Private and Confidential

John R. Rogers

, Austin

, Texas

- Section 333 Exemption Petition

February 12, 2016

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 of the Federal Aviation Regulations

from 14 C.F.R. 45.23(b); 14 C.F.R. Part 21; 14 C.F.R. 61.113(a)&(b); 91.7(a); 91.9(b) (2);

91.103(b); 91.109; 119.121; 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, I, John R. Rogers

, am writing pursuant to the FAA Modernization and

Reform Act of 2012 and the procedures contained within 14 C.F.R. 11, to request that I, John R.

Rogers an owner and operator of small unmanned aircraft, be exempte d from the Federal

Aviation Regulations (“FARs”) listed below so that I, John R. Rogers

, may operate my small

ultra

- lightweight unmanned aircraft system (“UAS”) in commercially regulated airspace by the

Federal Aviation Administration (“FAA”).

Following exemption and approval by the FAA, I, John R. Rogers, will primarily use my

professionally built Phantom 3 UAS equipped with cameras for the following applications: aerial

videography/cinematography to safely enhance films and commercials; augmentation of real

estate listing videos and photography ; agricultural inspections, building and construction zone

inspections and s till and video photography for fine art and stock use.

My, John R. Rogers’, exemption request would permit the operation of ultra

- lightwe ight,

unmanned (i.e. piloted by remote control) UAS’s for the development of community and

government use videos, permissible within property boundaries for individual homeowners and

within in tightly controlled, limited airspaces predetermined in areas aw ay from the general

public, airports, heliports and vehicular traffic. Currently, similar lightweight, remote controlled

UAS's are legally operated by unmonitored amateur hobbyists with no safety plan or controls in

place to prevent catastrophe. Furthermor e, it is my intent to assist future FAA safety protocols

and regulations exclusive to lightweight UAS's for specific video and photography usage by

sharing information with the FAA as I, John R. Rogers, record flight data and other pertinent

information ga ined through permitted flight operations.

In addition, granting my

, John R. Rogers’, exemption request will comply with the Secretary of

Transportation’s (FAA Administrator’s) instructions to not only integrate UAS's into the national2

2 airspace system, bu t to “...establish requirements for the safe operation of such aircraft systems

[UAS's] in the national airspace system” under Section 333(c) of the Reform Act specific to the

use of UAS's for real estate/Realtor purposes, educational videos, Search and Re scue, land/trusts

inspections, agricultural field monitoring, film/video productions, closed

- set motion picture film

operations and television, and structure inspections

, to aid state and local agencies.

Further I, John R. Rogers, will conduct my operati ons in compliance with the protocols

described herein or as otherwise established by the FAA. For the reasons stated below, I, John R.

Rogers, respectfully request the grant of an exempti on allowing me to operate ultra

- lightweight,

remote controlled UAS’s to aid academic community awareness, to benefit/stimulate attraction

to the metro Austin, Texas and to enhance personal and public video feeds. A grant that will

ultimately allow UAS’s to play a more positive role in our local community by increasing

emplo yment opportunities, heightening security measures and decreasing government

expenditures by reducing the need for heavier manned aircraft, containing costly, combustible

fuel

- a potential public hazard in and of itself.

I. Contact Information:

John R. Rogers

1803 W. Koenig Lane

Austin, Texas 78756

Phone: 512

- 699

- 6468

Email: john@johnrrogers.com

II. The Specific Sections of Title 14 of the Code of Federal Regulations f rom w hich

John R. Rogers Requests Exemption are:

14 CFR 21; 14 C.F.R. 45.23(b);

1 4 CFR 61.113 (a) & (b);

14 C.F.R. 91, et seq.;

14 CFR 407 (a) (1);

14 CFR 409 (a) (2); and,

14 CFR 417 (a) & (b).

III. The Extent of relief John R. Rogers Seeks and the Reason He Seeks Such Relief:

I, John R. Rogers, submit this application in acco rdance with the Reform Act, 112 P.L. 95 §§

331

- 334, seeking relief from any currently applicable FARs operating to prevent me, John R.

Rogers, contemplated commercial cinematic, academic and other flight operations within the

national airspace system. The Reform Act in Section 332 provides for such integration of civil

unmanned aircraft systems into our national airspace system as it is in the public’s interest to do

so. My, John R. Rogers ’

, ultra

- lightweight UAS meets the definition of “small unmanned

airc raft” as defined in Section 331 and theref ore the integration of my ultra

- light weight UAS is

expressly contemplated by the Reform Act. I would like to operate my ultra

- lightweight UAS3

3 prior to the time period by which the Reform Act requires the FAA to pr omulgate rules

governing such craft. Thereby, providing direct experience and valuable information for formal

regulation that can be administered uniformly to all related UAS aerial video and photography.

The Reform Act guides the Secretary in determining the types of UAS's that may operate safely

in our national airspace system. Considerations include: The weight, size, speed and over all

capabilities of the UAS's; w hether the UAS will be operated near airports or heavily populated

areas; and, Whether the U AS will be operated by line of sight. 112 P.L. 95 § 333 (a).

