Imagination Films, LLC Xavier Salinas 520 S Burnside Ave. Apt 9M (817) 939

- 8441 Xavier@imaginationinuse.com
July 1, 2015
U.S. Department of Transportation, Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590
RE: Petition of Imagination Films, LLC for Exemption Pursuant to Section 333 of the FAA Reform Act

Dear Sir or Madam:
Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform Act) and 14 C .F.R. P art 11, Imagination Films , LLC, operator of Small Unmanned Aircraft Systems (“sUASs”) equipped to conduct aerial photography and videography, hereby applies for an exemption from the listed Federal Aviation Regulations (“FARs”) to allow commercial operatio n of its sUASs, so long as such operations are conducted within and under the conditions outlined herein or as may be established by the FAA as required by Section 333.1
As described more fully below, the requested exemption would permit the operation of small, unmanned and relatively inexpensive sUAS under controlled conditions in airspace that is 1) limited 2) predetermined and 3) controlled. The proposed exemption, if grante d, would allow Imagination Films , LLC to conduct commercial operations of small unmanned aircraft systems (“UAS”) meeting or exceeding all of the operational and safety requirements Congress has set forth in Section 333.
Imagination Films , LLC is a production company owned and run by Xavier Salinas. Mr. Salinas has been active in Rad io Co ntrolled Aircraft for the past 5 years with experience rotary wing aircraft. Imagination Films , LLC plans to exploit the capabilities of Unmanned Aerial Systems to offer a multitude of services, including:

- Motion Picture Film Production/ Aerial F il mmaking and P hotography

- Aerial S urveying

- Event Photography/Videography

- Agriculture purposes

- Real Estate Photography /Videography

- Construction site inspections and monitoring
Statutory Authority Section 333, titled “Special Rules for Certain Unmanned Aircraft Systems”, provides a mechanism for seeking expedited FAA authorization of safe civil UAS operations in the NAS. Section 333(a) states that the FAA “shall determine if cert ain unmanned aircraft systems may operate safely in the national airspace system before completion of the (comprehensive) plan and rulemaking required by section 332(b)(1) of this Act or the guidance required by section 334 of this Act.” In Section 332(b)( 1), Congress made it clear that Section 333 provides a mechanism for “expedited operation authorization” if several factors are met. Petitioner meets all requirements to permit FAA approval of commercial UAS operations.The Petitioner Req uests Relief From the following r egulations from which the exemption is requested:

14 C.F.R. Part 21 14 C.F.R. 45.23 (b) 14 C.F.R. 61.113 (a) and (b) 14 C.F.R. 91.7 (a) 14 C.F.R. 91.9 (b) (2) 14 C.F.R. 91.109 14 C.F.R. 91.119 14 C.F.R. 91.121 14 C.F.R. 91.151 (a) 14 C.F. R. 91.203 (a) & (b) 14 C.F.R. 91.205 (b) 14 C.F.R. 91.215 14 C.F.R. (91.401

– 91. 417)

Unmanned Aircraft System sUASs are oftentimes seen as superior to helicopters due to the smaller devices , cheaper equipment, personnel cost, reduced noise and as such, a much smaller environmental impact which promotes public safety.
We are petitioning for exemption to enable Imagination Films , LLC to operate a DJI Inspire 1 upgraded to the latest firmware and equipped with a three

- axis camera gimbal and using a 4K came ra. This sUAS has a built

- in capability to limit the height it flies above the ground, to limit the radius of the distance it flies from the operator. The Inspire 1 also has the failsafe function of the autopilot system , which means when the communication between the Main Controller and the transmitter is disconnected, the outputs of all command sticks from controller will go to the center position. If the GPS signal is good enough, the system will automatically trigger Return to Home and will land safely.

Please refer to the link to the DJI Inspire 1 Instruction Manual for the performance limitations and flight operations.
http://download.dji

- innovations.com/downloads/inspire_1/en/Inspire_1_User_Manual_v1.2_en.pdf

Please find all the appropriate specifications for the DJI Inspire 1 on the next page.7/1/15, 11:31 AM Inspire 1 - Specs | DJI

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Aircraft

Gimbal Model Model T600

Weight (Battery Included) Weight (Battery Included) 2935 g

Hovering Accuracy (GPS Mode) Hovering Accuracy (GPS Mode) Vertical: 0.5 m Horizontal: 2.5 m

Max Angular Velocity Max Angular Velocity Pitch: 300°/s Yaw: 150°/s

Max Tilt Angle 35°

Max Ascent Max Ascent Speed 5 m/s

Max Descent Speed 4 m/s

Max Speed 22 m/s (ATTI mode, no wind)

