## ) )

)



## ) l J 

## ) ) I / 

## )

\ / 

## )
) FlyingTigerAviation, LLC FederaIAviation Regulations for Exemption 

## Flying TigerAviation, LLC

March 9, 2015 Docket Management Facility US Department ofTransportation 1200 NewJersey Avenue, SE West Building Ground Floor Room W12-140 Washington DC 20590-0001 RE: Section 333 Petitionfor Exemption for Precision Agriculture Dear FAA: Flying Tiger Aviation, LLC petitionsfor reliefofspecific regulations with regards to airworthiness certification under Section 333, 14 CFR 11.81. The proposed request for exemption would allowforthe use and operation of Unmanned Aircraft Systems (UAS) within the National Airspace (NAS) foragriculture crop surveillance, analysis, wildlife management and flighttraining. The application is to aid and assist in agriculture research with universities and farming communities to develop innovativefarmingtechnologies and flight crew training. Flying Tiger Aviation, LLC request thatthe FAA approve an exemption based on aspecific platform ofsize, weight, speed and limited operating range. Whereas, under normal circumstances might not otherwise conform to guidelines set forth in 8900.1, Volume 16, Chapter5, Section 4 (16-5-4-3) and (16-5-4-5) forOperations within the NationalAirspace. Operational control would remain within FlyingTigerAviation, LLC in which "due regard" for rules, regulations and operational procedures will be adheredto. The purpose ofissuance for an Agricultural COA exemption is:
• Development of newtechnologies • Improved agriculturetechniques and crops • Agriculture research • Flight crewtraining • Development of use for agricultural sensors and imagery

The platform in consideration forSection 333 Exemption is Drone America's DAx8. This platform is an eightblade rotorcraftthat has the capabilitiesto safely perform the applications for agriculture crop observations.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 1

### ) i / 

## ) ) /
1 ) \ J 

### ) \ ) 

### ) ) 

### ) 

## ) \ ) \ j 

### 'I ) 

## ) \ ) 

### )

j

\ / \ j ) Flying TigerAviation, LLC Federal Aviation Regulations for Exemption

Sincerely,

# ~~#-**~i*ger** Aviation, LLC Lawrence (Mo) L. Rolfs P.O. Box 238 Oak Ridge, LA 71264

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations

### ) 

## ) 

## ) \

\ )

\ ) 

## ) \ ) 

### ) \ J \ ) 

## ) ) 

## ) 

## ) ) ) 

## ) )\ ) 

## )

\ )

\ ) 

### ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

# SECTION 333 PETITION FOR EXEMPTION Flying TigerAviation, LLC request relieffrom thefollowing regulations in partorwhole thereof: PART 21 THAT DESCRIBES PROCEDURAL REQUIREMENTS FOR THE COMPLIANCE OF:
• Subpart G; Production Certificates • Subpart H; Airworthiness Certificates • Subpart I; Provisional Airworthiness Certificates • Subpart K; Parts Manufacturer Approval • Subpart N; Acceptance ofAircraft Engines/ Propellers and articles for Import • Subpart 0; Technical Standard Order Approvals 

### PART 45 THAT REQUIRES IDENTIFICATION AND REGISTRATION MARKINGS: Part45.11 (3); (b)(2); (c) 

### -Marking of Products- Prescribes that afire proof identification plate be visibly located on the exterior ofthe aircraft aft ofthe cabin doorand aircraft engines. The DAx8 does not have a cabin door or a pilot. Therefore request exemption for relocation of identification plate inside the fuselage thatwould be identifiable and protected from defacement and/or damage.


### Part45.15 - Marking requirementsfor PMA articles, TSO articles, and Critical parts: (1) Each TSO article with theTSO holder's namer trademark1 symbol/ or other FAA approved identification and part number; and (2) Each TSO article/ unless otherwise specified in the applicable TS0 1 with theTSO number and letterofdesignation/ all markings specifically required by the applicable TS0 1 and the serial number or the date of manufacture ofthe article or both. (c) Criticalparts. Each person who manufactures a partfor which a replacement timer inspection interval/ or related procedure is specified in the Airworthiness Limitations section ofa manufacturer's maintenance manual or Instructions for Continued Airworthiness must permanently and legibly markthat part with a serial number (or equivalent) unique to that part in addition to the other applicable requirements ofthis section. The DAx8 is an experimental aircraft and does not have TSO parts or critical parts. 

### 45.23 Display ofmarks; general: (a) Each operator ofan aircraft must display on that aircraft marks consisting ofthe Roman capital letter "N" (denoting United States registration) followed by the registration number ofthe aircraft. Each suffix letter used in the marks displayed must also be a Roman capital letter.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 1FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption
(b) When marks include only the Roman capital letter "N"and the registration number is displayed on limited, restricted or light-sport category aircraft or experimental or provisionally certificated aircraft, the operator must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches nor more than 6 inches high, the words "limited,""restricted,""light-sport,""experimental,"or "provisional,"as applicable. Due to platform size and airframe configuration, 2" regulation markings will notfit in accordance with Part 45.23 and therefore, request for modification to comply with only Part 45.11 fire proof identification plate located on the inside ofthe platform. 

### 45.29 Size ofmarks: (a) Except as provided in paragraph 

### (f) ofthis section, each operator ofan aircraft must display marks on the aircraft meeting the size requirements ofthis section. (b) 

### Height Except as provided in paragraph (h) ofthis part, the nationality and registration marks must be ofequal height. As described in Part 45.23 no surface is large enough to display full size or 2" numerals per 45.27.
PART 61 PRIVATE PILOT PRIVILEGES AND LIMITATIONS: 

### Part 61.113- (a) Except as provided in paragraphs (b) through (h), no person who holds a private pilot certificate may act as a pilot in command ofan aircraftthat is carrying passenger or property for compensation or hire; nor may that person, for compensation or hire, act as pilot in command. (b) A private pilot may, for compensation or hire, act as pilot in command ofaircraft in connection with any business or employment if: 1) The flight is only incidental to that business or employment; and 2) The aircraft does not carry passengers or property for compensation or hire. Flying TigerAviation, LLC request for relief of requiring a private pilots license and limitations, is thatthe aircraft size, weight, speed and limiting operational range are contributing factors that do not necessarily require a private pilots license to operate. The UA weighs less than 20 lbs. and does not exceed a maximum speed of 28 mph. The aircraft will be operated within a horizontal visual line of sight (VLOS) from the surface not to exceed 400 feet AGL. Operations are conducted from a handheld tabletthrough touch commands and waypoints with auto takeoff and landing capabilities. Operators are required to complete an FAA approve flight training ground school and hold a 2nd Class medical.

Flying TigerAviation, LLC 2015 2 Section 333 Exemption for UAS Operations \ )


# ' ) 

### ) 

## ) 

## ) ) )



## ' ) \ ) \ j 

## ) 

## ) 

## ) ) ) 

## ) ) 

## ) ) 

## ) ) \ / 

## ) ) I /
\ ) \ ) ) /\ )\ ) 

## ) ) 

## )
) ) 

## ) ) \ J 

## ) \ ) 

## ) ) 

## ) 

## ) ) 

## ) ) ) )

\ /
\ ) \ J

1 / 

### )

) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### Part 61.133 - Commercial pilot privileges and limitations. Prescribes in pertinent part, thata person who holds a commercial pilot certificate may act as pilot in command ofan aircraft: (a) 

### Privileges-(!) General. A person who holds a commercial pilot certificate may act as pilot in command ofan aircraft- (i) Carrying persons or property for compensation or hire, provided the person is qualified in accordance with this part and with the applicable parts ofthis chapter that apply to the operation; and (ii) For compensation or hire, provided the person is qualified in accordance with this part and with the applicable parts ofthis chapter that apply to the operation. Flying Tiger Aviation, LLC request for relief of requiring a commercial pilot certificate for the reasons thatthe aircraft is not carry persons or property for hire or compensation.


### PART 91 

### GENERAL OPERATING AND FLIGHT RULES PART 91.9 (8)(2) 

### CIVIL AIRCRAFT FLIGHT MANUAL, MARKING AND PLACARD REQUIREMENTS: (a) No person may operate a civil aircraft without complying with the operating limitations specified in the approved Airplane or Rotorcraft Flight Manual, markings and placards, or as otherwise prescribed by the certificating authority of the county of registry. Request for relief is thatthe DAx8 is not capable ofcomplying with Part 91.9, however, a flight manual with operating limitations and placards will be immediately accessible to the pilot in command during flight as prescribed. 

### 91.109 Flight instruction; Simulated instrumentflightand certain flight tests. (a) No person may operate a civil aircraft (except a manned free balloon) that is being used for flight instruction unless that aircraft has fully functioning dual controls. However, instrument flight instruction may be given in an airplane that is equipped with a single, functioning throw-over control wheel that controls the elevator and ailerons, in place offixed, dual controls, when- (1) The instructor has determined thatthe flight can be conducted safely; and (2) The person manipulating the controls has at least a private pilot certificate with appropriate category and class ratings.

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 3FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption A pilot using a ground control station tablet or laptop type ofcomputer flies the DAx8. There are no conventional controls. Inthe event ofthe ground control station failure, the pilot can manually land the aircraft utilizing a remote RC transmitter. 

### PART 91.119 MINIMUM SAFE ALTITUDES: Except when necessary for takeoffor landing, no person may operate an aircraft below the following altitudes: (a) Anywhere. An altitude allowing, ifa power unitfails, an emergency landing without undue hazard to persons or property on the surface. (b) Overcongestedareas. Over any congested area ofa city, town, or settlement, or over any open air assembly of persons, an altitude of 1,000 feet above the highest obstacle within a horizontal radius of2,000 feet ofthe aircraft. (c) Overotherthan congestedareas. An altitude of500 feet above the surface, except over open water or sparsely populated areas. In those cases, the aircraft may not be operated closer than 500 feet to any person, vessel, vehicle, orstructure. (d) Helicopters, poweredparachutes, andweight-shift-controlaircraft. 