Each of these items reflect in favor of an exemption for me, John R. Rogers

. My UAS’s utilize

eight (8) or less rotating propellers for balance, control and stability. My UAS’s are equipped

wit h the following via video and data telemetry:

1) Altimeter

2) Attitude indicator

3) Ground Speed indicator

4) Magnetic compass

5) Heading indicator

6) Vertical speed indicator

7) Course deviation indicator

8) Radio magnetic indicator

9) GPS locati on

10) Battery consumption and Battery Left with approximate time.

11) Loiter and circle mode.

12) Auto safety or RTL (Return t o Launch)

13) Auto landing technology.

Each UAS weighing less than fifteen ( 15 ) pounds (far below the maximum 55 pound limi t);

Including camera(s) with or without gimbal (a camera stabilizer). As a licensed I consider safety

as foremost with each flight. My small unmanned aircraft is designed to hover in place, circle in

a specific place or loiter via GPS and can be ope rated in winds up to 30.4 knots (35mph) wind.

For safety, stability and fear of financial loss I will not fly in winds exceeding 21.7 knots (25

mph). Built in safety systems include a GPS mode that allows my UAS to hover/circle in place

or land when radio contro ls are released.

With three (3) modes to choose from, I will fly with the modes safest to complete the videos for

aerial videography/photography and have the ability to choose the safest, most reliable and stable

mode to prevent accident and hazard. When pilot communication from the radio control is lost,

UAS is designed slowly descend to point of takeoff and or to land at point of launch after

ascending to a pre

- set altitude to ensure the UAS will clear any obstacles that may be between

the takeoff point and the current position of the UAS. This failsafe altitude will not be set more

than 200ft and is determined before each flight.

I, John R. Rogers

, will not operate my UAS near airports, hospitals nor police heliports, and do

not operate near areas whe re general public is within fifty to one hundred (50

- 100) yards

depending on location, conditions and weather. I am constantly on alert for any manned aircraft

(police/medical helicopters, etc.) and prepared to land/abort immediately to the nearest and saf est4

4 ground point should a manned aircraft approach my location or I suspect manned aircraft may

approach near my location. My UAS’s are capable of vertical and horizontal operations, and is

flown only within my line of sight, as the remote control pilot. M y UAS's are also flown with a

second operator who aids in watching for any obstacles, including manned aircraft, within the

flight zone of the UAS. Utilizing battery power rather than combustible fuels, flights generally

last between three (10) to fifteen (25) minutes, with an altitude under on e hundred fifty (150)

feet. (3 ) Smart Mode includes, position hold, self

- leveling, altitude command, GPS, return home

feature, and safety control to return home or land in the event of communication interruption

betw een RC transmitter and UAS.

I, John R. Rogers

, utilize a fresh fully charged battery with each flight as a safety precaution; full

flight time limit for each battery is eight (8) to thirty ( 20 ) minutes as tested. I do not operate my

UAS at or below manufa cturer recommend minimum charge levels for operation; preferring to

remain well within a safe operating range to insure adequate communication between radio

control and UAS to eliminate potential for crash, loss of control or hazard. Reserve batteries are

at hand with each exercise to insure replacement for sufficient safe level of operation. I do not

believe in taki ng risk that may cause a crash that could create hazard to the

public/property/manned aircraft, and have no desire to lose my investment. I hav e clocked

numerous practice flights in remote areas as a hobbyist simulating flights for future commercial

use to gain familiarization with the characteristics of this specific UAS's performance under

different temperature and weather conditions. I also pr actice computerized simulated flights to

maintain adequate skills and response reflex time. All for the sake of safety.

I, John R. Rogers

, am extremely cautious when operating of my UAS/ultra

- lightweight

unmanned aircraft and will not “create a hazard to users of the national airspace system or the

public.” 112 P.L. 95 § 333 (b). Given the small size and weight of my UAS it falls well within

Congress’s contemplated safety zone when it promulgated the Reform Act and the corresponding

directive to integrate UAS's into the national airspace system. John R. Rogers’ UAS, used in

hobby flight, has a demonstrable safety record and does not pose any threat to the general public

or national security

.

IV. How John R. Rogers’ Request Will Benefit the Public As A W hole:

Aerial videography for geographical awareness, education, search and rescue, land management,

structure inspections and for real estate marketing has been around for a long time through

manned fixed wing aircraft and helicopters. For small budget c ompanies, average homeowners

and property owners the expense of such aerial videography is cost prohibitive. Only large

companies and high end Realtors or luxury homeowners can afford to absorb such expense;

depriving non

- luxury owners and lower budget com panies from a valuable marketing tool.

