US Departm ent of Transportation Exem ption Request Pursuant to Section 333 of the FAA

Reform Act and Part 11 of the Federal Aviation April 6, 2015 JTS AERO VISIONS (Gregory J Spevak owner). 2024 N 91 Street Lincoln Nebraska 68505 Phone 1

-402

- 540

- 2444 Cell. Phone 1

-402

-477

- 7805 Hom e. U.S. Departm ent of Transportation Docket Managem ent System 1200 New Jersey Ave., SE Wa shington DC 20590

Re: Exem ption Request Pursuant to Section 333 of the FAA Reform Act and Part 11 of the Fed eral Aviation Regulations from: 14 CFR 21 subpart H ; 1 4 CFR 45.23(b) ; 14 CFR 61.113(a) and (b) ; 14 CFR 91.7(a) ; 14 CFR 91.9(b)(2) ; 14 CFR 91.103 ; 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 of the FAA,

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the “Reform Act”) and 14 CFR Part 11, JTS AERO V ISIONS (Gregory J Spevak) operator of Unm anned Aircraft System s (UAS), hereby applies for an exem ption 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 or as m ay be established by the FAA as required by Section 333. Thank you in for your consideration. Commercial operation of an UAS, as described herein, which are equipped with cam era(s) and sensors, would prov ide professional services in the follow ing areas: 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, cinem atography and newsgathering. 3. Aerial inspection/photography of residential/commercial structures under contract with the owners or local governm ent au thority. 4. Aerial inspection/photography of residential/commercial utility infrastructure including but not lim ited to electrical power lines, wind turbines and cell towers. 5. Aerial video/photography or providing live video feed to assist w ith search an d rescue operations in cases of an em ergency or natural disaster only when the local authorities or governm ent has requested it by contract or donation. 6. Training to persons individually or belonging to both private and/or public organizations to increas e awareness and im prove safety for current and future UAS operations within the NAS. As described fully below, the requested exem ption would perm it the operation of designated UAS as set forth in this docum ent under controlled conditions in the NAS that would be a) lim ited b) controlled c) predeterm ined and d) safe. Approval of this exem ption would increase public awareness of UAS operations and enhance safety to aid in fulfilling the Secretary of Transportation’s (the FAA Administrator’s) responsibiliti es to “....establish requirem ents for the safe operation of such aircraft system s in the national airspace system.”The nam e and address of the applicant is:

JTS AERO VISIONS (Gregory J Spevak owner). 2024 N 91 Street Lincoln Nebraska 68505

Em ail: kawam an39@aol.com Phone 1

-402

- 540

- 2444 Cell Phone 1

-402

-477

- 7805 Hom e Regulations from which the exem ption 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) 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)JTS AERO VISIONS (Gregory J Spevak) will operate one or m ore of the following m odel

UAS: 1. Yuneec Model Q500 Typhoon, specifications to follow below:

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# PRODUCT SPECIFICATIONS

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## Q500 TYPHOON **Ai rcraft**  **○ Flight Time**  **○ Up to 25 Minutes**  **○ Height**  **○ 240mm (9.45 in)**  **○ Width**  **○ 420mm (16.54 in)**  **○ Diagonal Length Without Rotor Blades**  **○ 565mm (22.2 in)**  **○ Propeller/Main Rotor Diameter**  **○ 330mm (13.0 in)**  **○ Weight Without Battery and Pay**  **load ○**  **1130g (40.0 oz) ○**  **Battery ○**  **5400m Ah**  **3S 11.1V LiPo (included) ○**  **Charger ○**  **3S 11.1V LiPo DC Balancing Smart Charger with AC A dapter (included)**  **○ Transmitter**  **○ 10-channel 2.4GHz with 5.8GHz video downlink (included)**  **○ 3 Flight Modes**  **○ Smart, A**  **ngle and Home Modes ○**  **Maximum Fly ing Height**  **○ Default 400 Feet A** **bove Ground Level (A dj**  **ustable via the Q500 GUI) ○**  **Maximum Rotational Velocity ○**  **65°/s ○**  **Maximum Bank A ngle**  **○ 35°**  **○ Maximum Climb Rate in Smart and A**  **ngle mode ○**  **3m/s ○**  **Maximum Descent Rate in Smart and A ngle mode**  **○ 2m/s**  **○ Takeoff Weight With Battery and CGO2-GB**  **○ 1700g (60.0 oz)**  **○ Radio Control Frequency**  **Band ○**  **2.4GHz ●**  

