From: Michael J Veer

 204 18th Ave SE

 Devils Lake, ND 58301 (Current Holder of FAA Commercial Pilot Certificate)

To: Federal Aviation Administration

 US Department of Transportation

 Docket Management System

 1200 New Jersey Ave S.E.

 Washington, DC 20590

 

Re: Exemption Request Pursuant to Section 333 of the FAA Reform Act and Part 11 of the Federal 

Aviation Regulations from: 14 CFR 21 subpart H; 14 CFR 45.23(b); 14 CFR 61.113(a) and (b); 14 CFR 

91.7(a); 14 CFR 91.9(b)(2); 14 CFR 91.103; 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:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the “Reform Act”) and 14 

CFR Part 11, Michael Veer, Commercial Pilot and operator of an Unmanned Aircraft System (UAS), 

hereby applies for an exemption from the listed Federal Aviation Regulations (“FARs”) to allow 

commercial operation of its UAS, so long as such operations are conducted within and under the 

conditions outlined herein or as may be established by the FAA as required by Section 333. 

Commercial operation of an UAS, as described herein, which are equipped with camera(s) and sensors, 

would operate in the following manner:

 Aerial photography and/or video for public and/or private use including real estate, architecture, land 

surveying, engineering and other related professional activities.

 Aerial video and/or photography for public and/or private use including television, public events,

cinematography and news gathering.

 Aerial inspection/photography of residential/commercial structures under contract with the owners or 

local government authority.

 Aerial inspection/photography of residential/commercial utility infrastructure including but not limited

to electrical power lines, wind turbines and cell towers.

 Aerial video/photography or providing live video feed to assist with search and rescue operations in 

cases of an emergency or natural disaster only when the local authorities or government has requested 

it by contract or donation.  The ability to offer training to persons individually or belonging to both 

private and/or public organizations that have interests in the use and application of a UAS for the 

purpose of the safe operation of a UAS to enhance the safety of the National Airspace System (NAS) as 

well as for the protection of the persons and property.
As described fully below, the requested exemption would permit the operation of a UAS under 

controlled conditions in the NAS that would be a) limited b) controlled c) predetermined and d) will 

provide safety enhancements to the already safe operations in the industry presently using conventional 

aircraft. Approval of this exemption would thereby enhance safety and fulfill 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 and address of the applicant is:

Michael Veer, Email: mveer@gondtc.com Address: 204 18th Ave SE Devils Lake, ND 58301

Regulations from which the exemption is requested:

14 CFR Part 21 subpart H 14 CFR 45.23 (b) 14 CFR 61.113 (a) & (b) 14 CFR 91.7 (a) 14 CFR 91.9 (b) (2) 14 

CFR91.103 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)

Michael Veer, will operate the DJI Inspire One, with a total weight of 2935g or 6.47lb. The dimensions 

are 438x451x301mm. Under still air the maximum speed is no more than 22m/s or 50mph. The DJI

Inspire one has four motors, Motor Model DJI 3510H, powered by a 5700mAh 6s LiPo LithiumPolymer 

battery. There are four propellers, Propeller Model DJI 1345T, in use. The DJI Inspire One will be 

controlled with the C1 remote controller with an operating frequency of 2.400GHz – 2.483GHz. The live 

video feed will have an operating frequency of 2.4GHz ISM with maximum range of 1.2 miles. The 

applicant will operate the UAS in line of sight within a closed off and predetermined area owned 

and/operated by the property representative.

DJI Inspire One 

GENERAL FEATURES

 Ready to fly  3-axis camera stabilization  Precision flight and stable hovering 

GPS/GLONASSpositioning & auto return home  Onscreenreal-time flight parameters  High Definition

4k Camera  Camera tilt control  Film straight down  Supports Adobe DNG RAW  Adobe lens profile

support  Camera parameter settings  Album synchronization  FAA no-fly zones locked out via 

installed software

TRANSMITTER

 Operating Frequency:2.400 GHz –2.483GHz  Communication Distance(open area): CE: 2000m; 

FCC: 2000m  Receiver Sensitivity(1%PER):-101dBm +/-2dBm  Transmitter Power: CE: 16dBm; FCC:

20dBm  Working Voltage: 1.2A @ 7.4V  Battery: 6000 mAh LiPo 2s

CAMERA  Operating Environment Temperature: 0°C-40°C  Max Resolution: 4096 x 2162p @ 