Manned aircraft pose a threat to the public through potential catastrophic crash that other

communities have experienced in the past with military aircraft, medical helicopters, and news

helicopters crashes. Each res ulting in loss of life and with c ombustible fuel that exploded and

burned on impact.5

5 My, John R. Rogers

, UAS poses no such threat since size and lack of combustible fuel alleviates

any potential threat to the public. Congress has already proclaimed that it is in the public’s

interest to integrate commercially flown UAS's into the national airspace system, hence the

passing of the Reform Act. Granting my, John R. Rogers’

, exemption request furthers the public

interest through academic/visual awareness of t he geographical benefits in and around the metro

Austin area. My ultra

- light weight UAS is battery powered and creates no emissions that can

harm the environment. The consequence of my ultra

- light weight UAS crashing is far less than a

full size helicopter or fixed wing aircraft; which are heavy, contain combustible fuel and can

cause catastrophic devastation to the public. The public’s interest is furthered by minimizing

ecological and crash threat by permitting aerial video/photo capture th rough my batter y operated

ultra

- lightweight UAS's.

Permitting me, John R. Rogers

, to immediately fly within national air space furthers economic

growth. Granting my exemption request substantially furthers the economic impact for the metro

Austin and surrounding commun ity for companies looking to relocate or build around the Austin

metro area as well as individuals looking to relocate for career advancement through academic

and geographical awareness. Both of which serve as a stimulus to the community.

V. Reasons Why John R. Rogers’ Exemption Wi ll Not Adversely Affect Safety o r How t he

Exemption Will Provide a Level of Safety At Least Equal To Existing Rule:

My, John R. Rogers’

, exemption will not adversely affect safety. Quite the contrary, for the

reasons stated p ermitting me, John R. Rogers

, to log more flight time in FAA controlled

airspace, with communication with the FAA, will allow me to contribute to the innovation and

implementation of new and novel, as of yet undiscovered safety protocols for Realtors, land and

structured owners. For development in cooperation with the FAA. In addition I, John R. Rogers

, submit the following representations of enhancements to current aerial videography and

photography: My UAS’s weigh less than seven (7) pounds complete with a an integrated ultra

light weight camera.; I only operate my UAS below 200 feet (well within the 400 foot

permissible ceiling set by the FAA Modernization and Reform Act of 2012); My UAS only

operate for 3

- 2 0 minutes per flight; I land my UAS prior to man ufacturer recommended

minimum level of battery power; I pilot my UAS through remote control only by line of sight;

and have live video to monitor video recording; I receive a live telemetry feed from my UAS

during all flights which include remaining batter y voltage, distance, altitude, and any anomalies

that may occur during flight;

My UAS’s Command and Control utilizes spread spectrum 2.4 Ghz

. - 2.485 Ghz

. frequencies in

accordance with CFR 47, Part 15 for model aircraft use.

My UAS’s camera system utili zes 5.725 Ghz

. - 5.875 Ghz

. frequencies in accordance with CFR

47, Part 15.

My UAS’s have a GPS controlled flight controller

- a flight safety feature whereby it hovers or

circles and then lands at the GPS takeoff point if communication with the remote con trol pilot6

6 is lost; I actively record and analyze flight data through the DJI phantom 3 flight controller app

to constantly update and enhance safety protocols; I only operate in reasonably safe environment

that are strictly controlled, are away from powe r lines, elevated lights, airports and actively

populated areas; I conduct extensive preflight inspections and protocol, during which safety

carries primary importance; I always obtain all necessary permissions prior to operation; and, I

have procedures in place to abort flights in the event of safety breaches or potential danger. My,

John R. Rogers’

, safety protocols provide a level of safety equal to or exceeding existing rules. It

is important to note that absent the integration of commercial UAS into ou r national airspace

system, helicopters are the primary means of aerial video and photography for community

awareness real estate, structured inspections, land management and search and rescue. While the

safety record of such helicopters is remarkably asto unding, there have been incidents involving

loss of life as well as extensive property damage; it is far safer to operate a battery powered ultra

lightweight UAS. First, the potential loss of life is diminished because UAS's carry no people on

board and I only operates my UAS in specific areas away from mass populations. Second, there

is no fuel on board a UAS and thus the potential for fire or explosions is greatly diminished.

Third, the small size and extreme maneuverability of my UAS allow me to remotely pilot away

from and avoid hazards quickly and safely. Lastly, given its small size and weight, even when

close enough to capture amazing images, my UAS need not be so close to the objects they are

focused on through the technology and use of post editing software allowing pan and zoom.

Accordingly, my UAS has been experimentally operated for familiarization/competency and will

continue to operate at and above current safety levels

.

