UAS is in 

compliance with the operating documents (i.e., the Jonathan Martin Aerial Operations 

Manual, Monthly Maintenance Log, and Tarot 650 Sport Instruction Manual).
Jonathan Martin seeks the requested relief because the Tarot 650 Sport UAS does 

not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. 

Therefore, Jonathan Martin will ensure that the Tarot 650 Sport UAS is in airworthy 

condition based upon its compliance with the operating documents (i.e., Monthly 

Maintenance Log, and Tarot 650 Sport Instruction Manual) prior to every flight, and 

further, determine that the aircraft are in condition for safe flight, as stated in the 

conditions and limitations below.

2. Extent Of Relief Jonathan Martin Seeks And The Reason Jonathan 

Martin Seeks Relief From Section 91.121.

Relief from Section 91.121, entitled Altimeter settings, may be required to allow 

flight operations of the Tarot 650 Sport UAS, which utilize a barometric pressure sensor, 

GPS equipment, and a radio communications telemetry data link to downlink altitude 

information from the UA to the PIC at the ground control station (GCS). Since the FAA 

requires that any altitude information concerning UAS operations be reported to air traffic 

control (ATC) in feet above ground level (AGL), Jonathan Martin seeks the requested 

relief because the Tarot 650 Sport UAS altimeter may be set on the ground to zero feet 

AGL, rather than the local barometric pressure or field altitude, before each flight.

Considering the limited altitude of the proposed operations, relief from 14 CFR

91.121 is sought to the extent necessary to comply with the applicable conditions and 

limitations stated below. As more fully set forth herein, an equivalent level of safety will

be maintained since the Tarot 650 Sport UAS is equipped with a barometric pressure 

sensor and GPS equipment, which automatically ensures that a ground level pressure 

setting will be established prior to each flight, and provides the PIC with altitude 

information of the UA on the heads-up display of the GCS. 

3. Extent Of Relief Jonathan Martin Seeks And The Reason Jonathan 

Martin Seeks Relief From Section 91.151(b).
Relief from Section 91.151(b) entitled Fuel requirements for flight in VFR conditions, is 

requested to the extent required to allow flights of the battery powered Tarot 650 Sport 

UAS during daylight hours in visual meteorological conditions (VMC), under visual flight 

rules (VFR), for a total duration of 13 minutes to the first point of intended landing and, 

assuming normal cruising speed, to fly after that for at least 4 minutes. Jonathan Martin 

seeks the requested relief because without an exemption from Section 91.151(b), the flight 

time duration of the battery powered Tarot 650 Sport UAS will severely constrain the 

practicality of any aerial video or still photo flight operations that Jonathan Martin 

proposes to conduct pursuant to this Petition.

Significantly, as set forth below, the technical specifications of the Tarot 650 Sport UAS, 

the Tarot 650 Sport operating documents, and Jonathan Martin’s proposed operating 

limitations, ensure that Jonathan Martin will safely operate the battery powered Tarot 650 

Sport UAS during daylight hours in visual meteorological conditions (VMC), under visual

flight rules (VFR), with enough battery power to fly for a total duration of 13 minutes to 

the first point of intended landing and, assuming normal cruising speed, to fly after that for 

at least 4 minutes.

4. Extent Of Relief Jonathan Martin Seeks And The Reason Jonathan 

Martin Seeks Relief From Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & 

(a)(2), And 91.417(a) & (b).

Since Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) 

only apply to aircraft with an airworthiness certificate, Jonathan Martin requests relief 

from these Sections because the Tarot 650 UAS does not require airworthiness certificates. 

As set forth more fully below, the Tarot 650 Sport UAS meet the conditions of FMRA 

Section 333 for operation without an airworthiness certificate. Accordingly, Jonathan 

Martin will use trained technicians to perform maintenance, alterations, or preventive 

maintenance on the UAS using the methods, techniques, and practices prescribed in the 

UAS operating documents (i.e., the Jonathan Martin Aerial Operations Manual, Monthly 

Maintenance Log, and Tarot 650 Sport Instruction Manual). Furthermore, Jonathan Martin 

will document and maintain all maintenance records for the Tarot 650 Sport UAS.

D.The Reasons Why Granting Jonathan Martin’s Request Would Be In The 

Public Interest; That Is, How It Would Benefit The Public As A Whole.
Granting the present Petition will further the public interest by allowing Jonathan 

Martin to safely, efficiently, and economically perform aerial video and photography of 

construction sites, real estate, and landscape over certain areas of the United States.

Additionally, use of the Tarot 650 Sport UAS will decrease congestion of the 

NAS, reduce pollution, and provide significant benefits to the economy. Notably, the 

benefits of Jonathan Martin’s proposed operation of the Tarot 650 Sport UAS will be 

realized without implicating any privacy issues.

