May 13, 2015

U.S. Department of Transportation Docket Management System

1200 New Jersey Avenue, SE Washington, DC 20590

RE: Exemption Request, under Section 333 of the FAA Modernization and Reform Act,

from 14 CFR Part 21; 14 CFR 61.113(a); 14 CFR 91.7(a); 14 CFR 91.9(b)(2); 14 CFR

91.105; 14 CFR 91.119(c); 14 CFR 91.121; 14 CFR 91.151(a)(1); 14 CFR 91.203(a)(1);

14 CFR 91.203(b); 14 CFR 91.405(a); 14 CFR 91.407(a)(1); 14 CFR 91.409(a)(1) &

(a)(2); 14 CFR 91.417(a) & (b).

Dear Sir or Madam:

I, Jesse Slesar, am writing pursuant to the FAA Modernization and Reform Act of 2012

and the procedures contained within 14 CFR Part 11 to request that I, Jesse Slesar, an

owner and operator of a small unmanned aircraft system, be exempted from certain

Federal Aviation Regulations (“FARs”) listed in Table 1 in order to allow commercial

operations of my small, unmanned aircraft system (sUAS) for aerial imaging,

photography, and videography of properties and events.

Section [1] enumerates the regulations from which exemption is being requested in order

to permit the operation of a small, lightweight sUAS under controlled conditions and in a

predetermined and clearly bounded space for the purpose of aerial imaging, photography,

and videography of properties and events. These regulations that pertain to the sUAS

platform itself are further discussed in Section [2], along with additional measures to

maintain the current level of safety. Section [4] discusses exemptions pertaining to the

operator, and how any potential risks are mitigated by limiting operation to a trained,

certificated pilot-in-command (PIC) with a visual observer (VO). Section [5] examines

exemptions pertaining to flight operations and how safety will be maintained at an

equivalent or higher level than current approaches by implementation of Standard

Operating Procedures (SOP). Finally, Sections [6] and [7] include a summary for the

Federal Register and concluding remarks, respectively.

With the platform, personnel, and procedures contained herein in place, as well any

additional guidance from the FAA in consideration of this exemption, it is my strong

belief that these sUAS operations will meet and exceed the current level of safety and

environmental impact of larger scale manned aircraft that currently perform these

functions. Approval of this exemption would thereby enhance safety, reduce

environmental impact, and fulfill the responsibility of the Secretary of Transportation (the

FAA Administrator) to “...establish requirements for the safe operation of such aircraft

Jesse Slesar

509-879-5128

jesseslesar@gmail.com

1704 E Dalke

Spokane, Wa

99208

SKY DEFINITION PHOTOGRAPHY
systems in the national airspace system” pursuant to Section 333(c) of the FAA

Modernization and Reform Act of 2012.

[1] REQUEST FOR EXEMPTION FROM CERTAIN PARTS OF 14 CFR

The applicant hereby petitions the Secretary of Transportation and Federal Aviation

Administration for exemption to the below referenced (in Table 1) and, in Sections [3] to

[5] more fully described, Federal Aviation Regulations that currently may apply to the

commercial use of a small, unmanned aircraft system.
Table 1 - List of Requested Exemptions

This exemption request is expressly submitted to fulfill Congress’s goal in passing the

FAA Modernization and Reform Act of 2012 (FMRA), Sections 333(a) through 333(c).

This law directs the Secretary of Transportation to consider whether certain UAS may

operate safely in the national airspace system before completion of the rulemaking called

for under Section 332 of the same Act.

The Modernization and Reform Act of 2012 further states, if “the Secretary determines

under [Section 333] that certain unmanned aircraft systems may operate safely in the

national airspace system, the Secretary shall establish requirements for the safe operation
of such aircraft systems in the national airspace system.” The applicant interprets this

provision to place the duty on the Secretary to not only process applications for

exemptions under Section 333, but for the Secretary to affirmatively craft conditions for

the safe operation of sUAS, should it be decided that the conditions of this application do

not fulfill the statutory requirements for approval.

Recently, the framework for precedent in this area has also been established with the

granting of several exemptions on the grounds of Section 333, whereby safety to the

national airspace system has been maintained. Some of these recent exemptions, which

provide some obvious and apparent similarities to the current exemption request, are

Exemption 11138 (Douglas Trudeau), Exemption 11062 (Astraeus Aerial), Exemption

11109 (Clayco, Inc), and Exemption 11110 (Trimble Navigation Ltd).

