Steven J Massi 

Tel 1 704 841 8090 

Charlotte, NC 

Cobra193@gmail.com

Mar 3, 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). 

To whom it may concern: 

I am writing this exemption request on my own behalf. I have no legal counsel. 

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform 

Act) and 14 C.F.R. Part 11, Steven Massi (the Application), owner and operator of Small 

Unmanned Aircraft Systems (“sUASs”) equipped to conduct aerial photography and 

videography. 

The applicant is requesting exemption from the listed FARs to allow for commercial 

operation of its sUASs for aerial images of events such as weddings, private parties, amateur 

sporting events and the like as well as aerial images for Real Estate, 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 as to access. 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: 

Steven J Massi 

Ph: 704 841 8090 

Email:cobra193@gmail.com 

Address: 2801 Providence Spring Lane, Charlotte, NC 28270 

Regulations 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) & (b) 

14 C.F.R. 91.7 (a) 
14 C.F.R 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 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 407 (a) (1) 

14 C.F.R 409 (a) (2) 

14 C.F.R 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) . 

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). 

The sUAS that the applicant currently owns (See images and information in Appendix A) 

are multi-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 areas that have been deemed safe to fly by the PIC during pre-flight 

planning. 

The sUAS currently owned is manufactured by DJI (model Phantom 2 Vision +). DJI is 

the leading manufacturer of multi-rotorcraft designed specifically for unmanned aerial 

photography and videography. It has an abundance of safety features built in including ‘Return 

To Home’ feature that allows the aircraft to return to its originating coordinates and land safely 

on its own should the controlling radios signal be lost or interfered with. 
See appendix A for more information on the manufacturer and safety data. 

Along with the safety features built into the DJI Phantom, the Applicant will be the acting 

PIC. The applicant also has a SEL Private Pilot’s certification and has more than 20 years of 

experience flying Radio Controlled airplanes and helicopters at a very high skill level for hobby 

purposes. 

Having a Pilot’s certification, the applicant understands the risks and dangers involved 

with flying aircraft near an airport and will make sure the sUASs are not flown within 5 miles of 

an airport. The DJI Phantom aircraft also has the most recent firmware update which has 

software in it that prevents the aircraft from being flown within 5 miles of an existing airport. 

Such experience and safety precautions will insure that the sUAS will “not create a 

hazard to users of the national airspace system or the public.” 

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 for aerial photographic operations, 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 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 for 

current Aerial photography services that use conventional, ‘full scale’, piston/jet driven aircraft. 

These limitations and conditions to which Steven Massi, the applicant, agrees to be bound when 

conducting commercial operations under an FAA issued exemption include: 

4 Reform Act Section 333 (b). 

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 

5. Minimum crew for each operation will consist of the sUAS Pilot and a Visual 

Observer. 

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

certificate. The observer will hold at least a third class medical. 
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 on location (i.e. the Aerial Coordinator), that person can also be 

designated as PIC. 

8. The UAS will only operate within a confined “Sterile Area” that has been 

investigated and evaluated before flight operations. 

9. The operator will obtain the consent of all persons involved in the filming 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. 

10. Pilot and observer will have been trained in operation of UAS generally and 

received up-to-date information on the particular UAS to be operated. 

11. Observer and pilot will at all times be able to communicate by voice and/or 

text. 

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

obtained. 

13. 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. 

14. 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. 

15. 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 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. § 61.113 (a) & (b): Private Pilot Privileges and Limitations: Pilot in Command. 

Sections 61.113 (a) & (b) limit private pilots to non-commercial operations. Because the 

UAS will not carry a pilot or passengers, the proposed operations can achieve the equivalent 

level of safety of current operations by requiring the PIC operating the aircraft to have a private 

pilot’s license rather than a commercial pilot’s license to operate this small UAS. Unlike a 

conventional aircraft that carries the pilot and passengers, the sUAS is remotely controlled with 

no living thing on board. The area of operation is controlled and restricted, and all flights are 

planned and coordinated in advance as set forth in the Manual. The level of safety provided by 

the requirements included in the Manual exceeds that provided by a single individual holding a 

commercial pilot’s certificate operating a conventional aircraft. The risks associated with the 

operation of the sUAS are so diminished from the level of risk associated with commercial 

operations contemplated by Part 61 when drafted, that allowing operations of the sUAS as 

requested with a private pilot as the PIC exceeds the present level of safety achieved by 14 

C.F.R. §61.113 (a) & (b). 

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 DJI Owner’s Manual for 

maintenance and use of safety check lists prior to each flight, 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. An equivalent level of safety will be provided as set forth in 

DJI Phantom Owner’s manual along with the applicant’s 20+ years of experience flying radio 

controlled aircraft without incident. 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, 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 sUASs are equipped with telemetry back to the operator. Telemetry includes 

altitude, vertical and horizontal ground speed, direction and distance from operator. 

The equivalent level of safety will be achieved given the size, weight, speed of the UAS 

as well 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 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 used in 

photography for Real Estate and Business. 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 25 minutes of powered flight. 

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. 

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 in compliance with Part 43. 

Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, 

these sections will not apply to the applicant. Maintenance will be accomplished by the operator 

pursuant to the manufacturer’s flight manual and operating handbook. 

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 Owner’s Manual, the operator will ensure that the 
UAS is in working order prior to initiating flight, perform required maintenance. 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) in motion picture and television 

operations. 

Approval of exemptions allowing commercial operations of sUASs will enhance safety by 

reducing risk. Conventional aerial photography/videography operations use jet or piston 

powered aircraft. Such aircraft must fly to and from the film 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 film 

location 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. Photographs will be of people who have also 

consented to being photographed or otherwise have agreed to be in the area where 

photography will take place. 

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 in the 

aerial photograpy industry. 
Sincerely, 

Steven J Massi 

 
Appendix A 

DJI Battery Safety Documentation: 

http://download.djiinnovations.com/downloads/phantom_2_vision_plus/Smart_Flight_Battery_Safety_Guid

elines.pdf

DJI Phantom 2 Vision + Owner’s Manual with pre-flight checklist and maintenance procedures: 

http://download.djiinnovations.com/downloads/phantom_2_vision_plus/en/Phantom_2_Vision_Plus_User_

Manual_v1.8_en.pdf

DJI’s Website resource to locate NO FLY ZONEs near your current location: 

http://www.dji.com/fly-safe/category-mc

Images to show relative size