24/25fps  FOV: 94°/ 85°  Sensor size:1/2.3"  HD Recording: 4k p 24/25fps/720p60fps

DJI VISION APP

 System Requirement of Mobile Device:iOS version 6.0 or above/ Android system version 4.0 or above

 Mobile Device Support:Recommended: iPhone4s, iPhone5, iPhone5s, iPod Touch4, iPod Touch5;
Given the small size of the UAS and the controlled environment provided the proposed operations will 

adhere to the Reform Act’s safety requirements. 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 environmental impacts, including but not limited to reduced emissions and noise, 

the grant of the requested exemption is in the public interest. Accordingly the applicant requests that 

the FAA grant the requested exemption with minimum delay.

AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY

The operation limitations proposed for an equivalent or higher level of safety because operations will 

further enhance the safety of the persons and/or property using conventional aircraft.

These limitations and conditions to which the applicant agrees to adhere to when conducting 

commercial operations under the FAA issued exemption as set forth in the Flight Operations Manual 

(FOM) include:

 The UAS will weigh less than 55 lbs. 

 The UAS will have a maximum operating speed of no more than 55mph.

 Flights will be operated within line of sight of the Pilot in Command (PIC) and/or Visual Observer (VO).

 Maximum flight time for each operational flight will be 20 minutes. Flights will be terminated at 25%

battery power reserve or 20 minutes of flight time whichever occurs first.

 Flights will be operated at an altitude of no more than 400 feet Above Ground Level (AGL).

 Minimum crew for each operation will consist of the UAS Pilot, the Visual Observer (VO) and may

include but not limited to a Camera Operator.

 The UAS pilot will be a designated Pilot in Command (PIC) and will take and pass all necessary 

certifications currently being approved by the FAA administration for commercial use.

 A briefing will be performed regarding the planned UAS operations prior to each day’s flight consisting

of all the days’ production activities.

 All flights will occur under Visual Flight Rules Meteorological Conditions (VMC) only.

 The flights will occur no closer than a 5 mile radius of the geographic center/Airport Reference Point

(ARP) of a tower controlled or uncontrolled airport. The DJI Inspire One has built in software for all FAA 

regulated ‘No Fly Zones’ and was uploaded by DJI (December 2015) for all DJI drones to download and 

prevent any possible flights occurring within no-fly zones. DJI Inspire One has installed software (code) 

that denies flights within the FAA no-fly zones.

 If operations will be within a 5 mile radius of the geographic center/Airport Reference Point (ARP) of a

tower controlled or uncontrolled airport the respective airports will be contacted advising them of the 

estimated flight time, flight duration, elevation of flight and other pertinent information.

 The operator will file FAA Form 7711-1, or its equivalent, as modified in light of the requested 

exemption, with the appropriate local Flight Standards District Office (FSDO) no more than 72 hours but 

no less than 48 hours from planned operation.
 The operator will obtain verbal/written consent of all persons involved with the planned operation

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

radius may be reduced to 30 feet based upon an equivalent level of safety determination, as required 

under the FOM. With the advanced permission of the FSDO, operations at closer range may be 

approved.

 The PIC and VO will have been trained in operation of UAS and receive up-to-date information for the 

particular UAS to be operated.

 The PIC and VO will be able to communicate by voice, radio, and/or text at all times.

 Written and/or verbal permission and permits will be obtained from territorial, state, county or city 

jurisdictions, including law enforcement, fire or other appropriate governmental agencies.

 If the UAS loses communications with the remote controller or loses GPS signal, the UAS will have the

capability to return to a pre-determined location within a designated location and land autonomously.

 The UAS will have the capability to abort a flight in case of unpredicted obstacles, weather, or

emergencies.

14 C.F.R. Part 21, Subpart H: Airworthiness Certificates 14 C.F.R. §91.203 (a) (1)

Subpart H, entitled Airworthiness Certificates, establishes the procedural requirements for the issuance 

of airworthiness certificates as required by FAR §91.203 (a) (1). Given the size and limited operating area 

associated with the 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. The 

Federal Aviation Act (49 U.S.C.§44701 (f)) 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 particular 

UAS. In all cases, an analysis of these criteria demonstrates that the UAS operated without an 

airworthiness certificate, in the restricted environment and under the conditions proposed will be at 

least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft) operating with an

airworthiness certificate without the restrictions and conditions proposed. 

The UAS to be operated hereunder is less than 55 lbs. (3 lbs.) fully loaded, carries neither a pilot nor 

passenger, carries no explosive materials or flammable liquid fuels, and operates exclusively within a 

secured and designated area. Unlike other civil aircraft, operations under this exemption will be tightly 

controlled and monitored by both the operator and under the requirements and in compliance with 

local public safety requirements. The FAA will have advance notice of all operations. These safety 

enhancements provide a greater 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 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 flammable liquid fuels, and inability to carry a substantial external load. 

14 C.F.R. § 45.23 (b).Marking of the Aircraft 

The regulation requires: When marks include only the Roman capital letter "N" and the registration 

number is displayed on limited, restricted or light-sport category aircraft or experimental or 
provisionally certificated aircraft, the operator must also display on that aircraft near each entrance 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. 

Even though the UAS will have no airworthiness certificate, an exemption will be needed as the UAS will 

have no entrance to the cabin, cockpit or pilot station on which the word “Experimental” can be placed. 

Given the size of the UAS, two-inch lettering will be impossible. The word “Experimental” will be placed 

on the fuselage in compliance with §45.29 (f). 

The equivalent level of safety will be provided by having the UAS marked 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 “Experimental.” 

14 C.F.R. § 61.113 (a) and (b): Private Pilot Privileges and Limitations: Pilot in Command.

Pursuant to 14 CFR 61.113 (a) & (b), no person who holds a private pilot certificate may act as a pilot in 

command of an aircraft that is carrying passengers or property for compensation or hire. An equivalent 

level of safety can be 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 inherent in the commercial activities outlined in 14 CFR 61. The operation and limitations 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 may operate a civil aircraft unless it is in airworthy condition. As 

there will be no airworthiness certificate issued for the aircraft, should this exemption be granted, no 

FAA regulatory standard will exist for determining airworthiness. 

Given the size of the aircraft for maintenance and use of safety check lists prior to each flight an 

equivalent level of safety will be provided. 

14 C.F.R. § 91.9 (b) (2): Civil Aircraft Flight Manual in the Aircraft. Section 91.9 (b) (2) provides: No 

person may operate a U.S.-registered civil aircraft ... (2) For which an Airplane or Rotorcraft Flight 

Manual is not required by §21.5 of this chapter, unless there is available in the aircraft a current 

approved airplane or Rotorcraft Flight Manual, approved manual material, markings, and placards, or 

any combination thereof. The UAS, given its size and configuration has no ability or place to carry such a 

flight manual on theaircraft, 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 

keeping the flight manual at the ground control point where the pilot flying the UAS 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 exemption 

will be needed. The PIC will take all actions as stated in the manufacturer FOM in the pre-flight 

inspection section, including but not limited to reviewing weather, flight battery requirements, landing 

and takeoff distances and aircraft performance data before initiation of flight. 
14 C.F.R. §91.109: Flight Instruction. 

Section 91.103 provides that no person may operate a civil aircraft (except a manned free balloon) that 

is being used for flight instruction unless that aircraft has fully functioning dual controls. UAS and 

remotely piloted aircraft, by their design do not have fully functional dual controls. Flight control is 

accomplished through the use of a control box that communicates with the aircraft via radio 

communications. The FAA has approved exemptions for flight training without fully functional dual 

controls for a number of aircraft and for flight instruction in experimental aircraft. The equivalent level 

of safety provided by the fact that neither a pilot nor passengers will be carried in the aircraft and by the 

size and speed of the aircraft. 

14 C.F.R. §91.119: Minimum Safe Altitudes. 

Section 91.119 establishes safe altitudes for operation of civil aircraft. Section 91.119 (d) allows 

helicopters to be operated at less than the minimums prescribed, provided the person operating the 

helicopter complies with any route or altitudes prescribed for helicopters by the FAA. As this exemption 

is for a UAS that is a helicopter and the exemption requests authority to operate at altitudes up to 400 

AGL, or not more than 200 above an elevated platform from which filming is planned, an exemption 

may be needed to allow such operations. As set forth herein, the UAS will never operate at higher than 

400 AGL with the exception that in circumstances where the UAS is used to survey or photograph a 

structure whose height exceeds 400 feet AGL, the UAS will not be operated more than 200 feet above 

the highest point on the structure. It will however be operated in a restricted area with security 

perimeter, where buildings and people will not be exposed to operations without their pre-obtained 

consent. 

