**'~ ~/**  ..--.._.. -T·**·r~** ITr;,r_**~ ·-.~** -.,...:...'**,.~·-;~--~ ·,-:':.~:-.**  us Department of Transportation Exemption Request Pursuant to Section 333 ofthe FAA ·.:.;:.•**:~_'·**·..,,**~ ,_··~·'.~.-.-c.:=~.~·~-~:~~··~:**  Reform Act and Part 11ofthe Federal Aviation October 8, 2015 Gerald Kerr GJKerr consulting LLC 9828 Whisperwood Ln Brighton, Ml48116-8859 gerald.kerr48@gmail.com 810-533-0174U.S Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington oc 20590**i~~~ ~~1** \5 :-_J**~~:**S2 Re: Exemption Request Pursuant to Section 333 ofthe FAA Reform Act and Part 11ofthe Federal AviationRegulations from: 14 CFR 21 subpart H;14 CFR 45.23(b); 14 CFR 61.113(a) and (b); 14 CFR 91. 7(a); 14 CFR 91.9(b)(2); 14 CFR 91.1 03; 14 CFR 91.1 09; 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 Siror Madam: Pursuant to Section 333 ofthe FAA Modernization and Reform Actof 2012 (the "Reform Act") And 14 CFR Part 11of Unmanned Aircraft Systems (UAS), Gerald Kerr hereby applies for ·an exemption from the listed Federal Aviation Regulations ("FARs") to allow commercial operation of Designated UAS, provided such operations are conducted within and under the conditions outlined herein oras may be established bythe FAA as required by Section 333.

Thank youin advance for your consideration. Commercial operation ofan UAS, as described herein, which are equipped with camera(s) and sensors, would provide professional services inthe following areas: 1. Search and Rescue with Thermo Imager 2. Cell Towers 3. Storm damage 4. Endangered Osprey Eagles I OffspringAs described fully below, the requested exemption would permit the operation of designated UAS asset forth inthis document under controlled conditions inthe NAS that would bea) limited b) controlled c) predetermined andd) safe. Approval of this exemption would increase public awareness of UAS operations and enhance safety toaidin fulfilling the Secretary of Transportation's (the FAA Administrator's) responsibilities to".... establish requirements for the safe operation of such aircraft systems inthe national airspace system." The name and address ofthe applicant is Gerald Kerr GJKerr consulting LLC 9828 Whisperwood Ln Brighton, Ml 48116-8859 gerald.kerr48@gmail.com 810-533-0174From which the exemption is requested: 14 CFR Part 21 subpart H 14 CFR 45.23 (b) 14 CFR 61.113 (a)&(b) 14 CFR 91.7 (a) 14 CFR 91.9 (b)(2) 14CFR91.103 14CFR91.10914 CFR 91.119 (c) 14 CFR 91.121 14 CFR 91.151 (a) 14 CFR 91.203 (a) 14 CFR 91.405 (a) 14 CFR 91.407 (a) 14 CFR 91.409 (a) 14 CFR 91.417 (a): And any you seem to deemed necessary for the exemption. Gerald Kerr will operate oneor more ofthe Following model UAS Yuneec QSOO safety requirements. The approval ofthis 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 ofthe requested exemption isinthe public interest. Accordingly, the applicant graciously requests that the FAA grant the requested exemption. AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY

.IThe operation limitations proposed foran equivalent or higher level of safety because operations will further enhance the safety ofthe 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 asset forth inthe Flight Operations Manual (FOM) include:1.The UAS will weigh significantly less than 55 lbs.It weighs less than4 pounds with battery and camera.2. The UAS, depending onthe model in operation, will have a maximum operating speed of no more than 50mph. 3. Flights willbe operated within lineof sight ofthe Pilot in Command (PIC) and/or Visual Observer (VO). 4. Maximum flight time tor each operational flight will be depending onthe UAS model in operation, but will not exceed 30 minutes. Flights willbe terminated at 25% battery power reserve or30 minutes of flight time whichever occurs first. 5. Flights willbe operated atan altitude ofno more than 400 teet Above Ground Level (AGL) and not more than 200 teet above an elevated platform from which filming is planned.