[2] RELATING TO THE SMALL, UNMANNED AIRCRAFT SYSTEM [3.1]

OVERVIEW AND SUPPORTING INFORMATION

The applicant petitions herein to exempt operations with a Phantom 2 and Syndrones

frame with Mikrokopter flight controller (the sUASs). The Phantom 2 and Syndrone are

lightweight sUASs, they carry no people or combustible fuel, and have several built-in

safety features in the event of flight emergencies. Based on the physical and safety

features of the Phantom 2 and Syndrone, along with previous findings in Exemption

11138 (Douglas Trudeau), it is believed that this platform falls under the purview of

Section 333, is able to meet or exceed acceptable safety levels, and is appropriate for

exemption.

Lightweight, small UAS. The complete specifications and operating limits for the

Phantom 2 can be found in the Phantom 2 User Manual, supplied as an attachment to this

petition and the Syndrones frame and Mikrokopter flight controller can be found on their

respective websites. However, it is instructive to highlight some of the more pertinent

operational limits that bound the risk of usage of these sUASs

 Maximum dimension of the Phantom 2 is less than 23 inches, which counts the

maximum diagonal distance including maximum swept area of the propellers and no less

than 49 inches on the Syndrome.

 Maximum weight for the Phantom 2 Vision + configurations flown under this petition

are less than 3 lbs with imaging sensors onboard and Maximum weight on the Syndrone is

30 lbs.

 Maximum speed for the Phantom 2 and Syndrone is 30 mph. In practice, neither

sUASs are ever flown at maximum speeds for the requested application (see Section
[5.1]) as it is contrary to the objective of sharp photographs or smooth video. For

reference, even at maximum speed, the momentum of the Phantom is comparable to a

kicked soccer ball.

 Maximum flight time is limited to 20 minutes by available charge stored in the onboard

battery.

 Exceptional agility is provided by yaw rates up to 200°/sec and 20 ft/sec climb rates.

This agility allows both sUASs to be safely operated in smaller, less accessible spaces

than could ever be imagined with conventional aircraft. Also, avoiding obstacles or

responding to flight emergencies can be accomplished with significantly less standoff

distance than is currently required for larger, manned aircraft.

No occupants and benign cargo. A significant risk mitigation is provided by virtue of the

fact that the sUAS is inherently unmanned. Any risk of injury to people onboard the

aircraft is completely eliminated. This provides a significant safety upgrade over current

operations that use manned helicopters to provide similar services. Low flying helicopters

near tree lines not only endanger occupants of the helicopter, but also people on the

ground. The sUAS avoids the risk to occupants completely. Additionally, both are electric

sUAS, the absence of a combustible fuel is an important factor in reducing risk to people

and property on the ground should an accident occur.

Built-in safety features. Both sUASs have safety features to mitigate two of the most

common malfunctions for sUAS – loss of communication with the base station and low

battery levels.

 Both mitigate loss of communication (e.g., exceeding transmitter range, blocked RF

signal, electrical malfunction) by incorporating GPS functionality. Both record the

“home” GPS coordinates (set automatically on startup, verified during the preflight

inspection). Then, if communication is lost during flight, the sUAS can hover in place to

see if signal is restored or initiate a “Return to Home,” returning to the “home” GPS

coordinates and executing a landing there.

 If the battery reaches a critically low level, the “Return to Home” feature is also

initiated. This feature returns the unit back to the “home” location and executes a landing

before power is lost. This feature, and Standard Operating Procedures discussed in

Section [4], mitigate one of the most tangible risks to sUAS – exhausting onboard battery

charge that often leads to a crash.
 The sUAS also features a programmable maximum altitude and horizontal range to

prevent accidental flight boundary excursions (limits set to 400 feet and 2000 feet,

respectively).

 Finally, the sUAS includes software-defined “restricted areas” around airports where

the

Neither will not be able to operate. This is supplemented by Standard Operating

Procedures which further reduce operating areas, as discussed later.

[2.2] REQUESTED EXEMPTION FROM 14 CFR Part 21 AND 14 CFR §91.203(a)(1)

Text of Cited Regulation:

 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. Each U.S.

airworthiness certificate used to comply with this subparagraph (except a

special flight permit, a copy of the applicable operations specifications

issued under § 21.197(c) of this chapter, appropriate sections of the air

carrier manual required by parts 121 and 135 of this chapter containing that

portion of the operations specifications issued under § 21.197(c), or an

authorization under § 91.611) must have on it the registration number

assigned to the aircraft under part 47 of this chapter. However, the

airworthiness certificate need not have on it an assigned special

identification number before 10 days after that number is first affixed to the

aircraft. A revised airworthiness certificate having on it an assigned special

identification number, that has been affixed to an aircraft, may only be

obtained upon application to an FAA Flight Standards district office.

