Ralph J. Boddicker Jr

2000 High St Unit 222

Des Moines, IA 50309

April 14th, 2015

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave., SE 

Washington DC 20590 

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

Aviation Regulations from: 14 CFR 21 subpart H; 14 CFR 45.23(b); 14 CFR 61.113(a); 14 CFR 91.7(a); 

14 CFR 91.9(b)(2); 14 CFR 91.103; 14 CFR 91.109; 14 CFR 91.119(c); 14 CFR 91.121; 14 CFR 

91.151(a); 14 CFR 91.203 (a) and (b); 14 CFR 91.405 (a); 14 CFR 91.407 (a) (1) 14 CFR 91.409 (a)(1) and 

(2); 14 CFR 91.417(a) and (b) 

Dear Sir or Madam: 

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the “Reform Act”) and 14 

CFR Part 11, Ralph J. Boddicker Jr., operator of Small Unmanned aircraft Systems (“sUAS”), hereby 

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

operation of its sUAS, so long as such operations are conducted within and under the conditions outlined 

herein or as my be established by the FAA as required by Section 333. 

Commercial operation sUAS, as described herein, which are equipped with cameras and sensors, would 

operate in the following manner: 

1. Aerial photography and/or video for public and/or private use including real estate, architecture, land 

surveying, engineering and other related professional activities. 

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

cinematography and news gathering. 

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

local government authority. 

4. Aerial video/photography or providing live video feed to assist with search and rescue operations in 

cases of an emergency or natural disaster only when the local authorities or government has requested it by 

contract or donation. 

5. The ability to offer training to persons individually or belonging to both private and/or public 

organizations that have interests in the use and application of sUAS for the purpose of the safe operation of 

sUAS to enhance the safety of the National Airspace System (NAS) as well as for the protection of the 

persons and property. 

U.S. Department of Transportation 

April 14th, 2015

As described fully below, the requested exemption would permit the operation of sUAS under controlled 

conditions in the NAS that would be a) limited b) controlled c) predetermined and d) will provide safety 

enhancements to the already safe operations in the industry presently using conventional aircraft. Approval 

of this exemption would thereby enhance safety and fulfill the Secretary of Transportation’s (the FAA 

Administrator’s) responsibilities to “....establish requirements for the safe operation of such aircraft 

systems in the national airspace system.” 

The name and address of the applicant is: 

Attn: Ralph J. Boddicker Jr.

Ph: 515-991-2257
Email: ralphboddicker@gmail.com

Address: 2000 High St Unit 222, Des Moines, IA 50309

Regulations from which the exemption is requested: 

14 CFR Part 21 subpart H 

14 CFR 45.23 (b) 

14 CFR 61.113 (a) 

14 CFR 91.7 (a) 

14 CFR 91.9 (b) (2) 

14 CFR 91.103 

14 CFR 91.109 

14 CFR 91.119 (c) 

14 CFR 91.121 

14 CFR 91.151 (a) 

14 CFR 91.203 (a) & (b) 

14 CFR 91.405 (a) 

14 CFR 91.407 (a) (1) 

14 CFR 91.409 (a) (2) 

14 CFR 91.417 (a) & (b) 

My sUAS are multi-rotor craft weighing no more than 55lbs including payload. Under normal conditions 

they operate at speeds of no more than 50kts and have the ability hover and move along a vertical and 

horizontal plane simultaneously. They will operate in line of sight and will operate within a closed off and 

predetermined area owned and/operated by the property representative. 

Given the small size of the sUAS and the controlled environment provided the proposed operations will 

adhere to the Reform Act’s safety requirements. The approval of this application presents no national 

security issues. Regarding the level of safety surrounding the proposed operations and the public benefit, 

reduction in environmental impacts, including but not limited to reduced emissions and noise, the grant of 

the requested exemption is in the public interest. Accordingly the applicant requests that the FAA grant the 

requested exemption with minimum delay. 

AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY 

The operation limitations proposed for an equivalent or higher level of safety because operations will 

further enhance the safety of the persons and/or property using conventional aircraft. 

These limitations and conditions to which the applicant agrees to adhere to when conducting commercial 

operations under the FAA issued exemption as set forth in the Flight Operations Manual (FOM) include: 

1. The sUAS will weigh less than 55 lbs. 

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

3. Maximum flight time for each operational flight will be 30 minutes. Flights will be terminated at 25% 

battery power reserve or 30 minutes of flight time whichever occurs first. 

4. Flights will be operated at an altitude of no more than 400 feet Above Ground Level (AGL) and not 

more than 200 feet above an elevated platform from which filming is planned. 

5. Minimum crew for each operation will consist of the sUAS Pilot, the Visual Observer (VO) and may 

include but not limited to a Camera Operator.

6. The sUAS pilot will be a designated Pilot in Command (PIC) and hold a current Third or higher Class 

Medical Certificate, along with a valid state driver’s license. If the PIC feels another operator to be 

qualified with the necessary skills to be PIC & possess a Third or higher Class Medical and a valid state 

driver’s license, that person may be designated PIC provided they have a minimum of 20 hours of flight 

time with the sUAS. 

7. A briefing will be performed regarding the planned sUAS operations prior to each day’s flight consisting 

of all the days’ production activities. 
8. The operator will file FAA Form 7711-1, or its equivalent, as modified in light of the requested 

exemption, with the appropriate local Flight Standards District Office (FSDO) no more than 72 hours but 

no less than 48 hours from planned operation. 

9. The operator will obtain verbal/written consent of all persons involved with the planned operation and 

ensure that only consenting persons will be allowed within 100 feet of the flight operation, and the radius 

may be reduced to 30 feet based upon an equivalent level of safety determination, as required under the 

FOM. With the advanced permission of the FSDO, operations at closer range may be approved. 

