October 1, 2015

U.S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590

Re: Exemption Request Pursuant to Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation Regulations from: 14 C.F.R. 21 Subpart H; 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. §91.103(b)(2); 14 C.F.R. §91.109; 14 C.F.R. §91.119(c); 14 C.F.R. §91.121; 14 C.F.R. §91.151(a); 14 C.F.R. §91.203 (a) and (b); 14 C.F.R. §91.405 (a); 14 C.F.R. §91.407 (a) (1) 14 C.F.R. §91.409 (a)(1) and (2); 14 C.F.R. §91.417(a) and (b)

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the “Reform Act”) and 14 CFR Part 11, Corsair Aviat ion, LLC (“Corsair”), an operator of Unmanned Aircraft Systems (“UASs”), hereby applies for an exemption from the listed Federal Aviation Regulations (“FARs”) to allow commercial operation of its sUAS, so long as such operations are conducted

within and un der the conditions outlined herein or as may be established by the FAA as required by Section 333.

Commercial operation of a sUAS, as described herein, which are equipped with camera(s) and sensor(s), would operate in the following manner:

1. Aerial photog raphy for the motion picture and television industry for scripted closed set filming. 1

2. Aerial p atrol/ i nspection and survey of commercial/residential utility infrastructure including but not limited to powerlines /pipelines , wind turbines, and cell towers.

3. Aerial video/photography or providing live video feed to assist with search and rescue operations, wild land firefighting support, wildlife and forestry monitoring, and law enforcement when local, state or federal authorities or government has requested it by contract or donation.

4. Aerial video/photography for public and/or private use including television, public /sporting events, cinematography and electronic news gathering (“ENG”)

. 5. Aerial video/photography for real estate, architecture, engineering, and su rvey.
6. Aerial data collection applications including but not limited to mapping, land surveying, precision agriculture, 3D modeling, R&D, and market research.

1 The conditions proposed by the applicant are drawn from Order 8900.1 CHG 0, Volume 3, Chapter 8

- Issue a Certificate of Waiv er for Motion Picture and Television Filming.2 | P a g e

7. Crew member/ cinematography training as well as the ability to offer training to persons individual ly or belonging to both private and/or public organizations that have interests in the safe use and operation of a UAS.

The requested exemption would permit the operation of a sUAS under controlled conditions in the NAS that would be a) limited b) control led c) predetermined, and d) will provide safety enhancements to the already safe operations in the industry presently using conventional aircraft. Approval of this exemption would thereby enhance safety and fulfill the Secretary of Transportation’s (the F AA Administrator’s) responsibilities to “....establish requirements for the safe operation of such aircraft systems in the national airspace system.” Section 333(c) of the

Reform Act

The name and address of the applicant is:

Corsair Aviation, LLC

Attn: Mike Killian, President Phone: (818) 906

- 4024
Email: corsairaviation@outlook.com Address: 12653 Osborne St. #28, Pacoima, CA 91331

Regulations from which the exemption is requested:

14 C.F.R. Part 21 Subpart H 14 C.F.R. § 91.119 (c)

14 C.F.R. Part 36 Subpart A, F & O 14 C.F.R. § 91.121

14 C.F.R. § 45.23 (b) 14 C.F.R. § 91.151 (a)

14 C.F.R. § 45.29

14 C.F.R. § 61.113 (a) & (b) 14 C.F.R. § 91.203 (a) & (b)

14 C.F.R. § 91.7 (a) 14 C.F.R. § 91.405 (a)

14 C.F.R. § 91.9 (b)(2) 14 C.F.R. § 9 1.407 (a)(1)

14 C.F.R. § 91.103(b)(2) 14 C.F.R. § 91.409 (a)(2)

14 C.F.R. § 91.109 14 C.F.R. § 91.417 (a) & (b)

Corsair proposes to operate the following sUASs:

