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## Seminole Club, Inc. DBA: Tower Specs April 6, 2015 U. S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590 Re: Exemption Request Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation Regulations from 14 C.F.R. 45.23(b); 14 CFR Part 21 ; 14 CFR 61.113 (a) & (b); 91.7 (a) ; 91 . 9 (b) (2); 91.103(b); 91 . 109; 91.119; 91 . 121; 91 . 151(a); 91.203(a) & (b); 91.405 (a); 91.407(a) (1); 91.409 (a) (2); 91.417 (a) & (b). Dear Sir or Madam : Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the Reform Act) and 14 C.F.R. Part 11, Seminole Club, Inc. , DBA: Tower Specs, hereby applies for an exemption from the listed Fed eral Aviation Regulations ("FAR") to allow commercial operation of its UAV’s, so long as such operations are conducted within and under the conditions outlined herein or as may be established by the FAA as required by Section 333 . As described more fully below, the requested exemption would permit the operation of small, unm anned UAV’s under controlled conditions in airspace that is 1) limited 2) predetermined 3) Controlled as to access and 4) would provide cell phone and antenna tower inspections. W e will be operating in airspace previously reviewed by the FAA for the construction of the tower therefore the airspace of the controlled operations area creates no additional hazard to the national airspace . Approval of this exemption would therefore create no safety concerns regarding national airspace and fulfil l 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 s ystem." Section 333(c) of the Reform Act. The name and address of the applicant is: Sem inole Club, Inc. DBA: Tower Specs Attn: Curt Daniels Em ail curt@towerspecs.com 707 W est Park Ave Suite D Edgewater, Florida 32132 (386) 410-4701 Regulations from which the exemption is requested : 14 C . F . R . Part 21 14 C . F . R. 45 . 23 (b) 14 C.F . R. 91 . 7 (a) 14 C . F . R . 91.9 (b) (2) 14 C.F . R. 91 . 103 14 C . F.R. 91.109

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14 C . F. R. 91.119 14 C . F . R. 91 . 121 14 C . F . R . 91 . 151 (a) 14 C . F . R . 91 . 203 (a) & (b) 14 C . F . R . 91.405 (a) 14 C . F . R . 407 (a) (1) 14 C . F . R . 409 (a) (2) 14 C . F . R . 417 (a) & (b) This exemption application is expressly submitted to fulfill Congress' goal in passing Section 333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to consider whether certain unmanned aircraft systems may operate safely in the national airspace system (NAS) before completion of the rulemaking required under Section 332 of the Reform Act. In making this determination, the Secretary is required to determ i ne which types of UAV do not create a hazard to users of the NAS or the public or pose a threat to national security in light of the following : • The UAV size , weight , speed , and operational capability; • Operation of the UAV i n close proximity to airports and populated areas ; and • Operation of the UAV within visua l line of sight of the operator Reform Act§ 333 (a). Lastly, if the Secretary determines that such vehicles "may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation of such aircraft in the national airspace system ." Applicant interprets this provision to place the duty on the Administrator to not only process applications for exemptions under section 333, but for the Administrator to craft conditions for the safe operation of the UAS , if it should be determined that the conditions set forth herein do not fulfill the statutory requirements for approval. The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This statutory authority by its terms includes exempting civil aircraft, as the term is defined under §401 01 of the Act that includes UAV , from the requirement that all civil aircraft must have a current airworthiness certificate . The Administrator may grant an exemption from a require ment of a regulation prescribed under subsection (a) or (b) of this section or any sections 44702 -44716 of this title if the Administrator finds the exemption in the public interest. 49 U . S . C . §44701 (f) See also 49 USC §44711 (a) ; 49 USC §44704 ; 14 CFR §91 . 203 (a) ( 1) . Tower Specs UAV’s are rotorcraft, weighing 55 or fewer lbs. including payload . They operate , under normal conditions , at a speed of no more than 50 knots and have the capability to hover, and move in the vertical and horizontal plane simultaneously. They will operate only in line of sight and will operate only within a small controlled area described in the Confidential Operations Procedures , attached as Exhibit A (hereinafter "Procedures" ) Such operations will insure that the UAV will " not create a hazard to users of the n ational airspace system or the public.'' Applicant submits this Procedure as a Confid ential and Proprietary document under 14 CFR 11 . 35 (b) as the entire Procedures contains proprietary information that the applicant has not and will not share with others. The Procedures contains operating conditions and procedures that are not available to the publ i c and are p rotected from release under the Freedom of Information Act 5 USC 552 et.seq . Given the small size of the UAV’s involved and the restricted con trolled environment within which they will operate , the applicant falls squarely within that zone of safety (an equivalent level of safety) in which Congress envisioned that the FAA must, by exemption , allow commercial operations of UAV’s to commence immed iately. Also due to the size of the UAV’s and the controlled areas i n which