### Ifthe operation is conducted without hazard to persons or property on the surface- (1) A helicopter may be operated at less than the minimums prescribed in paragraph (b) or (c) ofthis section, provided each person operating the helicopter complies with any routes or altitudes specifically prescribed for helicopters by the FAA; and (2) A powered parachute or weight-shift-control aircraft may be operated at less than the minimums prescribed in paragraph (c) ofthis section. Relief for exemption of minimum safe altitude is that agriculture observation will operate up to, but notexceeding 400 feetAGL. The pilots operating in remote locations in agriculture districts must ensure de-confliction ofobstacles and airspace encroachment. Mitigating factors will be considered prior to flight operations, and operational perimeter setbacks placed to ensure personnel safety. Procedural protocols will be enforced to ensure proper operational parameters are adhered to. 

### PART 91.203(8) CIVILAIRCRAFT: CERTIFICATIONS REQUIRED: (b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) ofthis section ora special flight authorization issued under §91.715 is displayed atthe cabin or cockpit entrance so that it is legible to passengers or crew. Flying Tiger Aviation, LLC request relieffor exemption of Part 91.203 (b) thatthe DAx8 is Experimental and does not require airworthiness certification based on size, weight, speed and limiting operating range. The DAX8 does not carry fuel or passengers. 

### PART 91.207 EMERGENCY LOCATOR TRANSMITTERS: (a) Except as provided in paragraphs (e) and 

### (f) ofthis section, no person may operate a U.S. registered civil airplane unlessFlying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 4 \. 

## ) 

## /)

\ } ) } 

## ) 

## ) ) 

# J )

., ) 

## ) ) ) ) ) 

## ) 

## ) \ ) 

## ) \ ) 

## ) 

## ) 1 J



## ) ) )\j '\ I 

### ) ) 

## ) l J 

## ) \ ) \ / 

## ) ) ) \, ) 

## ) \ ) 

## ) ) 

## ) ) \ ) 

## ) 

## )

\ ) 

### ) 1 J
\ ) 

## ) ) \ ) 

### )

\ ; FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption There is attached to the airplane an approved automatic type emergency locator transmitterthat is in operable condition for the following operations, except that after June 21, 1995, an emergency locator transmitter that meets the requirements ofTSOC91 may not be used for new installations. The DAx8 is equipped with an audible lost aircraft alarm that notifies the PIC of lost Comm in flight. In the event flight is non-recoverable the pilot or ground crew may retrieve the aircraft if lost by listening for the alarm. 

### PART 91.405(A) MAINTENANCE REQUIRED: Each owner or operator ofan aircraft: a) Shall have that aircraft inspected as prescribed in subpart Eofthis part and shall

between required inspections, except as provided in paragraph (c) ofthis section, have discrepancies repaired as prescribed in part 43 ofthis chapter. Flying Tiger Aviation, LLC requests for relief ofexemption of Part 91.405 (a) in part on the basis ofthe size, weight, speed and limited range ofthis unmanned aircraft. Flying Tiger Aviation, LLC pilots and ground crew technicians will be responsible for the inspection and safe operation ofthe aircraft. The aircraft will be inspected priorto each flight and maintenance performed as necessary to ensure flight safety. Ifthe condition cannot be resolved or repaired the flight will be terminated until discrepancies are corrected. 

### PART 91.407(A)(1) OPERATION AFTER MAINTENANCE, PREVENTIVE MAINTENANCE, REBUILDING, ORALTERATION: (a) No person may operate any aircraft that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless1) 

### It has been approved for return to service by a person authorized under 43.7 ofthis chapter; and Flying Tiger Aviation, LLC requests for relief ofexemption of Part 91.407 (a)(1) in part on the basis that Flying Tiger Aviation, LLC is the sole operator and the DAx8 is considered Experimental and the pilots and ground crew technicians are responsible for all maintenance, preventive maintenance, rebuilding and/or alterations. 

### PART 91.409 INSPECTIONS: (a) No person may operate an aircraft unless, within the preceding 12 calendarmonths

### 2)

Flying Tiger Aviation, LLC 2015 It has had an inspection for the issuance ofan airworthiness certificate in accordance with Part 21 ofthis chapter.

Section 333 Exemption for UAS Operations 5FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### Inspections and preventive maintenance is performed prior to each flight, therefore, Flying Tiger Aviation, 

### LLC requests for relief ofexemption of Part 91.409 (a)(2). 

### PART 91.417 MAINTENANCE RECORDS: (a) Each registered owner or pilot shall keep the following records forthe periods specified in paragraph (b) ofthis section: 1) Records ofthe maintenance, preventive maintenance, and alteration and records ofthe 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 ofan aircraft. The records must include: i) A description (or reference to data acceptable to the Administrator) of the work performed; and ii) The date ofcompletion ofthe work performed; and iii) The signature, and certificate number ofthe person approving the aircraft for return to service. 2) Records containing the following information:

Flying Tiger Aviation, LLC 2015 

### i) The total time in service ofthe airframe, each engine, each propeller and each rotor. ii) The current status of life-limited parts ofeach airframe, engine, propeller, rotor and appliance. iii) The time since last overhaul ofall items installed on the aircraft which are required to be overhauled on a specified time basis. iv) The current inspection status ofthe 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 ofapplicable airworthiness directives (AD) and safety directives including, for each, the method ofcompliance, the AD or safety directive number and revision date. 

### Ifthe AD or safety directive involves recurring action, the time and date when the next action is required. vi) Copies ofthe forms prescribed by 43.9(d) ofthis chapter for each major alteration to the airframe and currently installed engines, rotors, propellers, and appliances. a) The owner or operator shall retain the following records for the periods prescribed: i) The records specified in paragraph (a)(1) ofthis section shall be retained until the work is repeated or superseded by other work, or for 1year afterthe work is performed.

Section 333 Exemption for UAS Operations 6 

## ) 

## ' ) 

## )

) ) 

## ) ) ) 

### ) \ ) 

### ) 

## ) ) 

## ) l )

## ) ) 

## ) 'I ) 

## ) 

## /)



## ) ) } 

## ) \ 

## ) ) ) \ ) 

## ) \ ) \ ) l ) \ ) \ )

## ) \ } \ ) 

### 1 I 

## ) 

## ) ) 

## ' ) \ )

\. ) '; ) 

### ) \ } 

# -, ) 

## ) 

## ) ) \ ) \ ) 

### ) )

\ )

\ ) 

### ', J ) FlyingTiger Aviation, LLC Federal Aviation Regulations for Exemption II) The records specified in paragraph (a)(2) ofthis section shall be retained and transferred with the aircraft atthe time the aircraft is sold. III)A list ofdefects furnished to a registered owner, or operator under 43.11 ofthis chapter shall be retained until the defects are repaired and the aircraft is approved for return to service. Flying Tiger Aviation, LLC proposes a similar maintenance program that provides a general maintenance plan to maintain a safe condition for Unmanned Aircraft System (UAS) operations, with consideration for relief ofa licensed aircraft mechanic to perform maintenance. The Aircraft Maintenance Manual (AMM) predicates the scope of maintenance to be performed by the pilot or ground crew technicians prior to each flight followed by a post flight inspection. The maintenance manual is a separately controlled documentthat describes and compiles the scope ofdetail and maintenance procedures recommended by the manufacture, Drone America, Inc. This program is developed to identifythe maintenance and inspections to be performed progressively as each flight occurs. Major and minor components will require service, repairs and standard maintenance to maintain a condition ofsafe operations. To ensure flight safety and standards ofsafe conditions, the pilot is required to use the Preflight Checklist as referenced in 8130.34C; Appendix Afor a Maintenance and Inspection Program. Aircraft maintenance is recorded in the aircraft maintenance logbooks specific to that aircraft, describing all maintenance procedures and repairs as defined by the manufacturer's limitations. Maintenance, repairs and general conditions are in accordance with Title 14 CFR Part 43 Appendix D, as to the applicable aircraft and inspection schedules set forth by the aircraft manufacturer. The manufacturer's checklists and the Aircraft Maintenance Manual define inspection schedules and scope ofdetails.
The Progressive Maintenance and Inspection program is predicated to continuous safety and is conducted on a routine schedule throughout a 12-month calendar year. Inspections are to be performed based on the hours of UA, or cycles ofoperations
The inspection program prescribed is to be performed by a person who is an authorized manufacture's technician. The authorized technician is required to inspect the aircraft, document the findings and record all required maintenance, and return to service in a safe condition for flight. Inspections shall be done in compliance with 14 CFR 43.13 Appendix D and in accordance with the manufacturer's inspection checklist.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 7FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

# UMANNANED AIRCRAFT SYSTEM OPERATIONS 1. 

## OPERATIONALAND DESIGN CHARACTERISTICS: DAx8 is a VTOL (Vertical Takeoff and Landing) class aircraft. This UA is made of light-weight composite material for structural strength and increased payloads that is intended for hovering and low speed normal flight configurations. Configured as a land base Unmanned Aircraft Vehicle (UAV) this robust multirotor aircraft is designed for commercial applications such as agriculture. The unique 8-rotor configuration allows the DAx8 to carry a large payload while providing more safety and redundancyto the system. The advance software and GPS guidance system provide the aircraftwith self-stabilizing capability and multiwaypoint navigation. The DAx8 is powered by eight electric brushless motors that produce high level performance and thrust. The aircraft is intended to carry payloads such as atmospheric sensors, surveying sensors, mapping equipment, and high definition stabilized video and data links. Structural analysis and physical characteristics ofthe aircraft and electric motor analysis demonstrates that the airframe is capable of a thrust range of 19.9 to 29.2 pounds ofthrust. Through indoorflighttestingthe DAx8 will be evaluated in various flight maneuvers, and is not capable of fluttering throughout the flight envelope duetothe lack of moving parts. Throughout flight test parameters, stress analysis will provide data for positive or negative structural integrity. Based on other flight experience with similar platforms, flight data has not presented any unsafe conditions that would cause concern for safety while conducting flight within the normal category as defined in the user's manual. The airframe is constructed from 100% composite material, laid up in CNC molds utilizing standard wet layup bagging method. The carbon fiber airframe typically consists of four-layers that is applied one layer at a time, utilizing standard composite layup practices of sequenced alternating layers. The carbon fiber layup is alternated in a unilateral direction of 

## oo and 45° bias layers, which provides a light weight durable airframe capable of withstanding harsh environments and abuse. Manufactured parts are vacuum bagged and oven baked to a temperature of 160° and temperature controlled through a ramped up and ramped down process to assure proper cure as instructed perthe resin manufacturer. Work is performed in accordance with AC 20-1078 as guidance and in compliance with 14CFR Part 23.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 8 \) \ / \ J

\ ) 