Reason for Exemption: 14 CFR Part 21, Subpart H, establishes the procedural

requirements for the issuance of airworthiness certificates as required by 14 CFR

§91.203(a)(1). Given the small size, modest maximum speed, and limited operating area

associated with the sUAS to be used by the applicant, an exemption from Part 21 and

§91.203(a)(1) meets the requirements of an equivalent level of safety under Section 333

of the FAA Modernization and Reform Act of 2012. The Federal Aviation Act (49 USC

§44701(f)) and Section 333 of the FMRA both authorize the FAA to exempt aircraft from

the requirement of an airworthiness certificate, upon consideration of the size, weight,

speed, operational capability, proximity to airports and populated areas, and operation

within visual line of sight of the sUAS. In all cases, an analysis of these criteria
demonstrates that the sUAS operated without an airworthiness certificate, in the limited

environment and conditions proposed herein, will be at least as safe, or safer, than a

conventional rotorcraft aircraft operating with an airworthiness certificate. The applicant

respectfully requests confirmation that this sUAS does not require airworthiness

certification, as allowed under Section 333 of the FMRA.

Mitigation Basis: Safety of the general public and the national airspace will be preserved

by the safety features of the sUAS platform described in [2.1], the training and

certification of the operator described in [3.1], and the additional operational limitations

discussed in [4] and supplemented by the Standard Operating Procedures attached to this

petition.

Previous clarification that, in relation to a similar sUAS, Part 21 Subpart H was not

applicable, and therefore the sUAS does not require an airworthiness certification, was

granted in Exemption 11138 (Trudeau).

[2.3] REQUESTED EXEMPTION FROM 14 CFR §91.203(b)

Text of Cited Regulation:

(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.

Reason for Exemption: It is believed that, per the request for relief in [2.2] of this petition

and recent rulings by the FAA (cf., Exemptions 11138, 11062, and 11110), that an

airworthiness certificate is not required for this sUAS. The cited portion of § 91.203(b)

seemingly does not allow for aircraft that have been determined by the FAA to not need

an airworthiness certificate. Thus, if this sUAS is decided not to need an airworthiness

certificate (either under 14 CFR § 91.203(a)(1) or § 91.715), a waiver to 14 CFR

§91.203(b) is being requested.

Mitigation Basis: Safety of the general public and the national airspace will be preserved

by the safety features of the sUAS platform described in [3.1], the training and

certification of the operator described in [4.1], and the additional operational limitations

discussed in [5] and supplemented by the Standard Operating Procedures attached to this

petition.
Previous clarification that, in relation to a similar sUAS, Part 21 Subpart H was not

applicable, and therefore the sUAS does not require an Airworthiness certification, was

granted in Exemption 11138 (Trudeau).

[2.4] REQUESTED EXEMPTION FROM 14 CFR §91.7(a) Text of Cited Regulation:

(a) No person may operate a civil aircraft unless it is in an airworthy condition.

Reason for Exemption: This regulation requires that no person operate an aircraft unless it

is in an airworthy condition. However, should [2.2] of this exemption be granted, there

will be no airworthiness certificate issued to this aircraft. Therefore, no FAA regulatory

standard will exist for determining airworthiness to fulfill this requirement. Therefore,

relief from §91.7(a) is requested.

Mitigation Basis: An equivalent level of safety will be provided by the conflation of

several factors. These factors include the low weight of the sUAS (cf., [2.1]), the modest

maximum speed of the sUAS (cf., [2.1]), operation within the limits defined in [4.1] and

the attached Standard Operation Procedures, and the successful completion of a pre-flight

checklist before every flight. The pre-flight checklist has been crafted by the trained

applicant specifically for these sUASs and has been iterated over the course of dozens of

recreational flights. The pre-flight checklist can be found as an attachment to this petition

and includes pre-flight checks of weather, battery levels, propeller structural integrity,

other traffic in the area, and potential obstacles within the flight area (physical or

electromagnetic).

The rigorous pre-flight inspection is to allow the PIC to determine, before every flight,

whether the sUAS is in a condition safe for flight per §91.7(b). Relief from §91.7(b) is

therefore not expected to be necessary, nor is it being requested as part of this petition.