- Freefly Systems ALTA

- DJI S1000 Octocopter

- DJI Inspire 1

- Sensefly eBee

UASs operate d by Corsair weigh less than 55 pounds, including payload (i.e. camera, lens, and gimbal). They operate at speeds of no more than 50 knots, can hover, and can simultaneously move vertically and horizontally. Corsair will only operate its UASs in line of si ght

and during closed set productions, will operate within the sterile area described in Corsair ’ s Flight Operations and Motion Picture and Television Manual (FOPM) 2 . Such operations will

insure that the sUAS will “not create a hazard to users of the natio nal airspace system or the public.” 3

Similarly sized sUASs have been approved for use in prior Section 333 Grants of Exemption

from the FAA. See e.g., Grant of Exemption to Astraeus Aerial (Exemption No. 11 062 ); Grant of

2 Applicant submits this manual as a Confidential document under 14 CFR 11.35(b) as the entire manual contains proprietary information that the applicant has not and will not share with others. The manual conta ins operating conditions and procedures that are not available to the public and are protected from release under the Freedom of Information Act 5 USC 552 et. seq.

3 Reform Act Section 333(b)3 | P a g e

Exemption to Empire Unmanned, LLC (Exemption No. 11 881 ); Grant of Exemption to ArrowData, LLC (Exemption No. 11 408 ); Grant of Exemption to Alan Purwin (Exemption No. 11161); Grant of Exemption to Helinet Aviation Services , LLC (Exemption No. 11160); Grant of Exemption to 4 th Dimension Sig ht & Sound, Inc. (Exemption No. 1 2428 ) ; Grant of Exemption to Sensefly, Ltd

. (Exemption No. 11263).

Given the small size of the sUASs and the controlled environment provided, the proposed operations will adhere to the Reform Act’s safety requirements. Th e approval of this 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 of the requested exemption is in the public interest. Accordingly, the applicant requests that the FAA grant the requested exemption with minimum delay.

Aircraft and Equivalent Level of Safety

The applicant seeks to have this exemption cover the s UASs used to carry out the commercial operations described herein which are subject to the limitations proposed in this petition. Corsair proposes and agrees to the following limitations and conditions for commercial sUAS operations conducted under a grant ed FAA exemption:

1. The sUASs will weigh less than 55 lbs.

2. Flights will be operated within line of sight of the Pilot in Command (PIC) and/or Visual Observer (VO).

3. Maximum flight time for a multi

- rotor sUAS operational flight will be 3 0 minutes. Flights wi ll be terminated at 25% battery power reserve or 30 minutes of flight time whichever occurs first.

4. Maximum flight time for a fixed wing sUAS operational flight will be 40 minutes. Flights will be terminated at 25% battery power reserve or 30

minutes of fl ight time whichever occurs first.

5. Flights will be operated at an altitude of no more than 400 feet AGL or, not more than 200 feet above an elevated platform from which filming is planned.

6. Minimum crew for each operation will consist of the sUAS Pilot, the Visual Observer (VO), and may include but not limited to a Camera Operator.

7. The sUAS pilot will be a designated Pilot in Command (PIC) and hold either an airline transport, commercial, private, recreational, or sport pilot certificate.

The PIC will also ho ld a current FAA airmen medical certificate or a valid U.S. driver’s license issued by a state, District of Columbia, Puerto Rico, a territory, a possession, or the Federal government of the United States. The PIC will also meet the flight review requireme nts specified in 14 C.F.R. § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate. If a pilot certificate holder other than the sUAS pilot, who possesses the necessary PIC qualifications, is also present on set (i.e. the Aerial

Co ordinator), that person can also be designated as PIC.

8. During closed set filming for motion picture and television the sUAS will only operate within a confined “Sterile Area” as defined in the FOPM. The FOPM requires the establishment of a “Security Perime ter” for the flight operations

area.
9. A briefing will be conducted for planned sUAS operations prior to each day’s flight. All personnel performing duties within the boundaries of the safety perimeter are required to attend.

10. All flights will occur under Vis ual Meteorological Conditions (VMC) only.4 | P a g e 11. The flights will occur no closer than a 5 mile radius of the geographic center/Airport Reference Point (ARP) of a tower controlled or uncontrolled airport.

