October 20, 2015 

U. S. Department of Transportation

Docket Management System

1200 New Jersey Ave., SE

Washington, DC 20590 

Re: Exemption Request Section 333 of the FAA Reform Act and Part 11 of the Federal 

Aviation Regulations from 14 C.F.R. 45.23(b);14 CFR Part 21;14 CFR 61.113 (a) & (b);91.7 

(a);91.9 (b) (2);91.103(b); 91.109;91.119; 91.121; 91.151(a);91.203(a) & (b);91.405 (a); 

91.407(a) (1); 91.409 (a) (2);91.417 (a) & (b). 

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. Part 11, Alairis Development Group, Inc., operator of Small Unmanned Aircraft 

Systems (“sUASs”) equipped to offer on-demand commercial UAS operations for a host of 

industries and applications. These include: 

• Building/property damage inspection & assessment,

• Filmmaking, cinematography, and videography,

• Aerial surveying.

hereby applies for an exemption from the listed Federal Aviation Regulations (“FARs”) to allow 

commercial operation 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. 

Applicant requests that the issued exemption includes closed-set motion picture and television 

filming. 

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 3) controlled as to access and 4) would provide safety enhancements 

to the already safe operations using conventional aircraft. 

Approval of this exemption would thereby enhance safety and fulfill the Secretary of 

Transportation’s (the FAA 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: 

Alairis Development Group, Inc. (DBA: Alairis Interactive)

Attn: Jason Valore

PO Box 1758

Medina, OH 44258

Phone: (877) 770-0350

Web: www.alairis.com

Regulations from which the exemption is requested: 

14 CFR Part 21

14 C.F.R. 45.23(b)

14 CFR 61.113 (a) & (b) 

14 C.F.R. 91.7 (a)

14 CFR 91.9 (b) (2)

14 C.F.R. 91.103

14 C.F.R. 91.109

14 C.F. R. 91.119

14 C.F.R. 91.121

14 CFR 91.151 (a)

14 CFR 91.203 (a) & (b)

14 CFR 91.405 (a) 

14 CFR 407 (a) (1)

14 CFR 409 (a) (2)

14 CFR 417 (a) & (b) 

This exemption application is expressly submitted to fulfill Congress’ goal in passing Section 

333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to 

consider whether certain unmanned aircraft systems may operate safely in the national 

airspace system (NAS) before completion of the rulemaking required under Section 332 of the 

Reform Act. In making this determination, the Secretary is required to determine which types of 

UASs do not create a hazard to users of the NAS or the public or pose a threat to national 

security in light of the following: 

• The UAS’s size, weight, speed, and operational capability;

• Operation of the UAS in close proximity to airports and populated areas; and

• Operation of the UAS within visual line of sight of the operator. 
Reform Act § 333 (a). Lastly, if the Secretary determines that such vehicles “may operate 

safely in the national airspace system, the Secretary shall establish requirements for the safe 

operation of such aircraft in the national airspace system.” Id. §333(c) (emphasis added). 

Applicant interprets this provision to place the duty on the Administrator to not only process 

applications for exemptions under section 333, but for the Administrator to craft conditions for 

the safe operation of the UAS, if it should be determined that the conditions set forth herein do 

not fulfill the statutory requirements for approval. The Federal Aviation Act expressly grants the 

FAA the authority to issue exemptions. This statutory authority by its terms includes exempting 

civil aircraft, as the term is defined under §40101 of the Act that includes sUASs, from the 

requirement that all civil aircraft must have a current airworthiness certificate. 

The Administrator may grant an exemption from a requirement of a regulation prescribed 

under subsection (a) or (b) of this section or any sections 44702-44716 of this title if the 

Administrator finds the exemption in the public interest. 49 U.S.C. §44701(f) See also 49 USC 

§44711(a); 49 USC §44704; 14 CFR §91.203 (a) (1). 

Alairis Development Group, Inc.’s sUASs are rotorcraft, weighting 55 or fewer lbs. including 

payload. They operate, under normal conditions at a speed of no more than 50 knots and have 

the capability to hover, and move in the vertical and horizontal plane simultaneously. They will 

operate only in line of sight and will operate only within a sterile area. Such operations will 

insure that the sUAS will “not create a hazard to users of the national airspace system or the 

public.” 