1. The Public Will Benefit From Decreased Congestion Of The NAS.

Tarot 650 Sport is battery powered and serve as a safe, efficient, and economical 

alternative to the manned aircraft traditionally utilized to obtain aerial imagery. By 

reducing the amount of manned aircraft needed to perform aerial acquisitions, an 

exemption allowing the use of a Tarot 650 Sport UAS would reduce the amount of 

manned aircraft in the NAS, reduce noise and air pollution, as well as increase the safety 

of life and property in the air and on the ground.

Furthermore, by reducing the number of manned aircraft operating in the NAS, 

congestion around airports caused by arriving and departing aircraft will be reduced. The

Tarot 650 Sport UAS do not require an airport to takeoff or land.

Likewise, a reduction of manned aircraft conducting aerial video and photography 

missions would result in fewer aircraft that must be handled by air traffic control during

the ground, takeoff, departure, arrival, and landing phases of flight operations. 

2. The Public Will Benefit From The Safety And Efficiency Of The 

Tarot 650 Sport UAS.

Conducting aerial acquisitions with the Tarot 650 Sport and UAS, instead of 

manned aircraft, will greatly benefit the public by drastically reducing the levels of air and 

noise pollution generated during traditional aerial video and still photography flight 

operations. By using battery power and electric motors, the Tarot 650 Sport UAS produce 

no air pollution, and is the most viable environmentally conscious alternative to the cabin 

class, six cylinder internal combustion engine aircraft that are typically utilized for aerial 

video and photography, while burning approximately 15 gallons per hour of AVGAS. The 
Tarot 650 Sport UAS, while reducing the carbon footprint of aerial acquisitions, also 

eliminates noise pollution, as the UAS are propelled by battery powered electric motors, 

rather than an internal combustion engine.

By using the Tarot 650 Sport UAS to perform aerial acquisitions, the substantial 

risk to life and property in the air and on the ground, which is usually associated with 

traditional manned aircraft flight operations, will be substantially reduced or completely 

eliminated. Aside from the lack of flight crew members located onboard the aircraft, the 

Tarot 650 Sport UAS (weighing approximately 7 pounds, at their maximum gross weights 

with lengths of 20 inches and, widths of 20 inches, and with no fuel on board), has less 

physical potential for collateral damage to life and property on the ground, and in the air, 

compared to the manned aircraft that typically conduct similar operations (weighing 

approximately 6,000 pounds with a wingspan of approximately 36 feet, a length of 30

feet, and a fuel capacity of 70 gallons).

3. Performing Aerial Video and Photography Operations With The Tarot 

650 Sport UAS Will Benefit The Economy.

In addition to being safe and efficient, the Tarot 650 Sport and UAS is also an 

economical alternative to using manned aircraft to conduct similar aerial operations. As 

such, operation of the Tarot 650 Sport UAS will allow United States based companies, 

like Jonathan Martin, to remain competitive and contribute to growth of the U.S. 

economy. Specifically, with the rising cost of aviation fuel and the Environmental 

Protection Agency (“EPA”) regulatory actions phasing out leaded aviation fuels, U.S. 

owned and operated companies must adopt new and alternative technology in order to 

remain competitive. Operating the battery powered Tarot 650 Sport UAS is one such 

technology that not only allows companies greater operational flexibility compared to 

manned aircraft, but provides such flexibility without the high operational cost of a 

traditional manned aircraft.

By operating the Tarot 650 Sport, companies such as Jonathan Martin, can remain 

competitive and profitable, and therefore, provide greater job stability to employees and 

contractors, which will ultimately contribute to growth of the U.S. economy. Improved 
financial performance of U.S. companies, through commercial use of the Tarot 650 Sport 

UAS, provides a stable workforce that increases consumer spending; improves local, 

state, and federal tax revenues; and allows companies to invest in research and 

development in order to remain competitive both in the United States and abroad.

4. There Are No Privacy Issues.

Similar to the manned aerial acquisition flight operations that have been conducted for 

decades, Jonathan Martin’s proposed operation of the Tarot 650 Sport UAS will not 

implicate any privacy issues. Specifically, the Tarot 650 Sport UAS will be operated only 

in compliance with operating documents (i.e., the Jonathan Martin Aerial Operations 

Manual, Monthly Maintenance Log, and Tarot 650 Sport and Instruction Manual) which 

requires property owner involvement as well as local law enforcement notification, and in 

accordance with the Federal Aviation Regulations, including the minimum altitude

requirements of 14 C.F.R. § 91.119.

E. The Reasons Why Granting The Exemption Would Not Adversely Affect Safety, 

Or How The Exemption Would Provide A Level Of Safety At Least Equal To 

That Provided By The Rule From Which Jonathan Martin Seeks Exemption.

1. Reasons Why The Tarot 650 Sport UAS Meet The Conditions Of The FAA 

Modernization and Reform Act of 2012 (FMRA) Section 333.

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

with the unmanned aircraft and its operation, Jonathan Martin’s operation of the Tarot 650 

Sport UAS meets the conditions of FMRA Section 333, and will not require an 

airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H.

Section 333 provides authority for a UAS to operate without airworthiness 

certification and sets forth requirements for considering whether a UAS will create a

hazard to users of the NAS or the public, or otherwise pose a threat to national security.