Max Flight Altitude 4500 m

Max Wind Speed Resistance 10 m/s

Max Flight Time Approximately 18 minutes

Motor Model Motor Model DJI 3510

Propeller Model Propeller Model DJI 1345

Indoor Hovering Indoor Hovering Enabled by default

Operating Temperature Range -10° to 40° C

Diagonal Distance 559 to 581 mm

Dimensions Dimensions 438x451x301 mm

Model Model ZENMUSE X3 Search dji.com... #7/1/15, 11:31 AM Inspire 1 - Specs | DJI

Page 2 of 5 http://www.dji.com/product/inspire-1/spec Camera Output Power (With Camera) Output Power (With Camera) Static: 9 W In Motion: 11 W

Operating Current Operating Current Station: 750 mA Motion: 900 mA

Angular Vibration Range ±0.03°

Mounting Mounting Detachable

Controllable Range Pitch: -90° to +30° Pan: ±320°

Mechanical Range Pitch: -125° to +45° Pan: ±330°

Max Controllable Speed Pitch: 120°/s Pan: 180°/s

Name X3

Model Model FC350

Total Pixels Total Pixels 12.76M

E ff ective Pixels

ective Pixels 12.4M

Image Max Size 4000x3000

ISO Range 100-3200 (video) 100-1600 (photo)

Electronic Shutter Speed 8s

 1/8000s

FOV (Field Of View) FOV (Field Of View) 94°

CMOS CMOS Sony EXMOR 1/2.3”

Lens Lens 20mm (35mm format equivalent)f/2.8 focus at ∞ 9 Elements in 9 groups Anti-distortion

Still Photography Modes Still Photography Modes Single shoot Burst shooting: 3/5/7 frames Auto Exposure Bracketing (AEB): 3/5 bracketed frames at 0.7EV Bias Time-lapse

Video Recording Modes Video Recording Modes UHD (4K): 4096x2160p24/25, 3840x2160p24/25/30 FHD: 1920x1080p24/25/30/48/50/60 HD: 1280x720p24/25/30/48/50/60

Max Bitrate Of Video Storage 60 Mbps

Supported File Formats Supported File Formats FAT32/exFAT Photo: JPEG, DNG Video: MP4/MOV (MPEG-4 AVC/H.264)

Supported SD Card Types Supported SD Card Types Micro SD Max capacity: 64 GB. Class 10 or UHS-1 rating required.

Operating Temperature Range 0° to 40° C7/1/15, 11:31 AM Inspire 1 - Specs | DJI

Page 3 of 5 http://www.dji.com/product/inspire-1/spec Remote Controller

Charger

Battery (Standard) Name C1

Operating Frequency Operating Frequency 922.7~927.7 MHz (Japan Only) 5.725~5.825 GHz 2.400~2.483 GHz

Transmitting Distance (Outdoor And Unobstructed) Transmitting Distance (Outdoor And Unobstructed) 2 km

EIRP 10dBm@900m, 13dBm@5.8G, 20dBm@2.4G

Video Output Port Video Output Port USB, mini-HDMI

Power Supply Power Supply Built-in battery

Charging Charging DJI charger

Dual User Capability Dual User Capability Host-and-Slave connection

Mobile Device Holder Mobile Device Holder Tablet or Phone

Max Mobile Device Width 170mm

Output Power Output Power 9 W

Operating Temperature Range -10° to 40° C

Storage Temperature Range Less than 3 months: -20° to 45° C More than 3 months: 22° to 28° C

Charging Temperature Range 0-40° C

Battery Battery 6000 mAh LiPo 2S

Model Model A14-100P1A

Voltage 26.3 V

Rated Power Rated Power 100 W

Name Intelligent Flight Battery

Model Model TB47

Capacity Capacity 4500 mAh

Voltage 22.2 V

Battery Type LiPo 6S High voltage battery

Energy Energy 99.9 Wh7/1/15, 11:31 AM Inspire 1 - Specs | DJI

Page 4 of 5 http://www.dji.com/product/inspire-1/spec Battery (Optional)

Vision Positioning

DJI Pilot App Net Weight Net Weight 570 g

Operating Temperature Range -10° to 40° C

Storage Temperature Range Less than 3 months: -20° to 45° C More than 3 months: 22° C to 28° C