## ) ) 

## ) ) 

## ) ) ) 

## ) 

# " }
j 

## ) ) 

## ) ) 

## ) ) \ J 

## )

\ ) 

## ) \ ) 

## ) ) ) ) \

\ )\ J 

## ) \ ) 

## ) \ ) 

### ) 

## ) 

## ) \ 

## ) ) 

## ) 

## ) ) ) \ ) 

## ) ) ) \ j

### )

\ )

\ )


## ) 

## ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### UAS PreflightOperations: Preflight planning is a multi-task process requiringweather briefing, mission planning, preflightsafety checklist, and UAS walk-around inspections. Weather Briefings: Weather briefings may be obtained through various sources:
• Flight Service Station (FSS) • Telephone Information Broadcast System (TIBS) • Transcribed Weather Broadcast System (TWEBS) • Direct UserAccess Terminal System (DUATS) Weather analysis must be recorded priorto each flight and logged on thefollowingweather analysis tables denoting current and forecasted conditions within the time ofthe operation. Regional weather updates may be obtained within the vicinity of the airport or the operation area by contacting these agencies to obtain current weather information and verify suspected deteriorating conditions:
• The Automated WeatherObservation System (AWOS) • AutomatedTerminal Information Service (ATIS) The Mission Commander must present a detailed mission plan prior to the mission outlining the scope and objectives of the operation. The Mission Commander in conjunction with the Operations Manager is responsible forthe development and the outcome ofthe operation. The initial scope of preflight planning objectives will be developed as part ofthe operational flight testing, development and eventual marketing. This provides for expectations to be readily met, or exceeded in the operational preflight and planning process. Preflight communications amongst crewmembers and Operation Managers establishes the objective ofthe mission criteria and expectations. In the preflight briefing the Operations Manager will assign a Mission Commander for the test operation to be responsible for organizing personnel, UAS systems and equipment for the mission. Should the Mission Commander find the resources to conduct the mission adequately and safely are unavailable, he is to notify the Operations Managerto resolve the problem/s. At the time the Mission Commander is assigned the responsibility ofthe operation, he becomes the point of contactfor all mission-related issues. The Mission Commander must discuss mission objectives, weather and address any requests in regards to the mission. The Mission Commander must keep record of all correspondence and documentation pertainingtothetest operations. The Mission Commander must brief all personnel before the commencement of the test operations and allocate duties atthistime. The briefing should take place before departure ifoperations are at a remote site.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 9FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption

All personnel and support crew must be briefed on: 

## • 

## • • 

## • • 

## • • 

## • Mission objectives Crew Duties and responsibilities Operating conditions Flight planning Perceived difficulties (ifany) Emergency procedures Currency and training requirements Flight Planning Flight planning shall be the responsibility ofthe Mission Commander and is considered a key factor in the success of every operation. The Mission Commander must consider weather, UAS payloads, performance, and battery endurance. No person may begin a flight in the UA under VFR, or IFR conditions unless consideration for meteorological conditions is taken into consideration and conditions have been calculated to determine there is adequate battery life to complete the planned mission and return to the scheduled point of landing under normal operational speed. In addition, backup batteries must be fully charge and available for replacement when necessary for the duration ofthe operation. 

### Payloads: The DAx8 payload is client specific and the DAx8 is capable ofcarrying awide range ofpayloads weighing upto 4.4 pounds, includingstabilized EO/IR gimbal, multi-spectral sensors, gee-imaging payload, etc. Due tothe nature of UAS operations with awide range ofpayloads, all internal and external payloads requirethe UAto have weight and balance calculation priorto everyflight. The payload compartment is located in the center ofthe aircraft, directly overthe desired CG, makingthistask straightforward. 

### Flight: All commands duringflight operations are directed and changed via the GCS software controls interface in real-time. i.

ii. Duringflight, the PIC monitorstelemetrydata and makes appropriate changes in altitude, speed, heading and waypoints using keyboard/touch screen inputs and/or mouse point and click commands. Additionally, the PIC can also control the UA using astylus for point and touch to control the UA'sdirection. The systems required for normal flight operations includethe GCS, the ground side data link and associated antennas, the autopilot and 3D GPS, static air pressure sensor, and air data link.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 10 )



## ) ) 

## ) 

## ) .)

\ J 

### ) 

## ) 

## ) )


## ) ) 

## ) 

## ) ) ) ) ) 

# ' \ ) 

### )

\ )

\ )

\ )\,


### ) 

### ) 

## ) \ J 

### ) I / \ ) 

## ) ) 

## ) \ ) \ ) 

## ) ) ) 

## ) 

## )
\ ) \ ) 

### ) \ ) I J \ J \ )



### )
\ ) \, / FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption

iii. Critical process points include:
• Adequate numberofGPS satellites acquired to provide 3D solution
• Functional primary communication data link 

## • Functional autopilot Flight Core and IMU 

## • Current maps and weatherdata are loaded on the GCS 

## • Batteries are fully charged priortotakeoff 

## • Motors are inspected for proper rotation direction and correct propeller orientation is verified.
• Sensor/payload is installed correctly and securely.
a. The DAx8 control mode is selected by the flight mode switch on the PIC Hand Held Controller, or by selectingthe flight mode in the ground station user interface. The flight control modes available depend upon the hardware installed. The followingthree optionsforflight modes are available:
1. Manual - Direct control via RC controller 2. Attitude mode -Autopilot self-levels the aircraft, while still being guided bythe PIC 3. Autonomous- Fully controlled via the autopilot and uploaded waypoint set b. The control panel screen will displaythe control mode ofthe UA.

c. In-Flight Plan Deviations: In-flight deviations are madethrough the autopilot system. The course is quickly changed through the Command Loops screen by setting a newwaypoint and commandingthe UAV to tracktothe new course. The autopilotwill askthe PIC to confirm this command priorto makingthe deviation. The flight plan mayalso be changed through the EFIS by sliding, or clicking on the altitude, airspeed and heading bugs to set a new course. These methods also require a confirmation bythe PIC priorto execution ofthe command. d. Lost Communications: 1. Loss ofCommunications between the Observer and the Pilot in Command: The PIC and Observerwill be collocated during operationsforthis COA and communications will be through direct communication. However, ifan emergency event caused loss ofvisual sight between PIC and Observer and/or loss ofabilityto perform direct communication between the PIC and observer, the PIC will utilizethe following tools to re-establish communications with the Observer.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 11FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption
-Hand held radio -Cellular phone -Hand Signals (may be used solely or in conjunction withthe communication equipment) Iflost communication cannot be re-established the UA will be immediatelygrounded until communications can be regained. 2. Loss ofCommunications between the Pilot in Command and AirTraffic Control: Ifrequired, the PIC will communicate withATC through use oftwo-way radio communications oracellular phone based on the agreement between ATC and the PIC. In the eventthe PIC is unable to establish communications or loses communication, the PIC will immediately land the UA until communications can be regained. In all cases, when during Loss ofCommunications there is concern for people or property in the air or on the ground the PIC will immediately land the aircraft. 

### 4. Landing and Recovery: Landing is performed in the same wayas takeoffor launching in a hovered configuration.
5. Post Flight:
a. Systems required for safe postflight operations include aircraft retrieval, aircraftshut down, proprietary equipment properlystored and the aircraftsecured. i. After each flightthe UA will be plugged in so that its onboard telemetry data can be downloaded and avisual inspection can be performed. ii.
iii. During postflight, priorto power off, the datafrom the autopilot must be downloaded forfuture replay in software in loop simulation. Post flight inspection
• Inspectforvisible damage from hard landings/debris ingestion into

propellers (bugs, rocks, sand etc).
• Inspect all exposed fasteners and screws for security.
• Inspect camera/payload/sensorfor any damage.
• Inspect batteries and wiringfor excess heat generation which may

suggest a pending failure.
• Inspect all antennae and exposed equipmentto ensurethey are free

ofdamage.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 12 \ J 

## ) ) 

## ) ) \ ) l ) \ j \ } 

## ) \ ) 

## ) \ 7 

## ) 

# J

\ ) 

## ) ) 

## ) ) 1 /

# ' )

\ ) 

### )

\ )

' ) 

## ' )

\ /

## ) ) \ J \ } I J l J 

## ) \ ) \ ) \ ) \ ) 

## ) \ / 

## ) 

## ) ) 

## ) ) \ } 

### ) \ ) \ )



## ) )



### ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption

b. Post flight inspection happens afterthe electric motors are shut down and the DAx8 power is OFF. The Crew Chiefwill conduct avisual walk around inspection ofthe aircraft and connect the data terminal cable from the GCS tothe aircraftto download theflighttelemetry. 6. Operating History: Initial testflights have been conducted indoors at Drone America's production facility. Initial gain tuning has been completed and stable flight has been demonstrated. Initial flight-testing indoors has proven to show consistent stabilityand responsiveness. Flighttestingwill continue indoors until authorization is approved foroutdoortesting.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 13FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### 2. Maintenance, Inspection and Repairs: Referto page 7forthe description ofthe maintenance, inspection and repairs procedures. Prescribed Maintenance Procedures: 

# LIST OF EFFECTIVE PAGES CHPTR TITLE PAGE{s) REV EFFECTIVE DATE Contents 

### v, vi Original 1 DAx8 Progressive Inspection 

### 76 Original Conditionsfor Return to Service 76 Original 2 UAS Aircraft Data 

### 77 Original 3 Owner/OperatorAttitude 

### 77 Original 

### 4 DATA 

### 77 Original 5 Records 

### 77 & 78 Original 6 General Access and Conditions 

### 79 Original 7 General Cleanliness 

### 79 Original 8 Portable Ground Control Station 

### 79 &80 Original 9 Aircraft Electrical System 

### 81 Original 10 Aircraft Equipment/Furnishings 

### 81 Original 11 Miscellaneous Airframe Insp. 

### 82 Original 12 Aircraft Exterior Inspection 

### 82 Original 

### 13 landingGear Inspection 

### 82 Original 15 Electric Motor Inspection 

### 83 Original 16 BatterySystems 

### 83 Original 17 Propellers 

### 83 Original 18 Ground Control Station 

### 84 Original Equipment/Furnishings 19 Special Inspections 

### 85 Original 20 Conditions of Inspection 

### 86 Original Statement 21 Weight and Balance Sheet 

### 87 Original 22 Airworthiness Directive Sheet 

### 88 Original AppendixA 

### 1-A Original Airman's Preflight Checklist 1-A,thru 8-A Original 23 Appendix B 

### 1-B Original Squawk Sheet 1-B Original

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 14 

### ) 

## )

/ \

J 

## ) 

## )

) 