The equivalent level of safety will be achieved given the size, weight, speed of the UAS as well as the 

location where itis operated. No flight will be taken without the permission of the property owner or 

local officials. Because of the advance notice to the property owner and participants in the filming 

activity, all affected individuals will be aware of the planned flight operations. Compared to flight 

operations with aircraft or rotorcraft weighting far more than the maximum 55lbs. proposed herein and 

the lack of flammable fuel, any risk 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 UAS will ensure separation between these UAS operations and the operations of 

conventional aircraft that must comply with Section 91.119. 

14 C.F.R. §91.121 Altimeter Settings. 

This regulation requires each person operating an aircraft to maintain cruising altitude by reference to 

an altimeter that is set “...to the elevation of the departure airport or an appropriate altimeter setting 

available before departure.” As the UAS may not have a barometric altimeter, but instead a GPS altitude 

read out, an exemption may be needed. An equivalent level of safety will be achieved by the operator, 

pursuant to the safety check list and live flight data monitoring, confirming the altitude of the launch 

site shown on the GPS altitude indicator before flight. 

14 C.F.R. § 91.151(a): Fuel Requirements for Flight in VFR Conditions 

Section 91.151 (a) prohibits an 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 first point of 
intended landing, and, assuming normal cruising speed – (1) During the day, to fly after that for at least 

30 minutes; or (2) At night, to fly after that for at least 45 minutes.” 

The battery powering the UAS provides approximately 20 minutes of powered flight. To meet the 30 

minute reserve requirement in 14 CFR §91.151, UAS flights 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 flight in daylight or twilight 

VFR conditions is reasonable. 

Applicant believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. 

Operating the UAS, in a tightly controlled area where only people and property owners or official 

representatives who have signed waivers will be allowed, with less than 30 minutes of reserve fuel, does 

not engender the type of risks that Section 91.151(a) was intended to alleviate given the size and speed 

of the small UAS. Additionally, limiting UAS flights to 10 minutes would greatly reduce the utility for 

which the exemption will be granted. Applicant believes that an equivalent level of safety can be 

achieved by limiting flights to 20 minutes or 25% of battery power— whichever happens first. This 

restriction would be more than adequate to return the UAS to its planned landing zone from anywhere 

in its limited 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 may operate a civil aircraft unless it has within it the 

following: 

(1) An appropriate and current airworthiness certificate. . . . 

(b) No person may operate a civil aircraft unless the airworthiness certificate required by paragraph (a) 

of this section or a special flight authorization issued under §91.715 is displayed at the cabin or cockpit 

entrance so that it is legible to passengers or crew. 

The UAS fully loaded weighs no more than 55 lbs. and is operated without an onboard pilot. As such, 

there is no ability or place to carry certification and registration documents or to display them on the 

UAS. 

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

where the pilot flying the UAS will have immediate access to them; to the extent they are applicable 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 section, have discrepancies repaired as prescribed in part 43 of this chapter...,” and 

others shall inspect or maintain the aircraft in compliance with Part 43. 

Given that these section and Part 43 apply only to aircraft with an airworthiness certificate, these 

sections will not apply to the applicant. Maintenance will be accomplished by the operator pursuant to 

the flight manual and operating handbook. An equivalent level of safety will be achieved because the 
UAS is very limited in size and will carry a small payload and operate only in restricted areas for a limited 

period of time. If mechanical issues arise the UAS can land immediately and will be operating from no 

higher than 400 feet AGL. The operator will ensure that the UAS is in working order prior to initiating 

flight, perform required maintenance, and keep a log of any maintenance performed. 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. 

An equivalent level of safety will be achieved because maintenance 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 prior to initiating flight and perform required maintenance 

needed.

Additional Information

The applicant and primary pilot, Michael Veer, has an in-depth understanding of the capabilities and 

safety concerns involved in using this technology as an asset to the community. Satisfaction of criteria 

provided in Section 333 of the Reform Act of 2012 provide more than adequate justification for the 

grant of the requested exemptions allowing the commercial operation of the applicant’s UAS.

Sincerely,

Michael J Veer