Specifically, FMRA Section 333 states the following, in part:

(a) In General.--Notwithstanding any other requirement of this subtitle, and not

later than 180 days after the date of enactment of this Act, the Secretary of

Transportation shall determine if certain unmanned aircraft systems may

operate safely in the national airspace system before completion of the plan 

and rulemaking required by section 332 of this Act or the guidance required 

by section 334 of this Act.

(b) Assessment of Unmanned Aircraft Systems.--In making the determination 
under subsection (a), the Secretary shall determine, at a minimum--

(1) which types of unmanned aircraft systems, if any, as a result of 

their size, weight, speed, operational capability, proximity to 

airports and populated areas, and operation within visual line 

of sight do not create a hazard to users of the national 

airspace system or the public or pose a threat to national 

security; and whether a certificate of waiver, certificate of 

authorization, or airworthiness certification under section 

44704 of title 49, United States Code, is required for the 

operation of unmanned aircraft systems identified under 

paragraph (1).

(c) Requirements for Safe Operation.--If the Secretary determines under this 

section that certain unmanned aircraft systems may operate safely in the

national airspace system, the Secretary shall establish requirements for the

safe operation of such aircraft systems in the national airspace system.

In seeking this exemption, Jonathan Martin submits that the Tarot 650 Sport UAS 

can operate safely in the NAS pursuant to FMRA Section 333, as demonstrated by: (a) the 

characteristics of the Tarot 650 Sport UAS; (b) the pilot certification requirement; and (c) 

the specific operating limitations.

a. The Specifications Of The Tarot 650 Sport UAS Demonstrate Its 

Safe Characteristics.

The Tarot 650 Sport UAS does not create a hazard to users of the NAS or the 

public, or otherwise pose a threat to national security considering its size, weight, speed, 

and operational capability. 

i. Technical Specifications Of The Tarot 650 Sport UAS.

The technical specifications of the Tarot 650 Sport UAS is set forth by the Tarot 

650 Sport Specifications and Data Sheet, attached here to as Exhibit A.

ii. The Tarot 650 Sport UAS Autonomous Flight And Navigation 

Modes Enable The UAS To Remain Within A Defined Operational 

Area.

The Tarot 650 Sport UAS may be operated in both manual and fully autonomous 

flight modes. 

iii. The Tarot 650 Sport UAS Are Designed For Automatic Return To 

Home Point Or Hover In The Event Of Loss Of The Control Link Or 

Navigation.
When the Control Link is lost, the Tarot 650 Sport UAS will remain stationary, in 

flight, for 3 seconds or more. If, after 3 seconds, the Tarot 650 Sport UAS do not 

reacquire control link data from the GCS, the UAS will assume that the Control Link is 

lost and the UAS will return to the home position (i.e., failsafe mode) via GPS, and will 

descend to the takeoff position and shutdown.

iv. The Tarot 650 Sport GCS And Its Operation.

A complete description of the operation and specifications of the Tarot 650 Sport 

GCS and flight control software from Eagle Tree Systems is provided in the Tarot 650 

Sport User Manual. Tarot 650 Sport Eagle Tree Systems Vector User Manuals are attached 

hereto as Exhibits C. 

b. Flight Operations Of Tarot 650 Sport UAS Are Limited To The Line Of 

Sight Of A Certificated Pilot in Command With A Safety Observer.

Jonathan Martin will only utilize certificated pilots who possess a current and 

valid airman medical certificate to act as a pilot in command (PIC) of the Tarot 650 Sport 

UAS. Additionally, a safety observer will assist all pilots during flight time.

c. Flights Of Tarot 650 Sport UAS Will Be Conducted Pursuant To 

Specific Operating Limitations.

In seeking this exemption, Jonathan Martin proposes to commercially operate

Tarot 650 Sport UAS for the special purpose of conducting aerial video and photography 

over certain areas of United States, pursuant to the following specific operating 

limitations:

1. Operations authorized by this grant of exemption will be limited to the

following aircraft described in the operating documents, rotorcraft UASs 

weighing less than 55 pounds maximum gross weight: Tarot 650 Sport

Unmanned Aircraft Systems. Proposed operations of any other aircraft will 

require a new petition or a petition to amend this grant.

2. UAS operations under this exemption will be limited to conducting operations 

for the purpose of aerial video and photography.

3. The UAS may not be flown at an indicated airspeed exceeding 20 knots.
4. The UA must be operated at an altitude of no more than 200 feet above ground

level (AGL), as indicated by the procedures specified in the operating 

documents unless a special request is made and approved by ATC. All altitudes 

reported to ATC must be in feet AGL.

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

times. This requires the PIC to be able to use human vision unaided by any 

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

airman medical certificate.

6. The use of first person view (FPV) by the PIC or safety observer (SO) is not

permitted.

7. All operations must utilize a safety observer (SO). The SO may be used to 

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

capability. The SO and PIC must be able to communicate verbally at all times. 