## CGO2-GB Camera Gimbal Sy**stem ○**  **Focusing Sy stem**  **○ Aerial Optimized Fixed Focus**  **○ Video Resolution**  **○ FULL HD 1080p - A** **djustable 60, 50 or 48 FPS ○**  **Photo Resolution ○**  **12 Megapixels ○**  **Video Field of View ○**  **130° ○**  **Control A ngle Accuracy**  **○ ±0.02°**  **○ White Balance**  **○ Automatic Smart White Balance Feature**  **○ Transmission Band**  **○ 5.8GHz**  **○ Input/Operating Voltage**  **○ 7.0V to 14.0V DC**  **○ Video Transmission Distance/Range (Optimum Conditions)**  **○ FCC Compliance: Up to 600m (1968.5 ft) CE Compliance: Up to 300m**  **(984.252 ft ) with ST10 Warning: You Must Follow Local Laws and Maintain**  **Visual Line of Sight of A ircraft at A**  **ll T imes.**  **○ Current Consumption/Operating Current**  **○ 500mA (average) to 600mA**  **(peak) @ 12.0V (7.2W max) ○**  **Storage Temperature ○**  **-20°C-60°C ○**  **Working Temperature**  **○ 0°C-50°C**  **○ Storage (memory** **) ○**  **microSD Class 10 ~ 4 to 128GB ○**  **Height ○**  **115mm (4.5 in) ○**  **Weight ○**  **185g (6.5 oz) ○**  **Depth ○**  **135mm (1.4 in) ○**  **Width ○**  **74mm (2.9 in)**

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## ST **10 Personal Ground Station ○**  **Operating System ○**  **AndroidTM ○**  **Number of Channels ○**  **10 ○**  **Control Transmission Distance/Range (Optimum Conditions) ○**  **FCC Compliance: Up to 800m (2624.67 ft) CE Compliance: Up to 400m (1312.34 ft) Warning: You Must Follow Local Laws and Maintain Visual**  **Line of Sight of A ircraft at A**  **ll Times. ○**  **Robust Radio Control Modulation ○**  **Yuneec Protocol ○**  **Video link Frequency Band**  **○ 5.8GHz**  **○ Video Transmission Distance/Range (Optimum Conditions)**  **○ FCC Compliance: Up to 600m (1968.5 ft) CE Compliance: Up**  **to 300m (984.252 ft) Warning: You Must Follow Local Laws and Maintain Visual**  **Line of Sight of A ircraft at A**  **ll Times. ○**  **Flight Sy stems Telemetry**  **Data On Screen Display (OSD)**  **○ Yes**  **○ LED Backlit LCD Screen**  **○ Capacitive Multi-Touch 4.5”**  **○ Tactile (Vibrating) and A** **udible Feedback ○**  **Yes ○**  **Built-In LiPo Battery Voltage / Capacity**  **○ 3.6V/5200mAh 18.72Wh**  **○ Charger**  **○ Auto-Charge Mode via Micro-B USB Cable with A** **C to 5V DC USB Power Supply**  **(Included)**

Given the sm all size of the UAS in scope and the controlled environm ent provided, the proposed operations will adhere to the Reform Act’s safety requirem ents. 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 environm ental im pacts, including but not lim ited to reduced emissions and noise, the grant of the requested exem ption is in the public interest. Accordingly, the applicant graciou sly requests that the FAA grant the requested exem ption. AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY The operation lim itations proposed for an equivalent or higher level of safety because operations will further enhance the safety of the persons and/or p roperty using conventional aircraft. These lim itations and conditions to w hich the applicant agrees to adhere to when conducting commercial operations under the FAA issued exem ption as set forth in the Flight Operations Manual (FOM) include:1. The UAS w il l weigh significantly less than 55 lbs. It weighs less than 4 pounds with

