Jack Thorpe 

T: +1 919 538 4140 

Jlhprpe S41 nccer\,.Q[g 

May 5, 2015 

U.S. Department of Transportation 

Docket Management System 

1200 New Jersey Ave .. SE 

Washington, DC 20590 

Re: Ii~~mQ1iQJJ.RGqil.\;S.LS~\:;JjpoJ.jJgLtb.QJ~i1ARGfQrm.AgLiJJJQ J?.i.JcnJ_LQfJ:h .. ~ 

Federal Aviation Re!.!ulations from 14 C.P.R. 45.23(h): 14 CPR Part 21; 14 

Dear Sir or Madam: 

~fR_9),lJJ..(<.!2.&..Chl: 9L7L&tl; .. 2L2Jl!)t~_t2JJ.\2.J.Cb)_;_9JJQ2;_2LU2; 

91.121; 9l.l51 (a); 91.203( a) & (b): 9J.407(al ( J l: 91.409 (a) ( 2): 91.417 

(!J.t& . ..Lh) 

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

and I 4 C.F.R. Part 11, NC CER'r. INC, operator of small Viking Unmanned Aerial Systems Inc 

Unmanned Aircraft Systems CsU/\.5'') equipped to conduct aerial Serm;h and Rescue Operations in 

the US get higher success rates on (SAR) on operations and to help prevent contamination of lands if 

there was a manned aircraft accident. hereby applies for an exemption from the listed Federal 

Aviation Regulations (''FARs'·) to a!Io"v commercial operation fits sUASs. 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 33.3. 

As described more fully below, the requested exemption would pcnnit the operation of small 

Unmanned and relatively inexpensive sUAS under controlled conditions in airspace that is l) limited 

2) predetermined 3) controlled as to access and 4) would provide safety enhancements to the already 

safe operations in the SAR presently using conventional aircraft. Approval of this exemption would 

thereby enhance safety and fuUi!I 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 <md address of the applicant is: 

NCCERT, INC 

Attn: Jack Thorpe 

Ph: +1 919 538 4140 

Email: l!.Porpe@ncceli.org 

Address: 400 Evans Lane 

Wendell, NC 27591 
The conditions proposed by the applicant are drawn from order 8900. I CHG 0 

Regulations fiTml which the exemption is required 

14 CFR Part 21 

14 C.F.R. 45.23(b) 

14 CFR 6LI 13 (a) & (b) 

14 C.P.R. 91.7 (a) 

14 CF'R 9L9 (b) (2) 

14 C.P.R. 91.103 

14 C.F.R. 91. !09 

14C.F.R. 91.119 

14 C.P.R. 9J.l21 

l4CFR 9l.l5l (aJ 

14 CFR 91.203 (a) & (b) 

14 CFR 91.405 (a) 

14 CFR 407 (a) (l) 

14 Cl''R 409 (a) (2) 

14 CFR 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. [n making this 

determination, the Secretary is required to determine which types of U ASs do not create a hazard to 

users of the NAS or the public or pose a threat to national security in light of the f(lllowing.: 

• The lJAS's size. weight, speed, and operational capability 

• Operation of the UA.S in dose proximity to airports and populated areas; and 

• Operation of the UAS within visual line of sight of the operator. 

Reform Act Section 333 (a). Lastly. if the Secretary determines that such vehicles '·may operate 

safely in the national airspace system. the Secretary S.Jli!..l.LS':?..l~tl:!li§.b__I~QJJJJiLGn!.\':llJS. for the safe 

operation of such aircraft in the national airspace system.'' ID Section 333(c) {emphasis added) 

'J'he Federal Aviation Act expressively grants the FAA the authority to issue exemptions. 

This statutory authority by its terms includes exempting civil aircraft, as the term is defined under 

section 40101 of the A.ct that includes slJASs, from the requirement that civil aircraft must have a 

current airworthiness certificate. 

Applicant interprets this provision 1.QJ2iac~_J.l}~ dJJ..t.Y_..Q.D_1l!.G._.t\dminbtmmr not only process 

applicants for exemptions under section 333, but for the adn1inistrator to craft conditions for 

the safe operation of the liAS, if it should be deterrnined that the conditions set forth herein 

do not fulfill the statutory requirements for approval. 

2 
The Administrator may gram an exen1ption from a requirement of a regulation 

prescribed under subsection (a) or (b) of this section or any sections 44702-44716 of this title 

if the Administrator find the exemption in the public interest. 49 U.S.C. Section 4470 l (f) see 

also 49 USC Section 4471l(a); 49 USC Section 44704; 14 CFR Section 91.'203 (a) (1). 

NC CERT, INC, sUASs 11xed wing and rotorcraft. weighing 55 or fewer or lbs. including 

payload. They operate, under normal conditions at a speed of no more than 70 knots and in 

the case of our mu1rirotors have a capability to hover, and move in the vertical and horizontal 

plane simultaneously. They will operate in a line of sight and will operate only within the 

sterile area tnade up of farm land, power utility grid and towers. 

Given tl1e small size of the sUASs involved and restricted sterile environment witl1in 

which they wilJ 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 UASs to commence immediately. Also due to the size of t11e UASs 

and the restricted areas in which the relevant sUASs will operate, approval of the application 

presents no national security issue. Given tl1e clear direction in Section 333 of the Reform 

Act the authority contained in the Federal Aviation Act, as amended; the strong equivalent 

level of safety surrounding tl1e proposed operations, and the significant public benetit. 

including enhanced safety, reduction in environmental impacts, including reduced emissions 

and chen1ical spills, exemptions associated with a11owing UASs for agricultural operations, 

the grant of the requested exemptions is in the public interest. According] y, the applicant 

respectfully requests that the FAA grant the requested exemption without delay. 

AIRCRAFT AND EQUIVELANT LEVEL OF SAFETY 

The applicant proposes that the exemption requested herein apply to aircraft that have 

the characteristics and that operate witl1in the limitations listed herein. These limitations 

proyiLi.s;;:_fm:__at Jpast <l.!LQquiva.k'nt_ or even higher level of safety to operations under thq 

current regulatory stmcture because the proposed operations represent a safety enhancement 

to the alreadv safe agricultural services and crops dusted currently being used with 

conventional aircraft. 

3 
1. The sUASs will weigh less than 55 lbs. 

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

3. Maximum tota.l flight time for each operational flight will be 120 minutes for multirotor 

application and 90 minutes for tlxed wing operation. Flights will be terminated at 257~1 

battery power reserve should that occur prior to the 30 minute limit for fixed wing 

operations. 

4. Flights will be operated at an altitude of no more than 1,000 feet l\.GL. 

5. Minimum crew for each operation >vill consist of the sUAS Pilot, and Visual Observer. 

6. slJAS Pilot will be an certified by the aircraft manufacture for operations and have at 

least a sports pilots license, No Medical required. Most pilots wiU have military UAS 

training the observer will hold at least manufactures ground school certificate. No 

medical required. 

7. sUAS Pilot will be pilot in command (PIC). If a pilot certificate holder other than the 

sUAS Pilot vvho possess the necessary PJC qualifications. is also present on set (i.e. the 

aerial coordinator), that person can also be designated as PIC 

8 The U AS will only operate within a confined "sterile area" and have a ·'Security 

Perimeter'' for the flight operations area. 

9. A briefing will be conducted in regard to the planned sUAS operations prior to each 

day's production activities. 1t will be mandatory that all personal who wiLl be performing 

duties within boundaries of the safety perimeter be present for this briefing. 

10. The operator will file a FAA Form 7711-l, or its equivalent, as modified in light of the 

requested exemption, with the appropriate Flight Standards District Office. 

ll. The operator will obtain the consent of all persons involved in the flying area and ensure 

that only consenting persons be allowed within 100 feet of the flight operation, and this 

radius may be reduced to 30 feet based upon an equivalent level of safety and 

determination. With the advanced permissi.on of the FSDO, operations at closer range can 

be approved. 

1 2. The operator will notify a Plan of Activities to the FSDO 30 minutes before the proposed 

flights. 

13. Pilot and observer will have been trained in the operation of UAS generally and received 

up-to-date inl~mnation on the particular UAS. Observer and Pilot \:vill at all times be able 

to communicate by voice or text. 

J 4. Notification of SAR operations will be conducted and/or oral permission ti·om the 

relevant property holders will be obtained prior to flying operations over said location. 

15. All required permissions will be obtained from territorial, state, county, or city 

jurisdictions, including local law enforcement, fire, or other appropriate government 

agencies. 

16. If the sUAS losses communications or it losses its GPS signal, the UAS will have 

capability to return to a pre-determined location within the Security Perimeter and land. 

17. The sUAS will bavc capability to abort Hight in case of unpredictable obstacles or 

emergencies. 

4 
14 C.F.R Part 21, Subpm1 H: Air worthiness certificates 14 C.F.R. Section 91.203 (a) (1) 

Subpart H. entitled Ainvorthiness Certificates. establishes the procedural requirements for the 

issuance of airworthiness certificates as required by FAR Section 91.203 (a)(]). Given the size and 

limited operating area associated with 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 both authorize the FAA to exempt aircraft from the requirement for an airworthiness 

certificate, upon consideration of the size. \veight, speed, operational capability, proximity to airports 

and populated areas of the particular lJAS. In a]] cases, an analysis of these crite1ia demonstrates that 

the UAS operated without an airworthiness certificate. in a restricted environment and under the 

conditions proposed will be at lease as safe, or safer, than conventional aircraft (fixed wing or 

rotorcraft) operating with an airworthiness certificate without the retractions and conditions proposed. 

The sU AS to be operated here under is less than 55 lbs. fully loaded, carries neither a pilot 

nor passenger, cmTies no explosive materials or flammable materials liquid fuels, and operates 

exclusively within a secured area as set out in manual. Unlike other civil aircraft operations under 

this exemption will be tightly controHed and monitored by both the operator and, pursuant to the 

requirements, and in compliance to local public safety requirements, to provide security of the area of 

operation as is now done with conventional flag man. 'l'he FAA will have advance notice of all 

operations. 'l'hese safety enhancements, \vhich already apply to civil aircraft operated in connection 

to agricultural aerial applicators , provide a greater degree of safety to 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 UAS, due to its size, speed of operation, location of operation, lack 

of explosive materials or f1ammable liquid fuels, and inability to cmTy a substantial external load. 

14 C.:F.R. Section45.23 (b). Marking of the aircraft 

'rhe regulation requires: 

When marks include only the Roman capital letter "N'' and the registration of the 

number is displayed on limited. restricted or in a light-sport category aircraft or 

experimental or provisionally certified aircraft, the operator must also display on the 

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 

spot.'' "experimental,'' or ·'provisional,'' as applicable. 

Even though the UAS will have no airworthiness certificate, and exemption may he needed as 

the U AS will have no entrance to the cabin, cockpit or pilot station on which the \VOrd "experimental'· 

can be placed. Given the size of the sUA V, the two inch lettering will be impossible. The word 

''experimental" wi11 be placed on the fuselage in compliance with §45.29 (f). 

The equivalent level of safety will he provided by having the sUA V marked on it fuselage as 

required by *45.29 (f) where the pilot, observer and others working with the sUA V will see the 

identification of the sUA V as "ExperimentaL'' The FAA has issued the following exemptions to this 

regulation to exemptions to this regulation to Exemptions Nos. 10700, 8738. 10167 A. 

5 
14 C.F.R. § 6l.H3 (al & (b): Private pilots Privileges and Limitations: Pilot in Command. 

Sections 61.113 (a) & (b) limit pilots to non-commercial operations. Because the UAS will 

not carry a pilot or passengers, the proposed operations can achieve the equivalent level of safety of 

current operations by requiring the PIC operating the aircraft to have a sport pilot's Certificate rather 

than have than a commercial pilots Certificate to operate this small tJAS. Unlike a conventional 

aircraft that carries a pilot and passengers, the sUAS is remotely controlled with no living thing 

onboarcl. The area of operation is controlled and restricted, and all flights are planned and 

coordinated in advance as set forth by in the S.O.P. The level of safety provided by the requirements 

included in the S.O.P exceeds that provided by a single individual holding a commercial pilot's 

certificate operating a conventional aircraft. The risks associated with the operation of the sUAS are 

so diminished from the level of risk associated with the operation of a commercial operations 

contemplated with Part 61 when drafted. that allowing operations of the sUAS as requested with a 

recreational pilot as the PIC exceeds the present level of safety achieved by 14 C.FR. §61,1 13 (a) & 

(h). 

14 C.F.R. §91.7 (a): Civil A.ircraft Airworthiness. 

The regulation requires that no person may operate a civil aircraft unless it is in airworthiness 

condition. As there will be no ainvorthiness certificate issued for the aircraft should this should this 

exemption be granted, no I''AA regulatory standard will exist for determining airworthiness. Given 

the size of the aircraft and the requirements contained in the SOP for maintenance and use of safety 

check lists prior to each flight, and equivalent level of safety will be provided. 

14 C.l<'.R. § 91.9 (b) (2): Civil Aircraft !<'light Manual in the Aircraft 

Section 9 J .9 (b) (2) provides: 

No person may operate a lJ.S.-registered civil aircraft ... 

(.?.) For which an Airplane or Rotorcraft Flight Manual is not required by §2L5 of this 

chapter, unless there is available in the aircraft a current approved airplane or 

Rotorcraft Flight Manual, approved manual material, markings, and placard, or any 

combination thereof. 

The sUA.S, given its size and configuration has no ability or place to cany such a Hight 

manual on the aircraft, not only because there is no pilot onboard, hut 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 f1ying the sUAS will have access to it Tbe FAA has issued the 

following exemptions to this regulation: Exemption Nos. 8607, 8737. 8738, 9299. 9299/\, 9565. 

95658, 10167, 10602, 32827, and Hl700. 

6 
14 C.F.R. § 9LW3: Preflight action 

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

the safety of the flight. As the FAA approved rotor craft flight manuals will not be provided as set 

forth in sections the SOP. The PIC will take all actions including reviewing weather, night battery 

requirements, landing and takeoff distances and aircraft performance data before initiation of flight. 

14 C.F.R. §9LW9: Flight instruction 

Section 91.1 03 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. 

sUASs and remotely controlled aircraft, by there design do not have fully functioning dual 

controls. Flight control is accomplished though the use of a control box that communicates with the 

aircraft via radio communications. The FAA has approved exemptions for night training without 

fully functioning dual controls for a numher of aircraft and for flight instruction in experimental 

aircraft. See exemption Nos.5778K & 9862A The equivalent level of safety provided by 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 operations of civil aircraft Section 9l.ll9 (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 FA/\. As 

exemption is for the sUAS that is a helicopter and the exemption requests authority to operate at 

altitudes of up to 400 AGL rotorcraft and 1000 AGL for fixed-wing, or not more than 200 above an 

elevated platform such as radio towers. an exemption may be needed to allow such operations. As set 

t~lrth by herein. except for the limited conditions stated in the SOP, the UAS will never operate higher 

than 400 AGL roton:raft and l 000 AGL for fixed-wing. 1t \Viii however be operated in a restricted 

area >vith a security perimeter, where buildings and people will not be exposed to operations without 

their pre-obtained consent. 

·rhe equivalent level of safety will be achieved given the size. weight. speed of the UAS as 

well as the location where it is operated. No Hight will he taken without the permission of the 

property mvner or local officials. Because of the advance notice to the property owner and 

participants in the activity. all affected individuals will be aware of the planned night operations as 

set forth in the SOP. Compared to Hight operations with aircraft or rotorcraft weighing more far more 

than the maximum 551bs. proposed herein and the lack of Hammahk fuel, any risk of 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 i.s set '· ... to the elevation of the departure airport or an appropriate 

altimeter setting available before clepruture." As the sUAS may not have a barometric altimeter. hut 

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 Manual and Safety Check list, confirming the altitude of the 

launch site shown on the GPS altitude indicator before flight. 

7 
14 C.F.R. §91.15l(a): Fuel Requirements for :Flight in V:FR Conditions 

Section 91.151 (a) prohibits and 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 

Hrst 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 40 minutes of powered flight. 'fo 

meet the 30 minute reserve requirement in 14 CFR §91.15 l, slJAS nights would be limited to 

approximately 10 minutes in length. Given the limitations on the UAS's proposed flight area and the 

location of its proposed operations within a predetermined area, a longer time frame for night in 

daylight or night VFR conditions is reasonable. 

Applicant believes that ~m exemption from 14 CFR (a) falls within the scope of prior 

exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without 

compliance with FAR 91.15l(a)'). Operating the small UAS. in a tightly controlled area where only 

people and property owners or oiTicial representatives who have signed waivers will be aHowed. ;vith 

less than 30 minutes of reserve fuel, does not engender the type of risk that Section 91.15l(a) was 

intended to aJJeviate given the size speed of the small UAS. Additionally, limiting sUAS flights to IO 

minutes would greatly reduce the utility for which the exemption \vill be granted. 

Applicant believes that an equiva.lent level of safety can be achieved by limiting nights 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. 

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 

'I'he regulation provides in pertinent part: 

(a) Except as provided in §91.71 5, no person may operate a civil aircraft unless it 

has within it the following: 

(1 J An appropriate and current airworthiness celiiflcate ... 

(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 cockpit entrance so that it is legible to 

passengers or crew. 

'J'he UAS fuLly loaded weighs no more than 55lbs and is operated without an onboard pilot. 

As such, there is no ability or place to carry certification and registration documents or 

display them on the slJAS. 

An equivalent level of safety will be achieved by keeping these documents at the 

ground control point where the pilot flying the sUAS wiH have immediate access to them, to 

the extent they are applicable to the sUAS. The FAA has issued numerous exemptions to this 

8 
regulation. A representative sample of other exemptions includes Exemption Nos. 9565, 

9665, 9789, 9789A. 9797, 9816A, 10700. 

14 C.F.R. §91.405 (a); 407 (a) (2); 417 (a) & {b} 

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 t11at these section and Part 43 apply only to aircraft with an ainvorthiness 

certificate. these sections wiJJ not apply to the application. Maintenance wiLl be 

accomplished by the operator pursuant to the flight manual and operating handbook as 

referenced in the Manual. An equivalent level of safety will be achieved because these small 

UASs are very limited in size and will catTy a smaLl payload and operate only in restricted 

areas for limited periods of time. If mechanical issues arise the UAS can land immediately 

and wiH be operating from no higher than 400 feet AGL rotorcraft and J 000 AGL for fixedwing. As provided in the SOP, the operator will ensure that the UAS is in working order 

prior to initiating flight, perform required maintenance. and keep a log of any maintenance 

preformed. 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. 

Pursuant to 14 C.I•·.R Part l L the following summary is provided for publication in 

the Federal Register. should it be determined that publication is needed: 

Applicant seeks an exemption from the following mles: 

14 C.F.R. §21, subpart H: 14 C.F.R 45.23 (b); 14 C.F.R. §§ 6l.ll3 (a) & (b); 

9L7 (a): 91.9 (b) (2):9J.J03 (b): 9I.I09; 91.119:9U21:9J.l51 (a); 91.203 (a) and (b): 

91.405 (a); 91.407 (a) (1); 91.409 (a) (2) and 91.417 (a) & (h) to operate commercially a 

smaLl unmanned vehicle (551bs or less) in the Agricultural 3d Mapping Service Operations. 

Approval of exemptions allowing SAR operations of sUASs in the search of people 

and for training will enhance safety by reducing risk. Conventional operations using jet or 

piston aircraft, operate at extremely low altitudes just feet from the equipment and livestock 

and structures; and present the risks associated with vehicles that weigh in the neighborhood 

of 3.000-5.000 lbs., canying large amounts of jet A or other fuel in most cases helicopters 

operating with 140 gallon fuel tanks. The sUAS will carry no passengers or crew and. 

therefore, will not expose them to the risks associated with manned aircraft flights. 

The operations of small UASs, weighing less then 55 lbs., conducted in the strict 

conditions outlined above, will provide an equivalent level of safety supporting the grant of 

the Part 21 and aHowing commercial operations. These lightweight UAVs operate at slow 

speeds, close to the ground and in sterile environment and. as a result. are far safer than 

conventional operations conducted with a piston and or turbine aircraft operating close to the 

ground. 

Public Acknovvledgement/Privacy 

Aircraft that are going to be covered are seen in Appendix A 

9 
Appendix A. 

VK- .FF-X4 Mulitirotor 

Arm Length: 320 rnm 

GenVcr Frame Uianwter: 24U mm 

300 mrn {Length) ' 430 mm (Wtdth) 

> :l40 mm (··!ei9t1n 

{Center Piate: 25C rnrn} 

10 
VK>FF -XS Mu!itrotor 

~--·------ ------~! 

FREE FliGHT X8 

Dla;:y:ma} ~;Vt1eelt>ase : 800 mm 

Ann Len9lh ! :320 rnm 

Genter frame Oiarn~ttor: 2-JD mm 

Landing Gem Size : 

420 rnn (Lengtl1} x 4~jl) mrn (\·~·lidH;) 

·< -100 rnm 1}-le!\jtlt) 

{:C'f:.)nt.:::r P~ate: 25-fJ mm} 

ll 
VK-Patriot X4/X8-Photo of airframe for both X4 & X8 configurations 

VK- Ranger EX- SAR :Fixed Wing 

12 
VikingONE SAR Fixed Wing 

13 
VK- Skylark Radio Control.Flight System 

I I 

14 
SAR Autonomous Ground Station and AC Tracking System 

Satisfaction of the criteria provided in Section 333 of the Reform Act of 2012-size. 

weight, speed, operating capabilities, proximity to populated areas and or dose proximity to 

aiqxnts and operations within visual line of sight provides more then adequate justification 

for the grant of the requested exemptions allowing commercial operation of applicant's UAS 

in the agricultural scanning services industry. 

CC: Board Members NC CERT. INC 

Sincerely. 

~~~ .lack Thorpe 

NC CERT, INC 

15