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the relevant UAV’s will operate , approval of the application presents no national security issue . Given the following , the grant of the requested exemptions is clearly in the publi c interest: • Clear direction in Section 333 of the Reform Act, the authority contained in the Federal Aviation Act, as amended • The level of safety surrounding the proposed operations that implements the use of HD and thermal imagining , and the significant public benefit • Innovative reductions in physical dangers of personnel climbing towers (e.g., thermal imaging of active wasp/hornet nests, electrical “hot spots”...) and/or the use of high - rise heavy equipment thus reduced emissions associated with allowing UAV’s operations . Accordingly, the applicant respectfully requests that the FAA grant the requested exemption without delay . AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY The applicant proposes that the exemption requested herein apply to civil aircraft that have the characteristics and that operate with the limitations listed herein . These limitations provide for an exceptional level of safety to operations. These limitations and conditions to which Tower Specs agrees to be bound when conducting com mercial operations under an FAA issued exemption include : 1. The UAV will weigh less than 55 lbs. 2. Flights will be operated within line of sight of operator. 3. Maximum total flight time for each operational flight will be 30 minutes. Flights will be terminated at 15% battery power reserve should that occur prior to the 30 minute limit. 4 . Flights will be operated at an altitude of no more than 400 feet AGL 5 . UAV operator will be trained and certified in the prope r safety and operations of the UAV . In addition, the UAV operator shall be an FAA licensed airman with at least a private pilot’s certificate and third class medical. 6 . The UAV will only operate within a controlled area as defined in the Procedures . 7. The operator wi ll post advisor notice around the controlled area. 8. Operator will have been trained in operation of UAV ge nerally and received up-to-date information on the particular UAV to be operated as required. 9. If the UAV loses communications or loses its GPS si gnal, the UAS will have capability to return to a pre-determined location within the Security Perimeter and land . 10. The UAV will have the capability to abort a flight in case of unpredicted obstacles or emergencies. **14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. §91.203 (a) (1)**  Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements for the issuance of airworthiness certificates as required by FAR §91 . 203 (a) (1 ) . Given the size and limited ope rating area associated with the aircraft to be utilized by the Applicant, an exemption from Part 21 Subpart H meets the requ irements 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 autho rize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration of the size,

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weight, speed, operational capability, and proximity to airports and populated areas of the particular UA