Charging Temperature Range 0° to 40° C

Max Charging Power Max Charging Power 180 W

Name Intelligent Flight Battery

Model Model TB48

Capacity Capacity 5700 mAh

Voltage 22.8 V

Battery Type LiPo 6S

Energy Energy 129.96 Wh

Net Weight Net Weight 670 g

Operating Temperature Range -10° to 40° C

Storage Temperature Range Less than 3 months: -20 to 45° C More than 3 months: 22° to 28° C

Charging Temperature Range 0° to 40° C

Max Charging Power Max Charging Power 180 W

Velocity Range Below 8 m/s (2 m above ground)

Altitude Range 5-500 cm

Operating Environment Operating Environment Brightly lit (lux > 15) patterned surfaces

Operating Range 0-250 cm

Mobile Device System Requirements Mobile Device System Requirements iOS 8.0 or later Android 4.1.2 or later

Supported Mobile Devices Supported Mobile Devices * Compatible with iPhone 5s, iPhone 6, iPhone 6 Plus, iPad Air, iPad Air Wi-Fi + Cellular, iPad mini 2, iPad mini 2 Wi-Fi + Cellular, iPad Air 2, iPad Air 2 Wi-Fi + Cellular, iPad mini 3, and iPad mini 3 Wi-Fi + Cellular. This app is optimized for iPhone 5s, iPhone 6, and iPhone 6 Plus. * Samsung S5, Note 3, Sony Xperia Z3, Google Nexus 7 II, Google Nexus 9, Mi 3, Nubia Z7 mini *Support for additional Android devices available as testing and development continuesA Pre

- flight inspection will be performed by the PIC in accordance with the factory instruction manual. An added step will be the inspection of the propellers. A propeller will be replaced if it has any nicks and cracks with a manufacturers authorized prop eller.
The sUAS will be maintained in accordance with the manufacturers instruction manual and only manufacturer's authorized replacement parts will be used.

FCC Information
This DJI C1 transmitter used for controlling the sUAS complies with part 15 of the FCC rules. Operation is subject to the following two conditions: (1) This device may not cause harmful interference, and (2) this device must accept any interference receive d, including interference that may cause undesired operation. The DJI C1 radio transmitter used for controlling the sUAS is wireless technology which has been tested and found to be compliant with the applicable regulations governing a radio transmitter in the 2.400GHz to 2.4835GHz frequency range. Antenna Separation Distance When operating our DJI C1 transmitter, the PIC will maintain a separation distance of at least 5 cm between his body (excluding fingers, hands, wrists, ankles and feet) and the antenna to meet RF exposure safety requirements as determined by FCC regulations.
Pilot in Command and Observer Qualifications and Duties
The PIC will maintain at least 2 hours flying time and 3 takeoffs and landings within 30 days in the type of UAS utilized i n operations

. The PIC will have at least 50 hours total time and at least 30 hours flying Radio Controlled Model Aircraft of which will be 10 hours flying sUAS's.
Training will be conducted at a local Radio Control Club flying field. Imagination Films ha s the ability to provide "dual controls" utilizing two DJI C1 transmitters with a wireless link between the transmitters. One transmitter is designated the master transmitter and the other transmitter is designated as a slave. The PIC instructor, utilizing the master transmitter, will be at all times be able assume control of the sUAS.
The PIC is responsible for the safe and efficient operation of the aircraft. Specific duties include all preflight preparation, in flight operation, post flight requirements , all procedures including but not limited to:
Safe in flight operations Risk Mitigation to Persons and property Airfield Suitability
The Observer must have the visual acuity to observe the sUAV and be able to communicate clearly with the PIC. The Observ ers duties are;

- W arning the PIC of any impending obstacles in the flight path of the sUAS.

- W arning the PIC of any deviations in the planned flight path of the sUAS.

- W arning the PIC should any unauthorized personnel appear in the area of the planne d flight.
The Observer will have the authority to order the PIC to terminate the flight should he feel the flight cannot be conducted safely.
General Operating Standards
• Imagination Films , LLC will only operate its sUAS in line of sight of a pilot and /or observer and willoperate at sites that are a 'sufficient distance' from populated areas. Such operations will insure that the sUAS will "not create a hazard to users of the national airspace system or the public."
• Before an operation of a sUAV with in 5NM of an airport with a control tower, the control tower will be called to gain permission to operate the sUAS. The PIC will give the position, altitude and the times the sUAV will be operated. The sUAS will not be operated at an altitude of over 150 f eet AGL. Weather minimums will be 3 miles visibility and a 1000 foot ceiling.
Before an operation of a sUAS within 5NM of a non