VI. A Summary t he FAA May Publish in the Federal Register:

14 C.F.R. 21 and 14 C.F.R. 91: Airworthiness Certificates, Manuals and the l ike.

14 C.F.R. 21, Subpart H, entitled Airworthiness Certificat es, sets forth requirements for

procurement of necessary airworthiness certificates in relation to FAR §91.203(a)(1). The size,

weight and enclosed operational area of my, John R. Rogers’

, UAS permits exemption from Part

21 because my UAS meets (and exceeds) an equivalent level of safety pursuant to Section 333 of

the Reform Act. The FAA is authorized to exempt aircraft from the ai rworthiness certificate

requirement under both the Act (49 U.S.C. § 44701 (f)) and Section 333 of the Reform Act. Both

pieces of legislation permit the FAA to exempt UAS's from the airworthiness certificate

requirement in consideration of the weight, size, speed, maneuverability and proximity to areas

such as airports and dense populations. My, John R. Rogers’

, current and projected UAS's meet

or exceed each of the elements.

14 C.F.R. 91.7(a) prohibits the operation of an aircraft without an airworthiness certificate. As no

such certificate will be applicable in the form contemplated by the FARs, this Regulation is

inapplicable.

14 C.F.R. § 91.9 (b) (2) requires an aircraft flight manual in the aircraft. As there are no on board

pilots or passengers, and given the size of the UAS's, this Regulation is inapplicable. An

equivalent level of safety will be achieved by maintaining a safety/flight manual delineating

areas of where safety can be defined.7

7 The FAA has previously issued exemptions to this regulatio n in Exemption Nos. 8607, 8737,

8738, 9299, 9299A, 9565, 9565B, 10167, 10167A, 10602, 10700 and 32827.

14 C.F.R. § 91.121 regarding altimeter settings is inapplicable insofar as my UAS utilizes

electronic global positioning systems with a barometric sens or or controlled GPS “geo

- fencing”

14 C.F.R. § 91.203 (a) and (b) provides for the carrying of civil aircraft certifications and

registrations. They are inapplicable for the same reasons described above. The equivalent level

of safety will be achieved by maintaining any such required certifications and registrations by

me, John R. Rogers

.

B. 14 C.F.R. § 45.23: Marking of t he Aircraft. Applicable Codes of Federal Regulation require

aircraft to be marked according to certain specifications. My UAS can be marked with the

appropriate “N” number once this “N” number has been given.

C. 14 C.F.R. § 61.113: Private Pilot Privileges and Limitations: PIC. Pursuant to 14 C.F.R. §§

61.113 (a) & (b), private pilots are limited to non

- commercial operations. I, John R

. Rogers, t he

UAS Pilot in Command currently holds a Private Pilot license and a Texas driver's license. The

PIC must also meet the flight review requirements specified in 14 CFR § 61.56 in which the PIC

is rated on his/her pilot certificate as outlined in 14 C.F.R. § 61.

D. 14 C.F.R. 91.119: Minimum Safe Altitudes. 14 C.F.R. § 91.119 prescribes safe altitudes for

the operation of civil aircraft. It allows helicopters to be operated at lower altitudes in certain

conditions. My UAS will never operate at an altitude greater than 200’ AGL; safely below the

standard of 400’ AGL. I, John R. Rogers

, will however operate my UAS in safe areas away from

public and traffic, providing a level of safety at least equivalent to or below those in relation to

minimum safe altitudes. Given the size, weight, maneuverability and speed of my UAS, an

equivalent or higher level of safety will be achieved.

E. 14 C.F.R. 91.405 (a); 407 (a) (1); 409 (a) (2); 417(a) & (b): Maintenance Inspections.1,2,

Manual

The above

- cited Regulat ions require, amongst other things, aircraft owners and operators to

“have [the] 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 rep aired as

prescribed in part 43 of this chapter.

. . .” These Regulations only apply to aircraft with an

airworthiness certificate. They will not, therefore, apply to my, John R. Rogers’

, UAS. However,

as a safety precaution I inspect my UAS before and afte r each flight.

A Summary t he FAA May Publish in the Federal Register: A. 14 C.F.R. 21 and 14 C.F.R. 91:

Airworthiness Certificates, Manuals and t he Like. 14 C.F.R. 21, Subpart H, entitled

Airworthiness Certificates, sets forth requirements for procureme nt of necessary airworthiness

certificates in relation to FAR § 91.203(a) (1). The size, weight and enclosed operational area of

my UAS permits exemption from Part 21 because my, John R. Rogers’

, UAS meets an

equivalent level of safety pursuant to Section 333 of the Reform Act. The FAA is authorized to

exempt aircraft from the airworthiness certificate requirement under both the Act (49 U.S.C. §8

8 44701 (f)) and Section 333 of the Reform Act. Both pieces of legislation permit the FAA to

exempt UAS's from the airworthiness certificate requirement in consideration of the weight, size,

speed, maneuverability and proximity to areas such as airports and dense populations. My UAS

meets or exceeds each of the elements. 14 C.F.R. 91.7(a) prohibits the operation of an aircraft

without an airworthiness certificate. As no such certificate will be applicable in the form

contemplated by the FARs, this Regulation is inapplicable. 14 C.F.R. § 91.9 (b) (2) requires an

aircraft flight manual in the aircraft. As there are no pil ots or passengers, and given the size of

the UAS's, this Regulation is inapplicable. An equivalent level of safety will be achieved by

maintaining a manual. The FAA has previously issued exemptions to this regulation in

Exemption Nos. 8607, 8737, 8738, 929 9, 9299A, 9565, 9565B, 10167, maintenance program

that involves regular software updates and curative measures for any damaged hardware.