Electronic messaging or texting is not permitted during flight operations. The

PIC must be designated before the flight and cannot transfer his or her 

designation for the duration of the flight. The PIC must ensure that the SO can 

perform the functions prescribed in the operating documents.

8. The SO must not perform any other duties beyond assisting the PIC with seeing 

and avoiding other air traffic and other ground based obstacles/obstructions and 

is not permitted to operate the camera or other instruments.

9. The operating documents and the grant of exemption must be accessible during 

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

discrepancy exists between the conditions and limitations contained in the grant 

of exemption and the procedures outlined in the operating documents, the

conditions and limitations contained in the grant of exemption take precedence

and must be followed. Otherwise, the operator must follow the procedures as 

outlined in its operating documents. The operator may update or revise its 

operating documents. It is the operator’s responsibility to track such revisions 

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

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

extension or amendment to the grant of exemption. If the operator determines 

that any update or revision would affect the basis upon which the FAA granted 

the exemption, then the operator must petition for amendment to its grant of 

exemption. The FAA’s UAS Integration Office (AFS-80) may be contacted if

questions arise regarding updates or revisions to the operating documents.

10. Prior to each flight the PIC must inspect the UAS to ensure that it is in a

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

safe operation of the UAS, the aircraft is prohibited from operating until the

necessary maintenance has been performed and the UAS is found to be in a

condition for safe flight. The Ground Control Station must be included in the

preflight inspection. All maintenance and alterations must be properly 

documented in the aircraft records.

11. Any UAS that has undergone maintenance or alterations that affect the UAS 

operation or flight characteristics, e.g. replacement of a flight critical

component, must undergo a functional test flight. The PIC who conducts the

functional test flight must make an entry in the aircraft records.

12. The pre-flight inspection must account for all potential discrepancies, e.g. 

inoperable components, items, or equipment, not already covered in the

relevant sections of the operating documents.
13. The operator must follow the UAS manufacturer’s aircraft/component, 

maintenance, overhaul, replacement, inspection, and life limit requirements.

14. The operator must carry out its maintenance, inspections, and record keeping 

requirements, in accordance with the operating documents. Maintenance, 

inspection, alterations, and status of replacement/overhaul component parts 

must be noted in the aircraft records, including total time in service, 

description of work accomplished, and the signature of the authorized person 

returning the UAS to service.

15. Each UASs operated under this exemption must comply with all manufacturer 

Safety Bulletins.

16. The authorized person must make an entry in the aircraft record of the

corrective action taken against discrepancies discovered between inspections.

17. The PIC must possess at least a private pilot certificate and at least a current

third- class medical certificate.

18. The operator may not permit any PIC to operate unless the PIC meets the

operator’s qualification criteria and demonstrates the ability to safely operate

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

exemption, including evasive and emergency maneuvers and maintaining 

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

qualification flight hours must be logged in a manner consistent with 14 C.F.R.

§ 61.51(b). Flights for the purposes of training the operator’s PICs are

permitted under the terms of the exemption. However, training operations may 

only be conducted during dedicated training sessions. During training, 

proficiency, and experience-building flights, all persons not essential for flight

operations are considered nonparticipants, and the PIC must operate the UA 

with appropriate distance from nonparticipants in accordance with 14 C.F.R. § 

91.119.

19. UAS operations may not be conducted during night, as defined in 14 C.F.R. §

All operations must be conducted under visual meteorological conditions (VMC). If flight 

at night is required, a special request will be made at the FAA office closest to proposed 

area of operations. Flights under special visual flight rules (SVFR) are not authorized.

20. The UA may not operate within 5 nautical miles of an airport reference point

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

agreement with that airport’s management is obtained, and the operation is 

conducted in accordance with a NOTAM as required by the operator’s COA. 

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

to the Administrator upon request.

21. The UA may not be operated less than 500 feet below or less than 2,000 feet

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

the PIC.

22. If the UA loses communications or loses its GPS signal, it must return to a

pre- determined location within the planned operating area and land or be

recovered in accordance with the operating documents.

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

emergencies in accordance with the operating documents.
24. The PIC is prohibited from beginning a flight unless (considering wind and 

forecast weather conditions) there is enough power to fly at normal cruising 

speed to the intended landing point and land the UA with 25% battery power 

remaining.

25. The operator must obtain an Air Traffic Organization (ATO) issued Certificate 

of Waiver or Authorization (COA) prior to conducting any operations under 

the grant of exemption. This COA will also require the operator to request a 

Notice to Airman (NOTAM) not more than 72 hours in advance, but not less 

than 48 hours prior to the operation. All operations shall be conducted in 

accordance with airspace requirements in the ATO issued COA including 

class of airspace, altitude level and potential transponder requirements.

26. All aircraft operated in accordance with the exemption must be identified by 

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

identification (N- Number) markings in accordance with 14 C.F.R. part 45, 

Subpart C. Markings must be as large as practicable.

27. Before conducting operations, the radio frequency spectrum used for 

operation and control of the UA must comply with the Federal

Communications Commission (FCC) or other appropriate government

oversight agency requirements.