## ) ) 

## ) 

## ) ) } 

## ) 

## ) 'I ) 

## ) ) ) ) ) ) ) ) 

### l / \ ) \ /

\ ) \ ) 

## ) \ / 

## )

1 /

## .· \ 

### ) \ ) 

## ) ) 

## ) ) \ ) 

### ) 

## ) \ ) 

## ) ) \ ) 

## ) 

## ) 

# J ) ) 

## ) ) 

## ) ) \ / \. ) 

### ) 

### )

\ )
' ) 

### ) \ J 

### ) \ ) FlyingTiger Aviation, LLC Federal Aviation Regulations for Exemption 

# REVISION PAGE CONTROL SHEET

Removed Effected Page Date Inserted Effected Page Date Pages Description Pages Description

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 15FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption· 

# ProgressiveInspectionChecklist Currentdate of issue: September 16, 2014 Reference Data: FAA Order8130.34C, CFR 21 Certification Proceduresfor Products and Parts CFR 23 Airworthiness Standards, CFR 43 Maintenance, CFR 45 Markings, CFR 47 Registration, CFR 39 Airworthiness Directives, CFR 91 Subpart E, Maintenance, Preventative Maintenance and Alterations, CFR 145 Repair Stations, AC 43.13-1B Acceptable Methods,Techniques and Practices and 2B Major Repair and Alterations and the Manufacture's Maintenance Manual. 

# Conditionsfor Return to Service 1) The unmanned aircraft system (UAS) must be returned to service in condition for safe operation. Inspection is to ensure thatthe aircraft is not subjectto unusual wear, structural damage and/orsystem malfunctions. 2) Aircraft configuration and components installed must be consistent with manufacturer's drawings, specifications and otherdata thatare part ofthe equipment list. 

### NOTE:

NOTE: 

### Ifeitheroftheseconditionsarenotmet, theunmannedaircraftwouldnotbe consideredsafe foroperationandcannotbereturnedtoservice. This isamanufacturesreferenceguideforaProgressive Condition inspection checklistspecifictoDroneAmerica'sexperimentalUnmannedAircraft. This checklisthasnotbeenapprovedbytheFAA atthetimeof publishingthis original document. Referencetothemanufacturer'smaintenancemanualisnot exhaustiveandconsideration to CFR43AppendixDshouldbeconsulted. Inspection checklistsare updatedperiodicallyandpersonnelperformingsafety inspectionsshouldreferencewww.droneamerica.commaintenance for update revisionspriorto inspections. The owner/operatoris responsibleformaintainingthe UASin asafecondition, including compliancewith allmanufacturer'sdirectives andoperatinglimitations. The owner/operatoris also responsiblefor theinspectionofthe UASsystem to insure thattheaircraftis in compliance with CFR23AirworthinessStandards, andCFR43AircraftMaintenance.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 16 

### ) 

### ) 

## )

) j 

## )

) 

## ) ) ) ) 

## ) ) 

## ) 

## ) ) 

## ) 

## )

) \ / 

## ) )
I j 

### ) \ ) 

## )
\ ) \ ) 

### )') \ ) " \I



### )



### ) '\ ) 

## ) ) i / ) 1 ) \ ) 

## ) ) 

## ) 

## ) 

## ) 

## ) ) ) l J 

### ) \ ) \ J

\ ;' 

### ) 

### ) I J FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### UAS Aircraft Data: UAS Model:
_______ _ N-Number:



# ------------------- Serial Number:



## --------------- Year:
______ _ 

### Owner/OperatorAttitude: Does Owner/Operator have aconstructive attitudetoward Compliance? Order2150.3A Par. 205 

### Yes D No D N/ AD Verify MaintenanceTechnicians authorization CFR 65.91 

### DATA: 1. Manufacturer's Maintenance Manuals available? 2. Alterations- By what means are they approved? 3. Instructionsfor continued safe operations? CFR 23.1529 

### 4. Aircraft Flight Manual? AFM Date: /Rev# 5. Aircraft Placards CFR 45.13 

### 6. Verify all eight motors make/model are the same: Motors: KDE2814XF-775 CFR 45.11

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes D NoD N/AD

Yes D NoD N/AD Mfg. D Field Approval D or Other D Yes D NoD N/AD
Yes D NoD N/AD

Yes D NoD N/AD
1-Hours:

--- 

### 2-Hours:

--- 

### 3-Hours:
__ _ 4-Hours:
__ _ 5-Hours:
__ _ 6-Hours:
__ _ 7-Hours:

--- 

### 8-Hours:

---

17FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### 7. Verify critical component placards and serial numbers. 8. Verify life limited parts placards. 

### Records: 1. Verifycurrent Ground Control Station software updates CFR 91.9 

### Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD
2. Verify Experimental Airworthiness Certificate in GCS (Original Issue) Yes D NoD N/AD CFR 91.319 

### 3. Previous inspection: Total time:

---- 

### Date completed:
__ _ Certified MaintenanceTechnician#
_______ _ Yes D NoD N/AD CFR 43.11, 91.417 

### 4. Verify current and reoccurring AD's- Record in Aircraft maintenance logbooks: 1. Airframe Yes D NoD N/AD 2. Motors 3. Propellers 4. Appliances- See additional pages ifapplicable CFR 91.417 

### Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD
5. Verifystatus of life limited parts. Go to: www.droneamerica.com maintenance for Effective Date:
___ _ CFR 43.10 

### 6. Verify current Aircraft Flight Manual (AFM) is available CFR 91.9 

### 7. Verify currentweight and balance sheets are available Verify signature and date. 8. Verify ID plate is secured to UAS fuselage exterior. 9. Verify maintenance recordsfor each motor, propeller, airframe and appliance is in accordance with CFR 91.417. 10. VerifyATC Transponder/wADS-B has been checked within the past 24 calendar months per CFR 91.413 11. Verify autopilot/altimeter has been checked within the past 24 calendar months per CFR 91.411, 43 Appendix E

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes D NoD N/AD

Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD
Yes D NoD N/AD
Yes D NoD N/AD

18 

### ) \ )

) J 

### }


## ) ) ) 

### 1 / 

## ) 

## ) 

# ' J 

## ) ) / 

## ) ) ) ) ) _) 

## ) ) ) ) 

## ) ) \ / 

## ) \ ) 

### )

\, / 

## ) )

\ ) \ )\ j

\ J 

### ) ) 

## ) l**~~** \ j \. ) 

## ) 

## ) ) ) 1 / 

### 1 / 

## _) ) 

## /)

) ) ) ) \ ) 

## ) \ ) \ j \ ) \ I

\ )


### ) 

### ) 

### ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### 12. Verify autopilot-pitot/static system has been tested within the Past 24 calendar months per CFR 43 Appendix F 13. Record deferred items per Part 91 for daytimeVFR operations: a. Is the component placarded? b. Is there a maintenance record entry? c. Is the component disabled or removed?


### General Access and Conditions:

a. Remove lowerairframe hatches b. Remove optical payloads
c. 

### lOCK OUT- Install 

### ''T'' pin in ballistic recovery parachute


### General Cleanliness:

1. Wash/Clean exteriorofaircraft 

### 2. Clean aircraft interior 

### 3. Clean all motorsand propellers


### Portable Ground Control Station Inspection:

1. Verify placards are correct and readable perthe AFM. CFR 23.1541- 1567, CFR 91.31


### 2. Verify INOP placards: CFR 91.213 

### a. INOP instruments may only be disabled or removed byanA&P. b. Verify current equipment list. c. Verify maintenance records entries are updated. d. Verify Weight and Balance records are current. CFR 91.9

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes D NoD N/AD

Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD

Yes D NoD N/AD
Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD

19FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption



### 3. Verify compass is correct in the primaryflight display as shown in Electronic Flight InstrumentSystem (EFIS). 

### 4. Verify clock is set tothe correcttime zone on the monitor panels. 

### 5. Verify Handheld Nav Radios Part Numbers: 

### a. P/N 

### 1
_________ _ b. P/N 2
_________ _ 6. VerifyTransponder Part Number: Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD Yes D NoD N/AD

a. P/N Yes D NoD N/AD 7. Verifythere are no unusual odors {Such burning electrical smells). Yes D NoD N/AD 8. Verify Portable Ground Control Station registration concurs with Data plate. Yes D NoD N/AD 9. Verifyfire extinguisher is charged, properly rated and accessible. Yes D No D N/ AD 10. Verify speed controllers are operational. Yes D No D N/ AD 11. Verifythrottle travel is not restrictive and consistentwith RPM, figures {If applicable) on the Controller Configuration Screen. {Perform motor run-up -Idle, advance to max. RPM, backto Idle) Yes D NoD N/AD 12. Verify condition of Portable Ground Control Station. Yes D NoD N/AD 13. Verify electrical wires are properly identified. Yes D NoD N/AD 14. Verifythere are NO loose electrical connections. Yes D NoD N/AD 15. Verify electrical wires are secure. Yes D NoD N/AD 16. Instruments:Airware Autopilot System CFR 91.205 

### a. Verify autopilot-altimeter has been tested within 24 calendar months. CFR 91.411 

### b. Verify Electronic Flight Instrument System has been tested within the past 24 calendar months. c. Verify Direction Indicator is accurate perAirware Systems.

