January 9, 2016

U.S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590 Re: Exemption Request Under Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation Regulations 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, Focal Revolution, LLC (“Focal Revolution”), operators of small Unmanned Aircraft Systems (“sUAS”), seeks an exemption from the Federal Aviation Regulations (“FARs”) listed below and discussed in Appendix A. The requested exempti on would permit Focal Revolution commercial operation of AgEagle’s 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 (see details in Appendix B), in Precision Agriculture, survey/inspection, closed set cine matography, building inspection, public events, search and rescue, and commercial or reside ntial real estate videography consisting of still photographs, video, and other data taken by onboard sensors. The 2015 AgEagle and DJI Inspire 1 use DroneDeploy so ftware which produces high quality imagery and data that can be used independently – or in the case of surveying and thermal modeling, can be combined to produce precision charts, contour maps and d etermine the health of a crop. Applications for these sUAS include inspection of; mapping and surveying tasks in precision agriculture, crop scouting, crop insurance, hazard mitigation and in support of Federal Crop Management programs. Use of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phan tom 2, Phantom 3, and DJI Inspire 1 for these inspections and surveying applications reduces the need to operate conventional aircraft, providing data more quickly, accurately, economically, safely, and with reduced environmental impact. Operations under the exemption will be subject to strict operating requirements and conditions to ensure at least an equivalent level of safety to currently authorized operations using manned aircraft and under conditions as may be modified by the FAA as required by Sectio n 333. All sUAS will be registered in accordance with 49 U.S.C. 44103. As described more fully below, the requested exemption would authorize Focal Revolution to perform Precision Agriculture, survey/inspection, closed set cinematography, building inspection, public events, search and rescue, and commercial or residential real estate videography using the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1, which are small in size and powered electrically by battery.All sUAS will be operated under controlled conditions at low altitude (<400’ agl) in Class G airspace that

is limited in scope, described more fully herein. The 2015 AgEagle and DJI Inspire 1 will have automated control features, as described below. All sUAS are designed to be operated by one person but flight operations generally involve two people, an operator and an observer. The operator is responsible for flying the sUAS, monitoring its status and flight dynamics while maintaining visual - line - of- sight (VLOS), and keeping the flight within the specified factory limits (in terms of wind, flight range, battery life, et cetera.) to ensure safe operations of the sUAS itself. The observer is responsible for monitoring the airspace for other ai rcraft and hazards and instructing the operator before and during flight as necessary to ensure safe launching and de - confliction with ANY aircraft or identified hazards. The operator also will be and individual who has passed the FAA approved or military equivalent ground training exam. Finally, the airspace in which the sUAS will operate will be disclosed to and approved, as needed, by the FAA in advance. Focal Revolution respectfully submits that because these small, unmanned aerial systems will be us ed in lieu of comparatively hazardous operations now conducted with fixed and rotary wing conventional aircraft, the FAA can have confidence that the operations will achieve at least an equivalent - level or greater, of safety. Approval of this exemption wo uld thereby enhance safety and fulfill the Secretary of Transportation’s (the FAA Administrator’s) responsibilities under Section 333(c) of the Reform Act to “establish requirements for the safe operation of such aircraft systems in the national airspace system.” The name, address and contact information of the applicant are: Focal Revolution Attn: David Wenzlick PO Box 272 New Lothrop, MI 48460 +1 (517) 325 - 3976 david.wenzlick@focalrev.com The regulations from which the exemption is requested are as follows: 14 C.F.R. Part 21; 14 C.F.R. 45.23(b); 14 C.F.R. 6 1.113(a) & (b); 14 C.F.R. 6 1.133(a) 14 C.F.R. 91.7(a) 14 C.F.R. 91.9(b)(2) & (c); 14 C.F.R. 91.103; 14 C.F.R. 91.109(a); 14 C.F.R. 91.119; 1 4 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. 91.407(a)(1); 14 C.F.R. 91.409(a)(2); 14 C.F.R. 91.417(a).Appendix A discusses each rule listed above and explains why exemptions pursuant to the proposal set

forth in this letter are appropriate, provide an equivalent level of safety, and are in the public interest. **THE APPLICABLE LEGAL STANDARD UNDER SECTION 333** Focal Revolution submits that grant of this exemption application for use of the 2015 AgEagle, DJI Spreading Win gs series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 in Precision Agriculture, survey/inspection, closed set cinematography, building inspection, public events, search and rescue, and commercial or residential real estate videography will a dvance the Congressional mandate in Section 333 of the Reform Act to accelerate the introduction of sUASs into the national airspace system (“NAS”) if it can be accomplished safely. This law directs the Secretary of Transportation to consider whether cert ain sUASs may operate safely in the NAS before completion of the rulemaking required under Section 332 of the Reform Act. In making this determination, the Secretary is required to determine which types of sUASs 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 sUASs size, weight, speed, and operational capability;  Operation of the sUAS in close proximity to airports and populated areas; and  Operation of the sUAS within visual line of sight of the operator. Reform Act 333(a)(1). 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 ai rspace system.” Id. 333(c) 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 40101 of the Act, from the requirement that all civil aircraft must have a current airworthiness certificate and those regulations requiring commercial pilots to operate aircraft in commercial service: The Administrator may grant an exemption from a requirement of a regulation prescribed unde r subsection (a) or (b) of this section or any of sections 44702 -4471xx of this title if the Administrator finds the exemption is 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). The grant of the requested exemption is in the public interest based on the clear direction in Section 333 of the Reform Act; the additional authority in the Federal Aviation Act, as amended; the strong equivalent level of safety surrounding the proposed operations; and the significant public benefit, including enhanced safety and cost savings associated with transitioning to sUASs for Precision Agriculture, survey/inspection, closed set cinematography, building inspection, public events, search and rescue, and commercial or residential real estate videography. Accordingly, the applicant respectfully requests that the FAA grant the requested exemption without delay.Mandatory Operating Conditions