28. The documents required fewer than 14 C.F.R. 91.9 and 91.203 must be

available to the PIC at the Ground Control Station of the UAS any time the

UAS is operating. These documents must be made available to the

Administrator or any law enforcement official upon request.

29. The UA must remain clear and yield the right of way to all manned aviation 

operations and activities at all times.

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

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

persons (persons other than the PIC, SO, operator trainees or essential

persons), vessels, vehicles, and structures unless:

a. Barriers or structures are present that sufficiently protect

nonparticipating persons from the UA and/or debris in the event of an 

accident. The operator must ensure that nonparticipating persons 

remain under such protection. If a situation arises where

nonparticipating persons leave such protection and are within 500 feet

of the UA, flight operations must cease immediately and/or;

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

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

permission and the PIC has made a safety assessment of the risk of 

operating closer to those objects and determined that it does not present

an undue hazard, and;

c. Operations nearer to the PIC, SO, operator trainees or essential persons 

do not present an undue hazard to those persons per § 91.119(a).

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

with permission from the land owner/controller or authorized representative. 

Permission from land owner/controller or authorized representative will be

obtained for each flight to be conducted.
33. Any incident, accident, or flight operation that transgresses the lateral or 

vertical boundaries of the operational area as defined by the applicable COA 

must be reported to the FAA's UAS Integration Office (AFS-80) within 24 

hours. Accidents must be reported to the National Transportation Safety 

Board (NTSB) per instructions contained on the NTSB Web site:

www.ntsb.gov.

2. Reasons Why An Exemption From The Requirements Of Section 91.7(a) 

Would Not Adversely Affect Safety.

The equivalent level of safety established by Section 91.7(a) will be maintained 

because prior to every flight, Jonathan Martin will ensure that the Tarot 650 Sport UAS is 

in an airworthy condition based upon the UAS’s compliance with its operating documents 

and as stated in the conditions and limitations herein.

Additionally, the FAA has previously granted relief from Section 91.7(a) specific to UAS, 

in circumstances similar, in all material respects, to those presented herein (e.g. Exemption 

Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110,

11112, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161).

3. Reasons Why An Exemption From The Requirements Of Section 91.121 

Would Not Adversely Affect Safety.

The equivalent level of safety established by Section 91.121 will be maintained 

because the altitude information of the Tarot 650 Sport UAS will be provided to the PIC 

via GPS equipment and a radio communications telemetry data link, which downlinks 

from the UA to the GCS for active monitoring of the flight path and altitude. This altitude 

information, combined with Jonathan Martin’s operation of the Tarot 650 Sport within 

visual line of sight, at or below 200 feet AGL, will ensure a level of safety equivalent to 

Section 91.121. The altitude information will be generated by GPS equipment installed 

onboard the aircraft. Prior to each flight, a zero altitude initiation point is automatically 

established by the UASs at ground level.

The FAA has previously granted relief from Section 91.121 specific to UAS, in 

circumstances similar, in all material respects, to those presented herein (e.g. Exemption 

Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11112, 11136, 11138,

11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 
4. Reasons Why An Exemption From The Requirements Of Section 91.151(b) 

Would Not Adversely Affect Safety.

A grant of this exemption would ensure an equivalent level of safety established 

by 14 C.F.R. Section 91.151(b) as a result of (1) the technical specifications of the Tarot 

650 Sport and Tarot X4; (2) the limitations on the proposed flight operations; and (3) the 

location of the proposed flight operations. Accordingly, Jonathan Martin will ensure that 

it will safely operate the battery powered Tarot 650 Sport UAS during daylight hours in 

VFR conditions, with enough battery power to fly for a total duration of 13 minutes to the 

first point of intended landing and, assuming normal cruising speed, to fly after that for at 

least 4 minutes.

Here, as in Exemption No. 11109, the technical specifications of the Tarot 650 

Sport; the limitations on the proposed flight operations; and the location of the proposed 

operations, will ensure an equivalent level of safety established by 14 C.F.R. Section 

91.151(b). Furthermore, safety will be ensured as the Tarot 650 Sport UAS provide 

audible and visual warnings to the PIC at the GCS when the UAS experiences low battery 

voltage, the first warning occurring at approximately 33% remaining battery power, and 

again at approximately 10% remaining battery power. At the critically low battery level, 

the Tarot 650 Sport UAS will descend and land automatically.

Significantly, previous exemptions granted by the FAA concerning Section establish that 

safety is not adversely affected when the technical characteristics and operating 

limitations of the UAS are considered. Relief has been granted for manned aircraft to 

operate at less than the minimums prescribed in Section 91.151, including Exemption 

Nos. 2689, 5745, and 10650. Moreover, the FAA has previously granted relief from 

Section 91.151 specific to UAS, in circumstances similar, in all material respects, to those 

presented herein (e.g. Exemption Nos. 8811, 10808, 10673, 11042, 11062, 11063, 11064, 

11065, 11066, 11067, 11080, 11109, 11110, 11136, 11138, 11150, 11153, 11156, 11157, 

11158, 11159, 11160, 11161).