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes D NoD N/AD
Yes D NoD N/AD Yes D NoD N/AD 

### ) ) 

## ) ) 

### ) 

## ) 

## ) ) 

# " ) ) / 

## ) ) 

## ) 

# " ) 

## ) 

## ) 

## ) ) ) 

## ) ) )

-

## ) ) 

## ) \ } /\ ) \ ) ': / 

### ) \ ) I / \ } \ ) 

## ) \I /

### I _/ 

### I 20 / \ ) \, )

### ) 

## ) ) 

## ) \ ) 

## ) 

## ) ) l ) 

## ) \ J 

## ) 

## ) ) ) 

## ) )

l ) 

## ) 

## ) \ ) \, ) 

### ) ) 

### )
) ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### d. Verifythe operations ofthefollowingflight instruments have been inspected perAirware's inspection program: 1. Airspeed Indicator 2. Altimeter 

### Aircraft Electrical System: 1. Verify condition ofaircraft switch. Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD 2. Verifyvoltage and current draw (System Status Monitor).Yes D NoD N/AD 

### 3. Inspect aircraftwire harnesses for: AC43.13 Ch.n 

### a. Chafed orfrayed wires Yes 

## 0 No 

## 0 N/AD b. Insulation penetration Yes D NoD N/AD c. Outer insulation cracking Yes D NoD N/AD d. Damaged orexposed wires Yes 

## 0 NoD N/AD e. Evidence ofoverheating Yes D NoD N/AD f. Evidence ofarcing Yes D NoD N/AD g. Evidence ofchemical contamination Yes D NoD N/AD 

### 4. Verify aircraftwires are properly labeled. Yes D NoD N/AD 

### 5. Verify aircraftwires are marked by gage size. Yes D NoD N/AD 

### 6. Inspect bus barfor burned ortripped conditions. Yes D NoD N/AD 7. Verify grounding point nuts are tight and free ofcorrosion. Yes D NoD N/AD 8. Verify wires are properly clamped and secure. Yes D NoD N/AD 

### Aircraft Equipment/Furnishings: 1. Verify installed equipmentfunctions properly. Yes D NoD N/AD 2. Verify correct Flight Manual for applicable aircraft being operated from the Portable Ground Control Station is available. Yes D NoD N/AD 3. Verify batteries are charged. Yes D NoD N/AD 4. Verify batteries are properlysecured. Yes D NoD N/AD

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 21FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### 5. Verify backup batteriesare charged. Yes D NoD N/AD 6. Visually inspect ballistic recovery parachute. Yes D NoD N/AD 7. Visually inspect autopilotfor security and no adverse conditions.Yes D NoD N/AD


### MiscellaneousAirframe Inspection: 1. Verify antenna connections.
2. Inspectfor corrosion on, oraround antenna connections. 3. Inspect hatch seals for cleanliness, cuts, or abrasions. 4. Inspect lower hatch fastener blind nuts and hardware. 

### Aircraft Exterior Inspection: 1. Inspect airframefor delamination, pin holes, cracks, blisters and chipped paint. See manufacturesAMM for acceptable limits. 2. Inspect registration markings. (Replace or repair if required) CFR 45.ZZ{b) 

### 3. Inspect beacon. 4. Inspect condition of navigation lights. 

### Landing Gear Inspection: 1. Lift aircraft and turn overto inspect landing gear for bent, fatigued or cracked struts. 2. Inspectfor overweight landings. See Special Inspections and AMM for procedures.

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD Yes D NoD N/AD
Yes D NoD N/AD Yes D NoD N/AD

Yes D NoD N/AD

Yes D NoD N/AD 

## ) 

## )

\ ) 

## ) 

## ,)

) \ ) 

## ) 

## )

\ ) 

## ) ' ) \ ) 

## ) 

## ) ) ) ) ) ) 

## ) \ I / 

## ) \ ) \ )

\ ) \ ) 

### ) \**~** 

### 1 ) 

### I \ ) 

## zz

## ) \ } 

## )

) ) \ ) 

## ) ) 

## ) ) 

## ) ) ) 

## ) ) ) 

## ) \ ) 

## ) ) 

### ) ) I J i /

### ', / 

### ) \ )I / FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### Electric Motor Inspection: 1. Perform a motor inspection byvisually checking for debris in the windings or bearings. Physically turnthe propellers to ensure smoothness ofoperation. Yes 0 No 0 N/ AD CFR 43.15 

### 2. Inspect motorcontrol armsfor cracks ordelamination's. Yes 0 No 0 N/AD 3. Inspect condition ofmotorwires. Yes 0 No 0 N/AD 4. Inspect overall condition of motors Yes 0 No 0 N/AD 

### BatterySystems: 1. Inspect condition of batterycells. Yes 0 No 0 N/AD 2. Verify batteries are secure. Yes 0 No 0 N/AD 4. Verify batteries are charged. Yes 0 No 0 N/AD 

### Propellers:
The DAx8 uses 8 counter rotating propellers; 4 CW and 4 CCW. These alternate in rotation direction. The #1 propeller is thefront left. This is aCW propeller as viewed from above. Each consecutive propeller should alternate from CW to CCW to CW as inspected in aclockwise fashion aroundthe perimeter ofthe DAx8. Each propeller should be inspected as follows: 

### 1. Verify correct propeller rotation direction and orientation (thrust direction) 2. Inspect propellersfor physical signs ofdamage or abuse 3. Check that propeller bolts are tight Propellertype: Fixed Propeller Material: Composite 1. Is the propeller maintenance record logbook available? Yes 0 No 0 N/AD 2. Ifthere is no propeller maintenance logbook, sign inspection off in Airframe Logbook. 3. Inspect propellers condition for nicks, cracks and delamination's.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes 0 No 0 N/AD
Yes 0 No 0 N/AD

23FlyingTiger Aviation, LLC Federal Aviation Regulations for Exemption


### 4. In the event of propellerdamage, remove and replace propeller. Yes D No D N/ AD Special Inspection: 

### In the event of propellerdamage, DO NOT attemptto repair. 5. Verify proper propellerscrews are used per manufacturer's recommendations. 

### Ground Control Station Equipment/Furnishings: 1. Panasonic Tough Pad 

### 2. COMMS 

### 1 

### & 2- Garmin/GTR 

### 225 

### 3. Airware Autopilot Systems 

### 4. SageTech XPS-TR ModeSwith ADS-BOutTransponder 

### 5. Video Receiver

### 6. Video and Voice Recorder

### 7. Ground Data Terminal GDT

### 2100- TECOM Industries. 

### 8. Spectrum Analyzer

### 9. Range Attenuator

### 10. Antenna Selector Control - 

### 11. Verify Portable Ground Control Station batteries are charged. 

### 12. Verify Portable Ground Control Station is connected to main powersupply. 

### 13. Verify Ground Control Station Operating Handbook is readily available. 

### 14. VerifyAircraft Flight Manual {AFM) is applicable to aircraft currently being operated. 

### 15. Verify current aircraft registration.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 

### Yes D NoD N/AD
Yes D NoD N/AD

S/N S/N S/N S/N S/N S/N S/N S/N S/N S/N Yes D NoD N/AD

Yes D NoD N/AD

Yes D NoD N/AD
Yes D NoD N/AD Yes D NoD N/AD

24 --

### ) )

\ 

### y ) 

## ) 

## ) ) )

) J 

## ) ) \ ) \ ) 

## .)

) 

## ) 

## ) ) )

-

## ) ) \ ) \

### ' / 

## ) 

## ) ) \ ) \ / \ ) \ j 

### 1 1 _) \I /



### i /FlyingTigerAviation, LLC Federal Aviation Regulations for ExemptionFlyingTigerAviation, LLC Federal Aviation Regulations for Exemption
4. Lightningstrike damage. (Airframe 

### & Electronics Inspection) Upon landing In the event oflightning strike damage, inspect structure for burns, blisters and delamination. Consultthe AMM forstructural repairs. All electronics must be returned to Drone America for inspection. 5. Severe turbulence inspection. The DAx8 is not intended tofly in areas ofsevere turbulence. Its configuration however is nottypically susceptible to overload due toturbulence. Controllability may be affected, butstructural damage is highly unlikely. Condition of Inspection Statement: No person maysign-offany repair, alteration, or modification tothis aircraft unlessthey are aqualified mechanicthat has been authorized by the manufacture as a MaintenanceTechnician. The Maintenance Technician must provide astatement of release priorto returningthe aircraftto service. 

### Icertifythatthisaircrafthasbeeninspectedon 20

__ in accordancewith thescopeand detailof14CFR43,AppendixDandDroneAmerica'sAircraftMaintenanceManual(AMM}, andhave foundtobein aconditionforsafeoperationin compliancewithFAA'sacceptablemaintenanceand 100-HourInspection Program. Aircrafttotaltime:
__ _ A & P:
_________ _ 

### Print ------------Lie.#
_________ _ 

### Signature Maintenance Technician:---------- Print

__________Auth. #
______ _ 

### Signature

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 26 

### ) 

### )

\ ) 

## ) 

## ) ) 

## ) ) 

## ) ) 

## ) ) 

## ) 

# ) ) ) 

## ) )

## )

) ) l ) \. ) 

## ) )

·i / \, /

I j \ ) \ ) \ /\ )

\ ) 

### )


## ) ) ) 

## ) 

## ) ) l / \ ) 

## ) 

## ) 

## ) 

## ) )

l j

\ ) 

## ) 

## ) ) ) )



## )

\ ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### WEIGHT and BALANCE SHEET
Date:
__________ _ Aircraft Make/Model:
______ _ Serial Number:



### --------------------- Removed Equipment Weight Arm Moment



### Total
Installed Equipment Weight Arm Moment



### Total

Forward Limit Check (Limit?) 

### A/C Empty Weight Arm Moment Payload Total

Performed By:
________________ __ Signature:
_________ __ Mechanics License#:

-----------

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 27FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### 3. Communication and Frequencies: 1. The MicroHard control system architecture is described below: The primary data and pilot link is a 902- 928MHz spread spectrum frequency band with 400 kHz increment and an approximate 175kpbs data rate. The data link is configurable between 1Hz, 10Hz and 25Hz telemetry data update rate. 2. Communication data links used on DroneAmerica's DAx8
a. Data linkdescriptions: The 2.4Ghz spectrum will be used for command and control, as well as, potentiallyvideo downlinkforthe DAx8. The Microhard 2.4Ghz Nano series n2420will be used. Spectrum approval is not needed as 2.4Ghz is open to the public under FCC Part 15.247, IC RSS210, CE. b. The Microhard Nano series radio is not encrypted as standard, but has the abilityto support both 128bitand 256bitAES encryption in the USA, and with permitfor use outsidethe US and Canada.