Reform Act Section 333 (b). Given the small size of the sUASs involved and the restricted 

sterile environment within which they will operate, the applicant falls squarely within that zone 

of safety (an equivalent level of safety) in which Congress envisioned that the FAA must, by 

exemption, allow commercial operations of UASs to commence immediately. Also due to the 

size of the UASs and the restricted areas in which the relevant sUASs will operate, approval of 

the application presents no national security issue. Given the clear direction in Section 333 of 

the Reform Act, the authority contained in the Federal Aviation Act, as amended; the strong 

equivalent level of safety surrounding the proposed operations, and the significant public 

benefit, including enhanced safety, reduction in environmental impacts, including reduced 

emissions associated with allowing UASs, the grant of the requested exemptions is in the 

public interest. Accordingly, the applicant respectfully requests that the FAA grant the 

requested exemption without delay. 

AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY 
The applicant will operate the following aircraft : 

Chroma Blade

DJI Phantom 2

DJI Phantom 3 

The applicant proposes that the exemption requested herein apply to civil aircraft that have the 

characteristics and that operate with the limitations listed herein. These limitations provide for 

at least an equivalent or even higher level of safety to operations under the current regulatory 

structure because the proposed operations represent a safety enhancement to the already 

safe operations conducted with conventional aircraft. These limitations and conditions to which 

Alairis Development Group, Inc. agrees to be bound when conducting commercial operations 

under an FAA issued exemption include: 

1. The sUAS will weigh less than 55 lbs.

2. Flights will be operated within line of sight of a pilot and/or observer.

3. Maximum total flight time for each operational flight will be 30 minutes. Flights will be 

terminated at 25% battery power reserve should that occur prior to the 30 minute limit.

4. 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.

5. Minimum crew for each operation will consist of the sUAS Pilot, the Visual Observer, and/or 

the Camera Operator.

6. sUAS pilot will be an FAA licensed airman with at least a private pilot’s certificate.

7. sUAS Pilot will be Pilot in Command (PIC). If a pilot certificate holder other than the sUAS 

Pilot, who possess the necessary PIC qualifications, is also present (i.e. the Visual Observer), 

that person can also be designated as the PIC. 

8. The UAS will only operate within a confined “Sterile Area” of the flight operations area. 

9. A briefing will be conducted in regard to the planned sUAS operations prior to each day’s 

activities. It will be mandatory that all personnel who will be performing duties within the 

boundaries of the safety perimeter be present for this briefing. 

10. The operator will obtain the consent of all persons involved and ensure that only 

consenting persons will be allowed within 100 feet of the flight operation, and this radius may 
be reduced to 30 feet based upon an equivalent level of safety determination. 

11. Pilot and observer will have been trained in operation of UAS generally and received up-todate information on the particular UAS to be operated. 

12. Observer and pilot will at all times are able to communicate by voice and/or text.

13. Written and/or oral permission from the relevant property holders will be obtained.

14. All required permissions and permits will be obtained from territorial, state, county or city 

jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies.

15. If the sUAS loses communications or loses its GPS signal, the UAS will have capability to 

return to a pre-determined location within the Security Perimeter and land.

16. The sUAS 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 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 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 certificate, 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 

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 sUAS 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 area as set out in the Manual. Unlike other civil aircraft, operations under this 

exemption will be tightly controlled and monitored by both the operator, pursuant to the 

Manual’s requirements, and under the requirements and in compliance with local public safety 

requirements, to provide security for the area of operation as is now done with conventional 

filming. The FAA will have advance notice of all operations. These safety enhancements, 
which already apply to civil aircraft operated in connection with motion picture and television 

production, 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). Marking 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 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 of the sUAV, 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 sUAV marked on its fuselage as 

required by §45.29 (f) where the pilot, observer and others working with the sUAV will see the 

identification of the UAS as “Experimental.” The FAA has issued the following exemptions to 

this regulation to Exemptions Nos. 10700, 8738, 10167 and 10167A. 

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 and the requirements contained in the Manual for maintenance 

and use of safety check lists prior to each flight, as set forth in Sections J, L and Q, an 

equivalent level of safety will be provided. 

14 C.F.R. § 91.9 (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 
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 sUAS, 

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 sUAS will have immediate access to it. The FAA has 

issued the following exemptions to this 

regulation: Exemption Nos. 8607, 8737, 8738, 9299, 9299A, 9565, 9565B, 10167, 10167A, 

10602, 32827, and 10700. 

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 manuals will not be provided for the 

aircraft an exemption will be needed. The PIC will take all actions including reviewing weather, 

flight battery requirements, landing and takeoff distances and aircraft performance data before 

initiation of flight. 

14 C.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 instruction unless that aircraft has fully functioning dual 

controls. sUASs 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 of aircraft and for flight instruction in 

experimental aircraft. See Exemption Nos.5778K & 9862A. 