Therefore, an equivalent level of safety will be achieved. In summary, John R. Rogers seeks an

exemption from the follo wing Regulations: 14 C.F.R. 21, subpart H; 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);

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) and (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. § 91.409 (a ) (2); and, 14 C.F.R. §§ 91.417 (a) & (b) to commercially operate my,

John R. Rogers’

, small unmanned vehicle/lightweight unmanned aircraft vehicle in community

awareness, education, structural inspection land management, search and rescue and real estate

operations, and to develop economic platforms for the aforementioned to enhance the experience

of those seeking to relocate, rebui ld, reevaluate and to find in the metro Austin area.

F. Additional FAA Required Operating Conditions and Limitations

When not covered elsewhere in this Operations Manual, the following conditions and limitations

apply:

1. The UA must weigh less than 55 po unds (25kg), including energy source(s) and

equipment

2. The UA may not be flown at a speed exceeding a ground speed of 85 knots.

3. Flights must be operated at an altitude of no more than 500 feet above ground level

(AGL), as indicated by the procedures specif ied in the operator's manual. All altitudes

reported to ATC must be in feet AGL.

4. The UAS must be operated within visual line of sight (VLOS) of the PIC at all times.

This requires the PIC to be able to use human vision unaided by any device other than

cor rective lenses, as specified on the PIC's state driver’s license.

5. All operations must utilize a visual observer (VO). The VO may be used to satisfy the

VLOS requirement, as long as the PIC always maintains VLOS capability. The VO and

PIC must be able to c ommunicate verbally at all times.

6. If a discrepancy exists between these limitations and any procedure outlined elsewhere in

this operations manual, the conditions and limitations herein take precedence and must be

followed.9

9 7. Prior to each flight, the PIC must inspect the UAS to ensure it is in a condition for safe

flight. If the inspection reveals a condition that affects the safe operation of the UAS, the

aircraft is prohibited from operating until the necessary maintenance has been performed

and the UAS is found to be in a condition for safe flight. The Ground Control Station, if

utilized, must be included in the preflight inspection. All maintenance and alterations

must be properly documented in the aircraft records.

8. Any UAS that has undergone maintenan ce or alterations that affect the UAS operation or

flight characteristics, e.g. replacement of a flight critical component, must undergo a

functional test flight in accordance with the operator's manual. The PIC who conducts the

functional test flight must make an entry in the UAS aircraft records of the flight.

9. The operator must follow the manufacturer's UAS aircraft/component, maintenance,

overhaul, replacement, inspection, and life limit requirements. When unavailable, aircraft

maintenance/component/ove rhaul, replacement, and inspection/maintenance

requirements must be established and identified in the operator's manual. At a minimum,

the following must be included in the operator's manual:

a. Actuators / Servos

b. Transmission (single rotor)

c. Power plant (motors)

d. Propellers

e. Electronic speed controller

f. Batteries

g. Mechanical dynamic components (single rotor)

h. Remote command and control

i

. Ground control station (if used)

j. Any other components as determined by the operator

10. The Pilot in Command (PIC) must possess at least a sport pilot certificate and at least

a current state driver’s license. The PIC must also meet the flight review requirements

specified in 14 CFR § 61.56 in an aircraft in which the PIC i s rat ed on his/her pilot

certificate.

11. Prior to operations conducted for the purpose of motion picture filming (or similar

operations), the PIC must have accumulated and logged, in a manner consistent with10

10 14CFR § 61.51 (b), a minimum of 200 flight cyc les and 25 hours of total time as a UAS

rotorcraft pilot and at least ten hours logged as a UAS pilot with a similar UAS type

(single blade or multirotor). Prior documented flight experience that was obtained in

compliance with applicable regulations may s atisfy this requirement. Training,

proficiency, and experience

- building flights can also be conducted under this grant of

exemption to accomplish the required flight cycles and flight time. During training,

proficiency, and experience

- building flights, all persons not essential for flight operations

are considered non

- participants, and the PIC must operate the UAS with appropriate

distance from non

- participants in accordance with 14 CFR § 91.119.

12. Prior to operations conducted for the purpose of motion picture filming (or similar

operations), the PIC must have accumulated and logged, in a manner consistent with 14

CFR § 61.51 (b), a minimum of five hours as UAS pilot operating the make and model of

UAS to be utilized for operations under the exemption an d three take

- offs and three

landings in the preceding 90 days. Training, proficiency, experience

- building, and take

off and landing currency flights can be conducted under this grant of exemption to

accomplish the required flight time and 90 day currency. During training, proficiency,

experience

- building, and take

- off and landing currency flights, all persons not essential

for flight operations are considered non

- participants, and the PIC must operate the UAS

with appropriate distance from non

- participants in accordance with 14 CFR § 91.119.