### c. The primary command and control 2.4GHz data link has range up to 10 miles with the Omni antenna, and up to 40 miles with Vagi directional tracker antenna. The range was determined by the autopilot manufacturer through extensive testing. The DAx8 is not expected or intendedto operate at adistance greaterthan 3 miles from home base. Primary flight telemetry data such as airspeed, altitude, attitude, and position have precedent over all other telemetry. Telemetry update rate is selectable between 1Hz, 10Hz and 25Hz. d. The radio signal strength indication is displayed on the system window and the value is measured by the GCS software and displayed on the Radio Signal Strength Indicator (RSSI) with typical operational range of-71 to -115.
e. The DAx8 is not currently equipped with redundant control links. At the intended operating range, the single Microhard data link is very robust. In the event a lost link situation should occur, the lost link procedures pre-programmed into the autopilot are executed. This includes a return to home command. Should link be lost, the UAV will automatically head home, therefore reducing range, and typically the link will be reestablished. f. The DAx8 does not use satellite communications for command and control. g. Due to the sparsely populated location of operations there are no foreseen interferences from any outside influences that would affect UA operations. Areas of operations are unlikely to have inference with other communication sources due to the UA operating on an assigned frequency.

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 28 ) / 

## ) ' ) 

## )

\ J 

## ) ) 

## )**~** J \ ) 

## ) 

## ) ) 

## ) ) ) ) ) \ J 

## ) ) ) 

## )
\ /
\ ) 

### i /\ }
/ '\



## '\ J \ ) \ ) 

## ) 

## )

\ ) \ ) 

## ) \J \ ) '\ I / \ ) \ I / \ ) 

## ) ) 

## ) ) ) 

## ' ) 

## ) ) \i / \ ) \ I / \ ) 

### )



## ) \ j \, j

### )

\ ) \ / FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption



### 4. 3. Design characteristics and proceduresto prevent lost communication:
a. In regards to RF interference- Careful design and integration ofantennas and antenna locations are positioned to ensure minimal RF interference between different RF sources, and between different potential sources of RF interference. b. Pilots are trained extensively with an in depth knowledge of RF and aircraft limitation to prevent inadvertent flight beyond communication range. This requires careful flight planning with consideration for altitude and terrain masking. The flight control system also warns the pilot when the RSSI quality is below the threshold. A robust communication link capable of up to 40 miles with proper antennas is implemented on the DAx8, which is not expected to operate fartherthan 3 miles from home.
c. Antenna mounting locations are carefully calculated and tested to ensure that maximum communication is obtained. Exposure to each antenna is independent of the aircraft orientation. d. In the event of loss ofGCS communication and functionality, the UA will automatically execute a preprogramed lost communication flight plan which can include auto-return home and autoland.
e. Loss of UA functionality will activate flight termination which includes motor termination and deployment ofthe parachute, and/or aerodynamictermination ifrequired. f. Atmospheric attenuation including precipitation condition may cause degradation of the communication link quality. Careful flight planning must be performed while taking into account for atmospheric conditionsthat may decrease operational range. 

### Pilot/Crew Qualifications/Training Reference: Pilots must completethree DAx8 UAS missions every 90-days. Ifa PIC loses currencytheywill conduct a minimum ofthree successful training UAS missions underthe direction ofa current PIC to establish currency in accordance with FAA Flight Standards Information ManagementSystem (FSIMS) 8900.1, Volume 16, Chapter4, Section 16-4-1-3, B6. Pilots are required to hold a 2nd Class medical. 

### Observers: All observers have received FA Part 91 SpecificTraining as required underthe FAA Flight Standards Information ManagementSystem (FSIMS) 8900.1Volume 16, Chapter 4, Section 4, 16-4-4-1, B.
1. Training includes FAR Part 91, a. Section 91.113 Right ofWay Rules: Except forwater operations. b. Section 91.115, Right ofWay Rules: Water operations c. Section 91.119, Minimum Safe Altitudes (MSA):General d. Section 91.155, Basic VFR weather minimums

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 29FlyingTiger Aviation, LLC Federal Aviation Regulations for Exemption

2. Radio communications with airtraffic control (ATC) pilot phraseology. 3. Appropriate sections oftheAeronautical information Manual (AIM). 4. Observers are required to hold a 2nd Class Medical. 5. Observers must completethree DAx8 UAS observer missions every 90 Days. Ifthe observer loses currencytheywill conduct asuccessful observertraining mission underthe direction ofacurrent observerto establish currency. 

### 5. PilotType Ratings and Medical Standards: Qualified pilots tofly DAx8 in accordance with FAA Flight Standards Information Management System (FSIMS) 8900.1, Volume 16, Chapter4, Section 16-4-1-3, B6.

Total Pilot Manned TotalUnmanned Medical Certificate Ratings Hours Hours CFI, MEl, CPL & ATP 8,000 Class II CFI, CFII, CPL, 23,000+ Class II CFI, CPL 3000 Class II

CFI 2500 Class I CFI, CFII, 3000 Class II Total Time: 39,500 PilotCertifications, FlightExperience andMedica/s

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 30 I )



## ) ) 

## ) ) ) ) 

### 1 J 

## ) ) ) 

## ) ) 

## ) 

## ) ) 

## ) )

)

'1 / I J 

### l /
\ )\ j


### ) 

### )) 

## )

)

'', j 

## ) ) \

.**~J**



## ) 

## ' ) \ ) ' ) 

## ) \ J 

## )

'' J 

### )

\ J FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### 6. Operations a. UA Operational Visibility: The DAx8 is unique and is easily identified by its enclosed eight-rotor configuration and spheroidal design and by the bright red and/or orange paint scheme on the airframe. The DAx8 is equipped with red and green LED navigation lights. In the event the anti-collision lights are inoperativethe flight shall be terminated untilthe condition is corrected. 

### b. Critical system process points include: The most critical system process is the setup oftheflight configuration file for each airframe. This includes all ofthe data such as IMU orientation, ESC calibration, airframe weightand CG location relative tothe IMU. These parameters are configured per airframe type. The autopilot configuration, includinggains and all theflight parameters, can be copied to multiple vehicles with the exact same setup. In testing, it has been verified thatthe autopilot is robustto small changes in vehicle weight and balance, but itstill needs to be quantify how large the changes need to be before it is necessaryto re-tune the vehicle. When performingthe initial setup, it is necessaryto knowwhat PWM range the ESC's are calibrated to, and what PWM values correspond to min and maxthrottle parameters. These are entered as parameters intothe Airware configuration utility. These values are not available for most off-the-shelfspeed controllers; therefore, each ESC will have to be calibrated externallyto the same known PWM range. The configuration files are stored in theAirware cloud. Once created, they are stored inthe data base for easy access to new or existingvehicles as information is needed or required. Version control is provided on the Airware cloud. The Mapping Updates are derived from Terra Server Google and Bing. Maptiles are cached and gee-referenced automatically. For elevation data, we use SRTM (Shuttle RadarTopography Mission) data that can be downloaded from the USGS. All maps are updated in real timevia the internet. Engine Start Ground Procedures forthe DAx8 has a built in software algorithm for motorstart. The flight controller must receive asignal from the ground control station in ordertoturn on the motors, which is executed by the AVO. This start and takeoffcommand requires asecondary confirmation from the AVO before being sent tothe DAx8, thus preventing any chance ofan accidental start. All ground personnel are cleared and required to stand back 35 feetfrom the takeoffarea priorto motorstart.


### c. Flight: All commands duringflight operations are directed and changed via the GCS software control interface in real-time.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 31FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption
Duringflight, theAVO monitorstelemetrydata and makes appropriate changes in altitude, speed, heading and waypoints using keyboard/touch screen inputs and/or mouse point and click commands. Additionally, theAVO can also control the UA using astylus for point and touchto control the UA's direction. The systems required for normal flight operations includethe GCS, the ground side data link and associated antennas, the autopilot and 3D GPS, static air pressure sensor, and airdata link. Critical process points include:
• Adequate numberofGPS satellites acquired to provide 3D solution
• Functional primary communication data link
• Functional autopilot Flight Core and IMU
• Current maps and weatherdata are loaded on the GCS
• Batteries are fully charged priortotakeoff
• Motors are inspected for proper rotation direction and correct propeller orientation is verified. • Sensor/payload is installed correctly and securely. The DAx8 control mode is selected bytheflight mode switch on the AVO Hand Held Controller, or by selectingthe flight mode in the ground station user interface. The flight control modes available depend upon the hardware installed. The followingthree options forflight modes are available:
1. Manual - Direct control via RC controller 2. Attitude mode- Autopilot self-levels the aircraft, while still being guided bythe AVO 3. Autonomous- Fully controlled via the autopilot and uploaded waypointset 

### d. Flight envelope: Initial flighttestwill be done indoors within the production facility. Flight will continue indoors until authorization is approved for outdoor operations. Outdooroperationswill consist ofline sight not exceeding Visual Line ofSight (VLOS) and notto exceed 400' AGL. Operations will be performed in asafe manorand in accordance with 14CFR Part

### 6i and Part 91. All outdoorflights will be contained within a preplanned flight envelope that is determined bythe mission commander and approved bythe Flight Safety Officer.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 32 

### ) 

## ) 

# ' J 

## ) ) 

## ) )
'\ ) \ j 

### ) \

## ' / \ ) 

## ) ) 

## ) ))



## ) 

## ) ) ) )

\ )



### )\ I 

### ) 

## )

\ /\ ) ) \ /



### ) 

### ) )

l )

)

\ / FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### 7. OPERATING SPECIFICATIONS:
a. DAx8 operating specifications are:



## * Priortoflight, theAVO can set altitude limitationsfrom the Ground Control Station to

preventthe UA from exceeding specified altitudes. 

### b. Minimum Flight Visibility and Distance From Clouds: Flight operationswill be conducted in compliance with 

### 14CFR Part 

### 91.155 Basic VFR Weather Minimums. Operations are generally400' AGL and will be performed as stated in the Basic VFR Weather Minimumtable.

Less than 10,000feet MSL

At or above 10 000 feet MSL
1,200 feet or less above the surface (regardless of MSL altitu

ore than 1,200feet above the surface but less than 10,000feet SL
Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 

### 0 feet below. 1,000 feet above.

000 feet horizontal. 00 feet below. 1,000 feet above.

000 feet horizontal.
0 feet below. 1,000feet above.

,000 feet horizontal

33Flying TigerAviation, LLC Federal Aviation Regulations for Exemption



### c. Hazards: OutdoorOperationswill be conducted in day-light hours in VFR conditions at400' AGL, or less and within visual line ofsight. These flight parameters present a minimal meteorological hazard to the operations and will not be operated in icing conditions. 

### d. Safety Mitigations: Priortoflight, it is the responsibility oftheAVO, Mission Commanderand the Flight Safety Officerto verify and monitorcurrent and forecasted weatherconditions. In the eventthe weatherdeteriorates, theflight will be terminated until adequate VFR conditions can be met per 14CFR Part 91.155.

