June 17, 2015

U.S. Department of Transportation Docket Management System
Room W12-140
1200 New Jerse y Ave ., SE Washington, DC 20590

Subjec t: Ex empt ion reque st under Section 333 of the F AA R eform Act.

Dear Sir/Ma’am:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 Dobbs
Administrations , the operator of small Unmanned Aircraft Systems (UAS) seeks an exemption
from the Federal Aviation Regulations (FARs) 14 CFR §§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 91.7(a), 91.119(c), 91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), a nd 91.417( a) a nd (b), to t he extent necessar y to allow R PA/UAS
Consulti ng LL C to operate a UA S to perform aerial data c ollection.

You'll find that our request is similar to relief previously requested in Grant of Exemption Nos. 11062, 11109, 11112, 11213 , 11398 and 11277

.

The requested exemption would permit Dobbs Administrations to commercially operate UAS for the following purposes:

 Airborne photography and videography

 Emergency services support

 Search and rescue

 Emergency Services training

 UAS operations training

 UAS capability demonstrations

Furthermore, Dobbs Administrations wi ll research, develop, and commercial operate UAS to conduct:

 Agriculture and land surveying

 News gathering and reporting

 Railroad inspections

 Bridge inspections

 Infrastructure inspection

 Tall structure inspections (smokestacks, cell phone towers, windmills, and electrical transmission towers, ect.)

The primary purpose of Dobbs Administrations is to assist other industries by providing
safe a nd efficient UAS s upport. The uses of U AS to perform airborne phot ography a ndvideograph y a s we ll a s aerial inspections and surveyin g h a ve two major b enefits. F irst, small

UA S a re considerabl y sa fer than usin g manne d aircraft in t he pr eviousl y m entioned tasks, and
also reduce s the fa ll r isk of wor kers. Second, UA S a llows the completion of man y t asks at a
fraction of the cost us ing traditional means. Granti ng thi s exemption is in th e publi c int erest because it will dramaticall y e nhanc e sa fety, lower-cost, and impr ove the efficienc y of m any industries.

Dobbs Administrations will conduct the aforementioned tasks by using the following
small sized UAS: DJI Phantom 2 vision+, DJI Phantom 3 professional, DJI Inspire 1, DJI S1000,
the ASCTEC Falcon 8 and the 3DR Solo

. The listed UAS are very small, all weighing less than 25 pounds, and have advanced navigation systems and automated control features that enhance safety. With the exception of the DJI Phantom 3, which is merely an improvement of the
Phantom 2 vision+, all of the UAS there will be operated with this exemption have been previously approved in other Section 333 exemption requests.

All of Dobbs Administrations operations will strictly adhere to FAA regulations with safety being the number one priority. All operations will be conducted via unaided visual line of sight below 400 feet AGL and outside of any controlled airspace unless the controlling agency gives express permission.

Dobbs Administrations respectfully submits a grant of exemption is in the public interest
because the use of small UAS in lieu of comparatively more expensive and hazardous fixed and rotary wing aircraft or other conventional manned methods of inspection greatly enhances efficiency and achieves a level of safety that is significantly higher. Furthermore, Dobbs
Administrations will assist other industries in the safe application of UAS and promote the
benefits of safe UAS operations. Approval of this exemption would enhance safety and fulfilled the Secretary of Transportation's responsibility under the section 333(c) of the FAA
Modernization and Reform Act of 2012 to “establish requirements for the safe operation of such aircraft systems in the national airspace system.”

Name and address of the applicant:

Robert Dobbs
Dobbs Administrations Cell: ( 405 ) 408-3280
Email: Rdobbs@dobbsadmin.com
Address: 13100 S. Rockwell Ave Oklahoma City, OK 73173JUSTIFICTION UNDER SECTION 333

According to the FAA’s Public Guidance for Petitions for Exemption Filed under Section 333

“ Section 333 grants the Secretary of Transportation the authori ty to determine if an unmanned aircraft system, as a result of its size, weight, speed, operational capability, proximity to airports and populated areas, and operation within visual line of sight does not create a hazard to users of the national airspace system or the public or pose a threat to national security ” . RPA/UAS Consulting LLC submits that the small size and weight of the purposed UAS coupled with the fact that the operations will be conducted at low altitudes, slow airspeed

, and within visual l ine of sight of the operator ; our operations pose no potential hazard to the national airspace system, general public

, or present any threat to national security.

Airworthiness of the UAS

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 of the particular UAS. RPA/UAS Consulting LLC purposes using DJI Phantom 2 vision+, DJI Phantom 3 professional, DJI Inspire 1, DJI S1000, and the ASCTEC Falcon 8. The proposed systems have the inherent advantage of being small in size and battery

- operated therefore do not carry flammable fuel , this significantly
reduc es any pot ential damage in the event of a mishap. RPA/UAS Consulting LLC will operate the proposed UAS below 400 feet AGL

, at speeds less than that recommended by the manufacturer, and at all times less than 50 knots. Operations will only be conducted in during dayl ight hours, in uncontrolled airspace

, unless specific permission is granted by the controlling

agency , and within visual line of sight of the operator

.