V . In all cases, an analysis of these criteria demonstrates that the UAV 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 win g or rotorcraft) operating with an airworthiness certificate without the restrictions and conditions proposed. The UAV’s 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 controlled area as set out in the Procedures . Unlike other civil aircraft, operations under this exemption will be tightly controlled and monitored by the operator, pu rsuant to the Procedures requirements . Lastly, application of these same criteria demonstrates that there is no credible threat to national security posed by the UAV , due to its size, speed of operation, location of operation , lack of explosive materials o r flammable liquid fuels, and inability to carry a substantial external load. **14 C.F.R. § 45.23 (b). M**  **arking of the A ircraft**  The regulation requires: Wh en 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 inch es nor m ore than 6 inches high, the words "limited," "restricted," "light-sport," "experimental," or "provisional," as applicable . Even though the UAV will have no airworthiness certificate, an exemption may be needed as the UAS will have no entrance to the cabin, cockpit or pilot station on which the word "Experimental" can be placed . Given the size of the UAV, 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 UAV marked on its fuselage as required by §45 . 29 (f) where the operator wo rking with the UAV will see the identification of the UAV as " Experimental." The FAA has issued the following exemptions to this regul ation to Exemptions Nos . 10700, 8738 , 10167 and 10167 A **14 C.F.R. §91.7(a): Civil aircraft airworthiness.** The regulation requires that no person may operate a civil aircraft unless it is in airworthy condition. As there will be no airworthiness certificate issued for the aircraft, should this exemption be granted, no FAA regulatory standard will exist for determining airworthiness. Given the size of the aircraft and the requirements contained in the Procedures for maintenance and 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 A ircraft.**  Section 91 . 9(b) (2) provides : No person may operate a U.S. - registered civil aircraft ...

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(2) For whi ch 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 UAV , 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 equ i valent level of safety will be maintained by keeping the flight manual at the ground control point where the operator flying the UA V will have immed i ate access to it. The FAA has issued the following exemptions to this regulation : Exemption Nos . 8607, 8737, 8738 , 9299, 9299A, 9565 , 95658, 10167 , 10167A, 10602 , 32827, and 10700 . **14 C.F.R. § 91.103: Preflight action** This regulation requires each operator to take certain actions before flight to insure the safety of flight. As FAA approved rotorcraft fl ight manuals will not be provided for the aircraft an exemption will be needed . An equivalent level of safety will be provided as set forth in Procedures. The operator 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. UAV’s and remotely piloted aircraft, by their design do not have fully functional dual controls . Flight control is accomplished through the use of a control box that communicates with the aircraft via radio communications . The FAA has approved exemptions for flight training without fully functional dual controls for a number of aircraft and for flight instruction in experimental aircraft . See Exemption Nos.5778K & 9862A. The equivalent level of safety provided by the fact that neither a pilot nor passengers will be carried in the aircraft and by the size and speed of the aircraft . **14 C.F .**  **R. §91.119: Minimum safe altitudes** Section 91.119 establishes safe altitudes for operation of civi l 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 UAV that is a helicopter and the exemption requests authority to operate at altitudes up to 400 AGL, an exemption may be needed to allow such operations. As set forth herein , except for the limited conditions stated in the Procedures , the UAV will never operate at higher than 400 AGL. The equivalent level of safety will be achieved given the size, we i ght, and speed of the UAV

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as well as the location where it is operated. In addition, the low-altitude operations of the UAV will ensure separation between these small - UAS o perations and the operations of conventional aircraft that must comply with Section 91.119 . **14 C.F.R. §91.121 A ltimeter 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 UA V 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 Procedures and Safety Check list, confirming the altitude of the launch site shown on the GPS altitude indicator before flight. **14 C.F.R. § 91.151(a): Fuel Requiremen ts for Flight in VFR Conditions**  Section 91 . 151 (a) prohibits an individual from beg i nning "a flight in an a i rplane 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 UAV provides approximately 4 0 minutes of powered flight. To meet the 30-minute reserve requirement in 14 CFR §91 . 151 , UAV flights would be limited to approximately 10 minutes in length . G i ven the limitation s on the UAV's proposed flight area and the location of its proposed operations within a predetermined area, a longer time frame for flight in daylight or night VFR conditions is reasonable . Applicant believes that an exemption from 1 4 CFR §91 . 15 1 (a) falls within the scope of p rior exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without compliance with FAR 91.151 (a)) . Operating the small UAS , in a tightly controlled area, 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 UAV 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 15% of battery power whichever happens first. This restriction would be more than adequate to return the UAV to its planned landing zone from anywhere in its limited operating area . Similar exemptions have been granted to other operations , including Exemptions 2689F , 5745, 10673 , and 10808. **14 C.F.R. §91.203 (a) and (b): Carrying Civil Aircraft Certification and Registration** The regulation provides in pertinent part : (a) Except as provided in § 91 . 715, no pe rson may operate a civil a ircraft unless it has within