10. The PIC and VO will have been trained in operation of sUAS and receive up-to-date information for the 

particular sUAS to be operated. 

11. The PIC and VO will be able to communicate by voice, radio, and/or text at all times. 

12. Written and/or verbal permission and permits will be obtained from territorial, state, county or city 

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

13. If the sUAS loses communications or loses GPS signal, the sUAS will have the capability to return to a 

pre-determined location within a designated location and land autonomously. 

14. The sUAS will have the capability to abort a flight in case of unpredicted obstacles, weather, 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 sUAS. In all cases, an 

analysis of these criteria demonstrates that the sUAS 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 and 

designated area. Unlike other civil aircraft, operations under this exemption will be tightly controlled and 

monitored by both the operator and under the requirements and in compliance with local public safety 

requirements. The FAA will have advance notice of all operations. These safety 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 sUAS, 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 sUAS will have 

no airworthiness certificate, an exemption may be needed as the sUAS will have no entrance to the cabin, 

cockpit or pilot station on which the word “Experimental” can be placed. Given the size of the sUAS, twoinch 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 sUAS marked on its fuselage 

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

identification of the sUAS as “Experimental.” 
14 C.F.R. § 61.113 (a): Private Pilot Privileges and Limitations: Pilot in Command. 

Pursuant to 14 CFR 61.113 (a), no person who holds a private pilot certificate may act as a pilot in 

command of an aircraft that is carrying passengers or property for compensation or hire. Our sUAS do not 

carry any pilots or passengers nor property therefore I am seeking an exemption to 14 CFR 61.113(a). 

Although helpful, a pilot’s license will not ensure remote control piloting skills. The risks attendant to the 

operation of sUAS is far less than the risk levels inherent in the commercial activities outlined in 14 CFR 

61. I feel the operation and limitations set forth in the FOM will equate to the safe operation of the sUAS. 

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 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. 

14 C.F.R. § 91.103: Preflight Action. 

This regulation requires each pilot in command to take certain actions before flight to insure the safety of 

flight. As FAA approved rotorcraft flight manuals will not be provided for the aircraft an exemption will be 

needed. The PIC will take all actions including reviewing weather, flight battery requirements, landing and 

takeoff distances and aircraft performance data before initiation of flight. 

14 C.F.R. §91.109: Flight Instruction. 

Section 91.103 provides that no person may operate a civil aircraft (except a manned free balloon) that is 

being used for flight instruction unless that aircraft has fully functioning dual controls. sUAS 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. The equivalent level of safety provided by the fact that 

neither a pilot nor passengers will be carried in the aircraft and by the size and speed of the aircraft. 

14 C.F.R. §91.119: Minimum Safe Altitudes. 

Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119 (d) allows helicopters 

to be operated at less than the minimums prescribed, provided the person operating the helicopter complies 

with any route or altitudes prescribed for helicopters by the FAA. As this exemption is for a sUAS that is a 

helicopter and the exemption requests authority to operate at altitudes up to 400 AGL, or not more than 200 

above an elevated platform from which filming is planned, an exemption may be needed to allow such 

operations. As set forth herein, the sUAS will never operate at higher than 400 AGL with the exception that 

in circumstances where the sUAS is used to survey or photograph a structure whose height exceeds 400 

feet AGL, the sUAS will not be operated more than 100' above the highest point on the structure. It will 

however be operated in a restricted area with security perimeter, where buildings and people will not be 

exposed to operations without their pre-obtained consent. 
The equivalent level of safety will be achieved given the size, weight, speed of the sUAS 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 operating at or below 500 AGL. 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 safety check list and live flight data monitoring, confirming the altitude of the launch site shown on the 

GPS altitude indicator before flight. 

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

Section 91.151 (a) prohibits an 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 30 minutes of powered flight. To meet the 30 

minute reserve requirement in 14 CFR §91.151, sUAS flights would be limited to approximately 10 

minutes in length. Given the limitations on the sUAS’s proposed flight area and the location of its proposed 

operations within a predetermined area, a longer time frame for flight in daylight or twilight VFR 

conditions is reasonable. 

Applicant believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. 

Operating the small UAS, in a tightly controlled area where only people and property owners or official 

representatives who have signed waivers will be allowed, with less than 30 minutes of reserve fuel, does 

not engender the type of risks that Section 91.151(a) was intended to alleviate given the size and speed of 

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

the exemption will be granted. Applicant believes that an equivalent level of safety can be achieved by 

limiting flights to 30 minutes or 25% of battery power— whichever happens first. This restriction would be 

more than adequate to return the sUAS to its planned landing zone from anywhere in its limited operating 

area. 

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 sUAS 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. 

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

will not apply to the applicant. Maintenance will be accomplished by the operator pursuant to the flight 

manual and operating handbook. An equivalent level of safety will be achieved because 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 sUAS can land immediately and will be operating from no 

higher than 400 feet AGL. The operator will ensure that the sUAS is in working order prior to initiating 

flight, perform required maintenance, and keep a log of any maintenance performed. Moreover, the 

operator is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy 

condition to provide the equivalent level of safety. 

An equivalent level of safety will be achieved because maintenance and inspections will be performed in 

accordance with the sUAS Manufacturer's Manual, as referenced in the Aircraft Operations Manual 

(AOM). As provided in the FOM, the operator will ensure that the sUAS is in working order prior to 

initiating flight and perform required maintenance needed. 

Satisfaction of criteria provided in Section 333 of the Reform Act of 2012 provide more than adequate 

justification for the grant of the requested exemptions allowing the commercial operation of the applicant’s 

sUAS. 

Sincerely,

Ralph J. Boddicker Jr.