8. 

### OPERATIONS AREA: Log Cabin East- The Log Cabin East exemption area is a remote, diverse row crop area of agricultural activity located in Morehouse Parish, Louisiana. It is owned by Barham Brothers, LLC, Partners in the development ofthe E. Edwards Barham Aerial Application Center of Excellence with several state universities researching drones for agricultural use. The area is located 6 Nautical Miles (NM) Northwest ofthe city of Bastrop and 7 NM from the nearest public airfield or air operation. Unmanned aircraft operating in the area would be transported via over land vehicle and launched from within the area. There are no man-made structures within the area boundaries. The nearest structure is a barn used for farm equipment storage, located 1500'due east ofthe area along the Wilmot Highway. An electrical substation is located 1700' east/northeast ofthe area. The nearest occupied structured is a house located 3000' from the nearest area boundary. Aerial activity inside the area will be restricted to periods when farming operations 

### are not being conducted in the fields within the area boundaries. 

### Oak Ridge Northwest- The Oak Ridge Northwest area is a remote, diverse row crop area of agricultural activity located in Morehouse Parish, Louisiana. 

### It is owned by Barham Brothers, LLC, Partners in the development ofthe E. Edwards Barham Aerial Application Center of Excellence with several state universities researching drones for agricultural use. The area is located 2 Nautical Miles (NM) Northwest ofthe city ofOak Ridge and 9 NM from the nearest public airfield or air operation. Unmanned aircraft operating in the area would be transported via over land vehicle and launched from within the area. There are two man-made structures within the area boundaries: A pivot irrigation system in the northwest corner and an equipment storage and field maintenance shed in the southeast corner. The nearest occupied structured is a farmhouse located 4000'from the nearest area boundary, the southwest corner. Aerial activity inside the area will be restricted to periods when farming operations 

### are not being conducted in the fields within the area boundaries. 

### Bastrop AirportTraining Airspace- The Bastrop AirportTraining Airspace area is located at a remote airfield 2NM southeast ofthe town of Bastrop, Louisiana in Morehouse Parish. 

### It is owned bythe City of Bastrop, partners in the development ofthe E. Edwards Barham Aerial Application Center of Excellence with several state universities researching drones for agricultural use. Unmanned aircraft operating in the area would be launched and recovered

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 34 '\ ) 

### ) 

### )



## )

) \ ) 

### ) 

## ) 

## ) 

## )

)

..

# ) /)

) ) )

\ )

\ ) 

### )\, )

\ ) \**~)** 

## ) ) ) 1 j**"~** ) \ ) 

## ) 

## ' I J 

## )

\ j \ ) 

## )

\ ) ) 

### )

\ ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

### from within the exemption airspace. There are two man-made structure within the area boundaries: an ASOS transmission tower and awindsock. The area is within the airfield boundaries. All UAS flights will occur within the defined area and in compliance with the radius and altitudes defined for avoiding interference with theASOS transmitter. The higher ofthe two structures is the ASOS antenna with a height of33'AGL. The nearest man-made structures are hangers located across the runway to the west and 1500'from the west boundary ofthe training area. The nearest inhabited structures are the Louisiana Delta College facility 2000' west ofthe east boundary. The airfield manager will approve UAS flights in this airspace and a NOT AM posted the day prior defining times of UAS operations and prohibiting any manned flights into or out ofthe airportwhile UAS operations are being conducted. In the event ofa manned aircraft entry into the airport environment, the UAs will be recovered and grounded until the aircraft has cleared the runway if landing or departed the airspace if transient ortaking off.

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 35FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption

Bastrop AirportTrainingAirspace NWCorner 32 45 49.00 N09152 57.00W NNE Corner 32 45 49.00 n091 52 38.00W NE Lower 3245 37.00 N09152 37.57 W ENE Corner 32 45 37.00 N0915114.78W SE Corner 32 45 25.00 N091 52 14.25 W SW Corner 3245 02.67 N09152 39.81 W Log Cabin East SE Corner 32 49 40.36 N 09146 37.93 W SW Corner 32 49 40.36 N09147 55.85 W NW Corner 32 5117.37 N091 47 55.85 W NE Corner 32 5117.37 N091 46 37.93 W Oak Ridge NW NW Corner 32 39 18.00 N 0914845.00 W NE Corner 32 39 18.00 N09147 25.41 W SE Corner 32 37 30.35 N09147 25.41W SW Corner 32 37 30.35 N091 48 45.00W

{;:



### Bastrop, Log Cabin East and Oak Ridge NW Operations areas

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations /

36 

## ' )

\ / \ J 

## ) )


## ) ) J 

### ) 

## ) 

## ) 

## ) ) \ J 

## ) 

## ) ) ) )

\

,.) )

\ ) \ ) 

### ) \ / 

## )\)

\ / 

## ) ) 1 I 

## ) \ ) \ ;' 

# ' ) 

### ) 

### ) \ )

) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

## Google Earth Detail of Bastrop Agriculture Area BastropAirportTrainingAirspace NW Corner 3245 49.00 N 09152 57.00W NNE Corner 3245 49.00n 091 52 38.00W NE Lower 3245 37.00 N 09152 37.57 W ENE Corner 32 45 37.00 N 091 5114.78 W SE Corner 32 45 25.00 N 091 52 14.25W SW Corner 3245 02.67 N 091 52 39.81W

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 37FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

## Google Earth Detail of Log Cabin EastAgriculture area Log Cabin East SE Corner 

### 3249 40.36 N09146 37.93W SW Corner 

### 3249 40.36 N0914755.85W NWCorner 

### 32 5117.37 N0914755.85 W NE Corner 

### 32 5117.37 N09146 37.93W

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 38 

# '· I 

## ) \ / 

## ) ) 

## ) J / '\ )) 7 

### ) ) 

### ) 

## ) ) 

# ) ) 

## )

\ 

### .J 

## )
) 

### )

' ;

\ /)

'! /

# l 1 /

\ ) \ ) '\ J ', \ /

'I ) 

# ,, ) I J 

## )



# ,, ) 'j j ) 

### ) ) ' 1

)

### ' i / \ )\ )

) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption 

## Google Earth Detail ofOak Ridge NWAgriculture area

Oak Ridge NW NW Corner 32 39 18.00 N091 48 45.00 W NE Corner 32 39 18.00 N09147 25.41 W SE Corner 32 37 30.35 N09147 25.41 W SW Corner 32 37 30.35 N0914845.00 W

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 39FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption



### A. OPERATIONS AREA DESCRIPTION:

1. 

### Reno/Stead Airport- The Reno-Stead Airport has been designated by the FAA as a UAS test site range. As proposed, the initial outdoorflighttesting is to be performed in Class Gairspace within an FAA designated test area at Reno/Stead Airport. The testfacility area is 812acres 2.2 miles north ofthe main active runways 8/26. Runways 14/32does have the capabilityto be closed bythe airport authority duringflighttest operations. The airport authoritywill post an AWOS and aNOTAM notice broadcastingthe date and times of Unmanned Aircrafttesting and airoperations forthe Reno/Stead Airport. The Reno/Stead Airport is secured by perimeterfencing and therefore, restricts unauthorized activities ofpublic access and/or events. The test area is in aremote location 1.8 miles northeast ofahousing subdivision. 

### 2. Washoe County Emergency Operations Centerand Homeland Security Training facility-The regional Emergency Operations Center (EOC) is a 72 acre training facility that provides disastertraining for HAZMAT and environmental containment, and natural disaster remediation. The operation area is located 5 

### V2 miles northwestofthe Reno/Tahoe International Airport under Class C airspace. The Class Cairspace extends from 7,200' MSL to 8,400' MSL. Whereas, flight operations within the EOC facility will notexceed 5,550' MSL, it is contained within a small canyon. This facility is 

### V2 mile from a sparely populated area and does not pose a flight risk or noise nuisance to surrounding structures due to the speed and weight ofthe UA. 

### 3. Verdi Mountain Training Center- Is located in the Mount Rose Wilderness Area at an elevation of 7,500' MSL. This operation area is 5 square miles with no structures or population within 6 miles ofa population center. The purpose for this location provides UAS search and rescue training and implementation. 

### 4. Washoe County DesertTraining Center-This location is an isolated part of Northern Nevada in Washoe County. The operations area is 10 miles square and 10 miles from the nearest establishment. Operations will be conducted from Black Rock Airport (3,904' MSL), which is a private airstrip that has no structures in the middle ofthe Black Rock Playa. The purpose of location is to provide UAS emergency service training to law enforcement in the Northern Nevada and medical relief exercises. The operations area underlies the Reno Military Operation Area (MOA). The Reno MOA's floor is 13,000' MSL. Emergency operations training will notexceed 4,500' MSL and will be conducted in day light hours under VFR conditions. De-confliction ofthe airspace does not present a problem since the DAx8 power supply will be depleted prior to UA reaching altitudes of 13,000'; therefore this alleviates potential cause of hazardous situations. 

### 5. Washoe County Urban Training Center- Is an area thatwill demonstrate UAS capabilities in and around vacant structures. Emergency services will train with several environmental sensors to detect air quality, IR and heat imagery sensors to assess safe conditions prior to entering a structure. The area is sparely populated and does not pose a hazard to persons or air traffic. Operations are low level flight around the vacant structures for emergency training and urban assessment. 

### 9. AIRPORT OPERATIONS: Airport operations have been described in Section 8 underOperationsArea Reno/Stead Airport and Washoe County DesertTraining Center. The airports selected foroperations have been eitherdeemed as a UAS test site and Black Rock City Airport is a private field in which authorization has been sought and approved for UAS emergencytraining exercises. Black Rock City Airport isjust adirt strip runway and does not have any structures oraircraft parked on the ramp. All safety mitigations have been taken into consideration, including radio communications and lost link procedures. Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 40 

### ) 

## ' ; 

### ) 1 I

\ ) 

# ' } \ 

## ) ) 

## ) ) 

## ) ) ) I 

## ) 

# J ) ) ,/



## ) 

## .) ')



## ) )

. \

) '.. )

\ )

I / 

### )

' )

### ', ;



## ) )
'\ .)



### ) l )

)

' .J 

## ) \ _)

I /

)


### ) Flying TigerAviation, LLC Federal Aviation Regulations for Exemption 

### 10. VISUAL LINE OF SIGHT (VLOS): Observers will be placed within the operations area not more than 

### V2 NM from the operator at any given time. Each observer will be equipped with a two-way radio to communicate with the operator to maintain situational awareness and ensure persons and property is safe from flight hazards. In the event flights are extended over 1 12 nautical miles, additional observers will be place appropriately with two-way radio communications with the operator atall times to maintain flight safety within the operations area.