Grant of the exemption to Focal Revolution will be subject to the following mandatory conditions, which are based upon operating conditions set forth for operation of sUAS by public entities pursuant to Certificates of Authorization, with additional restrictions:

 All operations to occur in Class G airspace.  Operations to avoid c ongested or populated areas, which are depicted in yellow on VFR charts.  Operations to be conducted over private or controlled - access property.  Permission from land owner/controller required before commencing any flight.  Operations to occur during Visual Flight Rules Meteorological Conditions (VMC).  Aircraft to remain within Visual Line of Sight (VLOS).  VLOS guaranteed with a cylinder of operation around operator of 1⁄2 nautical miles (NM).  Cylinder walls may be expanded by observer with ability to control a ircraft.  Operations to occur during daylight hours.  Above Ground Level (AGL) altitude to be restricted to 400 feet.  All operations conducted in vicinity of airport to remain more than 2.5 NM from centerline azimuth of runway centerline measured from runway thresholds.  Operator will file a NOTAM for each flight.  All required permissions and permits will be obtained from territorial, state, county or city jurisdictions, including local law enforcement, fire, or other appropriate governmental agencies.  All ope rations will include one pilot for flight control and one observer for VLOS enhancement of surrounding area near the aircraft. **Operator Requirements** Focal Revolution respectfully proposes that operator requirements should take into account the characteristics of the particular sUAS. Certain sUASs, such as the 2015 AgEagle, are characterized by a high degree of pre - programmed control and various built - in technical capabilities that limit the potential for operation outside of the operating condi tions set forth above. The 2015 AgEagle sUAS also provides many built - in functional and safety features to assist the operator in safe and reliable operation powered by DroneDeploy risk- mitigation software. The 2015 AgEagle provides two semi - autonomous flight modes using a point - and - click map and video interface. 1 The user clicks on a map to direct the 2015 AgEagle to fly to the point on the map where the operator is pointing, or programmed flight plans may be entered for a series of waypoints or grid ba sed area. Additional navigation aids including landing zones and flight areas may be designated to ensure the 2015

1 AgEagle can submit under confidentiality the following documents in support of this exemption application for the 2015 AgEagl e: 1) AgEagle 2015 AgEagle User Guide which includes Safety and PreFlight Checklists; and 2) Training Manual.AgEagle operates only within user- specified flight parameters. All flight operations are GPS controlled

making the system easy to navigate, and the flight control system also employs a variety of sensors including sonar, barometric pressure, temperature, wind speed and others to ensure the high stability and reliability in challenging weather conditions. At all times during flight operations , the operator can intervene a programmed flight and take immediate control. Using DroneDeploy’s software package, additional automated safety functions and safety enhancing features of the 2015 AgEagle include the following:  Automated pre -flight system p erformance checks  User pre -flight checklist  “Hit the deck” mode can be activated by simply pushing a button on the controller which causes the aircraft to drop from its cruising altitude to 50 feet above the ground and circle there to avoid a collision wit h another aircraft.  Automated condition or fault detection, warnings, and pre - defined responses to a number of flight and system conditions. o High winds with system and user defined safety thresholds. o Low battery with system and user defined safety thresholds. o High temperature or other system safety thresholds. o Lost - link communication  Pre - defined responses include behavior such as attempting to re -establish radio communication, return to home position and hover, return to home position and land, or l and in current position.  In the case of lost GPS, a manual user flight mode is enabled which allows the operator to provide manual navigation inputs to assist in landing the vehicle. Additional automated safety functions and safety enhancing features of t he DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 include the following:  Auto - pilot detection of lost GPS or of insufficient satellites initiates a return home and land  Low power on the sUAS triggers escalating alarms at Ground Control System (“GCS”) at 35% and 10% levels  If the auto - pilot detects a lost - link to the GCS for longer than 30 seconds, landing procedure begins  The sUAS is inherently unstable, so auto - pilot fail will result in very rapid exit from flight  Aircraft has an on - board failsafe Given these safety features, Focal Revolution proposes that operators of the 2015 AgEagle , DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 should not be required to hold a commercial or private pilot certification. Instead, operators should be required to:

 Have successfully completed, at a minimum, FAA private pilot ground instruction and passed the FAA Private Pilot written examination or FAA- recognized equivalents including commercial or private license and ground school issued from an ICAO recognized country;  Have completed AgEagle’s authorized training program for operation and maintenance of the ir sUAS.Focal Revolution notes that the FAA has found that safety factors permitted ope ration of sUAS by

