## DroneslOllnternational LLC

US Department of Transportation Exemption Request Pursuant to Section 333 ofthe FAA Reform Act and Part 11 ofthe Federal Aviation November 18, 2015 Orones 1011nternationaf LLC 1163 Andalusia Loop Davenport, Florida 33837 ATTN : Gerard F alcone U .S. Department ofTransportation Docket Management System 1200 NewJersey Ave ., SE Washington DC 20590 Re : Exemption Request Pursuant to Section 333 ofthe FAA Reform Act and Part 11 ofthe Federal Aviation Regulations from: 14 CFR 21 subpart H; 14 CFR 45 .23(b); 14 CFR 61.113(a) and (b); 14 CFR 91.7(a); 14 CFR91.9 (b)(2); 14 CFR91 .103; 14 CFR 91.109; 14 CFR 91.119(c); 14 CFR 91 .1 21; 14 CFR 91.151(a); 14 CFR 91.203(a) and (b); 14 CFR 91 .405 (a); 14 CFR 91.407 (a) (1) 14 CFR 91.409 (a) {1) and (2); 14 CFR 91.417{a) and (b) Dear Sir or Madam: Pursuant to Section 333 ofthe FAA Modernization and Reform Act of 2012 (the " Reform Act" ) and 14 CFR Part 11 , Drones1011nternational LLC operator of Unmanned Aircraft Systems (UAS), hereby applies for an exemption from the listed Federal Aviation Regulations (" FARs" ) to allow commercial operation of designated UAS, provided such operations are conducted within and under the conditions outlined herein or as may be established by the FAA as required by Section 333. Thank you in advance for your consideration.

### Commercial operation of an UAS, as described herein, which are equipped with camera(s) and sensors, would provide professional services in the following areas: 

### 1. Aerial photography and/orvideo for public and/or private use including real estate, architecture, land surveying, engineering and other related professional activities. 2. Aerial video and/or photography for public and/or private use including television, public events, cinematography and newsgathering. 3. Aerial inspection/photography of residential/commercial structures under contract with the owners or local government authority. 4. Aerial inspection/photography of residential/commercial utility infrastructure including but not limited to electrical power lines, wind turbines and cell towers. 5. Aerial video/photography or providing live video feed to assist with search and rescue operations in cases of an emergency or natural disaster only when the local authorities or government has requested it by contract or donation . 6. Training to persons individually or belonging to both private and/or public organizations to increase awareness and improve safety for current and future UAS operations within the NAS. As described fully below, the requested exemption would permit the operation of designated UAS as set forth in this document under controlled conditions in the NAS that would be a) limited b) controlled c) predetermined and d) safe. Approval ofthis exemption would increase public awareness of UAS operations and enhance safety to aid in fulfilling the Secretary of Transportation's (the FAA Administrator's) responsibilities to " ....establish requirements for the safe operation ofsuch aircraft systems in the national airspace system." The name and address ofthe applicant is:Orones1011nternational LLC Ph : (732) 814.0728 Email : Drones101international@gmail .com Address: 1163 Andalusia Loop Davenport, Florida 33837 ATIN : Gerard Falcone Regulations from which the exemption is requested: 14 CFR Part 21 subpart H 14 CFR 45.23 (b) 14 CFR 61.113 (a) 

### & (b) 14 CFR 91.7 (a) 14 CFR 91.9 (b) (2) 14 CFR 91.103 14 CFR 91.109 14 CFR 91.119 (c) 14 CFR 91 . 121 14 CFR 91.151 (a) 14 CFR 91.203 (a) 

### & (b) 14 CFR 91.405 (a) 14 CFR 91.407 (a) {1) 14 CFR 91.409 (a) (2) 14 CFR 91.417 (a) 

### & (b) Drones1011nternational LLC will operate one or more of the 

### Following model UAS: DJI Phantom 3 Yuneec Typhoon 500 

### +

### DJI Phantom 3: 

### Ai rcraft Weight (including battery and propellers)-1280 g Diagonal size (including propellers)-590 mm Max Ascent Speed-S m/s Max Descent Speed-3 m/s Hover Accuracy-