battery and cam era. 2. The UAS, depending on the m odel in operation, w ill have a m axim um operating speed of no more than 50m ph. 3. Flights w ill be operated within line of sight of th e Pilot in Command (PIC) and/or Visual Observer (VO). 4. Maxim um flight time for each operational flight will be depending on the UAS m odel in operation, but w ill not exceed 30 m inutes. Flights will be term inated at 25% battery power reserve or 30 m inutes of flight tim e whic hever occurs first. 5. Flights w ill be operated at an altitude of no more than 400 feet Above Ground Level (AGL) and not m ore than 200 feet above an elevated platform from which film ing is planned. 6. Minim um crew

for each operation will consist of the UAS Pilot and at least one Visual Observe r (VO), and m ay include a third, but separate, Cam era Operator (CO). 7. The UAS pilot w ill be a designated Pilot in Command (PIC) . The PIC will have logged a minim um of 20 hours on the designated UAS. 8. A safety briefing w ill be perform ed prior to each d ay’s flights consisting of all the days’ production activities. 9. All flight activities will be logged. 10. All flights will occur under Visual Flight Rules Meteorological Conditions (VMC) only. 11. The flights w ill occur in Class G airspace no closer than a 5-m ile radius of the geographic center/Airport Reference Point (ARP) of a tower controlled or uncontrolled airport. 12. Flights w ill not be closer than a 5 m ile radius of the geographic center/Airport. 13. The operator will file FAA Form 7711-1, or its equ ivalent, as m odified in light of the requested exem ption, with the appropriate local Flight Standards District Office (FSDO) no m ore than 72 hours but no less than 48 hours from planned operation. 14. The operator will obtain verbal/written consent of all p ersons involved with the planned operation and ensure that only consenting persons will be allowed within 100 feet of theflight operation, and the radius m ay be reduced to 30 feet based upon an equivalent

level of safety determ ination, as U.S. Departm ent of Transportation required under the FOM. W ith the advanced perm ission of the FSDO, operations at closer range m ay be approved. 15. The PIC and VO w ill have been trained in operation of UAS and receive up-to-date inform ation for the particular UAS to be ope rated. 16. The PIC and VO w ill be able to comm unicate by voice and/or radio at all tim es. 17. Written and/or verbal perm ission and perm its w ill be obtained from territorial, state, county or city jurisdictions, including law enforcem ent, fire or other appropriate governm ental agencies as appropriate to flight operations. 18. If the UAS loses communi cations with the remote controller or loses GPS signal, the UAS w ill have the capability to return to a pre-determ ined location within a designated location and land autonom ously. 19. The UAS w ill have the capability to abort a flight in case of em ergencies with an autom ated “Return Home and Land” function. 20. The UAS w ill have the capability to abort a flight in case of unpredicted obstacles, weather, or em ergencies 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 requirem ents for the issuance of airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and lim ited operating area associated with the aircraf t to be utilized by the Applicant, an exem ption from Part 21 Subpart H m eets the requirem ents 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 exem pt aircraft from the requirem ent for an airworthiness certificate, upon consideration of the size, weight, speed, operational capability, and proxim ity to airports and populated areas of the particular UAS. In all cases, an analysis of these criteria dem onstrates that the UAS operated without an airworthiness certificate in the restricted environm ent and under the conditions proposed will be at least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) o perating with an airworthiness certificate w ithout the restrictions and conditions proposed. The UAS to be operated hereunder is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, carries no explosive m aterials or flammable liquid fuels , and operates exclusively within a secured and designated area. Unlike other civil aircraft, operations under this exem ption w ill be tightly controlled and m onitored by both the operator and under the requirem ents and in com pliance with local public safety requirem ents. These safety enhancem ents provide agreater 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 sa me criteria dem onstrates that there is no credible threat to national security posed by the UAS, due to its size, speed of operation, location of operation, lack of explosive m aterials or flammable liquid fuels, and inability to carry a substantial externa l load. 14 C.F.R. § 45.23 (b). Marking of the Aircraft The regulation requires: W hen m arks include only the Rom an capital letter "N" and the registration num ber is displayed on lim ited, restricted or light-sport category aircraft or experim ental or provisi onally certificated aircraft, the operator m ust also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches nor m ore than 6 inches high, the words "lim ited," "restricted," "light-sport," "expe ri me ntal," or "provisional," as applicable 14 C.F.R. § 45.23 (b). Marking of the Aircraft The regulation requires: W hen marks include only the Rom an capital letter "N" and the registration num ber is displayed on lim ited, restricted or light-sport catego ry aircraft or experim ental or provisionally certificated aircraft, the operator m ust also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches nor m ore than 6 inches high, the words "lim ite d," "restricted," "light-sport," "experim ental," or "provisional," as applicable. Even though the UAS will have no airworthiness certificate, an exem ption m ay be needed as the UAS w ill have no entrance to the cabin, cockpit or pilot station on which the wo rd “Experim ental” can be placed. Given the size of the UAS, two-inch lettering will be im possible. The word “Experim ental” w ill be placed on the fuselage in com pliance with §45.29 (f). US Department of Transportation February 20, 2015 The equivalent level of safety w ill be provided by having the UAS m arked 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 “Experim ental.” 14 C.F.R. § 61.113 (a) and (b): Private Pilot Privileges and Lim itations: Pilot in Command. Pursuant to 14 CFR 61.113 (a) & (b), no person who holds a private pilot certificate m ay act as a pilot in command of an aircraft that is carrying passengers or property for com pensation or hire. The proposed UAS operations m ay 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 to the operation of UAS is far less than the risk levels inheren t in the commercial activities outlined in 14 CFR 61. The PIC of the UAS will be, or be under the direct supervision of, a FAA Certificated Private Pilot with current Third Class or higher m edical certificate. It is believed that the operation and limitati ons set forth in the FOM will equate to the safe operation of the UAS. 14 C.F.R. §91.7(a): Civil Aircraft Airworthiness. The regulation requires that no person m ay operate a civil aircraft unless it is in airworthy condition. As there w ill be no airworthiness certificate issued for the aircraft, should this exemption be granted, no FAA regulatory standard will exist for determ ining airworthiness. Given the size of the aircraft for maintenance and use of safety checklists prior to each flight, an equival ent level of safety will be provided. 14 C.F.R. § 91.9 (b) (2): Civil Aircraft Flight Manual in the Aircraft. Section91.9 (b) (2) provides: No person m ay operate a U.S.-registered civil aircraft ... (2) For which