operators with these qualifications in the case of operations pursuant to public COAs when the mandatory operating conditions specified above were present. See Federal Aviation Administration, Notice N - 8900.227, Unmanned Aircraft Systems (UAS) Operational Approval, at 20 - 21 (July 30, 2013). The FAA has the statutory authority to grant exemptions to the requirements for and privileges associated with the grant of airmen’s certificates. 49 USC 44701 (f). In summary, applicant seeks an exe mption from the FARs set forth above and in Appendix C to allow Precision Agriculture, survey/inspection, closed set cinematography, building inspection, public events, search and rescue, and commercial or residential real estate videography operations. Approval of the exemption allowing commercial operations of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 for Precision Agriculture, survey/inspection, closed set cinematography, building inspection , public events, search and rescue, and commercial or residential real estate videography operations will enhance safety by reducing risk. Conventional aerial survey and inspection operations using manned aircraft involve very heavy aerial vehicles carryi ng significant quantities of combustible fuels, and a multi - person crew in piloting and observation roles. These operations require transit to and from the location of the activity, and often take place in congested environments and include close proximity to physical obstacles and/or presence of the general public. By contrast, sUAS are small and use battery for power, transported or carried to/from the area of activity, removes the need for airborne pilots/observers, and poses less risk to people and in frastructure on the ground. Additionally, no national security issue is raised by the grant of the requested exemptions. Given the size, load carrying capacity, speed at which it operates, and the fact that it carries no explosives or other dangerous mat erials, the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 pose no threat to national security. The operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 for Precision Agriculture, survey/inspection, closed set cinematography, building inspection, public events, search and rescue, and commercial or residential real estate videography operations in accordance with the strict conditions outline d above, will provide an equivalent level of safety supporting the grant of the exemptions requested herein, including exempting Focal Revolution from the requirements of Part 21. The 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1’s satisfaction of the criteria set forth in Section 333 of the Reform Act (i.e. size, weight, speed, operating capabilities, operation within VLOS and lack of proximity to airports, populated or areas of national security) and demonstrated equivalent level of safety as it relates to the requirement for FAA pilot certification, provide more than adequate justification for the grant of the requested exemptions allowing Focal Revolution commercial operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 for Precision Agriculture, survey/inspection,closed set cinematography, building inspection, public events, search and rescue, and commercial or

residential real estate vid eography operations. In conclusion, the safe operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 is of utmost concern and safety remains paramount. Focal Revolution intends to operate within the spirit of all applicable FAA regulations and will adhere to any further refinements. Best Regards, David Wenzlick Focal Revolution
**APPENDIX A EXEMPTION REQUEST AND EQUIVALENT LEVEL OF SAFETY SHOWINGS UNDER APPLICABLE RULES**  **SUBJECT TO EXEMPTIO N**  Focal Revolution requests an exemption from the following regulations as well as any additional regulations that may technically apply to the operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Insp ire 1: **14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. 91.203(a)(1)**  Section 91.203(a)(1) requires all civil aircraft to have a certificate of airworthiness. Part 21, Subpart H, entitled Airworthiness Certificates, establishes the proce dural requirements for the issuance of airworthiness certificates as required by FAR § 91.203(a)(1). Given the size of the aircraft (7.5 lbs.) and the limited operating area associated with its utilization, it is unnecessary to go through the certificate of airworthiness process under Part 21 Subpart H to achieve or exceed current safety levels. Such an exemption meets the requirements of an equivalent level of safety under Part 11 and Section 333 of the Reform Act. The Federal Aviation Act and Section 333 of the Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness certificate, upon consideration of the size, weight, speed, operational capability, and proximity to airports and populated areas of the sUAS involved. In this case, an analysis of these criteria demonstrates that the 2015 AgEagle , DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 operated without an airworthiness certificate, under the conditions proposed herein, will be at least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) with an airworthiness certificate. The 2015 AgEagle , DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 weighs less than 50 lbs. fully l oaded. It will not carry a pilot or passenger, will not carry flammable fuel, and will operate exclusively within an area pre - disclosed and in compliance with conditions set forth herein. Operations under this exemption will be tightly controlled and monit ored by both the operator, pursuant to the conditions set forth above, and by local public safety requirements. The FAA will have advance notice ofall operations through the filing of NOTAMs. Receipt of the prior permission of the land owner, the size

of the aircraft, the lack of flammable fuel, and the fact that the aircraft is carried to the location and not flown there all establish the equivalent level of safety. The 2015 AgEagle , DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 provides at least an equi valent, and most likely exceeds, level of safety to that of such operations being conducted with conventional manned aircraft that would be significantly larger and would be carrying additional personnel, cargo, and flammable fuel. **14 C.F.R. 45.23 & 91.9(c): Marking of the Aircraft** Regulation 45.23 provides: (a) Each operator of an aircraft must display on that aircraft marks consisting of the Roman capital letter “N” (denoting United States registration) followed by the registration number of the aircraft. Each suffix letter used in the marks displayed must also be a Roman capital letter. (b) When marks include only the Roman capital letter “N” and the registration number is displayed on limited, restricted or light - sport category aircraft or experimental or provisionally certificated aircraft, the operator must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not less than 2 inches nor more than 6 inches high, the words “limited,” “restricted,” “light - sport,” “experimental,” or “provisional,” as applicable. Regulation 91.9(c) provides: No person may operate a U.S. - registered civil aircraft unless that aircraft is identified in accordance with part 45 of this chapter. The 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 has no entrance to the cabin, cockpit, or pilot station on which the markings can be placed. Given the size of the sUAS, two inch lettering will be imp ossible. **14 C.F.R. 61.113(a) & (b); 61.133(a): Private Pilot Privileges and Limitations; Pilot in Command; Commercial Pilot Privileges and Limitations.**  Section 61.113(a) & (b) limit private pilots to non - commercial operations. Unlike a conventional airc raft that carries a pilot, passengers, and cargo, the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 in this case is remotely controlled with no passengers or property of others on board. Section 61.133 (a) requires an individual with a commercial pilot’s license to be pilot in command of an aircraft for compensation or hire. Focal Revolution respectfully proposes that operator requirements should take into account the characteristics of the particular s UAS. Flight safety is a priority, no matter the operating environment or project. The 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 offers superior safety over manned aircraft by removing the need for people to be onboard in potentially dangeroussituations. With multiple built - in safety features, the AgEagle platform leads other sUAS with respect to