- tower controlled, airport operators will be notified and the PIC will give the right of way to avoid flying in the proximity of full

- scale aircraft. At no time will the sUAV be operated within the final approach course and the takeoff course of any runway. The sUAV will not be operated at an altitude of over 150 feet AGL. Weather minimums will be 3 miles visibility and a 1000 foot ceiling.
• Maximum flight time for each operational flight will be 25 minutes.
• Flights will be terminated at 25% battery power reserve should that occur prior to the 25 minute limit.
• The sUAV will be programmed so that it will not be operated at an altitude of no more than 400 feet AGL, and not more than 200 feet above an elevated platform from which filming is planned.
• Minimum crew for each operation will consist of the sUAS Pilot, and Visual Observer.
• The sUAV operated by the petitioner weighs less than 55 pounds, including the payload (i.e. camera, lens, and gimbals).
• The sUAV will operate at speeds of no more than 60 knots, can hover, and can simultaneously move vertically and horizontally.

• Gi ven the small size of the sUAV and the restricted sterile environment within which they will operate, our sUAV operations adhere to the Reform Act's safety requirements.
The UAS, powered by batteries, is smaller, lighter and more maneuverable than larger aircraft running on combustible fuel, it operates at lower altitudes with no people on board and will thereby reduce current risk levels and thereby enhance safety and diminish the likelihood of death or serious bodily injury. With a small payload and maxi mum flight time of only 20 minutes, this is offers little or no risk to national security.
Low level oblique photos and video from several angles are far more effective than ground based imagery for displaying the characteristics of large, complex propert ies with several buildings and large trees. The applicants in the past have chartered 2

- seat full

- sized helicopters for this purpose, which has proven more costly than many potential clients have been able to afford. The benefits of reduced cost and impro ved quality of presentation from the UA will be valuable to and benefit many buyers and sellers of real property.
Additionally, we request that we be allowed to use our system to benefit first responders nearby who might require assistance, including fire fighters, the police, the sheriff, et al., while remaining subject to all limitations cited in this application as we do so.
(a) No flight will be made with a Gross weight exceeding 35 pounds;
(b) All operations must occur in FAA Class G airspace at no more than 400 ft AGL, at an airspeed of no more than 60 knots and no further than 1 NM from the PIC;
(c) All operations must utilize a visual observer (VO). The VO and PIC must be able to communicate byvoice at all times during a flight operation;
(d) Operations will be restricted to flights over private property with the permission of the property owner;
(e) All required permits will be obtained from state and local government prior to operation; (f) Imagination Films , LLC will not be operated ove r densely popula ted areas; (g) Imagination Films , LLC will not be operating over any open

- air assembly of people; (h) Imagination Films , LLC will not be operating over heavily trafficked roads;
EXEMPTION REQUESTS AND EQUIVALENT LEVEL OF SAFETY
Imaginatio n Films , LLC requests an exemption from the following regulations as well as any additional regulations that may technically apply to the operation of the sUAV System:
14 CFR Part 21, Airworthiness Certificates
This part establishes the procedures for th e issuance of an airworthiness certificate. While the FAA continues to work to develop airworthiness standards for Unmanned Aerial Systems, we request an experimental certificate be issued for the DJI Inspire 1 under either or both of the following provisi ons: 21.191 Experimental certificates. Experimental certificates are issued for the following purposes:
(a) Research and development

. Testing new aircraft design concepts, new aircraft equipment, new aircraft installations, new aircraft operating techniq ues, or new uses for aircraft.
(b) Showing compliance with regulations