•Vertical:+/- 0.1 m (when Vision Positioning is active) or+/ - 0.5 m

• Horizontal : +/- 1 .5 m Max Speed-16 m/s (ATil mode, no wind) Max Altitude Above Sea Level -6000 m Operating Temperature-o· c to 40"C GPS Mode-GPS / GLONASS 

### Camera Sensor-Sony EXMOR 1/2.3" Effective pixels: 12.4 M (total pixels: 12.76 M) Lens-FOV 94" 20 mm (35 mm format equivalent) f/2.8, focus at oo ISO Range-100-3200 (video) 100-1600 (photo) Shutter Speed-8s -1/8000s Image Max Size-4000 x 3000 Still Photography Modes *Single Shot *Burs t Shooting: 3/5/7 shots *Auto Exposure Bracketi ng (AEB) : 3/5

* Bracketed Frames at 0.7EV Bias *Time-lapse

### Video Recording Modes Phantom 3 Professional

• UHO: 4096x2160p 24/25, 3840x2160p 24/25/30

• FHO: 1920x1080p 24/25/30/48/50/60

• HO: 1280x720p 24/25/30/48/50/60 Phantom 3 Advanced

• FHO: 1920x1080p 24/25/30/48/50/60

• HO: 1280x720p 24/25/30/48/50/60 Supported SO Card Types- * Micro SO *Max capacity: 64GB. Class 10 or UHS-1 rating required Max Bitrate of Video Storage- 

## **Phantom 3 Professional

60 Mbps **Phantom 3 Advanced

40 Mbps Supported File Formats-

• FAT32/exFAT

• Photo: JPEG, ONG

• Video: MP4, MOV (MPEG-4 AVC/H.264) Operating Temperature-0°C to 40°C

## Gimbal Controllable Range-Pitch -90° to +30° Stabi lization -3-axis (pitch, roll, yaw) 

## Vision Positioning Max Velocity-Less than 8 m/s (when 2 m above ground) Altitude Range-30 cm -300 em Operating Range-30 cm -300 em Operati ng Environment-Surface with clear pattern and adequate lighting (Lux> 15) 

## Remote Controller Operating F requency-2.400 GHz-2.483 GHz Max Distance-2000m (outdoors and unobstructed) Video Output Port-USB Operating Temperature-0°C - 40°C Battery-6000 mAh LiPo 25 Mobile Device Holder-For tablet or phone Receiver Sensitivity (1 %PER)--101 dBm ±2 dBm Transmitter Power (EIRP) *FCC: 20 dBm *CE: 16 dBm Working Voltage-1.2 A @7.4 V

### Battery ChargerVoltage-17.4 V Rated Power: Phantom 3 Professional

• 100W Phantom 3 Advanced

• 57W



### Intelligent Flight Battery Capacity-4480 mAh Voltage-15.2 V Battery Type-LiPo 4S Energy-68 Wh Net Weight-365 g Max Flight Time-Approximately 23 minutes Operating Temperature--10°( to 40°( Max Charging Power-100 W

### Yuneec 500 

## + Flight Time Weight with Battery and Payload Weight without Battery and Payload Battery Charger Transmitter 3 Flight Modes Maxi mum Flying Height Maximum Rotation Rate Maximum Roll Angle Operating Temperature Range Radio Control Frequency Band up to 25 minutes 60.0 oz (1700g)

40.0 oz (1130g) 5400mAh 35 

### ll.lV LiPo (included) 35 

### ll.lV LiPo DC Balancing Smart Charger with AC Adapter (included) 10-channel 2.4GHz with 5.8GHz video downlink (included) Smart (Follow Me and Watch Me), Angle and Home Default 122m (400ft) above Ground Level (Adjustable via the Typhoon GUI) 65./s 35°

2.4GHzMax. Descent Speed 2m/s Max. Flight Speed 8m/s

Battery Charger Transmitter 3 Fl ight Modes Maximum Flying Height Maximum Rotation Rate M aximum Roll Angle Operating Temperature Range Rad io Control Frequency Band 5400mAh 3S 