safety.  Intelligent fault handling: The system automatically detects potential issues – with configura ble automated response behavior such as a return - home -and - land routine.  Automatic pre -flight checks: The system self- calibrates all of its sensors and performs self-tests prior to takeoff to check for errors.  No -fly zones: The system has the ability to set up visual no -fly zones.  Self- monitoring: Monitoring battery levels, in -flight wind speeds, and other system and environmental conditions are automatically handled by the system.  Battery communication: Battery minutes and flight time are displayed at all t imes. The system will return home and land automatically if user- configurable limits are reached. Additional automated safety functions and safety enhancing features of the 2015 AgEagle include the following:  Auto detection of lost GPS warns the pilot and initiates an immediate landing.  Low battery on the 2015 AgEagle triggers a Non - Fatal Warning alarm to return home, land and replace the battery.  Very low battery on the 2015 AgEagle triggers a Fatal Error Alarm and initiates an emergency high speed des cent landing.  If the 2015 AgEagle detects a lost- link to the base station the vehicle will perform its pre - defined Non - Fatal Condition Response. Additional automated safety functions and safety enhancing features of the DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 include the following:  Auto - pilot detection of lost GPS or of insufficient satellites initiates a return home and land  Low power on the sUAS triggers escalating alarms at Ground Control System (“GCS”) at 3 5% and 10% levels  If the auto - pilot detects a lost - link to the GCS for longer than 30 seconds, landing procedure begins  The sUAS is inherently unstable, so auto - pilot fail will result in very rapid exit from flight  Aircraft has an on - board failsafe Given these safety features, Focal Revolution proposes that operators of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 should not be required to hold a commercial or private pilot certification. Instead, operators should be required to:  Have successfully completed, at a minimum, FAA private pilot ground instruction and passed the FAA Private Pilot written examination or FAA- equivalents including ICAO issued commercial, private license and ground school;  H ave completed AgEagle’s training program for operation of the sUAS. Focal Revolution notes that the FAA has found that safety factors permitted operation of sUASs by operators with these qualifications in the case of operations pursuant to public COAs whe re the mandatory operating conditions specified above are present. See Federal Aviation Administration, Notice N - 8900.227, Unmanned Aircraft Systems (UAS) Operational Approval, at 20 - 21 (July 30, 2013).The FAA has the statutory authority, granted at 49 U.S.C. 44701(f) to waive the pilot requirements for

commercial operations. Given these conditions and restrictions, an equivalent level of safety will be provided by allowing operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phan tom 2, Phantom 3, and DJI Inspire 1 without a private pilot’s certificate or a commercial pilot’s certificate, under the conditions set forth herein. The risks associated with the operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJ I Phantom 2, Phantom 3, and DJI Inspire 1 (given their size, speed, operational capabilities, and lack of combustible fuel) are so diminished from the level of risk associated with private pilot operations or commercial operations contemplated by Part 61 w ith conventional aircraft (fixed wing or rotorcraft), that allowing operations of the sUAS as set forth above meets or exceeds the present level of safety provided under 14 C.F.R. 61.113(a) & (b) and does not rise to the level of requiring a commercial pil ot to operate the aircraft under 61.133(a). **14 C.F.R. 91.7(a): Civil Aircraft Airworthiness.** This regulation requires that no person may operate a civil aircraft unless it is in airworthy condition. Should the exemption be granted allowing commercial operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 without an airworthiness certificate, no standard will exist for airworthiness of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1. **14 C.F.R. 91.9(b)(2): Civil Aircraft Flight Manual in the Aircraft.** This regulation provides: No person may operate a U.S. - registered civil aircraft... (2) For which an Airplane or Rotorcraft Flight Manual is not required by 21.5 of this chapter, unless there is available in the aircraft a current approved Airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or any combination thereof. Given the size and configuration of t he 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1, it 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 c apacity to carry such an item on the aircraft. The equivalent level of safety will be achieved by keeping the flight manual at the ground control point where the pilot flying the sUAS will have immediate access to it. **14 C.F.R. 91.103: Preflight Action.** This regulation requires each pilot in command to take certain actions before flight to insure the safety of flight. As FAA approved rotorcraft flight manuals will not be provided for the aircraft an exemptionwill be needed. The PIC will take all actio ns including reviewing weather, flight battery requirements,