12. If operations will be within a 5 mile radius of the geogra phic center/Airport Reference Point (ARP) of a tower controlled or uncontrolled airport the respective airports will be contacted advising them of the estimated flight time, flight duration, elevation of flight and other pertinent information.

13. The operator will file FAA Form 7711

- 1, or its equivalent, as modified in light of the requested exemption, with the appropriate local Flight Standards District Office (FSDO).

14. The operator will obtain consent of all persons involved in the filming and ensure that only consenting persons will be allowed within 100 feet of the flight operation. This radius may be reduced to 30 feet based upon an equivalent level of safety determination, as required under the FOPM. With the advanced permission of the FSDO, operations at c loser range can be approved.

15. The operator will submit a written Plan of Activities to the FSDO three days before the proposed shoot as required in the FOPM.

16. The PIC and VO must be trained in s UAS operations and have received current information on the part icular s UAS to be operated as required by the

FOPM.

17. The PIC and VO will be able to communicate by voice and/or text at all times.

18. Written and/or verbal permission from the relevant property holders will be

obtained.

19. All required permissions and permits wil l be obtained from territorial, state, county, or city jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies.

20. If the sUAS loses communications or loses its GPS signal, the sUAS will have capability to return to a pre

- determined location within the Security

Perimeter and land.

21. The sUAS will have the capability to abort a flight in case of unpredicted obstacles, weather, or emergencies.

22. The sUAS will not be operated less than 500 feet below or less than 2,000

feet ho rizontally from a cloud or when visibility is less than 3 statute miles

from the PIC.

23. A Flight Operations and Motion Picture and Television Operations Manual (FOPM) will be used to help govern all closed

- set motion picture and television filming operations

.

14 C.F.R. Part 21, Subpart H: Certification Procedures

- Airworthiness Certificates

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 by the applicant, an exemption from Part 21, Subpart H meets the requirements of an equivalent level of safety

under Part 11 and Section 333 of the Reform Act. The Fe deral Aviation Act 49 U.S.C.§44701 (f)

and Section 333 of the Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration of the size, weight, speed, operational capability, and proximity to airports and populated areas of the particular sUAS. In all cases, an analysis of these criteria demonstrates that the sUAS operated without an

a irworthiness 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.5 | P a g e

The sUAS to be operated is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, carries no explosive materials or flammable 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 the operator in com pliance with local public safety requirements. These enhancements provide a greater degree of safety to the public and property owners than conventional civil aircraft operations conducted with airworthiness

certificates issued under 14 C.F.R. Part 21, Sub part H. Lastly, there is no credible threat to national security posed by the sUAS, due to its size, speed of operation, location of operation, lack of explosive materials or flammable liquid fuels, and its inability to carry a substantial

e xternal load. T here have been exemptions granted by the FAA to petitioners seeking identical relief; See Grant of Exemption No. 11062 to Astraeus Aerial (FAA

- 2014

- 0352 at pgs. 13

- 14, 22).

14 C.F.R. Part 36, Subparts A, F and O: Noise Standards

- Aircraft Type and

Airwor thiness Certification

Pursuant to 14 C.F.R. Part 36, Subparts A, F and O, establish certain noise standards for certification of various aircraft types. Because the Subject sUAS would not have an airworthiness certificate, and given its small size and neg ligible noise impact, the petitioner requests an exemption from 14 C.F.R. Part 36.

14 C.F.R. § 45.23 (b): Display of Marks; General.

Pursuant to 14 C.F.R. 45.23(b); When marks include only the Roman capital letter “N” and the registration number is displ ayed 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 inch es nor more than 6 inches high, the words “limited,” “restricted,” “light

- sport,” “experimental,” or “provisional,” as applicable.

While the sUAS will have no airworthiness certificate, an exemption may be needed as

the sUAS will have no entrance to the c abin, cockpit or pilot station on which the word “Experimental” can be placed. Given the size of the sUAS, two

- inch lettering will be impractical. The word “Experimental” will be placed on the fuselage in compliance with §45.29 (f). The equivalent level of safety will be provided by having the sUAS marked on its fuselage as required by §45.29(f) where the pilot, observer, and others working with the sUAS will see the identification of the sUAS as “Experimental.” In a previous Grant of Exemption, the FAA

det ermined that exemption from these requirements was warranted provided that the aircraft “have identification (N

- Number) markings in accordance with 14 C.F.R Part 45, Subpart C if the markings are as large as practicable.” See FAA Docket No. FAA

- 2014

- 0352. All sUASs flown by

Corsair will bear N

- number markings that are as large as practicable in accordance with 14 C.F.R. Part 45, Subpart C.

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

- Pilot in Command.

Pursuant to 14 C.F.R. 61 .113 (a) & (b); No person who holds a private pilot certificate may act as a pilot in command of an aircraft that is carrying passengers or property for compensation or hire. Because the applicant’s sUAS does not carry any pilots, passengers, or
property, Corsair may achieve an equivalent level of safety as achi eved under current regulations. The risks attendant to the operation of a sUAS is far less than the risk levels

inherent in the commercial activities outlined in 14 C.F.R. 61. The PIC of the sUAS wil l have either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC

will also hold a current FAA airman medical certificate or a valid U.S. driver’s license issued by a state, District of Columbia, Puerto Rico, a terr itory, a possession, or the Federal government of6 | P a g e

the United States. In meeting those limitations as listed in previous FAA exemption approvals,

the PIC of Corsair’s sUASs will exceed current safety levels in relation to 14 C.F.R. 61.113 (a) & (b).

14 C.F .R. §91.7(a): Civil Aircraft Airworthiness.

Pursuant to 14 C.F.R. 91.7(a); No person may operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for the sUAS, should this exemption be granted, no FAA regulatory standard will exist for determining airworthiness. Given the size of the aircraft and the maintenance requirements detailed in the sUAS User and/or Operations Manual combined with safety check lists prior to each flight, an equivalent

level of safety will be provided. See Grant of Exemption No. 11671 to Dronair Solutions (FAA

– 2015

– 0648 page 18) for previous FAA granted exemption.

14 C.F.R. § 91.9 (b) (2): Civil Aircraft Flight Manual, Marking, and Placard Requirements.

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 of this 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. Given the size and configuration of the sUAS used by Corsair , there is no capacity to carry such a flight manual on the aircraft. An equivalent level of safety will be ac hieved by keeping the sUAS Operation Manual at the ground control point where the pilot in command will have immediate access. See Memorandum from Mark Bury, FAA Assistant Chief Counsel for International Law, Legislation and Regulation, to John Duncan, FAA Flight Standards Service (Aug. 8, 2014); see also Docket

No. FAA

- 2014

- 0352 at 16

- 18.

14 C.F.R. § 91.103(b)(2): General Operating and Flight Rules

- Preflight Action.

Pursuant to 14 C.F.R. 91.103(b)(2); For civil aircraft other than those specified in

pa ragraph (b)(1) of this section, other reliable information appropriate to the aircraft, relating to aircraft performance under expected values of airport elevation and runway slope, aircraft gross weight, and wind and temperature. An equivalent level of sa fety will be provided by a preflight checklist and other safety measures detailed in the sUAS Operation Manual. The PIC will take actions including reviewing weather, flight battery requirements, landing and takeoff distances, aircraft performance data, an d setting the pre

- determined safe landing area in case of loss of GPS communication before initiation of flight. See Grant of Exemption No. 11671 to Dronair Solutions (FAA

– 2015

– 0648 page 18)

14 C.F.R. §91.109: Flight instruction; Simulated Instrument Flig ht and Certain Flight

Tests.

Section 91.109 provides that 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. Remotely piloted aircraft a nd sUAS, 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. The FAA has approved exemptions for flight training without fully functiona l dual controls for a number of aircraft and for flight instruction in experimental aircraft. Due to the

size and speed of the sUAS and the fact that neither a pilot nor passengers will be carried in the aircraft, and all persons will be a safe distance aw ay in the event that the UAS experiences any difficulties during flight instruction, an equivalent level of safety is provided. The FAA has granted exemption for the same operation, See Grant of Exemption No. 11671 to Dronair Solutions (FAA

– 2015

– 0648 page 19)7 | P a g e

14 C.F.R. §91.119: General Operating and Flight Rules

- 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, provi ded the person operating the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. As this exemption is for sUAS operation at altitudes up to 400 feet AGL, an exemption may be needed. In cases where the sUAS is used to surv ey, inspect, or photograph a structure that exceeds 400 feet AGL, the sUAS will not be operated more than 200 feet above the highest point of that structure. An exemption was granted by the FAA for like operations

- See Grant of Exemption No. 11138 to Doug las Trudeau (FAA

- 2014

- 0481 page 19)

An equivalent level of safety will be achieved given the size, weight, and speed of the

sUAS as well as the location where it is operated. No flight will be taken without the permission of the property owner or local of ficials. Compared to flight operations with aircraft or rotorcraft operating below 500 feet AGL, weighing far more than the proposed 55 pound maximum, and carrying flammable fuel, the sUASs employed by Corsair provide a much safer alternative. In
addition, the low

- altitude operations of the sUAS will ensure safe separation from those of conventional aircraft that must comply with Section 91.119.

14 C.F.R. §91.121: General Operating and Flight Rules

- Altimeter settings.

Section 91.121 requires each person operating an aircraft to maintain cruising altitude by

reference to an altimeter that is set “...to the elevation of the departure airport or an appropriate altimeter setting available before departure.” As the sUAS may not have a barometric altimeter,

bu t instead a GPS altitude read out, an 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 of the launch site shown on the GPS al titude indicator before flight. See

e.g., Grant of Exemption No. 11062 to Astraeus Aerial (FAA

- 2014

- 0352 at 21).

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

Section 91.151 (a) prohibits an individual from beginning “a 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 minute s; or (2) At night, to fly after that for at least 45 minutes.” For similarly FAA granted exemption, see Grant of Exemption to Alan Purwin (Exemption No. 11161). The battery powering t he sUAS provides approximately 4 0 minutes of powered flight. Because the 30 minute reserve requirement in 14 C.F.R. §91.151 cannot be met by the sUAS, an exemption is needed. With a limited flight time of 30 minutes or 25% battery power and line of sight operation in a limited area, an equivalent level of safety is achieved. T his time/power restriction is more than adequate to safely return the sUAS to its planned landing

zone from anywhere in its limited operating area.

14 C.F.R. §91.203 (a) and (b): Civil Aircraft: Certifications Required

The regulation provides in pertinen t part: (a) Except as provided in § 91.715, no person may operate a civil aircraft unless it has within it the following: (1) An appropriate and current

airworthiness certificate... (b) No person may operate a civil aircraft unless the airworthiness

certif icate required by paragraph (a) of this section or a special flight authorization issued under §91.715 is displayed at the cabin or cockpit entrance so that it is legible to passengers or crew. The sUAS fully loaded weighs no more than 55 lbs. and is opera ted without an onboard pilot. As such, it is impractical to carry certification and registration documents or to display them on

the sUAS. An equivalent level of safety will be achieved by keeping these documents at the8 | P a g e

ground control point where the pilot in command will have immediate access. The FAA has granted exemption for same, See Grant of Exemption No. 11671 to Dronair Solutions (FAA

– 2015

– 0648 page 18)

14 C.F.R. §91.405 (a); §91.407 (a) (1); §91.409 (a) (2); §91.417(a) & (b): Maintenance required.

Sections 91.405(a), 407(a)(1), 409(a)(2), 417(a)(b) require that an aircraft operator or

owner “shall have that aircraft inspected as prescribed in Subpart E of this part and shall between required inspections, except as provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and others shall inspect or maintain the aircraft in compliance with Part 43. Corsair proposes that the maintenance of the sUAS will be accomplished by the owner/operator ac cording to the operation manual. As provided in the attached manuals, the operator will ensure that the sUAS is in working order prior to initiating flight, perform required maintenance, and keep a log of any maintenance that is performed. Moreover, the op erator is the person most familiar with the aircraft and is best suited to maintain the aircraft in an airworthy condition thereby ensuring an equivalent level of safety. See e.g. , Grant of Exemption No. 11671 to Dronair Solutions (FAA