13. Prior to any flight operations authorized by this grant of exemption, the PIC and

visual observer (VO) must have successfully completed a qualification process, as

outlined in the operator’s manual. As this is a req uirement stipulated by the operator, the

test must be developed and implemented by a qualified person designated at the sole

discretion of the operator. A record of completion of this qualification process must be

documented and made available to the Admin istrator upon request.

14. Prior to operations conducted for the purpose of motion picture filming (or similar

operations), a flight demonstration, administered by an operator

- approved and

- qualified

pilot must be successfully completed and documented. Th is documentation must be

available for review upon request by the Administrator. Because the knowledge and

airmanship test qualifications have been developed by the operator, and there are no

established practical test standards that support a jurisdiction al FAA FSDO evaluation

and approval of company designated examiners, the petitioner will conduct these tests in

accordance with the operator’s manual.

15. The UAS may not be operated directly over any person, except authorized and

consenting production pe rsonnel, below an altitude that is hazardous to persons or

property on the surface in the event of a UAS failure or emergency.

16. Regarding the distance from participating persons, the operator’s manual has safety

mitigations for authorized and consentin g production personnel. At all times, those

persons must be essential to the closed

- set film operations. Because these procedures are

specific to participating persons, no further FSDO or Aviation Safety Inspector (ASI)

approval is necessary for reductions to the distances specified in the petitioner’s manuals.11

11 This is consistent with the manned aircraft procedures described in FAA Order 8900.1,

V3, C8, S1 Issue a Certificate of Waiver for Motion Picture and Television Filming.

17. Regarding distance from non

- participating persons, the operator must ensure that no

persons are allowed within 500 feet of the area except those consenting to be involved

and necessary for the filming production. This provision may be reduced to no less than

200 feet if it would not adversely affect safety and the Administrator has approved it. For

example, an equivalent level of safety may be determined by an aviation safety

inspector’s evaluation of the filming production area to note terrain features, obstructions,

buildings, s afety barriers, etc. Such barriers may protect non

- participating persons

(observers, the public, news media, etc.) from debris in the event of an accident. This is

also consistent with the same FAA Order 8900.1, V3, C8, S1. 18. If the UAS loses

communicati ons or loses its GPS signal, the UA must return to a pre

- determined location

within the security perimeter and land or be recovered in accordance with the operator’s

manual.

18. If the UAS loses communications or loses its GPS signal, the UA must return t o a

pre

- determined location within the security perimeter and land or be recovered in

accordance with the operator’s manual.

19. The UAS must abort the flight in the event of unpredicted obstacles or emergencies in

accordance with the operator’s manual.

20. Each UAS operation must be completed within 30 minutes flight time or with 25%

battery power remaining, whichever occurs first

.

21. The operator must obtain an Air Traffic Organization (ATO) issued Certificate of

Waiver or Authorization (COA) prior t o conducting any operations under this grant of

exemption. This COA will also require the operator to request a Notice to Airman

(NOTAM) not more than 72 hours in advance, but not less than 48 hours prior to the

operation.

22. All aircraft operated in ac cordance with this exemption must be identified by serial

number, registered in accordance with 14 CFR part 47, and have identification (N

Number) markings in accordance with 14 CFR part 45, Subpart C. Markings must be as

large as practicable.

23. The ope rator must develop procedures to document and maintain a record of the UAS

maintenance, preventative maintenance, alterations, status of replacement/overhaul

component parts, and the total time in service of the UAS. These procedures must be

added to the o perator’s manual.

24. Each UAS operated under this exemption must comply with all manufacturer Safety

Bulletins.12

12 25. The operator must develop UAS technician qualification criteria. These criteria must

be added to the operator’s manual.

26. The prefligh t inspection section in the operator’s manual must be amended to include

the following requirement: The preflight inspection must account for all discrepancies,

i.e. inoperable components, items, or equipment, not covered in the relevant preflight

inspecti on sections of the operator’s manual.

27. Before conducting operations, the radio frequency spectrum used for operation and

control of the UAS must comply with the Federal Communications Commission (FCC)

or other appropriate government oversight agency re quirements.

28. At least three days before scheduled filming, the operator of the UAS affected by this

exemption must submit a written Plan of Activities to the local FSDO with jurisdiction

over the area of proposed filming. The 3

- day notification may be waived with the

concurrence of the FSDO. The plan of activities must include at least the following:

a. Dates and times for all flights

b. Name and phone number of the person responsible for the UAS filming

production under this grant of exemption

c. Name and phone number of the person responsible for the on

- scene operation

of the UAS.

d. Make, model and serial or N

- number of the UAS to be used

e. Name and certificate number of the UAS PIC's involved in the filming

production event

f. A statem ent that the operator has obtained permission from property owners

and/or local officials to conduct the filming production event; the list of those

who gave permission must be made available to the inspector upon request.

g. Signature of exemption

- holde r or representative

h. A description of the flight activity, including maps or diagrams of any area,

city, town, county, and/or state over which filming will be conducted and the

altitudes essential to accomplish the operation

29. The documents required under 14 CFR § 91.9 and § 91.203 must be available to the

PIC at the ground control station of the UAS any time the aircraft is operating. These

documents must be made available to the Administrator or any law enforcement official

upon request.

30. The UA S must remain clear and yield the right of way to all other manned operations

and activities at all times (including, but not limited to, ultralight vehicles, parachute

activities, parasailing activities, hang gliders, etc.).

31. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All

operations must be conducted under visual meteorological conditions (VMC). Flights

under special visual flight rules (SVFR) are not authorized.13

13 32. The UAS cannot be operated by the PIC from any mov ing device or vehicle.33. The

UAS may not be operated less than 500 feet below or less than 2,000 feet horizontally

from a cloud or when visibility is less than 3 statute miles from the PIC.

34. The UAS may not operate in Class B, C, or D airspace without written approval from

the FAA. The UAS may not operate within 5 miles of the geographic center of a non

towered airport as denoted on a current FAA

- published aeronautical chart unless a letter

of agreement with that airport’s management is obtained, and t he operation is conducted

in accordance with a NOTAM as required by the operator’s COA. The letter of

agreement with the airport management must be made available to the Administrator

upon request.

35. Any 1) incident, 2) accident, or 3) flight operation that transgresses the lateral or

vertical boundaries of the operational area as defined by the applicable COA must be

reported to the Federal Aviation Administration’s (FAA) UAS Integration Office (AFS

80) within 24 hours. Accidents must be reported to the National Transportation Safety

Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov. Further

flight operations may not be conducted until the incident, accident, or transgression is

reviewed by AFS

- 80 and authorization to resume oper ations is provided.

Currently, the aforementioned aerial videography/photography relies primarily on the use of

larger aircraft running on combustible fuel. Posing potential risk to the public. Granting my,

John R. Rogers’

, request for exemption will red uce current risk levels and thereby enhance

safety. My UAS craft do not contain potentially explosive fuel, is smaller, lighter and more

maneuverable than conventional video and photographic aircraft with much less flight time.

Further, I operate at lower altitudes and in controlled airspace eliminating potential public risk

flying to and from established airfields. I, John R. Rogers

, have been informally analyzing and

recording flight information and will compile safety protocols and the implementation of a flight

operations manual for usage that exceeds currently accepted means and methods for safe flight.

Formal collection of information shared with the FAA will enhance the FAA's internal efforts to

establish protocols for complying with the FAA Moderniz ation and Reform Act of 2012. There

are no personnel on board my, John R. Rogers

, UAS and therefore the likelihood of death or

serious bodily injury is significantly diminished. My, John R. Rogers operation of my UAS,

weighing less than forty (40) pounds a nd traveling at lower speeds within limited areas low to

the ground will provide an equivalent level of safety as that achieved under current FARs.

Accordingly I, John R. Rogers

, respectfully request that the FAA grant my exemption request

and am willing t o cooperate in sharing information to benefit the FAA, safety of manned aircraft,

and the general public at large.

Respectfully submitted,

John R. Rogers

1803 West Koenig Lane

Austin, Texas 78756

512

- 699

- 6468

1014

14 Appendix A



### List of Aircraft

No. Mak e and

Model Description Serial No. Registration

No.

1 DJI Phantom

3 Electric powered, 4 rotor small

unmanned multirotor

helicopter P77DCH1101

7420 N4 56PA15

15 DJI Phantom 3

The operation of the DJI Phantom 3 system is as follows.

1. Build Mater ials

I. Plastic

II. Aluminum

2. Motor Configuration

I. The Phantom 3 flight in a 4 motor quadcopter setup.

3. Payload

I. The Phantom 3 it’s own integrated camera.

II. Maximum All

- up Weight

- 4lbs

4. Maintaining the Phantom 3

Before each flight:

Check a ll hardware to ensure it is securely tightened.

Check that the motor is level and locked in place.

Check the propeller to ensure it is tight and there are no visible signs of cracks,

stress,

Check all wiring to motors, motor controllers, batteries, and fl ight controller for

signs of

Check all navigational lighting to ensure it is properly working.

After 45 hours of flight :

Remove and check all motors and motor mounts for signs of wear and tear.

Replace as necessary.

Remove motor controllers and visually inspect and check for damage. Replace as

necessary.

Remove flight controllers and visually inspect and check fo r damage. Replace as

necessary

. Replace if propeller is questionable.

Check for cuts, fraying, cracks, and/or loose/cold solder connections. Fi x before

flying.

Check for updates to flight controller firmware. If available, install and perform a

minimum of 15 test flights before conducting commercial work.16

16 A ppendix B

Personal Protocols/Controls/Flight Manual

Protocols and Controls, John R R ogers, Austin TX

.