### ll.lV liPo (included)

3S 11.1 V LiPo DC Balancing S mart Charger w ith AC Adapter (included) 10-channei2.4GHz with 5.8GHz video downlink (included) Smart (Follow Me and Watch Me), Angle and Home

Default 122m (400ft) above Ground Level (Adjustable via the Typhoon GUI)

2.4GHzMax. Descent Speed Max. Flight Speed

Gimbal Camera Type Weight Focusing Sys tem Field of View 2m/s

8m/s

Video Transmission Range

Video Resolution

Photo Resolution Storage (memory) Control Angle Accuracy CG03 6.9oz (19Sg) Aerial Optimized Fixed Focus

FCC Com pliance: Up to 600m (1968.5 ft) CE Compliance: Up to 300m (984.252 ft) with STlO UHD: 4K at 30FPS, 2 .7K at 30FPS, 2.5K at 30FPS - FULL HD: 1080p at 24/25/30/ 48/S0/60/120 FPS 12 Megapixels microSD Class 10- 4 to 128 GBWhite Balance Transmission Band Input/Operating Voltage Working Temperature Storage Temperature Angular Vibration Range Control Range Microphone Camera lens Sensor

Type Automatic or manual settings 5.2GHz-5.8GHz 12V

-20°C-60°C

±0.02° Pitch: between -90° and 

# oo Yaw: between 

# oo and 360° Yes 0.6in (14mm)/f2.8 (1.4in/35mm)-No distortion 1/2.3" CMOS



### ST10+Operating System Number of Channels Cont rol Transmission Range (Optimum Conditions) Robust Rad io Control Modulation Video Link Frequency Band Video Transmission Range (Optimum Conditions) Flight SystemsTelemetry Data On Screen Display LED Backlit LCD Screen Tactile (Vibrating) and Audible Feedback Built-in liPo Battery Voltage 

## I Capacity Screen Resolution Camera Settings AndroidTM 1 0 FCC Compliance: Up to BOOm (2624.67 

### ft) CE Compliance : Up to 400m {1312.34 

### ft) Warning : Y o u Must Follow Local Laws and Maintain Visual Line ofSight of Aircraft at All Times Yuneec Protocol 5.8GHz FCC Com pliance: Up to 600m (1 968.5 

### ft) CE Compliance : Up to 300m {984.252 ft) Warni ng : You Must Follow Local Laws and Mai ntain Visua l Line ofSight of Ai rcraft at All Times Yes Capacitive M ulti-touch 5.5" Yes

3.6V/5200mAh 18.72Wh 854 x 480px White balance, light exposure, ISO, shutter speed, video resolution, FPS, record video, take pictu resGiven the small size ofthe UAS in scope and the controlled environment provided, the proposed operations will adhere to the Reform Act's safety requirements. The approval ofthis application presents no national security issues. Regarding the level of safety surrounding the proposed operations and the public benefit, reduction in environmental impacts, including but not limited to reduced emissions and noise, the grant ofthe requested exemption is in the public interest. Accordingly, the applicant graciously requests that the FAA grant the requested exemption. AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY The operation limitations proposed for an equivalent or higher level of safety because operations will further enhance the safety ofthe persons and/or property using conventional aircraft. These limitations and conditions to which the applicant agrees to adhere to when conducting commercial operations under the FAA issued exemption as set forth in the Flight Operations Manual (FOM) include: 