5. Reasons Why An Exemption From The Requirements Of Sections 

91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), And 91.417(a) & (b) Would 

Not Adversely Affect Safety.

In seeking this exemption, Jonathan Martin submits that the equivalent level of 
safety with regard to the regulatory maintenance and alteration requirements established 

by Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) will be

met because Jonathan Martin will use trained technicians to perform maintenance, 

alterations, or preventive maintenance on the UASs using the methods, techniques, and 

practices prescribed in the operating documents (i.e., the Jonathan Martin Aerial

Operations Manual, Monthly Maintenance Log, and Tarot 650 Sport Instruction Manual). 

Furthermore, Jonathan Martin will document and maintain all maintenance records for the 

Tarot 650 Sport UAS.

Since the Tarot 650 Sport UAS will be inspected as prescribed by the operating 

documents, Jonathan Martin will maintain the equivalent level of safety established by 

Sections 91.405(a), 91.409(a)(1), and 91.409(a)(2). A copy of the Tarot 650 Sport User 

Manuals are attached hereto as Exhibit C; a copy of the Tarot 650 Sport and UAS 

Maintenance LOG is attached hereto as Exhibit D.

Likewise, the exemption sought will not adversely affect safety because Jonathan 

Martin will use trained technicians to perform maintenance, alterations or preventive

maintenance on the UAS using the methods, techniques, and practices prescribed by the

operating documents.

Furthermore, the exemption sought would maintain an equivalent level of safety 

established by Sections 91.407, 91.417(a) and 91.417(b), because all maintenance of the

Tarot 650 Sport and Tarot X4 UASs will be performed by trained technicians. 

Maintenance will be documented and maintained utilizing the monthly maintenance log.

Significantly, previous exemptions granted by the FAA concerning Sections 

91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) establish that safety is 

not adversely affected when the technical characteristics and operating limitations of the 

UAS are considered.

In consideration of Jonathan Martin’s proposed operating limitations, the

operating documents, and the technical aspects of the Tarot 650 Sport UAS, Jonathan 

Martin submits that safety will not be adversely affected by granting exemption from 14 

C.F.R. Sections 91.405(a), 91.407(a)(1) and (a)(2), 91.409(a)(2), and 91.417(a) and (b). 
The FAA has previously granted relief specific to UAS in circumstances similar, in all 

material respects, to those presented herein (e.g. Exemption Nos. 11062, 11063, 11064, 

11065, 11066, 11067, 11080, 11109, 11110, 11112, 11136, 11138, 11150, 11153, 11156, 

11157, 11158, 11159, 11160, 11161).

6. The FAA May Prescribe Any Other Conditions For Safe Operation.

In accordance with Section 333 of the FAA Modernization and Reform Act of 

2012 (FMRA) and 14 C.F.R. § 21.16 entitled Special Conditions, Jonathan Martin 

requests that the FAA prescribe special conditions for the intended operation of the Tarot 

650 Sport and UAS, which contain such safety standards that the Administrator finds 

necessary to establish a level of safety equivalent to that established by 14 C.F.R. Part 21, 

Subpart H, and 14 C.F.R §§ 61.113(a) & (b), 91.7 (a), 91.121, 91.151(b), 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). Such special conditions will 

permit safe operation of the UAS for the limited purpose of conducting aerial video and 

photography over certain areas of the United States for compensation or hire. FMRA 

Section 333 sets forth the requirements for considering whether a UAS will create a 

hazard to users of the NAS or the public, or otherwise pose a threat to national security; 

and further, provides the authority for such UAS to operate without airworthiness 

certification in accordance with any requirements that must be established for the safe 

operation of the UAS in the NAS.

Likewise, the Administrator may prescribe special conditions pursuant to 14

C.F.R. § 21.16, for operation of the Tarot 650 Sport, since the airworthiness regulations of 

14 C.F.R. Part 21 do not contain adequate or appropriate safety standards, due to the novel 

or unusual design features of the aircraft. Section 21.16, entitled Special Conditions, states 

the following:

If the FAA finds that the airworthiness regulations of this subchapter do not contain 

adequate or appropriate safety standards for an aircraft, aircraft engine, or propeller 

because of a novel or unusual design feature of the aircraft, aircraft engine or propeller, he 

prescribes special conditions and amendments thereto for the product. The special 

conditions are issued in accordance with Part 11 of this chapter and contain such safety 

standards for the aircraft, aircraft engine or propeller as the FAA finds necessary to 
establish a level of safety equivalent to that established in the regulations. See 14 C.F.R. § 

21.16.

Therefore, in accordance with FMRA Section 333 and 14 C.F.R. § 21.16, the

FAA may prescribe special conditions for Jonathan Martin’s intended operation of the 

Tarot 650 Sport UAS, which contain such safety standards that the Administrator finds 

necessary to establish a level of safety equivalent to that established by 14 C.F.R. Part 21, 

Subpart H, and 14 C.F.R Sections 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(1) & (a)(2), and 91.417(a) & (b). 