Safety for public on the ground as well as manned aircraft above is an essential and utmost

consideration for aerial videos and photography. As such, safety protocols and controls must be

implemented through pre

‐ flight preparation and du ring flight. Pre

‐ Flight Protocol:

1. Check batteries with voltage meter to insure fully charged and ready for use.

2. Inspect batteries for damage or leakage that may affect proper operation.

3. Inspect propellers for cracks, chips or damage that may cause su dden loss of propulsion

or

4. Unmanageable or uncontrolled flight.

5. Check all GPS and Telemetry connections prior to flight.

6. Check weather forecasts for wind advisory or other conditions that my impact flight.

7. Consult Sky Vector aeronautical Charts (Sky vector.com) for airport vicinity and flight

paths of possible air traffic.

8. Contact respective airport to advise of estimated flight time, estimated flight duration,

estimated elevation of flight, and any other pertinent information.

Inspect flight area for:

1. Vicinity of public safety helipads/heliports

2. Vicinity of medical helipads/heliports

3. Vicinity of light poles vicinity or utility wires

4. Vicinity of trees flocks of birds that may cause interference and potential flight impact

5. Vicinity of any ele vated obstructions that may pose potential flight hazard

6. Vicinity of roadways with moderate to heavy traffic that can be distracted public

Gatherings that may attract viewers

.

7. O ptional point of control for best visual site of UAS while in flight ; e merge ncy landing

areas17

17 Takeoff and landing:

Inspect area for best and safest point of takeoff and landing

If in a subdivision or area that is within 150 feet of a residential street, post warning

Sign(s)/stand(s) "Attention Aerial Photography In

- Progress

‐ Remain Back 150 Feet "

Flight Protocol: takeof

f and land from same location ( have alternate landing areas in case of

emergencies) remain alert to birds, sound or aircraft, curious public, and approaching vehicles do

not allow anyone to engage in conversa tion or distract the remote control pilot restrict flight to

minimal elevation sufficient to acquire desired results remained prepared for emergency landing

at all times pay attention to flight time

– warning meter for low voltage.

Set voltage meter alar m for low voltage and flight timer as a safety alert land UAS and shut

down propulsion immediately following landing

– priority of disconnecting batteries

Post flight:

1. Disconnect battery to prevent accidental activation of propulsion system

2. Sec ure UAS in a safe location

3. Remove all warning signs from public access areas Emergency or Suspected Hazard:

Immediate land UAS at safest and closet ground location in the event

Manned aircraft is heard or seen in vicinity of flight

There is a pub lic gathering within established safety boundary wanting to observe flight

Pilot is being distracted from focusing on flight and safety

Sudden change in weather (wind bursts)

Sudden increase in vehicular traffic in vicinity of flight

Birds enter into p roximity of flight

Any sudden unsafe event that can cause collision, distraction or interruption of control

Safety for public on the ground as well as manned aircraft above is an essential and utmost

consideration for aerial videos and photography.

Ma intaining a record of safe flight for FAA request and for determining future UAS safety

protocols is imperative.

Date:____________________

_____________________________________________________ Location:____________________

______________________________ ____________________18

18 P re

‐ flight Inspection:

o Yes o No

Comment:

__________________

____________________________________________________

Elements:

_______________________________________________________________________

Proximity to airport:

_________________ __________________ ___________________ (see attached map pinpointing approximate location of flight)

Airport notified: No Yes

Date:_______________ Time:

______________

Phone Number:

__________________________________ Contact Name:___________________________________

N earest major intersection:

______________________________________________________________ _________ _

Proximity to medium traffic road:

__________________________ _____________________________________________ _

Proximity to heavily traveled roadway road:

_________________________ ________________________ ______________________ _

Proximity to congested population:

________________________________________________________ _______________ _

Approx. Takeoff Time : GMT:_______________________________________________

Weather : Good/ Fair / Poor Comment :

_________________________________

Visibility : Good/ Fair/ Poor Comment :_________________________________

Wind Speed ___mph ___Gusts/MPH

___avg/MPH Comment :_______________

Approx. Landing Time: GMT:_______________________________________________

Es timated Elevation Ground level:____________________________________________

Safety Concerns:

____________________________________ ______________________19

19 Additional Comments:_____________________________________________________

S ea L evel:

________________________________________________________________20

20 Appendix C

Aircraft Manuals

This Appendix includes UAS manufacturer's user manuals, maintenance instructions, and

illustrated parts catalogs. These manuals may be attached to the docket when submitted.

Information regarding design, aircraft performance, fail

- safe features, operating limitations,

normal and emergency procedures, and maintenance and inspection proce dures is contained

within the manuals and supplemental information documents listed below:

1

. Phantom 3 Professional Manual V1.0

2

. Phantom 3 Intelligent Flight Battery Safety Guidelines v1.0 (EN)

For more information or questions about this manu al please contact:

John R Rogers

1803 W Koenig Ln

Austin, TX 78756

(512) 699

- 6468