landing and takeoff distances and aircraft performance data before initiation of flight. **14 C.F.R. 91.109(a) & 91.319(a)(1): Flight Instruction.** These regulations provide 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. The 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspi re 1 are remotely piloted aircraft and by design, do not have fully functioning dual controls. Flight control is accomplished through the use of a control box that communicates with the aircraft via radio communications. If instruction is accomplished th rough a training program, an equivalent level of safety will be assured. 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 Exemptio n Nos. 5778K & 9862A. The equivalent level of safety will be achieved by the manufacturer providing the training as outlined, and through the use of experienced and qualified pilots familiar with the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1. **14 C.F.R. 91.119: Minimum Safe Altitudes.** Section 91.119 establishes safe altitudes for operation of civil aircraft. Specifically, 91.119(c) limits aircraft flying over areas other than congested areas to an altitude of 400 feet above the surface, except over open water or sparsely populated areas. In those cases, the aircraft may not be operated closer than 400 feet to any person, vessel, vehicle, or structure. As set forth herein, the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 will never operate at higher than 400 feet AGL. It will, however, be operated to avoid congested or populated areas that are depicted in yellow on VFR sectional charts. Becau se aerial survey, mapping and inspection work must be accomplished at relatively low altitudes and at altitudes less than 400 feet AGL, an exemption from Section 91.119(c) is needed. The equivalent level of safety will be achieved given the size, weight, speed, and material with which the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 is built. Also, no flight will be taken without the permission of the land owner or those who control the land. Because o f the advance notice to the landowner, all affected individuals will be aware of the flights. Compared to aerial survey operations conducted with aircraft or rotorcraft weighing far more than 50 lbs. and carrying flammable fuel, any risk associated with th ese operations will be far less than those currently allowed with conventional aircraft operating at or below 400 feet AGL. Indeed, the lowaltitude operations of the sUAS will maintain separation between these sUAS operations and the operations of convent ional aircraft that must comply with Section 91.119. **14 C.F.R. 91.151(a): Fuel Requirements for Flight in VFR Conditions.** This regulation prohibits an individual from beginning “a flight in an airplane under VFR conditions unless (considering wind and fo recast weather conditions) there is enough fuel to fly to the first point ofintended 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 2015 AgEagle batteries provide approximately 40 minutes of powered flight. Without an exemption from 14 CFR 91.151, the sUASs flights would be limited to approximately 20 minutes in length. Given the limitations on its proposed operations and the locat ion of those proposed operations, a longer time frame for flight in daylight VFR conditions is reasonable. Operating the sUAS without 30 minutes of reserve fuel does not engender the type of risks that Section 91.151(a) was meant to prevent given the size and speed at which the sUAS operates. The fact that it carries no pilot, passenger, or cargo also enhances its safety. Additionally, limiting flights to 20 minutes would greatly reduce their utility. In the unlikely event that the sUAS should run out of fuel (battery power), it would simply land. Given its weight and construction material, the risks are less than contemplated by the current regulation. Focal Revolution believes that an equivalent level of safety can be achieved by maintaining 10 minutes of reserve fuel, which, allowing 30 minutes of flight time, would be more than adequate to return the sUAS to its planned landing zone from anywhere in its operating area. **14 C.F.R. 91.203(a) & (b): Carrying Civil Aircraft Certification and Registration** T his regulation provides as follows: (a) ... no person may operate a civil aircraft unless it has ... an appropriate and current airworthiness certificate. (b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) of thi s 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 and crew. The 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspi re 1 fully loaded weigh no more than 50 lbs. As such, there is no ability or place to carry certification and registration documents or to display them on the sUAS. In addition, there is no pilot on board the aircraft. An equivalent level of safety will be achieved by keeping these documents at the ground control point where the pilot flying the sUAS will have immediate access to them. The FAA has issued numerous exemptions to this regulation. A representative sample of other exemptions includes Exempt ion 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): Maintenance Inspections.** Section 91.405(a) requires 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 ...”Section 91.407 similarly makes reference to requirements in Pa rt 43; Section 91.409(a)(2) requires an

annual inspection for the issuance of an air worthiness certificate. Section 91.417(a) requires the owner or operator to keep records showing certain maintenance work that has been accomplished by certificated mechan ics, under Part 43, or licensed pilots and records of approval of the aircraft for return to service. The 2015 AgEagle is nearly maintenance free, DroneDeploy’s software performs automatic pre -flight checks and the failure of any check will prevent take -off. Checks which cannot be done by the system will be performed by a qualified person prior to each flight and at predefined intervals as part of the Maintenance Schedule in the User Manual. Pre -flight checklist includes: 1. Visual inspection of the airframe . 2. Visual inspections of rotor integrity. 3. Check charge of all batteries (aerial vehicle, command station, radio repeater station). An equivalent level of safety will be achieved because the sUAS is small in size, will carry no external payload, will operat e only in restricted predetermined areas and is not a complex mechanical device. The operator of 2015 AgEagle will ensure that the sUAS is in working order prior to initiating flight, perform required maintenance, and keep a log of any maintenance that is performed. Moreover, the operator is the person most familiar with the aircraft and is best suited to maintain the aircraft in an airworthy condition and to ensure an equivalent level of safety. The 2015 AgEagle’s Maintenance guidelines ensure an equiva lent level of safety to the maintenance requirements in Part 91. In addition, any component failure detectable by the system will be reported to the control station and will cause the UAV to perform a Fatal Condition Response (FCR) or Non - Fatal Conditioned Response (NFCR), depending on the type of failure. Maintenance of the DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 will be accomplished by Focal Revolution pursuant to the manuals provided by DJI. An equivalent l evel of safety will be achieved because the sUAS is small in size, will carry no external payload, will operation only in restricted predetermined areas and is not a complex mechanical device. Focal Revolution will ensure that the sUAS is in working order prior to initiating flight, perform required maintenance, and keep a log of any maintenance that is performed. Moreover, the operator is the person most familiar with the aircraft and is best suited to maintain the aircraft in an airworthy condition and to ensure an equivalent level of safety. In addition, should a mechanical issue arise, the aircraft will either return to its launch site or immediately land.**APPENDIX B SMALL UNMANNED AERIAL SYSTEM DESCRIPTION** 

**2015 AgEagle 2**  The 2015 AgEagle can carry payloads up to 2.5 pounds. The 2015 AgEagle flies at a maximum wind threshold of 43 M.P.H. for sustained winds and wind gusts up to 55 M.P.H. What is unique about the 2015 AgEagle is the system automatically compensates for wind versus relying on the operator’s ‘sense of feel’ for what the impact of the wind is at the altitude the system is flying. The end result is a system capable of gathering high quality aerial intelligence at much higher wind thresholds. A trait that is imperative for many ae rial inspection operations. The 2015 AgEagle has an operational range of up to 20 statute miles (17.38 Nautical Miles). All flight operations are GPS controlled making the system extremely easy to navigate. At any point if the operator is not explicitly commanding the system to move, the system automatically holds its GPS position (i.e. GPS hold for reliable location hover). Camera positioning is also GPS controlled allowing for the most sophisticated camera targeting available. The flight control system employs not only GPS positioning but a variety of sensors including sonar, barometric pressure, temperature, wind speed and others to ensure the most stability of any system in its class - regardless of the wind. Powered by DroneDeploy, the 2015 AgEagle c an be operated in both semi and fully autonomous flight modes. Creating preplanned flight paths to fly in autonomous mode is as simple as clicking on the map to create a preplanned flight path. In semi - autonomous mode, the operator clicks on the map and th e AgEagle 2015 AgEagle automatically flies to the point on the map where the operator is pointing. Pre mission waypoints, Landing zone points and flight area dimensions can all be entered during preflight ensuring the 2015 AgEagle operates only within spec ified parameters. The 2015 AgEagle includes many advanced safety features that make it the safest choice for both urban and non - urban environments. Built - in intelligent fault handling allows the 2015 AgEagle to detect a system fault while in the air, and to automatically fly back to its take -off location and land. Faults that can be detected include: loss of communication; pre - set wind thresholds exceeded; and low battery levels. In addition, the operator can create no fly zones or maximum flight ranges an d altitudes so the system cannot enter areas deemed unsafe or unnecessary to fly over. And before every take -off automated flight checks ensure the system is flight ready before it takes off. The 2015 AgEagle can be operated entirely by a touch - screen, m ap based interface. This means the operator only needs to command the system where to go, and the system does all the flying for the operator. Maps can be saved and flight plans can be made or recalled.

2 All system specifications are from manufacturer.**2015 AgEagle Operating Manual** - System user manual a vailable upon request.

**2015 AgEagle Continued...** Physical Characteristics: Measurements – 56” wingspan x 6.5” long Weight (without payload but with batteries) – 7 lbs. Weight with payload (T/O weight) – 7.5 lbs. Fuel – Batteries Landing style/type – Belly landing Propulsion System  Engines – The 2015 AgEagle is powered by 1 electric brushless DC motor.  Batteries – Lithium polymer batteries are self- contained high duration systems with SMART intelligence on - board. This includes cycle charge times, locations, GPS antenna, chemical management, and real -time data feeds to ensure maximum flight duration and sub - system safety processes. Charging is done in the included AgEagle Battery charger and can be charged via standard wall outlet, or via a vehicle. Perform ance Characteristics:

 Maximum Altitude – 400’ AGL  Maximum Endurance – 40 minutes  Maximum Range – VLOS (Visual Line of Sight)  Weather Minimums – NA  Winds Maximum – 40 MPH  Minimum Ceiling – VLOS (Visual Line of Sight)  Minimum Visibility – VLOS (Visual Line of Sight)  Icing Conditions – No icing conditions  Precipitation – No visible moisture Maintenance - The UAS is nearly maintenance free, it performs automatic pre -flight checks and the failure of any check will prevent take -off. Checks which cannot be done by the system will be performed by a qualified person prior to each flight. Preflight Checklist:

 Visual inspection of the airframe  Visual inspections of rotor integrity  Check charge of all batteries (aerial vehicle, command station, radio repeater station) Reliability - The system is designed for maximum reliability and to maintain performance over its life.The only components experience routine wear are rotors, batteries, motors, and legs. Battery and motor

conditions are monitored by the syste m with deviations reported to the operator. **2015 AgEagle Continued...** Contact with other objects during flight may cause other components, particularly rotors, and motor arms, to become damaged. Damaged components are likely to be detected during the full visual inspection of the airframe performed before each flight. Structural damage affecting flight characteristics will be detected by on - board sensors. The UAV system detects numerous conditions which may make flying unsafe, such as reduced GPS accuracy, magnetic anomalies, low battery charge, battery cell imbalances, and temperature fluctuations. Automatic pre -flight checks prevent the sUAS from taking off if such conditions are present; or, if the condition is detected during flight, the system will tri gger a Fatal Conditioned Response. Command and Control Systems - The 2015 AgEagle Ground Control station allows the operator simultaneous control over aircraft and payloads. The touch screen control allows for quick navigation and data entry while the dis play screen provides all essential flight data to the operator. Telemetry data is transmitted to the command station at least once per second. Displayed on GCS:  sUAS Position  Navigation Route  sUAS Tail Number  sUAS Position  sUAS Altitude  sUAS Heading  North Seeking Arrow  Range to Target  Calculated Target Position  Date/Time  Sensor Heading and Orientation Relative to sUAS On - Board Flight Instruments - The sUAS is equipped with an Inertial Navigation System (3 - axis gyroscope, 3 - axis magnetometer, GPS receiver, and static pressure sensor) and a sonar sensor for precision AGL altitude measurement. On - Board Computer Systems - The sUAS is equipped with on - board com puter systems to monitor (sensors, battery, etc.), control (speeds, altitude, position, etc.), and communicate (control, telemetry, etc.). Frequency Allocations - 900 MHz, 2.4 GHz, 5.8 GHz, 1,700 – 2,100 MHz, custom Flight Termination Link – To prevent a “fly away” or other potentially dangerous situation a flight termination link is available to the operator at the GCS.**2015 AgEagle Continued...**

Takeoff and Landing - The 2015 AgEagle has vertical lift autonomous launch and recovery. A Landing Zone “LZ” is designated by the operators and identified in the GCS software. Navigation System - Specific maps can be downloaded to the display screen (such as air sectional and geographic maps) which are overlaid with GPS positional data. Waypoints can be created before and during flight operation creating specific locations and sequences for the aircraft. Redundant Systems - The sUAS combines the input from a multitude of sensors. Even though the data from all sensors is required for optimal system performance, a single sensor malfunction is likely to result in degraded performance rather than leading to a catastrophic failure. **Emergency Procedures and System Failures** Failure Handling - The sUAS has extensive failure detection and handling capabilities. All fail ures are deeded to be either fatal or non -fatal. Failures classified as fatal result in a Fatal Condition Response (FCR); and failures classified as non -fatal result in a Non - Fatal Condition Response (NFCR). Sensor Failure - Failure of on - board flight instruments/sensors will degrade the sUAS performance and will result in either a FCR or a NFCR, depending on their severity. Airframe Failure - If airframe is damaged in ways that impacts flight characteristics, the sUAS will behave similar to if an on - board flight instrument failed. Navigati on System Failure – In a navigation system failure, degraded GPS will result in FCR or NFCR‘s depending on failures. Power Failure – A complete battery failure which results in power loss to the sUAS will result in degraded flight performance. Low Battery Condition - Operator will be alerted of a low battery condition and will land the aircraft as soon as able. Line of Sight Loss - All flight operations will be conducted with the sUAS within visual sight of the pil ot. If the pilot’s view becomes obstructed and line -of- sight is lost, the pilot may instruct the UAS to hover in place until line -of- sight is reestablished, to return to the take - off position, or to land at the current position. Security – The system and communication links are encrypted by the manufacturers proprietary software.**DJI Spreading Wings S1000+ 3** 

**Frame:** Diagonal wheelbase: 1045mm Frame Arm Length: 386mm Frame Arm Weight: 325g (including motor, ESC, propeller) Center Frame Diameter: 337mm Center Frame Weight: 1520g (with landing gear mounting base, servos) Landing Gear Size: 460mm length x 511mm width x 305mm height **Motor:** Stator Size: 41x14mm KV: rpm/v Max Power: 500W Weight: 158g (with cooling fan) **Electronic Speed Control:** Working Current: 40A Working voltage: 6S LiP o Signal Frequency: 30Hz – 450Hz Drive PWM Frequency: 8 KHz Weight: 35g (with radiators) **Foldable Propeller:** Material: High strength performance engineered plastics Size: 15x5.2Inch Weight: 13g **Flight Parameters:** Takeoff Weight: 6 - 11Kg Total Weight: 4.4Kg Power Battery: LiPo (6S, 10000mAh & 9.Kg Takeoff Weight) Working Environment Temperature: - 10C - +40C **Gain Value Settings:** For A2 Flight Controller: Basic: Roll 120%, Pitch120%, Yaw 120% Attitude: Roll 170%, Pitch 170%, Vertical 170% For WooKong- M Flight Controller: Basic: Roll 130%, Pitch130%, Yaw 120% Attitude: Roll 180%, Pitch 180%, Vertical 120%

3 All system specifications are from manufacturer.**DJI Spreading Wings S1000 4** 

**Frame:** Diagonal wheelbase: 1045mm Frame Arm Length: 386mm Frame Arm Weight: 325g (including motor, ESC, propeller) Center Frame Diameter: 337.5mm Center Frame Weight: 1330g (with landing gear mounting base, servos) Landing Gear Size: 460mm length x 511mm width x 305mm height **Motor:** Stator Size: 41x14mm KV: 400rpm/V Max Power: 500W Wei ght: 158g (with cooling fan) **Electronic Speed Control:** Working Current: 40A Working voltage: 6S LiPo Signal Frequency: 30Hz – 450Hz Drive PWM Frequency: 8 KHz Weight: 35g (with radiators) **Foldable Propeller:** Material: High strength performance engineered plastics Size: 15x5.2Inch Weight: 13g **Flight Parameters:** Takeoff Weight: 6 - 11Kg Total Weight: 4.2Kg Power Battery: LiPo (6S, 10000mAh & 9.Kg Takeoff Weight) Max Power Consumption: 4000W Hover Power Consumption: 1500W (@9.5Kg Takeoff Weight) Hover Time: 15min (@15000 mAh & 9.5Kg Takeoff Weight) Working Environment Temperature: - 10C - +40C **Gain Value Settings:** For A2 Flight Controller: Basic: Roll 120%, Pitch120%, Yaw 120% Attitude: Roll 170%, Pitch 170%, Vertical 170%

4 All system specifications are from manufacturer.For WooKong- M Flight Controller: Ba sic: Roll 130%, Pitch130%, Yaw 120%

Attitude: Roll 180%, Pitch 180%, Vertical 120% **DJI Phantom 2 5**  General Features –  Ready to Fly, Multifunctional Quad - rotor System  Customized H3 - 2D and H3 - 3D Gimbal Support  Precision Flight and Stable Hovering  25min Flig ht Time & Smart Battery  Auto Return -to - Home & Landing  Advanced Power Management  Intelligent Orientation Control (IOC)  Easy Battery Replacement  Self-tightening Propeller  Video Downlink Support  CAN - Bus Expansion Module Aircraft –  Weight (Battery & Propellers Included) o 1000g  Hover Accuracy (Ready to Fly) o Vertical: 0.8m; o Horizontal: 2.5m  Max Yaw Angular Velocity o 200 degrees/second  Max Tilt Angle o 35 degrees  Max Ascent/Descent Speed o Ascent: 6m/s; o Descent: 2m/s  Max Flight Speed o 15m/s (not recommended)  Diagonal Length o 350mm  Flight Time o 25 minutes  Take - off Weight o <1300g  Operating Temperature o - 10C ~ 50C  Supported Battery o DJI Smart Battery  Battery Type o 3S LiPo  Battery Capacity
5 All system specifications are from manufacturer.o 5200mAh, 11.1V