an Airplane or Rotorcraft Flight Manual i s 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 m aterial, markings, and placards, or any com bination thereof. The UAS, given its size and configurat ion has no ability or place to carry such a flight m anual 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 kee ping the flight manual at the ground control point where the pilot flying the UAS will have im mediate 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 w ill not be provided for the aircraft an exem ption w ill be needed. The PIC will take all actions as stated in the FOM in Section 4 under Norm al Procedures including but not lim ited to reviewing weather, flight battery requirem ents, 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 m ay operate a civil aircraft (except a manned free balloon) that is being used for flight instruction unless that aircraft has fully functioning dual controls. UAS and rem otely 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 exem ptions for flight training without fully functional dual controls for a num ber of aircraft and for flight instruction in experim ental aircraft. The equivale nt level of safety is 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 m inim um s prescribed, provided the person operating the helicopter com plies w ith any route or altitudes prescribed for helicopters by the FAA. As this exem ption is for a UAS that is a helicopter and the exem ption requests authority to operate at altitudes up to 400 AGL, or not m ore than 200 above an elevated platform from w hich film ing is planned, an exem ption m ay be needed to allow such operations. As set forth herein, the UAS will never operate at higher than 400 AGL w ith the exception that in circum stances w here the UAS is used to survey or photograph a structure whose height exceeds 400 feet AGL, the UAS will not be operated m ore than 200 feet above the highest point on the structure. It will however be operated in a restricted area with security perim eter, w here buildings and people will not be exposed to operations w ithout their pre-obtained consent. The equivalent level of safety will be achieved given the size, we ight, and speed of the UAS as well as the location where it is operated. No flight will be taken without the perm ission of the property owner or local officials. Because of the advance notice to the property owner and participants in the film ing activity, all affected individuals will be aware of the planned flight operations. Com pared toflight operations with aircraft or rotorcraft weighting far more than the maxim um 55lbs.

proposed herein and the lack of flamm able fuel, any risk associated with these ope rations is far less than those presently presented with conventional aircraft operating at or below 500 AGL. In addition, the low altitude operations of the UAS w ill ensure separation between these UAS operations and the operations of conventional aircraft that must com ply w ith Section 91.119. 14 C.F.R. §91.121 Altim eter 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 altim eter setting available before departure.” As the UAS may not have a barom etric altim eter, but instead a GPS altitude read out, an U.S. exemption m ay be needed. An equivalent level of safety will be achieved by the operator, pursuant to the safety check list and live flight data m onitoring, confirm ing the altitude of the launch site shown on the GPS altitude indicator before flight. 14 C.F.R. § 91.151(a): Fuel Requirem ents for Flight in VFR Conditions Section 91.151 (a) prohibits an i ndividual 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, assum ing 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 m inutes.” The applicant believes that an exem ption from 14 CFR §91.151(a) falls w ithin the scope of prior exem ptions. Operating the UAS in a tightly controlled are a where only people and property owners or official representatives who have signed waivers will be allowed does not engender the type of risks that Section 91.151(a) was intended to alleviate given the size and speed of the sm all UAS. The applicant believ es that an equivalent level of safety can be achieved by lim iting flights to 30 m inutes or 25% of battery power — whichever happens first. This restriction would be m ore than adequate to return the UAS to its planned landing zone from anywhere in its lim ited 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 m ay operate a civil aircraft unless it has within it the follow ing: (1) An appropriate and current airworthiness certificate. . . . (b) No person m ay 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 di splayed at the cabin or cockpit entrance so that it is legible to passengers or crew . The UAS fully loaded weighs well under the proposed 55-lb lim it and is operated without an onboard pilot. As such, there is no ability or place to carry certification and registration docum ents or to display them on the UAS. An equivalent level of safety w ill be achieved by keeping these docum ents at the ground control point w here the pilot flying the UAS will have imm ediate access to them, to the extent they are applicabl e to the 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 E of this part and shall between required inspections,except as provided in paragraph (c) of this sect ion, have discrepancies repaired as

prescribed in part 43 of this chapter...,” and others shall inspect or m aintain the aircraft in com pliance with Part 43. Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, the se sections w ill not apply to the applicant. Maintenance will be accom plished by the operator pursuant to the flight m anual and operating handbook. An equivalent level of safety will be achieved because the UAS is very lim ited in size and will carry a sm al l payload and operate only in restricted areas for a limited period of tim e. 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 UAS is in working order prior to initiating flight, perform required m aintenance, and keep a log of any m aintenance perform ed. Moreover, the operator is the person m ost familiar w ith the aircraft and best suited to m aintain the aircraft in an airworthy condition to provide the equivalent level of safety. An equivalent level of safety will be achieved because m aintenance and inspections will be performed in accordance with the UAS Manufacturer's User Manual. As provided in the FOM, the operator will ensure that the UAS is in working order p rior to initiating flight and perform required maintenance needed. Additional Information about JTS AERO VISIONS: The applicant JTS AERO VISIONS (Gregory J Spevak) has been around R.C aircraft and models for several years. The applicate JTS AERO VISIO NS (Gregory J Spevak) holds his private license and holds his A&P aircraft license. The applicant currently works at a large FBO located in Lincoln , Nebraska located on the Lincoln Airport field. The Applicate at this current tim e m aintains corporate aircraft in the following m odels such as the Falcon group 7X, F2000, F2000EX, F900, F900EX, F50, F50EX, F20 and the F10. Also JTS AERO VISIONS (Gregory J Spevak) would like to m ention the 25 years of experience of maintaining several other m odels of corporate j ets. Including the Hawker group, the Cessna group, the Lear group and the Gulfstream group. The applicant, JTS AERO VISIONS (Gregory J Spevak) , believes this exem ption request and associated safety considerations adequately satisfy criteria provided in Section 333 of the Reform Act of 2012, providing sufficient justification for the granting of comm ercial operations of the applicant’s UAS. The applicant, JTS AERO VISIONS (Gregory J Spevak), requests your respective approval of this Section 333 exempt ion petition request. Thank you for your interest and attention in this matter. Please notify JTS AERO VISIONS (Gregory J Spevak) of your actions, and or approvals. Thank You for your interest in this request.Sincerely,

JTS AERO VISIONS (G regory J Spevak owner). 2034 N 91 Street Lincoln Nebraska 68505 1

-402 540

- 2444 Cell 1

-402

-477

- 7805 Hom e Em ail: kawam an39@aol.com