 A Summary That Can Be Published In The Federal Register, stating: The

Rules From Which Jonathan Martin Seeks Exemption:

Jonathan Martin commercial pilot certificate number 2784208 seeks exemption 

from the requirements of 14 C.F.R Sections 91.7(a), 91.121, 91.151(b), 91.405(a), 

91.407(a)(1), 91.409(a)(1)

& (a)(2), and 91.417(a) & (b).

A Brief Description Of The Nature Of The Exemption Jonathan Martin 

Seeks:

This exemption will permit Jonathan Martin commercial pilot certificate number 

2784208 to commercially operate an Unmanned Aircraft System (UAS) for the 

purpose of conducting aerial video and photography over certain areas of the 

United States.

 Any Additional Information, Views, Or Arguments Available To Support 

Jonathan Martin’s Request.

This Petition is made pursuant to the FAA Modernization and Reform Act of 

2012 (FMRA) Section 333, which directs the Secretary of Transportation to determine if 

certain UAS may operate safely in the NAS. As such, Jonathan Martin’s request for 

exemption may be granted pursuant to the authority of FMRA Section 333 and 14 C.F.R. 

Part 11, as set forth above.

FMRA Section 333 sets forth the requirements for considering whether a UAS 

will create a hazard to users of the NAS or the public, or otherwise pose a threat to 

national security; and further, provides the authority for such UAS to operate without

airworthiness certification.

As discussed in detail above, Jonathan Martin will operate the Tarot 650 Sport UAS safely 

in the NAS, without creating a hazard to users of the NAS, or the public, or otherwise 
pose a threat to national security.

CONCLUSION

As set forth herein, Jonathan Martin commercial pilot certificate number 2784208 seeks 

an exemption pursuant to 14 C.F.R. §11.61 and Section 333 of the FAA Modernization 

and Reform Act of 2012 (FMRA), which will permit safe operation of the Tarot 650 

Sport and UASs commercially, without an airworthiness certificate, for the limited 

purpose of conducting aerial video and photography over certain areas of the United 

States. By granting this Petition, the FAA Administrator will be fulfilling the 

Congressional mandate of the FAA Modernization and Reform Act of 2012, while also 

advancing the interests of the public, by allowing Jonathan Martin to safely, efficiently, 

and economically operate the Tarot 650 Sport UAS commercially within the NAS.

WHEREFORE, in accordance with the Federal Aviation Regulations and the

FAA Modernization and Reform Act of 2012, Section 333, Jonathan Martin respectfully 

requests that the Administrator grant this Petition for an exemption from the requirements 

of 14 C.F.R Sections 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & 

(a)(2), and 91.417(a) & (b), and permit Jonathan Martin to operate the Tarot 650 Sport 

UAS commercially for the purpose of conducting aerial video and photography over 

certain areas of the United States.

Dated: June 3, 2015

Respectfully submitted, 

Jonathan Martin

582 Coatesville RD 

West Grove PA 19390
Appendices:

A – Tarot 650 Sport Specifications Data Sheet 

B – Tarot 650 Sport Manufactures User Manual

C – Eagle Tree Systems Vector User Manuel 

(ATTACHED) 

D – Monthly Maintenance Log 
EXHIBIT – A 

TAROT 650 SPORT UAS TECHNICAL 

SPECIFICATIONS

The Tarot 650 Sport and Tarot X4 UAS’s are professional grade all carbon fiber UAS’s 

which are installed with Eagle Tree Vector software enabling the user to set parameters 

which will not allow flight into controlled airspace. Parameters can also be set to limit 

flight to no higher than a predetermined and set altitude as well as limit flight to a 

predetermined and set distance. In addition, the installed Eagle Tree Vector software 

provides real-time altitude and location information to the PIC via the linked monitor and 

on screen display visually as well as audibly. 

Tarot 650 Sport 

Aircraft 

Supported Battery – Storm 5500mAH LiPo Battery 

Weight (Battery & Propellers Included) – 5 lbs 

Hover Accuracy (Ready to Fly) – Vertical: .8m; Horizontal: 2.5m 

Max Yaw Angular Velocity - 2001/s 

Max Tilt Angel - 351

Max Ascent Speed – 6m/s 

Max Descent Speed – 2m/s 

Max Flight Speed – 15m/s (NOT RECOMMENDED) 

Gimbal 

Tarot 2D Vs. 2 

Operating Current – 200mA-500mA 

Control Accuracy - ±0.1 

Controllable Range – Pitch: -135 - 90

Maximum Angular Speed – Pitch: 2000/s 

Camera 

GoPro Hero 3+ 

Lens Aperature – f/2.8 

Effective Pixels – 12mp 

Resolution – 12 mega pixels 

HD Video Recording – 1080p30 & 720p 

Transmitter 

Operating Frequency – 5.728GHz – 5.85GHz 

Communication Distance (unobstructed) – FCC Compliance: 800m 

Receiver Sensitivity (1%PER) - -93dBm 

Transmitter Power – FCC Compliance: 100mW 

Working Voltage – 120mA@3.7V 
Range Extender 

Operating Frequency – 2412-2462MHz 

Communication Distance (unobstructed) – 500-700m 

Transmitter Power – 20dBm 

Power Consumption – 2W 
EXHIBIT-B 

Tarot 650 SPORT USER MANUEL 

Tarot FY650 Sport - A Portable size Quadcopter with Motorized Landing Gear

This is Tarot's only Quadcopter frame, 650 size, came with Motorized Landing Gear and it takes maximum 15" propeller. 