The equivalent level of safety provided by the fact that neither a pilot nor passengers will be 

carried in the aircraft and by the size and speed of the 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 sUAS 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, except for the limited conditions stated in the Manual, the UAS will never operate at 

higher than 400 AGL. It will however be operated in a restricted area with security perimeter, 

where buildings and people will not be exposed to operations without their pre-obtained 

consent. The equivalent level of safety will be achieved given the size, weight, and speed of 

the UAS as well as the location where it is operated. No flight will be taken without the required 

permission of the property owner or local officials. Because of the advance notice to the 

property owner and participants in the aerial activity, all affected individuals will be 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 other industries. In addition, the low-altitude operations 

of the sUAS will ensure separation between these small-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 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, 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 Manual and 

Safety Check list, 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 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 minutes; or 

(2) At night, to fly after that for at least 45 minutes.” The battery powering the sUAS provides 

approximately 40 minutes of powered flight. To meet the 30-minute reserve requirement in 14 

CFR §91.151, sUAS flights would be limited to approximately 10 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 night VFR conditions is 
reasonable. Applicant believes that an exemption from 14 CFR §91.151(a) falls within the 

scope of prior exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to 

operate without compliance with FAR 91.151 (a)). Operating the small UAS, in a tightly 

controlled area where only people and property owners or official representatives who have 

signed waivers will be allowed, with less than 30 minutes of reserve fuel, does not engender 

the type of risks that Section 91.151(a) was intended to alleviate given the size and speed of 

the small UAS. Additionally, limiting sUAS flights to 10 minutes would greatly reduce the utility 

for which the exemption will be granted. 

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 sUAS to its planned landing zone from anywhere in its limited operating 

area. Similar exemptions have been granted to other operations, including Exemptions 2689F,

5745, 10673, and 10808. 

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 issued 

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 55 lbs 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 sUAS. 

An equivalent level of safety will be achieved by keeping these documents at the ground 

control point where the pilot flying the sUAS will have immediate access to them, to the extent 

they are applicable to the sUAS. The FAA has issued numerous exemptions to this regulation. 

A representative sample of other exceptions includes Exemption Nos. 9565, 9665, 9789, 

9789A, 9797, 9797A, 9816A, and 10700. 

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 shall inspect or maintain the aircraft incompliance 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. The operator pursuant to the flight manual and 

operating handbook will accomplish maintenance. An equivalent level of safety will be 

achieved because these small UASs are very limited in size and will carry a small payload and 

operate only in restricted areas for limited periods of time. If mechanical issues arise the UAS 

can land immediately and will be operating from no higher than 400 feet AGL. As provided in 

the Manual, 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. 

***** 

Pursuant to 14 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. §21, subpart H; 14 C.F.R 45.23(b);14 C.F.R. §§ 61.113( a) & (b);91.7 (a); 91.9(b) 

(2);91.103(b);91.109; 91.119; 91.121; 91.151(a);91.203(a) and (b); 91.405 (a); 91.407 (a) (1); 

91.409 (a) (2); 91.409 (a) (2) and 91.417 (a) & (b) to operate commercially a small unmanned 

vehicle (55lbs or less). Approval of exemptions allowing commercial operations of sUASs, will 

enhance safety by reducing risk. Conventional operations, using jet or piston power aircraft, 

operate at extremely low altitudes just feet from the subjects being filmed and in extreme 

proximity to people and structures and present the risks associated with vehicles that weigh in 

the neighborhood of 4,000lbs, carrying large amounts of jet A or other fuel. Such aircraft must 

fly to and from the operational location. In contrast, a sUAS weighing fewer than 55 lbs. and 

powered by batteries eliminates virtually all of that risk given the reduced mass and lack of 

combustible fuel carried on board. The sUAS is carried to the operation site and not flown. The 

sUAS will carry no passengers or crew and, therefore, will not expose them to the risks 

associated with manned aircraft flights. The operation of small UASs, weighting less than 55 

lbs., conducted in the strict conditions outlined above, will provide an equivalent level of safety 

supporting the grant of the exemptions requested herein, including exempting 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 sterile environment and, as a 

result, are far safer than conventional operations conducted with turbine helicopters operating 

in close proximity to the ground and people. 

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 will take place. The grant of this 

exemption request will provide improved safety in both day and night operations. 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 for the grant of the 

requested exemptions allowing commercial operation of applicant’s UAS. 

Jason Valore

Alairis Development Group, Inc.

(877) 770-0350