6. Minimum crew for each operation will consist ofthe UAS Pilot and at least one Visual Observer (VO), and may include a third, but separate, Camera Operator (CO). 7. The UAS pilot will bea designated Pilot in Command (PIC) .The PIC will have logged a minimum of20 hours on the designated UAS. 8.A safety briefing willbe performed prior to each day's flights consisting ofallthe days' Production activities. 9.All flight activities willbe logged. 10.All flights will occur under Visual Flight Rules Meteorological Conditions (VMC) only. 11. The flights will occur in Class G airspace no closer than a Smile radius ofthe geographic center/Airport Reference Point (ARP) ofa tower controlled or uncontrolled airport. 12. Flights will notbe closer than a5mile radius ofthe geographic center/Airport. 13. The operator will doapre check of aircraft prior to each flight. And log each flight. 14. The operator will obtain verbal/written consent ofall persons involved with the planned operation and ensure that only consenting persons willbe allowed within 100 feet ofthe flightoperation, and the radius may be reduced to30 feet based upon an equivalent level of safety determination, asu.s. Department of Transportation required under the FOM. With the advanced permission ofthe FSDO, operations at closer range may be approved. 15. The PIC and VO will have been trained in operation of UAS and receive upto date information for the particular UAS tobe operated. 16. The PIC and VO will be able to communicate by voice and/or radio atall times. 17. The PIC will abide byall rules 18.Ifthe UAS loses communications with the remote controller or loses GPS signal, the UAS will have the capability to return toa predetermined location within a designated location and land autonomously.

19. The UAS will have the capability to abort a flight in case of emergencies with an automated "Return Home and Land" function. 20. The UAS will have the capability to abort a flight in case of unpredicted obstacles, weather, or emergencies such as low battery. 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 tobe utilized by the Applicant, an exemption from Part 21 Subpart H meets the requirements ofan equivalent level of safety under Part 11 and Section 333 ofthe Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333 ofthe Reform Act both authorize the FAA to exempt aircraft from the requirement foran airworthiness certificate, upon consideration ofthe size, weight, speed, operational capability, and proximity to airports and populated areas ofthe particular UAS. Inall 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 beat 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 UAS tobe operated hereunder isless 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. These safety enhancements provide a greater degree of safety tothe public and property owners than conventional operations conducted with airworthiness certificates issued under 14 C.F.R. Part 2/, Subpart H. Lastly, application of these same criteria demonstrates that there isno credible threat to national security posed bythe 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 ofthe Aircraft The regulation requires: When marks include only the Roman capital letter "N" and theregistration 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 tothe 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 applicable14 C.F.R. § 45.23 (b). Marking ofthe 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 tothe 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 asthe UAS will have no entrance tothe cabin, cockpit or pilot station on which the word "Experimental" can be placed. Given the size ofthe UAS, two inch lettering will be impossible. The word "Experimental" will be placed on the fuselage in compliance with §45.29 (f).us Department of Transportation February 20, 2015 The equivalent level of safety will be provided by having the UAS marked onits fuselage as required by §45.29 (f) where the pilot, observer and others working with the UAS will see the identification ofthe UAS as "Experimental." 14 C.F.R. § 61.113 (a) and (b The proposed UASoperations may achieve an equivalent level of safety as achieved by current Regulations because the applicant's UAS do not carry any pilots or passengers nor property. The risks attendant tothe

Itis believed that the operation and limitations set forth inthe FOM will equate tothe safe operation ofthe UAS. 14 C.F.R. §91. 7{a): Civil Aircraft Airworthiness. The regulation requires that no person may operate acivil aircraft unless itisin 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 ofthe aircraft for maintenance and useof 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 inthe 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 isnot required by §21.5 ofthis chapter, unless there is available inthe aircraft a current approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or any combination thereof. 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 isno pilot on board, but because there isno room or capacity to carry such an item on the aircraft. The equivalent level of safety will be maintained by keeping the flight manual atthe ground control point where the pilot flying the UAS will have immediate access toit.

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 willbe needed. The PIC will take all actions as stated in the FOM in Section 4 under Normal Procedures including but not limited to reviewing weather, flight battery requirements, landing and takeoff distances and aircraft performance data before initiation of flight**~** 14 C.F.R. §91.1 09: Flight Instruction. Section 91.103 provides that no person may operate a civil aircraft (except a manned free balloon) thatis being used for flight instruction unless that aircraft has fully functioning dual controls. UAS and remotely piloted aircraft, by their design do not have fully functional dual controls. Flight control is accomplished through the useofa control box that communicates with the aircraft via radio communications. the FAA has approved exemptions for flight training without fully functional dual controls fora number of aircraft and for flight instruction in experimental aircraft. The equivalent level of safety is provided bythe fact that neither apilot nor passengers willbe carried inthe aircraft and bythe size and speed ofthe aircraft. · 14 C.F.R. §91.119: Minimum Safe Altitudes. Section 91.119 establishes safe altitudes for operation ofcivil aircraft. Section 91.119 (d) allows helicopters tobe operated at less than the minimums prescribed, provided the person operating the helicopter complies with any route or

altitudes prescribed for helicopters bythe FAA. As this exemption isforaUAS thatisa helicopter and the exemption requests authority to operate at altitudes upto 400 AGL, ornot more than 200 above an elevated platform from which filming is planned, an exemption may be needed to allow

such operations. Asset forth herein, the UAS will never operate at higher than 400 AGL with the exception thatin circumstances where the UASis used to survey or photograph a structure whose height exceeds 400 feet AGL, the UAS will notbe operated more than 200 feet above the highest

point onthe structure. Itwill however be operated ina restricted area with security perimeter, where buildings and people will notbe exposed to operations without their pre obtained consent.