The Tarot FY650 Sport has a lot in common with the bigger Tarot FY680-Pro (it has Six rotors), both have a Carbon Fiber 

Deck and a Integrated PCB Board, user can solder the ESC's power cable directly onto this PCB board and save a lot of 

heavy and messy cables. The movable battery mount is also a good feature to balance the best C.G., because when you put 

a Tarot T-2D gimbal in the front of the drone, you need to off-set the weight with battery. The best of all is the Motorized 

Landing Gear, they connected to a Controller (included) and through a switch on your RC transmitter, you can retract and 

deploy the legs, so you will not see the legs in your Video anymore, this is a nice touch as the Motorized Landing Gear 

usually is "DIY" item, now Tarot includes them in the package. 

The Tarot FY650 Sport airframe is versatile, you can put small but high speed motors and smaller props on it to become an 

agile GoPro Camera platform, or use with big motors and props on it to be a long flight time platform, it's a great choice for 

you in Price and Performance for shooting beautiful scenery or interesting footage for YouTube. 

We recommend 4S 14.8V, Tarot 4006 620kv and 13" prop, or even more powerful config like 6S 22.2V Li-Po, Tarot 4008 

380kv motor 13" propeller, this can carry payload up to 1kg to 1.3kg, that means GoPro and similar size camera are no 

problem. Remember that if you put the camera in front, please adjust the battery's position at the rear to have best C.G. 

Great all around drone

You can put a lot of different gadgets on the drone, for lighter payload you can use lighter and cheaper config like small 

motors and battery, if you want to go big, just increase the size of the motor and props, we like this FY650 Sport. 

Motorized Landing Gear

Came with the package, 100% made by Tarot, fully integrated with the FY650 Sport Airframe. 

Retract and Deploy with a flip of a switch

The two landing gears connect to a controller, and connect the controller to the RC receiver. 

Four rotor drones will have longer flight time, but less payload capacity

Two motor less then Hexacopter, that means less energy consumption and fly longer. 

The new designed Integrated PCB Upper Deck

The Tarot FY650 Sport has a PCB Upper Deck and Carbon Fiber Lower Deck. You can solder the ESC's power directly onto 

the PCB Upper Deck, no need to handle a bunch of power cables, much clean layout in the drone. 

The soldering points on the PCB Board

This is the PCB Board of the FY680 Pro, very similar to the FY650 Sport. 
Light weight and easy to adjust motor mount

Support motor up to 45mm Dia., with 16mm, 19mm, 25mm and 27.7mm hole spacing. 

Came with Mounting Rail and Movable Battery Mount

No need to spend money for the mounting rail. It is 60mm apart, you can put T-2D Gimbal on it and move that battery 

position for best C.G. 

A Portable 650 Size Hexacopter Frame

Easy transportation is very important, especially when you try to put it in the car by yourself... 

Fold it up, it's very portable

It's foldable, easy to put in the back seat of your car. 

Specifications :

- Frame weight : 750g 

- Arms diameter : 16mm 

- Drone dia : 650mm 

- Center body dimension : 190 x 200 x 2.0mm 

- Mount mounting hole : 16mm hole x 2 / 19mm hole x 2 / 25mm hole x 4 / 28mm hole x 3 

- Drone's weight (everything it needs to fly) : around 2.3kg 

- Payload (it can carry) : 1~1.3kg 

Our Flight Reference :

- Battery Supply : One 4S 14.8V 5500mah for 13 minutes 

- Motor : Tarot 4006 620kv Motor 

- ESC : Hobbywing Platinum 30A-OPTO 

- Propeller : Tarot 1355 Carbon Propellers 

- Carrying : Tarot T-2D Brushless Motor Gimbal, TS352 FPV Transmitter, GoPro Hero 3+ (They weight about 700g) 

This package includes :

1. 1 X Tarot 650 Sport Airframe and Motorized Landing Gear 

2. 1 X Controller for the Landing Gears 

3. 1 X Manual with English 

4. Battery Velcro Tape 

EXHIBIT-C 

Eagle Tree Systems Vector Manuel 

(Attached) 
EXHIBIT – D 

MONTHLY$MAINTENANCE$LOG

month: (year: 

UAS$#:$ Date(Issue(

Discovered 

Date(Issue(

Addressed Issue(Description(&(Maintenance(Conducted Maintenance(Performed(By:(((

Print(&(Sign 

Software(Updates      

Airframe(

Engines 

Propellers 

Camera(Gimbal 

Landing(Gear 

Vibration(Dampening

Other: