### Brittany Newton Program Analyst, Airmen and Airport Rules Division

As requested

, I submit the following information:

Regulations from which the exemption is requested: 14 CFR subpart H 14 CFR 45.23(b) 14 CFR 61.113(a) and (b)

14 CFR 91.103 14 CFR 91.119(c) 14 CFR 91.121; 91.151(a) 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)

Commercial operation of an UAS, as described herein, which is equipped with a camera would operate
in the following manner:

1. Aerial photography and/or video for public and/or private use including real estate, land surveying, and other related professional activities.

2. Aerial video and/or photography for public and/or private use including television, public events, and news gathering.

3. Aerial inspection/photography of residential/commercial structures under contract with the owners

or local government authority.

4. Aerial video and or photography to provide a live video feed to assist of an emergency or natural disaster only when the local authorities o r government has requested it and will be provided at NO cost
of the l ocal government

.

6. The ability to offer training to individually or someone belonging to both private and/or public organizations that have interests in the use and application of a UAS for the purpose of the safe operation of a UAS to enhance the safety of the National Airspace System (NAS) as well as for the protection of th e persons and property.

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 of the 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 Opera tions Manual (FOM) include:

- The UAS weighs less than 55 lbs.- The UAS has a maximum operating speed of no more than 50mph.

- Flights will be operated at an altitude of no more than 400 feet Above Ground Level (AGL).

- A flight check list will be perform ed regarding the planned UAS operations prior to each flight.

- All flights will occur under Visual Flight Rules.

- A 2

- man crew for each operation consists of a properly certified UAS Pilot in Command (PIC), according

t o FAA regulations, and the Visual Ob server (VO).

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

- The PIC and VO will be able to communicate by voice or radio at all times.

- Maximum flight time for each operational flight is 15

- 20 min utes.

- The flights will occur no closer than a 5 mile radius of local airports.

- If operations will be within a 5 mile radius of an airport, the control tower or operations manager of
the respective airports will be contacted contacted advising them of th e estimated flight time, flight duration, elevation of flight and other pertinent information.

- 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 Distric t Office (FSDO) no more than 72 hours but no less than 48 hours from planned operation.

- We will always obtain verbal/written consent of all persons involved with the planned operation ensuring that only consenting persons will be allowed within 100 feet of our flight operation. This radius may be reduced to 30 feet based upon an equivalent level of safety determination.

- All required permissions and permits will be obtained from territorial, state, county, or city jurisdictions, including local law enforc ement, fire, or other appropriate governmental agencies.

- If the UAS loses communications or loses its GPS signal, the UAS will have the capability to return to a predetermined location within the Security Perimeter and land.

- The UAS will have the capability to abort a flight in case of unpredicted obstacles or emergencies.

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 procedur al 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 require ments of an equivalent level of safety under Part 11 and Section 333 of the Reform Act. The
Federal 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 cer tificate, upon consideration of the size, weight, speed, operational capability, and proximity to airports and populated areas of the particular UAS. In all cases, an analysis of these criteria demonstrates that the UAS operated without an
airworthiness ce rtificate, in the restricted environment and under the conditions proposed will be atleast as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) operating with an
airworthiness certificate without the restrictions and conditions propo sed.

The UAS to be operated hereunder 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 airc raft, operations under this exemption will be tightly controlled and monitored by both the operator and under the requirements and in compliance with local public safety requirements. The FAA will have advance notice of all operations. These safety enhance ments provide a greater degree of safety to the public and property owners than conventional operations
conducted with airworthiness certificates issued under 14 C.F.R. Part 21, Subpart H. Lastly, application of
these 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). Marki ng of the 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 aircraf t 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," "restr icted," "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 “ Experi mental ” can be placed. Given the size of the UAS, two

- inch lettering will be impossible. 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 UAS marked on its f uselage as required by §45.29 (f) where the pilot, observer and others working with the UAS will see the identification of the

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 of an aircraft that is carrying passengers or property for compensation or hire. We may
achieve an equivalent level of safety as achieved by current regula tions 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 of the UAS will
have the proper certifications.

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 of the aircraft formaintenance and use of safety check lists prior to each flight an equivalent level of safety will be provided.

14 C.F.R. § 9 1.9 (b) (2): Civil Aircraft Flight Manual in the 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 of this chapter, unless ther e 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
of flight. As FAA approved rotorcraft flight ma nuals will not be provided for the aircraft an exemption
will be needed. The PIC will take all actions including but not limited to reviewing weather, flight battery requirements, landing and takeoff distances and aircraft performance data before initiatio n of flight.

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 pl atform 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.

The equivalent level of safety will be achieved given the size, weight, speed of the UAS as w ell as the
location where it is operated. No flight will be taken without the permission of the property owner or
local officials. Because of the advance notice to the property owner and participants in the filming activity, all affected individuals will b e aware of the planned flight operations. Compared to flight operations with aircraft or rotorcraft weighting far more than the maximum 55lbs. 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 of the UAS will ensure separation between these UAS operations and the operations of conventional 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 toA n altimeter that is set “ ...to the elevation of the departure airport or an appropriate altimeter settin g available before departure. ” As the UAS may not have a barometric altimeter, but 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 altitude indicator before flight.

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

Section 91.151 (a) prohibits an individua l 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 af ter that for at least 30 minutes; or (2) At night, to fly after that for at least 45 minutes. ”

The battery powering the UAS provides approximately 25 minutes of powered flight. To meet the 30

minute reserve requirement in 14 CFR §91.151, UAS flights would be limited to approximately

- 5 minutes in length. Given the limitations on the UAS ’ s proposed flight area and the location of its proposed operations within a predetermined area, a longer time frame for flight in daylight or twilight
VFR conditions is reas onable.

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 b e allowed. Applicant believes that an equivalent level of safety can be achieved by limiting flights to 15 minutes or 75% of battery power

— whichever happens
first. This restriction would be more than adequate to return the UAS to its planned landing zone from anywhere in its 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 it the following:

(1) An appropriate and current airworthiness certificate. . . . (b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a)
of this section or a special flight authorization issu ed under §91.715 is displayed at the cabin or cockpit entrance so that it is legible to passengers or crew.

The UAS fully loaded weighs no more than 5 lbs. and is operated without an onboard pilot. As such,
there is no ability or place to carry certificati on 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 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 sh all inspect or maintain the aircraft in compliance with Part 43. Given that these section 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 of time. If mechanical is sues 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 inspe ctions 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.

In satisfaction of the criteria provided in Section 333 of the Reform Act of 2012 (size, weight, speed, operating capabilities, proximity to airports and populated areas and operation within visual line
of sight and national security) provide more than adequate justification to grant the my request for exemptions.

N orman Whitehurst

530

- 402

- 9178