### 1. The UAS will weigh significantly less than 55 lbs. Itweighs less than 4 pounds with battery and camera. 2. The UAS, depending on the model in operation, will have a maximum operating speed of no more than 50mph. 3. Flights will be operated within line of sight ofthe Pilot in Command (PIC) and/or Visual Observer (VO) . 4. Maximum flight time for each operational flight will be depending on the UAS model in operation, but will not exceed 30 minutes. Flights will be terminated at 25% battery power reserve or 30 minutes offlight time whichever occurs first. 5. Flights will be operated at an altitude of no morethan 400 feet Above Ground Level (AGL) and not more than 200 feet above an elevated platform from which filming is planned.6. Minimum crew for each operation will consist ofthe UAS Pilot and at least one Visual Observer (VO), and may include a third, but separate, Camera Operator (CO) . 7. The UAS pilot will be a designated Pilot in Command (PIC}. The PIC will have logged a minimum of 20 hours on the designated UAS. 8. A safety briefing will be performed prior to each day's flights consisting of all the days' production activities. 9. All flight activities will be logged . 10. All flights will occur under Visual Flight Rules Meteorological Conditions (VMC} only. 11 . The fl ights will occur in Class G airspace no closer than a Smile radius ofthe geographic center/Airport Reference Point (ARP) of a tower controlled or uncontrolled airport. 12. Flights will not be closer than a 5 mile radius ofthe geographic center/Airport. 13. The operator will file FAA Form 77111, or its equ ivalent, as modified in light ofthe requested exemption, with the appropriate local Flight Standards District Office (FSDO) no more than 72 hours but no less than 48 hours from planned operation. 14. The operator will obtain verbal/written consent of all persons involved with the planned operation and ensure that only consenting persons will be allowed within 100 feet ofthe flight operation, and the radius may be reduced to 30 feet based upon an equivalent level of safety determination, as U.S. Department ofTransportation required under the FOM. With the advanced perm ission ofthe FSDO, operations at closer range may be approved. 15. The PIC and VO will have been trained in operation of UAS and receive up to date information for the particular UAS to be operated. 16. The PIC and VO will be able to communicate by voice and/or radio at all times. 17. Written and/orverbal permission and permits will be obtained from territorial, state, county or cityjurisdictions, including law enforcement, fire or other appropriate governmental agencies as appropriate to flight operations.18. Ifthe UAS loses communications with the remote controller or loses GPS signal, the UAS will have the capability to return to a predetermined location within a designated location and land autonomously. 19. The UAS will have the capability to abort a flight in case of emergencies with an automated "Return Home and Land" function. 20. The UAS will have the capability to abort a flight in case of unpredicted obstacles, weather, or emergencies such as low battery. 14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. §91.203 (a) (1) Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements for the issuance of airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and limited operating area associated with the aircraft to be utilized bythe Applicant, an exemption from Part 21 Subpart H meets the requirements of an equivalent level of safety under Part 11 and Section 333 ofthe Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333 ofthe Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration ofthe size, weight, speed, operational capability, and proximity to airports and populated areas ofthe particular UAS. In all cases, an analysis ofthese criteria demonstrates that the UAS operated without an airworthiness certificate in the restricted environment and under the conditions proposed will be at least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate without the restrictions and conditions proposed. The UAS to be operated hereunder is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, carries no explosive materials orflammable liquid fuels, and operates exclusively within a secured and designated area. Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by both the operator and under the requirements and in compliance with local publ ic safety requirements. These safety enhancements provide a greater degree of safety to the public and property owners than conventional operations conducted with airworthinesscertificates issued under 14 C.F.R. Part 21, Subpart H. Lastly, application ofthese same criteria demonstrates that there is no credible threat to national security posed by the UAS, due to its size, speed of operation, location of operation, lack of explosive materials or flammable liquid fuels, and inability to carry a substantial external load. 14 C.F.R. § 45.23 (b). Marking ofthe Aircraft The regulation requires: 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 14 C.F.R. § 45.23 (b). Marking ofthe Aircraft The regulation requires: 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. Even though the UAS will have no airworthiness certificate, an exemption may be needed as the UAS will have no entrance to the cabin, cockpit or pilot station on which the word "Experimental" can be placed. Given the size ofthe UAS, two inch lettering will be impossible. The word "Experimental" will be placed on the fuselage in compliance with §45.29 

### (f). US Department ofTransportation February 20, 2015 The equivalent level of safety will be provided by having the UAS marked on its fuselage as required by §45.29 