With the exception of the DJI Phantom 3, which is merely an improvement of the DJI Phantom 2, all of t he UAS th at will be operated with this exemption have been previously approved in other Section 333 exemption requests. The DJI Phantom 2 vision+, DJI Inspire 1, DJI S1000 were approved for use in Exemption No. 11398. The ASCTEC Falcon 8 was approved in Exemption Number 11277. An analysis of these criteria demonstrates that the purposed 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 or helicopter) operating with an airworthiness certificate without the restrictions and conditions proposed.

Operation of the UAS

RPA/UAS Consulting LLC will ensure that the exemption does not adversely affect safety and will operate at a level of safety at least equal to existing rule s by operating with the following
limitations and conditions:

 All operations will strictly adhere to manufactures owners, operators and maintenance
manual.

 All operations will occur in class G airspace, unle ss specifically authorized by the controlling authority. All operations will be conducted during daylight hours

.

 All operations will occur be low 400 feet AGL.

 All operations will be conducted and visual meteorological conditions with visibility of at
least three nautical miles.

 All operations will be conducted with at least 500 feet below clouds and with a horizontal separation of at least 2000 feet.

 At no time will the operator allow the aircraft within 500 feet of nonparticipating person

, structure

, or ve hicle.

 Preflight operations will be conducted in accordance with the manufacturer's
recommendation and preflight checklist.

 All maintenance will be conducted in accordance with manufacturers recommendations and documented in the aircraft logbook

PIC Requi rements

RPA/UAS Consulting LLC respectfully submits that the operator requirements should take into account the advanced internal navigation and autopilot systems of the proposed UAS. The DJI and ASCTEC systems both have a high degree of control and are e xtremely stable even in high wind environments. Both companies incorporate various built

- in capabilities that limit the potential for operations outside of the aircraft capability.

The pilot in charge (PIC) is solely responsible for the safe operation of the UAS. RPA/UAS Consulting LLC will only use PIC’s who possess and FAA commercial or private pilot's license and a class III medical. RPA/UAS Consulting LLC will also ensure that all PICs comply with manufacturer training requirements, and have been deeme d safe and proficient by the chief pilot.

The regulations from which the exemption is requested are as follows:

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. 61.133(a); 14 C.F.R. 91.7(b); 14 C.F.R. 91.9(b)(2);
14 C.F.R. 91. 109(a); 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. 91.407(a)(1); 14 C.F.R. 91.409(a)(2); 14 C.F.R. 91.417(a) & (b).14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 CFR § 91.203(a)(1)

Subpart H, 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 ut ilized by RPA/UAS Consulting LLC

, 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. Our
small UAS's wil l be operated at low speed in a controlled environment, away from airports and any densely populated area. An analysis of these criteria demonstrates that the UAS's 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 helicopter) operating with an airworthiness certificate without the restrictions and conditions proposed.

The UAS to be operated is less than 25 lbs. fully loaded, carries neither a pilot nor passenger, carries no flammable liquid fuels, and operates exclusively within a secured area. Like other civil aircraft, operations under this exemption will be tightly controlled and monitored by the PIC

. If required, the FAA and general public will have advance notice of all operations

.

These safety enhancements, which already apply to civil aircraft operated in connection
with private property, industrial sites , railroad yards and the like 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 and the NAS posed by the UAS, due to its size, speed of operation, location of operation, lack flammable liquid fuels, and limited ability to carry an external load.

14 C.F.R. § 45.23(b): Marking of the Aircraft

This regulation requ ires certain experimental, provisionally certificated aircraft, or light

sport category aircraft to be marked with letters between 2 inches and 6 inches high "limited," "restricted," "light

- sport," "experimental," or "provisional," near each entrance to a cabin, cockpit, or pilot station.

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 siz e of the UAS, two

- inch lettering will be impossible. The word "Experimental" will be placed on the fuselage in compliance with §45.29 (f).

The equivalent level of safety will be provided by having the UAS marked on its fuselage as required by §45.29 (f) where the pilot, observer and others working with the UAS will see the identification of the UAS as "Experimental." The FAA has issued the following exemptions to this regulation: Exemptions Nos. 10700, 8738, 10167 and 10167A.14 C.F.R. § 61.113(a) & ( b); 61.133(a): Private Pilot Privileges and Limitations; Pilot in

Command; Commercial Pilot Privileges and Limitations

.