DJI Smart Battery –  Charging Environmental Range o 0C to 40C  Discharging Environmental Range o - 20C to 50C 2.4GHz Remote Control –  Operating Frequency o 2.4GHz ISM  Communication Distance (Open Area) o 1000m  Receiver Sensitivity (1%PER) o - 97dBm  Working Current/Voltage o 120 mA@3.7V  Built - In LiPo Battery Working Current/Capacity o 3.7V, 2000mAh **DJI Phantom 3 6**  Aircraft –  Weight (Battery & Propellers Included) o 1280g  Diagonal Length (Including Propellers) o 350mm  Max Ascent/Descent Speed o Ascent: 5m/s; o Descent: 3m/s  Hover Accuracy o Vertical: +/
- 0.1m (when Vision Positioning is active) or +/
- 0.5 m o Horizontal: +/
- 1.5 m  Max Flight Speed o 16m/s (ATTI Mode, no wind)  Max Altitude Above Sea Level o 6000m  Operating Temperature o 0C to 40C Camera –  GPS Mode o GPS/GLONASS  Sensor o Sony EXMOR 1⁄2.3” Effective pixels: 12.4 M (total pixels: 12.76 M)  Lens

6 All system specifications are from manufacturer.o FOV 94 degree 20mm (35mm format equivalent) f/2.8

 ISO Range o 100- 3200 (video) 100 - 1600 (photo)  Shutter Speed o 8s – 1/8000s  Image Maximum Size o 4000 x 3000  Still Photography Modes o Single shot o Burst shooting: 3/5/7 shots o Auto Exposure Bracketing (AEB): 3/5 o Bracketed Frames at 0.7EV Bias o Time - lapse  Video Recording Modes o Phantom 3 Pro  UHD: 4096x2160p 24/25, 3840x2160p 24/25/30  FHD: 1920x1080p 24/25/30/48/50/60  HD: 1280x720p 24/25/30/48/50/60 o Phantom 3 Advanced  FHD: 192 0x1080p 24/25/30/48/50/60  HD: 1280x720p 24/25/30/48/50/60  Supported SD Card Types  Micro SD  Max Capacity: 64 GB Class 10 or UHS - 1 rating required  Max Bitrate of Video Storage  Phantom 3 Pro o 60 Mbps  Phantom 3 Advanced o 40 Mbps  Supported File Formats  FAT32/exFAT  Photo: JPEG, DNG  Video: MP4, MOV (MPEG -4 AVC/H.264)  Gimbal o Operating Temperature  0C to 40C o Controllable Range  Pitch - 90 degrees to +30 degrees o Stabilization  3 axis (pitch, roll, yaw) o Max Velocity  Less than 8 m/s (when 2m above ground)  Vision Position ing o Altitude Range  30cm – 300cm o Operating Range  30cm – 300cmo Operating Environment  Surface with clear pattern and adequate lighting (Lux > 15)  Remote Controller o Operating Frequency  2.400 GHz – 2.483 GHz o Maximum Distance  2000m (outdoors and unobstructed) o Video Output Port  USB o Operating Temperature  0C to 40C o Battery  6000 mAh LiPo 2S o Mobile Device Holder  For tablet or phone o Receiver Sensitivity  - 101 dBm +/
- 2dBm o Transmitter Power (EIRP)  FCC: 20 dBm  CE: 16 dBm o Working Voltage  1.2 A @ 7.4 V o Voltage  17.4 V  Batt ery Charger o Phantom 3 Pro  100w o Phantom 3 Advanced  57w o Capacity o 4480 mAh o Voltage o 15.2 V o Battery Type o LiPo 4S o Energy o 68 Wh o Net Weight o 365g o Maximum Flight Time o Approximately 23 minutes o Operating Temperature o - 10C to 40C**DJI Inspire 1 7** 

Weight (Battery Included)  2935 g Hovering Accuracy (GPS Mode)  Vertical: 0.5m  Horizontal: 2.5m Maximum Angular Velocity  Pitch: 300 degrees/s  Yaw: 150 degrees/s Maximum Tilt Angle  35 degrees Maximum Ascent Speed  5 m/s Maximum Descent Speed  4 m/s Maximum Speed  22 m/s (ATTI m ode, no wind) Maximum Flight Altitude  4500 m Maximum Wind Speed Resi stance  10 m/s Maximum Flight Time  Approximately 18 minutes Motor Model  DJI 3510 Propeller Model  DJI 1345 Indoor Hovering  Enabled by default Operating Temperature Range  - 10C to 40C Diagonal Distance  559 to 581 mm Dimensions  438x451x301 mm

7 All system specifications are from manufacturer.**APPENDIX C SUMMARY OF FOCAL REVOLUTION SECTION 333 EXEMPTION REQUEST** 

Focal Revolution provides pursuant to Part 11, a summary of its exemption application to allow commercial operation of the 2015 AgEagle, DJI Spreading Wings series S1000+, S1000, DJI Phantom 2, Phantom 3, and DJI Inspire 1 small unmanned system in: Precision Agriculture, survey/inspection, closed set cinematography, building inspection, public events, search and rescue, and commerci al or residential real estate videography operations. An exemption is requested from the following regulations: 14 C.F.R. Part 21; 14 C.F.R. 45.23(b); 14 C.F.R. 61.113(a) & (b); 14 C.F.R. 61.133(a) 14 C.F.R. 91.7(a) 14 C.F.R. 91.9(b)(2) & (c); 14 C.F.R. 91.103; 14 C.F.R. 91.109(a); 14 C.F.R. 91.119; 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. 91.407(a)(1); 14 C.F.R. 91.409(a)(2); 14 C.F.R. 91.417(a).