– 2015

– 0648 page 15)

Privacy

All flights will occur over private or controlled access property with the property owner’s prior consent and knowledge. Filming will be of people who have also consented to being filmed or otherwise have agreed to be in the area where filming wi ll take place.

Public I nterest

Corsair is convinced that approval of the exemptions requested in this petition are in the public’s interest. Our conviction stems from the thorough survey of the applications and safety enhancements that sUAS operations o ffer to a wide variety of existing and future markets. Many of the current flight operations that are addressed using manned civil aircraft can be performed by small unmanned aircraft systems with reduced environmental impact, lower cost, and

increased saf ety. Consider the following comparison between the sUAS and manned civil

aircraft:

- The sUAS is smaller and weighs considerably less than manned civil aircraft.

o Reduces hazard to property, livestock, and general population.

o The sUAS can operate in smaller areas not possible with large aircraft.

- The sUAS uses batteries rather than combustible fuel.

o Reduces environmental impact by eliminating hydrocarbon emissions.

o Non

- flammable power source reduces fire risk.

- The sUAS does not require onboard crew members fl ying at low altitudes.

o Reduces risk of injury to flight operations personnel.

Emerging in the marketplace are many applications that are well suited for sUAS operations. Corsair has positioned itself to provide professional sUAS services that will benefi t the public in support of commercial, private, and governmental sectors. Examples of these areas may include:

Land Planning and Development Agriculture

Solar Power Power Generation and Distribution Local Infrastructure & Agencies Environmental Res earch Architecture and Engineering Search and Rescue9 | P a g e

Although video and photography are main features of sUAS operations, there are a multitude of other applications that will come to benefit the public. In addition to providing videography/photography for markets like real estate and public/private events, there are others

that address the needs of far

- reaching markets. Examples include:

Closed

- Set Filmmaking and Cinematography

Typically, the motion picture and television industry uses manned airpla nes and helicopters to carry out aerial filming of subject matter. They are usually large, heavy, and powered by combustible fuel. Using a sUAS offers a level of safety that cannot be provided by its larger counterparts. The small size, light weight aircra ft are powered by batteries giving them the advantage to film in more confined areas while reducing risk to structure and persons.

Closed

- Set filming using sUAS is in the interest of the public as it takes place in a controlled area, away from spectators a nd persons not involved in the filming.

Agriculture

Special lenses fitted to the sUAS camera allow data to be collected from images that

determine the health of plants growing in a field. That data is used to calculate more precise application of pestic ide, fertilizer, and water thereby limiting and conserving resources. This can ultimately lead to increased crop yield at reduced cost.

Structural Inspection

Image data collected using a sUAS can be utilized to create 3

- dimensional models of

structures. Engineers can use these 3D models to navigate and make measurements using

their own in

- house CAD software. A considerable advantage is gained in being able to determine repair costs and design modifications in office without having to make measurements

th at rely on costly high

- risk methods. Engineering firms can benefit by reduced cost and enhanced safety.

Environmental Conservation

Images collected from sUAS flights over areas of interest can be used to create accurate maps and models of parks, reserve s, and nature conservation areas in an efficient and

a ffordable way. Rather than collecting data, personnel can spend their time analyzing the maps and models for various actions like assessing environmental regulation adherence or creating

extensive inven tories of natural resources.

Accident Scene Reconstruction

A traffic accident is a good example where the sUAS size and maneuverability can provide a timely and accurate method of data collection. Following a traffic accident, there is a

limited amount of time to gather information for use in reconstruction of the event. The sUAS can capture ground and aerial imagery to be used in constructing 3

- dimensional representations of the accident scene. The resulting models can be used at any given time to perfo rm accurate measurements and to view every conceivable angle of the scene. The use of sUAS data collection provides an immediate response, saves expense, and offers highly accurate output.