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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 UAV fully loaded weighs no more than 55 lbs and is operated without an on board pilot. As such , there is no ability or place to carry certification and registration documents or to display them on the UAV . An equivalent level of safety will be achieved by keepin g these documents at the ground control point where the operator flying the UAV will have immediate access to them , to the extent they are applicable to the UA V . The FAA has issued numerous exemptions to this regulation . A representative sample of other exceptions includes Exemption Nos. 9565, 9665, 9789 , 9789A, 9797, 9797A, 9816A, and 10700. **14 C.F.R. §91.405 (a); 407 (a) (1); 409**  (a) **(2); 417(a) & (b): Maintenance Inspections** These regulations require that an aircraft operator or owner "shall have that aircraft inspected as prescribed in subpart E of this part and shall between required inspections, except as provided in paragraph (c) of this section , have discrepancies repaired as prescribed in part 43 of this chapter. " and others shall inspect or maintain the aircraft in compliance with Part 43. Given that these section and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to the applicant. The operator will accomplish maintenance pursuant to the flight manual and operating handbook as referenced in the Procedures. An equivalent level of safety will be achieved because these small UAV’s are very limited in size and will carry a small payload and operate only in controlled areas for limited periods of time. If mechanical issues arise the UAV can land immediately and will be operating from no higher than 400 feet AGL . As provided in the Procedures, the operator will ensure that the UAV is in working order prior to initiating flight, perform required maintenance , and keep a log of any ma intenance performed . Moreover, the operator is the person most familiar with the aircraf t and best suited to maintain the aircraft in an airworthy condition to provide the equivalent level of safety. Pursuant to 14 C.F . R. Part 11 , the following summary is provided for publication in the Federal Register, should it be determined that publicat ion is needed: Applicant seeks an exemption from the following rules: 14 C . F.R. §21, subpart H ; 14 C.F . R 45.23(b) ; 14 C.F.R. §§ 61 . 113(a) & (b) ; 91.7(a); 91.9(b) (2); 91.103(b); 91 . 109; 91.119; 91.121; 91 . 151(a); 91 . 203(a) and (b); 91.405 (a) ; 91.407 (a) (1) ; 91.409 (a) (2); 91.409 (a) (2) and 91.417 (a) & (b) to operate commercially a small unmanned vehicle (551bs or less) for the purpose of inspection, monitoring , ma pping and photographing attached equipment and engineering studies involving co mmunicati on tower operations. Approval of exemptions all owing commercial operations of UAV’s will create a level of safety by reducing risk . Conventional tower structure inspections and associated tasks involve extreme risks to personnel physically climbing such structures and/or utilizing high rise equipment both of which create numerous and extreme risk to such personnel. In contrast , a UAV weighing fewer than 55 lbs. and powered by batteries eliminates virtually all of that risk. The UAV will carry no passengers or crew and, therefore, will not expose personnel to any of the risks described above. The operation of small UA V’s , weighing less than 55 lbs . , conducted in the strict conditions

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outlined above, will provide a level of safety supporting the grant of the exemptions requested herein , including exempting the applicant from the requirements of Part 21 and allowing commercial operations. These lightweight aircraft operate at slow speeds, close to the ground , and in a controlled environment. **Privacy** All fli ghts will occur over private or controlled access property with the property owner's prior consent and knowledge . The granting of this exemption request will provide innovative safety operations. Satisfaction of the criteria provided in Section 3 33 of the Reform Act of 2012-- size, weight, speed, operating capabilities, proximity to airports and populated areas and operation within visual line of sight and national security - provide more than adequate justification for the grant of the requested exemptions allowing comme rcial operation of applicant's UAV in and pursuant to the Procedures appended hereto . Sincerely,

Curt Daniels Vice President Seminole Club, Inc DBA: Tower Specs Em ail curt@towerspecs.com 707 W est Park Ave Suite D Edgewater, Florida 32132 (386) 410-4701