### 11. DAXS PREFLIGHT: i. The preflight process of Drone America's DAxS consists of: • Preflight check ofthe DAxS • Preflight check ofthe Portable Ground Control Station (GCS) All preflight processes for the UA and portable GCS, as well as all other flight critical equipment requires the use ofchecklists. The technicians are responsible for performing the preflight inspection of the UA, which will include checking ofall eight electric motors, the battery system, electrical systems and physical inspection of the airframe. The technicians will recharge the batteries and assure that backup batteries are available and ready for replacement. All defects and repairs are noted in the UA maintenance logbook and signed off by the certified technician. The technicians shall also perform weight and balance checks for the UA at empty weight and takeoff weight to ensure proper center ofgravity calculation for each UA payload configuration. Upon receiving the UA from the crew chief, the AVO will review the UA logbook and sign off to receive all maintenance items and the weight and balance, as well as reviewing the airframe, electric motors and autopilot total flight time. The AVO will then perform a final walk-around to visually inspect the UA, and remove any safety pins/flags from the UA in preparation for flight. The AVO shall also perform the preflight of the portable GCS using associated checklists to ensure the GCS is programmed for flight. This preflight process consists of procedural inspections ofthe ground data terminal (GDT), antennas and cabling and all electrical connectors. GCS preflight includes system power up of the Tough Pad screens, and verify payload control and communication panel. The AVO shall perform communication checks for all radio equipment, as well as, crew radio squawk checks. The AVO must cycle the speed controller throttle and respective autopilotflight controls to verify control accuracy and operations ofTough Pad systems.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 41FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### As part of the GCS preflight, the ground station software and the UA software are updated to the latestversion approved for flight operations. ii. System criteria require system preparation for flightthat includes software, electrical systems, control systems and electric motors. Each system is required to be checked and tested prior to every mission during the preflight operation. As part ofthe startup checklist, theAVO will verify thatthe GCS and autopilot software are updated tothe correct and approved version.

Preflight ofelectrical systems includes: • Aircraft batteries are fully charged
• Verify the onboard power management units (PMU) are powered up and regulated to the correct voltage- 14.8V
• Ensure power is on and connected tothe portable GCS main and USB transmitter

## Ireceiver
• Check backup batteries are charged/charging
• The inverters are turned on and have correct voltage output Control systems preflight includes: • AVO verifies flight autopilot and speed controls are operational
• Verification ofthrottle control is responsive
• The AVO will also perform an Inertial Navigation System (INS) check to verifythat pitch, yaw and roll gyros/accelerometers are oriented correctly
• Verify electric motors are functioning normally
• Verify electric motors are responsive in correlation with the portable GCS interface Preflight Safety Check/Walk-Around Inspection: Preflight Safety Checklist shall be performed by trained ground personnel to inspect the UAS priorto each flight utilizing the checklist referenced below.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 42 

### ; \ )

\ ) \ J 

### )

\ ) 

### ) \ ) 

### ) 

## ) 

## ) ) )
\ ) 

## )**.~** \ } 

## ")

) 

## ) ) )

\ /\)



### \ / \ ) 

## ) 

## )
) / 

## ' ) 

### )

\, / ) \ ) 

## ) 

## ) )

1 j

\ ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption



### iii. Walk-Around Inspection:

1. Inspect all 8 motorsfor security 

### 2. Inspect all 8 Propellers for cracks, chips and delamination's and screws forsecurity 3. Inspect all 8 motorarmsfor security 4. LED Navigation Light Inspection 5. Fuselage Inspection for abrasions, cracking or 6. Antenna Inspections: delamination's GPS, Transponder/Receiver 7. Lower hatch secure 8. Camera Inspection and Cleaning

DAxB Top View

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 43FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption**--~**

# .......

# ___ ;:i:_.

ILLUSTRATION2-DAXB SIDE VIEW 

### iv. PreflightChecklist: Electric Motor Preflight SafetyChecklist



## .. Flight Operation: 

# IPreflightTech:

1. Verifysystem is off 2. Verify motors are secure (Check bytwisting, pushing/pulling) 3. Verifyspeed controllers cables are connected tothe bus barfor all 8 motors 4. Inspect all wires for cuts or abrasions 5. Inspect propellersfor nicks or cracks 6. Inspect motors for smoothness ofoperation and cleanliness

ELECTRIC MOTOR PREFLIGHTSAFETYCHECKLIST

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations Date: Tech lnt./Stamp

44 

### )

I / 1 / 

## ) 

## ")

) ) \ 

## ) 

## ) ) ) 

## ) ) ) ) 

## )**~)** 

## ) 

## ) ) i ; \ j J.

\ J

\ '

### '!

) 

### ) \ J 

### ) 

## ) \ ) 

### ) 

## ) ) 

# ' l J ) 

## ) 

## ) 

## ) )**:~** ./ 

## ) 

## ) \ ) 

### )

\ j \ ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption
BatterySystem Preflight Checklist: 

## ;(··

..... 

### .· .. •.......... >• 

# .. .. :::

# . Battery System**PreflightChec~list**

### ·. ·.· ··.··· ·· .. 

# ... . .•.... 

### c•<i•
... Flight Operation: 

# I Date: Aircraft S/N: Tech lnt./Stamp 1. Verify proper batteries are installed (USE ONLY MANUFACTURER RECOMMENDED BATIERIES} 2. Verify batteries are secure 3. Verify batteries are charged 

### 4. Verify backup batteries are charged and on standby BATTERYPREFLIGHTCHECKLIST Avionics Preflight Checklist: 

### Avionics Safety Checklist Flight Operation: 

# I Date: Aircraft5/N: Tech lnt./Stamp 1. Inspect avionics compartmentfor debris 

### 2. Inspect bus harness connections 3. Verify avionics are secure and properly mounted 4. Verify analog connectors are connected and inspectfor damage 

### 5. Verify power cable is connected and inspectfor damage 6. Inspect GPS antenna and verify connection
A VIONJCS SAFETYCHECKLIST

Flying TigerAviation, LLC 2015 Section 333 Exemption for UAS Operations 45FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption Airframe Preflight Checklist:**l?{~J(/** 

# \

.**~·** < ·/·) )< 

### Airframe Preflight

## Chec~lis{. ;

# ~- .F**;··~:····.:·.** 

### _}'- ; 

## .. ·.: ·.c._· ··••• 

### .. .. ; 

# ... .·. ;· Aircraft S/N: Tech N-Number: Date: Jnt./Stamp 1. Verifyfuselage serial number 

### 2. Turn powerON 3. Inspectfuselage for defects 

### 4. Inspect navigation lights 6. Inspecttransponder/transponderantenna and verify connection (if installed) 7. Inspectsensor/payload for damage 8. Remove camera cover and clean lenses AIRFRAME PREFLIGHTCHECKLIST 

## v. Center ofGravity Preflight Checklist: Due to the configuration ofthe DAx8, CG is fixed within a small range in the center of its circular perimeter. Weight is the only driving factor in stability. The DAx8 is designed to fly at a max weight notto exceed 85% of its maximum thrust. The thrust outputfor the DAx8 is expected to be a maximum of 13.5kg, or 29.751bs at sea level. This yields a maximum possible takeoffweight of roughly 25 lbs. Depending upon the location and base elevation this weight will decrease. 

### It is up tothe AVO to calculate the approximate density altitude and determine the maximum takeoffweight for a given situation based upon weather and location. These statistics are subject to change during testing, and upon completion offlighttrials, a detailed weight table will be presented as a guideline for safe operations. 

### Weightand Balance Sheet Aircraft S/N: 

# I N-Number: 

# I Model#: 

# IDate: Prepared by: Max Empty weight: weight: COMPONENTS: WEIGHT/LBS. Payload Aux. Payloads USEFUL LOAD REMAINING WEIGHTAND BALANCESHEET
Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 46 

### ) '1 J 

### ) 

## ) )

\ ) 

## ) 

## ) ) ) 

## ) 

## ) 

## ) 

# )**~)** •) '.J



### ) )

I / \ ) \ .J\ ; 

### .'I

J \j 

# ' ) 

## ' )

/ \

./ 

## ) )



## )
)

·,I /

\ /

### ) FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption


### 12. PURPOSE FOR UAS EXEMPTION: The purpose for exemption is to enhance the situational awareness capabilities of emergency service agencies and first responders by employing unmanned aircraft systems (UAS), with high-resolution sensing and imaging capabilities for disaster remediation. Emergency service agencies and first responders face significant challenges during an emergency event such as, a natural or anthropogenic disaster (earthquake, tsunami, fire, hurricane, tornado, floods, power or nuclear accident, act ofwar, orterror). One ofthe majorchallenges is acting decisively based on available information with consideration of human factors. In addition to, providing high-quality real-time situational awareness that is critical to effectively manage and safeguard civilians and field personnel. This project focuses on creating a smart emergency-response service system utilizing UA and ground-based systems. These systems are equipped with state ofthe art imaging, sensing and communications to provide first responders with high-quality, real time information to act decisively and effectivelyvia human machine interactions. 

### Theobjectives include: (1) Develop and integrate UAS platforms, sensors, imaging, communication systems and control and path planning algorithms to create a UAS based smart service system for first response. (2) Model the state of human and structural infrastructure during and/or post a disaster that identifies the scene, and creates mapping access paths to safety. (3) Test prototypes and pursue commercialization opportunities. (4) Educate the public and train first responders on the technology. 

### 13. 

### CERTIFICATE OF AUTHORIZATION - COA: A certificate ofAuthorization is currently pending approval through the Reno Regional Emergency Operations Center. The COA identifies Platform, Performance and Procedures, in which are identified within this request for relief ofexemption.

Flying Tiger Aviation, LLC 2015 Section 333 Exemption for UAS Operations 47FlyingTigerAviation, LLC Federal Aviation Regulations for Exemption



# INTENTIALLYLEFT BLANK

Drone America, Inc. 2015 Section 333 Exemption for UAS Operations 48 ;



## ) 

## )**~)**



## )



## <)

)

\ /