Solar Power Land Development10 | P a g e

Development of a potential solar fa rm site requires a topographic survey to help plan the placement of the photovoltaic cells. A sUAS can serve as a valuable data collection tool for rendering complex 3

- dimensional models of the land under consideration or development. Slope angles and heig ht measurements can be made using the image data collected by the sUAS cameras. The use of sUAS technology reduces time and cost compared with traditional surveying methods while providing increased accuracy and accessibility.

Search and Rescue (SAR)

In regard to search and rescue operations, the public stands to benefit from the use of sUAS technology. The sUAS aircraft are able to perform missions with a high level of complexity
and, at the same time, require less human operator involvement due to thei r autonomous behavior. Because the search phase in SAR missions is critical to guarantee broad coverage of wide areas, the sUAS can execute missions autonomously repeating area coverage multiple times when needed. During the rescue phase, the sUAS can be u sed to deliver medicine, food, water, etc. to a temporarily non

- accessible person or persons.

The applications and services discussed above are only a small sample of a virtually limitless set of potential benefits the public, private, and governmental se ctors stand to gain.

Corsair is purposeful in providing safe and valuable services and is convinced that approval of the exemptions requested in this petition are, without a doubt, in the public’s interest.

Corsair would like to thank the FAA for consider ing this request. We look forward to working with the FAA in its determination, and to being part of the discussions as the FAA considers how to expand, certify, test, register, track, and control commercial sUAS use in the

United States.

If you have any questions or need any additional information, please contact the undersigned at (818) 906

- 4024 or at corsairaviation@outlook.com.

Respectfully Yours,

Michael Killian

President Corsair Aviation, LLC11 | P a g e APPENDIX A

SUMMARY OF SECTION 333 EXE MPTION REQUEST

Pursuant to C.F.R. Part 11, the following summary is provided for publication in the

Federal Register, should it be determined that publication is needed:

Applicant seeks an exemption from the following rules: 14 C.F.R. Part 21 Subpart H

, 14 C.F.R. Part 36 Subpart A, F & O

, 14 C.F.R. §45.23 (b)

, 14 C.F.R. §61.113 (a) & (b)

, 14 C.F.R. §91.7 (a)

, 14 C.F.R. §91.9 (b) (2)

, 14 C.F.R. §91.103(b)(2)

, 14 C.F.R. §91.109

, 14 C.F.R. §91 .119 (c)

, 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. §91.405 (a)

, 14 C.F.R. §91.407 (a) (1)

, 14 C.F.R. §91.409 (a) (2)

, 14 C.F.R. §91.417 (a) & (b) to operate commercially a small unmanned vehicle (55 lbs. or less) in aerial photography operations.

Approval of exemption s allowing c ommercial operations of sUAS in the aerial photography

, patrol and inspection, mapping and survey, wildlife and forestry , search and

rescue, and film industries enhances safety while reducing risk

. Conventional manned aircraft currently used in these industries creates a greater risk because the aircraft are much larger

, have com bustible fuel , an d carry an onboard human crew. In contrast, a sUAS weighing fewer

than 50 lbs. and powered by batt eries eliminates virtually all of that risk , given the reduced mass and lack of combustible fuel carried on board . The sUAS will carry no passengers or crew and, therefore, will not expose them to the risks associated with manned aircraft fligh ts.

The operation of small s UAS, weighing less than 50 lbs. , conducted in the strict

conditions outlined above, will provide an eq uivalent level of safety supporting the grant of the exemptions requested here in, including exempt ing the applicant from the requirements of Part

21 and allowing commercial operations. These lightweight aircraft operate at slow speeds, close

to the ground, and in a controlled environment and, as a result , are far safer than conventional operations conducted with turbine or re ciprocating helicopters or full scale manned aircraft operating in close proxim ity to the ground or people.