Part 61.113 (a) states that no person who holds a private pilot certificate may act as pilot in command of an aircraft that is carryin g passengers or property for compensation or hire; nor may that person, for compensation or hire, act as pilot in command or an aircraft. Part 61.113 (b) states that a private pilot may, for compensation or hire, act as pilot in command of an aircraft in

c onnection with any business or employment if: (1) The flight is only incidental to that business or employment; and (2) The aircraft does not carry passengers or property for compensation or hire. Section 61.133(a) requires an individual with a commercial pilot’s license to be pilot in
command of an aircraft for compensation or hire

. RPA/UAS Consulting LLC proposes that all operations require that the PIC must either hold an either a Commercial or Private Pilot Certificate issued by the FAA. Since there are currently no means available for the pilot of a UAS to gain the experience in an equivalent category and class in order to apply for a commercial UAS pilot's license, using pilots qualified
under other categories and classes meets or exceeds the present level of safety provided under 14 C.F.R. § 61.113(a) & (b) . Given the unique nature of commercial UAS operations we do not
believe that it rises to the level of requiring a commercial pilot to operate the aircraft under§ 61.133(a).

14 C.F.R. § 91. 7(a): Civil aircraft airworthiness.

This regulation requires that no person may operate a civil aircraft unless it is in airworthy condition. Should the exemption be granted allowing commercial operation of the UAS without an airworthiness certificate, no standard will exist for airworthiness of the UAS. Given the size of the aircraft and the requirements published by the manufacture for maintenance
and the use of safety checklists 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.

The UAS, given its size and configuration has no ability or place to carry such a flight manual on the aircraft, not only because there is no pilot on board, but because there is no room or capaci ty to carry such an item on the aircraft.

The equivalent level of safety will be maintained by keeping the flight manual at the ground control point where the pilot flying the UAS will have immediate access to it. The FAA has issued the following exempti ons 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 take certain actions before flight to
ensure the safety of flight. An exemption is needed from this requirement as the pilot will take separate preflight actions, including checking for weather conditions, checking flight battery requirements, checking takeoff and landing distances, and all other action s in the m anufactures preflight checklist . These actions will provide an equivalent level of safety.14 C.F.R. § 91.109(a) & 91.319(a)(1): Flight Instruction

These regulations provide 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.

By design, UASs and remotely piloted aircraft do not have fully functional dual controls. Flight control is accomplished thro ugh the use of a control station that communicates with the aircraft via radio communications. The FAA has previously approved exemptions for aircraft without fully functional dual controls. The equivalent level of safety provided by the fact that neither a pi lot nor passengers will be carried in the aircraft, the ability to control the UAS via radio signals from the controller, and by the size and speed of the aircraft.

14 CFR § 91.119: Minimum Safe Altitudes

Section 91.119 establishes safe altitudes for ope ration of civil aircraft. Specifically, 91.119(c) limits aircraft flying over areas other than congested areas to an altitude of 500 feet above the surface, except over open water or sparsely populated areas. In those cases, the aircraft may not be operat ed closer than 500 feet to any person, vessel, vehicle, or structure.

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 . Compared to flight operations with aircraft weighting far more than the maximum 55 lbs. proposed herein and carrying flammable fuel, any risk associated with our operations is far less than those present ly presented with helicopters and other conventional aircraft operating at or below 500 AGL. In addition, the low

- altitude operations of the UAS will ensure separation between these UAS operations and the operations of conventional aircraft

.

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 appro priate altimeter setting available before departure." As the UAS does not have a barometric altimeter, but instead a GPS altitude read out, an exemption is needed. An equivalent level of safety will be achieved by the operator confirming the altitude o f 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

This regulation prohibits an individual from beginning “a flight in an airplane under VFR conditions unless (consid ering 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

. ”An equivalent level of safety can be achieved by limiting flights to what the manufacturer

recommends , or enough battery reserve to ensure that the UAS lands at the ground station with at least 25% of battery power (as determined by the o nboard monitoring system and the pilot), whichever happens first. This restriction would be more than adequate to return the UAS to its planned landing zone from anywhere in its limited operating area. Similar exemptions have been granted to other operatio ns, including Exemptions 2689F, 5745, 10673, and 10808.

14 C.F.R. § 91.203 (a) & (b): Carrying Civil Aircraft Certification and Registration

This regulation requires : “ no person may operate a civil aircraft unless it has [

. . . ] an
app ropriate 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 c ockpit entrance so that it is legible to passengers or crew ”

.

An equivalent level of safety will be achieved by keeping these documents at the ground control point where the pilot flying the UAS will have immediate access to them. The FAA has
issued numer ous 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

Section 9 1.405(a) requires 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 pre scribed in part 43 of this chapter . . . .” Section 91.407 similarly makes reference to requirements in Part 43; Section 91.409(a)(2) requires an annual inspection for the issuance of an air worthiness certificate. Section 91.417(a) requires the owner or operator to keep records showing certain maintenance work that has been accomplished by certificated mechanics, under Part 43, or licensed pilots and records of approval of the aircraft for return to service.

Given that these section and Part 43 apply onl y to aircraft with an airworthiness certificate, these sections will not apply to RPA/UAS Consulting LLC UAS. An equivalent level of safety, given the small size and unique characteristics of the aircraft, will be maintained by the operator accomplishing a nd documenting all required maintenance specified by the
manufacturer.