### (f) where the pilot, observer and others working with the UAS will see the identification ofthe UAS as "Experimental." 14 C.F.R. § 61.113 (a) and (b): Private Pilot Privileges and Limitations: Pilot in Command. Pursuant to 14 CFR 61.113 (a) 

### &(b), no person who holds a private pilot certificate may act as a pilot in command ofan aircraft that is carrying passengers or property for compensation or hire. The proposed UAS operations may achieve an equivalent level of safety as achieved by current Regulations because the applicant's UAS do not carry any pilots or passengers nor property. The risks attendant to the operation of UAS is far less than the risk levels inherent in the commercial activities outlined in 14 CFR 61. The PIC ofthe UAS will 

### be, or be underthe direct supervision 

### of, a FAA Certificated Private Pilot with current Third Class or higher medical certificate . It is believed that the operation and limitations set forth in the FOM will equate to the safe operation ofthe UAS. 14 C.F.R. §91.7(a): Civil Aircraft Airworthiness . The regulation requires that no person may operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for the aircraft, should this exemption be granted, no FAA regulatory standard will exist for determining airworthiness. Given the size ofthe aircraft for maintenance and use of safety checklists prior to each flight, an equivalent level of safety will be provided. 14 C.F.R. § 91 .9 (b) (2): Civil Aircraft Flight Manual inthe Aircraft. Section 91.9 (b) (2) provides: No person may operate a U.S. registered civil aircraft . . . (2) For which an Airplane or Rotorcraft Flight Manual is not required by §21.5 ofthis chapter, unless there is available in the aircraft a current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or any combination thereof. The UAS, given its size and configuration has no ability or place to carry such a flight manual on the aircraft, not only because there is no pilot on board, but because there is no room or capacity to carry such an item on the aircraft. The equivalent level of safety will be maintained by keeping the flight manual at the ground control point where the pilot flying the UAS will have immediate access to it. 14 C.F.R. § 91.103: Preflight Action. This regulation requires each pilot in command to take certain actions before flight to insure the safety offlight. As FAA approved rotorcraft flightmanuals will not be provided for the aircraft an exemption will be needed. The PIC will take all actions as stated in the FOM in Section 4 under Normal Procedures including but not limited to reviewing weather, flight battery requirements, landing and takeoff distances and aircraft performance data before initiation offlight 14C.F.R. §91.109: Flight Instruction. Section 91.103 provides that no person may operate a civil aircraft (except a manned free balloon) that is being used for flight instructions unless that aircraft has fully functioning dual controls. UAS and remotely piloted aircraft, by their design do not have fully functional dual controls. Flight control is accomplished through the use of a control box that communicates with the aircraft via radio communications. The FAA has approved exemptions for flight training without fully functional dual controls for a number ofaircraft and for flight instruction in experimental aircraft. The equivalent level ofsafety is provided by the fact that neither a pilot nor passengers will be carried in the aircraft and by the size and speed ofthe aircraft. 14 C.F.R. §91.119: Minimum Safe Altitudes. Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119 (d) allows helicopters to be operated at less than the minimums prescribed, provided the person operating the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. As this exemption is for a UAS that is a helicopter and the exemption requests authority to operate at altitudes up to 400 AGL, or not more than 200 above an elevated platform from which filming is planned, an exemption may be needed to allow such operations. As set forth herein, the UAS will never operate at higher than 400 AGL with the exception that in circumstances where the UAS is used to survey or photograph a structure whose height exceeds 400 feet AGL, the UAS will not be operated more than 200 feet above the highest point on the structure. It will however be operated in a restricted area with security perimeter, where buildings and people will not be exposed tooperations without their pre obtained consent. The equivalent level of safety will be achieved given the size, weight, and speed ofthe UAS as well as the location where it is operated. No flight will be taken without the permission ofthe property owner or local officials. Because ofthe advance notice to the property owner and participants in the filming activity, all affected individuals will be aware ofthe planned flight operations. Compared to flight operations with aircraft or rotorcraft weighting far more than the maximum SSibs. proposed herein and the lack of flammable fuel, any risk associated with these operations is far less than those presently presented with conventional aircraft operating at or below 500 AGL. In addition, the low altitude operations ofthe UAS will ensure separation between these UAS operations and the operations ofconventional aircraft that must comply with Section 91.119. 14 C.F.R. §91.121 Altimeter Settings. This regulation requires each person operating an aircraft to maintain cruising altitude by reference to an altimeterthat is set 11