The equivalent level of safety willbe achieved given the size, weight, and speed ofthe UAS as well asthe location where itis operated. No flight

willbe taken without the permission ofthe property owner or local officials. Because ofthe advance notice tothe property owner and participants inthe filming activity, all affected individuals will be aware ofthe planned flight operations. Compared to flight operations with aircraft or rotorcraft weighting far more than the maximum SSibs. proposed herein and the lack of flammable fuel, any risk associated with these operations isfar less than those presently presented with conventional aircraft operating ator below 500 AGL. In addition, the low altitude operations ofthe UAS will ensure separation between these 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 toan altimeter thatisset"...tothe elevation ofthe departure airport oran appropriate altimeter setting available before departure." Asthe UAS may not have a barometric

altimeter, but instead aGPS altitude read out, anu.s. exemption may be needed. An equivalent level of safety will be achieved bythe operator, ·pursuant tothe safety check list and live flight data monitoring, confirming the altitude ofthe launch site shown on the GPS altitude indicator before flight. 14 C.F.R. § 91.151 (a): Fuel Requirements for Flight inVFR Conditions Section 91.151 (a) prohibits an individual from beginning "a flight inan airplane under VFR conditions unless (considering wind and forecast weather conditions) there is enough fueltoflytothe first

point of intended landing, and, assuming normal cruising speed- (1) During the day, tofly after

that forat least 30 minutes; or(2)At night, tofly after that forat least 45 minutes." The applicant believes that an exemption from 14 CFR §91.151 (a) falls within the scope of prior exemptions. Operating the UASina tightly controlled area where only people and property owners or official representatives who have signed waivers willbe allowed does not engender the type of risks that Section 91.151 (a) was intended to alleviate given the size and speed ofthe small UAS. The applicant believes that an equivalent level of safety can be achieved by limiting flights to30

minutes or 25% of battery power- whichever happens first. This restriction would be more than adequate to return the UAS toits planned landing zone from anywhere inits limited operating area.14 C.F.R. §91.203 (a) and (b): Carrying Civil Aircraft Certification and Registration The regulationprovides in pertinent part: (a) Except as provided in§ 91.715, no person may operate acivil aircraft unless ithas within itthe following: (1)An appropriate and current airworthiness certificate

.... (b)No person may operate acivil aircraft unless the airworthiness certificate required by paragraph (a)ofthis section ora special flight authorization issued under §91.715 is displayed at the cabin or cockpit entrance so thatitis legible to passengers or crew. The UAS fully loaded weighs well under the proposed 551b limit andis operated without an onboard pilot. As such, there isno ability or place to carry certification and registration documents orto display them onthe UAS. An equivalent level of safety willbe achieved by keeping these documents atthe ground control point where the pilot

flying the UAS will have immediate access to them, tothe extent they are applicable tothe UAS. 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 Eofthis part and shall between required inspections, except as provided in paragraph (c)ofthis section, have discrepancies repaired as prescribed inpart 43ofthis 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 tothe applicant. Maintenance willbe accomplished bythe operator pursuant tothe flight manual and operating handbook. An equivalent level of safety will be achieved because the UASisvery limited in size and will carry a small payload and operate only in restricted areas tora limited period of time. If mechanical issues arise the UAS can land immediately and will be operating from no higher than 400 feet AGL. The operator will ensure that the UASisin working order prior to initiating flight, perform required maintenance, and keep alogofany maintenance performed. Moreover, the operator isthe person most familiar with the aircraft and best suited to maintain the aircraft inan airworthy condition to provide the equivalent level of safety. An equivalent level of safety willbe achieved because maintenance and inspections will be performed in accordance with the UAS Manufacturer's User Manual. As provided inthe FOM, and alink on last page, the operator will ensure that the UASisin working order prior to initiating flight and perform required maintenance needed. I Believe everything isinthe publics intrest. Additional Information. The applicant Gerald Kerr believes this exemption request and associated safety considerations adequately satisfy criteria provided in Section 333 ofthe Reform Actof 2012, providing sufficient justification for the granting of commercial operations ofthe applicant's UAS.The applicant, Gerald Kerr requests your respective approval ofthis Section 333 exemption petition request.... Thank you for your attention inthis matter. Please notify Gerald Kerr of your actions, and or approvals. Thank you, for your interest inthis request Sincerely, Gerald**Kerr~.,J);:)(~~.JoV\/**

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