. Conducting flight tests and other operations to show compliance with the airworthiness regulations including flights to show compliance for issuance of type and supplemental type cert ificates, flights to substantiate major design changes, and flights to show compliance with the function and reliability requirements of the regulations. Since the experimental certificate can be used for commercial purposes such as market surveys, sales d emonstrations, and customer crew training, we would expect that an experimental certificate would permit our commercial purpose as well. The aircraft will not carry persons or property, will not carry fuel, and will only fly under strict operational requir ements. Combined with the UA's lightweight , being constructed primarily of carbon fiber and plastic, we propose that the UA will be at least as safe, if not safer, than a conventionally certificated aircraft performing the same mission. If an experimental airworthiness certificate is not appropriate for this application, then we request an exemption of 14 CFR Part 21, Subpart H, and the requirement for an airworthiness certificate in general, citing the equivalent level of safety outlined in the previous pa ragraph.
14 CFR 45.23 Display of marks; general and 45.29 Size of marks
These regulations provide that each aircraft must display "N" and the aircraft's registration number in letters at least 3 inches high. Additionally, the aircraft must display the word "EXPERIMENTAL" in letters at least 2 inches high near the entrance to t he cabin, cockpit, or pilot station. The sUAV does not have an entrance in which the word "EXPERIMENTAL" can be placed, and may not have a registration number assigned to it by the FAA. We propose to achieve an equivalent level of safety by including the w ord "EXPERIMENTAL" in the placard on the top of the aircraft, as shown above, where the PIC (Pilot In Control), VO (Visual Observer) and others in the vicinity of the aircraft while it is preparing for launch will be able to see the designation. Additional ly, we feel that the permanent placard discussed in the previous paragraph will provide the aircraft's registration information at the ground station. Finally, we will display at the ground station a high contrast flag or banner that contains the words "Un manned Aircraft Ground Station" in letters 3 inches high or greater. Since the aircraft will operate within 3/4 NM of the ground station, the banner should be visible to anyone that observes the aircraft and chooses to investigate its point of origin.1 4 CFR 61.113 Private pilot privileges and limitations: Pilot in Command and 61.133 Commercial pilot privileges and limitations
The regulation provides that no person that holds a Private Pilot certificate may act as pilot in Command of an aircraft for comp ensation or hire. Subparagraph (b) allows a private pilot to act as pilot in command of an aircraft in connection with any business or employment if: (1) The flight is only incidental to that business or employment; and (2) The aircraft does not carry pass engers or property for compensation or hire. Our proposed operations require that the PIC must hold at least a Private Pilot Certificate with a Class III Medical issued by the FAA and since the aircraft cannot carry passengers or property, we feel we meet the intent of 61.113 Subparagraph (b) even though the intent of this application is to conduct a business.
14 CFR 91.7 Prohibits the Operation of an aircraft without an airworthiness certificate
As no such certificate will be applicable in the form contem plated by the FARs, this Regulation is inapplicable.
14 CFR 91.9 Civil aircraft flight manual, marking, and placard requirements
This regulation provides that no person may operate an aircraft unless a current, approved flight manual is in the aircraft. We assume that the intent of this requirement is to ensure that flight manual information is available to the aircrew while operati ng the aircraft. We request an exemption to this requirement since the aircraft is not only too small to carry documentation, the documentation would not be available to the crew during flight operations. To obtain an equivalent level of safety and meet th e intent of 91.9, we propose that a current, approved sUAS Flight Manual must be available to the crew at the ground station anytime the aircraft is in, or preparing for, flight.
14 CFR 91.109 Flight Instruction; Simulated instrument flight and certain fl ight tests
The regulation states, "No person may operate a civil aircraft that is being used for flight instruction unless that aircraft has fully functioning dual controls." Training will be conducted at a local Radio Control Club flying field. Imaginati on Films has the ability to provide "dual controls" utilizing two DJI C1 transmitters with a wireless link between the transmitters. One transmitter is designated the master transmitter and the other transmitter is designated as a slave. The PIC instructor , utilizing the master transmitter, will be at all times be able assume control of the sUAV.

91.119 Minimum safe altitudes
General. The regulation states that over sparsely populated areas the aircraft cannot be operated closer than 500 feet to any person , vessel, vehicle, or structure. Since the typical mission of the sUAS would be photography or survey of persons, vessels, vehicles or structures it would be necessary to operate closer than 500 feet to the items listed. Operations will only be flown over property or persons where permission has been obtained and careful pre

- planned flight path has been performed. The aircraft will be operated at a low altitude allowing, if a power unit fails, an emergency landing without undue hazard to persons or property on the surface. Therefore we maintain that due to the small size of the UAS, the hazard to persons, vehicles and structures is minimal compared to manned aircraft, which should be considered in granting the exemption.
CFR 91.121 Altimeter settings

The re gulation requires that aircraft shall maintain cruising altitudes by reference to an altimeter setting available within 100 NM of the aircraft. The sUAS will always fly below 400 feet AGL and will not needto maintain cruising altitudes in order to prevent conflict with other aircraft. An Above Ground Level altimeter measurement above the takeoff point is transmitted via radio from the sUAS on

- board computer to the display screen held by the PIC, providing a constantly updated AGL readout.