...to the elevation ofthe departure airport or an appropriate altimeter setting available before departure." As the UAS may not have a barometric altimeter, but instead a GPS altitude read out, an U.S. exemption may be needed. An equivalent level of safety will be achieved by the operator, pursuant to the safety check list and live flight data monitoring, confirming the altitude ofthe launch site shown on the GPS altitude indicator before flight. 14 C.F.R. § 91.151(a): Fuel Requirements for Flight in VFR Conditions Section 91.151 (a) prohibits an individual from beginning 

### (Ia flight in an airplane under VFR conditions unless (considering wind and forecast weather conditions) there is enough fuel to fly to the first point of intended landing, and, assuming normal cruising speed- (1) During the day, to fly after that for at least 30 minutes; or (2) At night, to fly after that for at least 45 minutes." The applicant believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. Operating the UAS in a tightly controlled area where only people and property owners or official representatives who have signed waivers will be allowed does not engender the type of risks that Section 91.151(a) was intended to alleviate given the size and speed ofthe small UAS. The applicant believes that an equivalent level of safety can be achieved by limiting flights to 30 minutes or 25% of battery power - whichever happens first. This restriction would be more than adequate to return the UAS to its planned landing zone from anywhere inits limited operating area. 14 C.F.R. §91.203 (a) and (b): Carrying Civil Aircraft Certification and Registration The regulation provides in pertinent part: (a) Except as provided in 

### § 91.715, no person may operate a civil aircraft unless it has within itthe following: (1) An appropriate and current airworthiness certificate.... (b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) ofthis section or a special flight authorization issued under §91.715 is displayed atthe cabin or cockpit entrance so that it is legible to passengers or crew. The UAS fully loaded weighs well under the proposed 5Sib limit and is operated without an onboard pilot. As such, there is no ability or place to carry certification and registration documents or to display them on the UAS. An equivalent level of safety will be achieved by keeping these documents at the ground control point where the pilot flying the UAS will have immediate access to them, to the extent they are applicable to the UAS. 14 C.F.R. §91.405 (a); 407 (a) (1); 409 (a) (2); 417(a) 

### & (b): Maintenance Inspections. These regulations require that an aircraft operator or owner "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...," and others shall inspect or maintain the aircraft in compliance with Part 43. Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to the applicant. Maintenance will be accomplished by the operator pursuant to the flight manual and operating handbook. An equivalent level of safety will be achieved because the UAS is very limited in size and will carry a small payload and operate only in restricted areas for a limited period oftime. If mechanical issues arise the UAS can land immediately and will be operating from no higher than 400 feet AGL. The operator will ensure that the UAS is in working order prior to initiating flight, perform required

### maintenance, and keep a log of any maintenance performed. Moreover, the operator is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivalent level of safety. An equivalent level of safety will be achieved because maintenance and inspections will be performed in accordance with the UAS Manufacturer's User Manual. As provided in the FOM, the operator will ensure that the UAS is in working order prior to initiating flight and perform required maintenance needed. Additional Information. The applicant, Drones1011nternational LLC, 

### believes this exemption request and associated safety considerations adequately satisfy criteria provided in Section 333 ofthe Reform Act of 2012, providing sufficient justification for the granting of commercial operations ofthe applicant's UAS. The applicant, Drones1011nternational LLC 

### respects your respective approval ofthis Section 333 exemption petition request. Thank you for your attention in this matter. Please contact Drones1011nternational LLC 

### ofyour actions, and or approvals. Thank You for your i nterest in this request. Sincerely,



# '};;)_~;fit~~..L Li-Z

,....- Drones1011nternational LLC 

### 1163 Andalusia Loop Davenport, Florida 33837 ATIN: Gerard Falcone