14 CFR 91.151 Fu el requirements for flight in VFR conditions
The regulation provides that no person may begin a flight in an airplane under day

- vFR conditions unless there is enough fuel to fly to the first point of intended landing and to fly after that for at least 20 m inutes. We feel the intention of this paragraph is to provide an energy reserve as a safety buffer for delays to landing. The sUAV is battery operated and the maximum duration of flight from a single battery charge is 15 minutes with a 20% reserve. Since t he aircraft will never fly more than 1 NM from the point of intended landing, a full battery charge at launch will ensure that we meet the reserve energy requirement of this paragraph. We request an exemption to the word "fuel" and ask for an equivalent in terpretation with the word "energy".
14 CFR 91.203(a) & (b) Civil aircraft: Certifications required
The regulation provides that an airworthiness certificate, with the registration number assigned to the aircraft and a registration certificate must be abo ard the aircraft. Additionally, subparagraph (b) provides that the airworthiness certificate be "displayed at the cabin or cockpit entrance so that it is legible to passengers or crew." At a maximum gross weight of 5.3 pounds, the sUAS is too small to carr y documentation, does not have an entrance, and is not capable of carrying passengers or crew. To obtain an equivalent level of safety and meet the intent of 91.203, we propose that documents deemed appropriate for this aircraft by the FAA will be with the crew at the ground control station and available for inspection upon request. In order to identify the aircraft, we propose that the information found on airworthiness and registration certificates be permanently affixed to the aircraft via placard contai ning the following information plus the word "EXPERIMENTAL" to satisfy the requirement of 14 CFR 45.23.
14 CFR Subpart E (91.401

- 91.417)

- Maintenance, Preventive Maintenance, Alterations
The regulation provides that the operator is primarily responsible for maintaining the aircraft in an airworthy condition, including compliance with part 39 and 43. Paragraphs 91.407 and 91.409 require that the aircraft be "approved for return to service by a person authorized under 43.7" after maintenance and inspection . It is our intention that the PIC perform maintenance and inspection of the aircraft and "be authorized to approve the aircraft for return to service." The PIC will ensure that the aircraft is in an airworthy condition prior to every flight and in additio n conduct detailed inspections after every two hours of flight. Maintenance performed by the PIC is limited to repairing small cracks, replacing a propeller, checking electrical connections and updating software and firmware for the on

- board computer. The manufacturer or their designated repair facility will perform all other maintenance . The PIC will document work performed in accordance with 91.417. We feel that due to the size, construction, and simplicity of the aircraft, the PIC can ensure an equivalent level of safety.
Safety and Benefits of the UAS
Imagination Films , LLC will be using the UAS in a variety of applications that generally require expensive full

- size manned aircraft to complete. Small, light, unmanned aerial vehicles offer myriad benefits over the use of full

- sized manned aircraft for electric power line inspection, o il/gas pipeline inspection, advanced agriculture, film and still photography, just to name a few. Replacing significantly larger manned aircraft carrying crew and flammable fuel with small UAS carrying no passengers or crew creates a much greater margin of safety for the pilots and cre w. By granting Imagination Films ‘s requested exemptions, the FAA will help drive development of safe and successful commercial UAS operations and will advance the public knowledge base for such operations. Imagination Films , L LC is committed to promoting the UAS research efforts of policymakers including the FAA, NASA, DOD and DARPA by sharing data from its commercial UAS operations and serving as a resource for future UAS research operations. Thus, the FAA has good cause to gr ant this Petition.Conclusion
As pointed ou t in this application, all the s UA S which our company would use, under authorization by the US DOT

- FAA, are small, light

- weight devices operated within the line of sight of the Pilot

- in

- Command (PIC), less tha n 400 feet above the ground and outside 5 miles from any airport, heliport, seaplane base, spaceport, or other location with aviation activities, unless the air traffic control authorities (ATC) have been notified and have authorized each flight within a r adius of this distance.

All our sUAS have proven capability for controlled flight. They are devices offered for general sale on the market around the world and have often been used as Model Aircraft in the USA. We are certain that the studies conducted un til now by the FAA, ab out Section 332 , Public Law 112

- 95, 2014, have already provided you with the assu rances on the airworthiness of sUAS such as ours.
For the foregoing reasons, the exemptions requested herein should be granted and Imagination Films , LL C should be permitted to conduct small UAS operations in accordance with its manuals and all other operating parameters deemed necessary and appropriate by the FAA. The submission of this application and its contents is the best demonstration that indeed i t is possible to pursue the auth orization process so that some sUAS may be used for legitimate commercial activities and under reasonably safe conditions.

Signed,

Xavier Salinas Managing Member

- Imagination Films, LLC