Relief from §91.7(a) has previously been granted to similar petitions, for example

Exemption 11138 (Douglas Trudeau) and Exemption 11110 (Trimble Navigation Ltd).

[2.5] REQUESTED EXEMPTION FROM 14 CFR §91.9(b)(2)

Text of Cited Regulation:

(b) No person may operate a U.S.-registered civil aircraft

(1) For which an Airplane or Rotorcraft Flight Manual is required by § 21.5 of this

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

Flight Manual or the manual provided for in § 121.141(b); and
(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.

Reason for Exemption: As the sUAS will not be certificated under Part 21, a Flight

Manual is not required by §21.5. Therefore, §91.9(b)(2) requires that there be available, in

the aircraft, a “current approved Rotorcraft Flight Manual, approved manual material,

markings, and placards, or any combination thereof.” This exemption is requested for

three reasons. The first reason derives from the fact that there is no officially FAAapproved manual for this system, making the requirement inapplicable. Second, the

inherent small size of the platform makes stowage of such material impossible onboard

the aircraft as required by §91.9(b)(2). Third, stowage of such a manual onboard the

aircraft would not allow the PIC access to it during flight, causing a potential safety

concern. Therefore, relief is requested for §91.9(b)(2).

Mitigation Basis: Safety of the general public and the national airspace will be preserved

by best capturing the intent of the original regulation as it pertains to the sUAS at hand.

The manufacturer’s User Manual (attached) will be used in place of an approved Flight

Manual. The manufacturer’s User Manual captures pertinent information for safe flight

and operation, including general performance data, proper takeoff/landing procedures,

and procedures for emergency situations such as loss of a communications link. Stowage

of this manual onboard the aircraft is both impossible and believed to be contrary to the

intent of the regulation, as the PIC would not be able to access it during flight if it were

onboard the aircraft. Therefore, the manufacturer’s User Manual will be stored with the

sUAS control station such that it is available to the PIC, consistent with the findings from

FAA Memorandum “Interpretation regarding whether certain required documents may be

kept at an UA’s control station” dated 8 August 2014.

[2.6] REQUESTED EXEMPTION FROM 14 CFR §91.121

Text of Cited Regulation:

(a) Each person operating an aircraft shall maintain the cruising altitude or flight level of

that aircraft, as the case may be, by reference to an altimeter that is set, when operating

(1) Below 18,000 feet MSL, to

(i) The current reported altimeter setting of a station along the route and within 100

nautical miles of the aircraft;
(ii) If there is no station within the area prescribed in paragraph (a)(1)(i) of this section,

the current reported altimeter setting of an appropriate available station; or

(iii) In the case of an aircraft not equipped with a radio, the elevation of the departure

airport or an appropriate altimeter setting available before departure; or

(2) At or above 18,000 feet MSL, to 29.92′′ Hg.

(b) The lowest usable flight level is determined by the atmospheric pressure in the area of

operation as shown in the [table omitted]

(c) To convert minimum altitude prescribed under §§ 91.119 and 91.177 to the minimum

flight level, the pilot shall take the flight level equivalent of the minimum altitude in feet

and add the appropriate number of feet specified below, according to the current reported

altimeter setting.

Reason for Exemption: 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. The sUAS

may not have a barometric altimeter, but rather a GPS altitude readout from the flight

system telemetry. Therefore, an exemption may be needed.

Mitigation Basis: An equivalent level of safety will be achieved by the operator by means

of the Pre-flight checklist which records the altitude readout at the launch site as shown

on the GPS altitude indicator before flight. This site altitude will be subtracted from

subsequent GPS altitude readouts to arrive at altitude AGL. This compensates for fieldsite barometric pressure variations when calculating altitude AGL. All altitudes reported

to ATC will be in feet AGL.

Relief from §91.121 has previously been granted to similar petitions, for example

Exemption 11062 (Astraeus Aerial) and Exemption 11138 (Douglas Trudeau).

[2.7] REQUESTED EXEMPTION FROM 14 CFR §91.405(a), §91.407(a)(1),

§91.409(a)(1) & (2), §91.417(a) & (b)

Text of Cited Regulation:

(.405) Each owner or operator of an aircraft—

(a) 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;
*****

(.407) (a) No person may operate any aircraft that has undergone maintenance, preventive

maintenance, rebuilding, or alteration unless—

(1) It has been approved for return to service by a person authorized under § 43.7 of this

chapter

*****

(.409) (a) Except as provided in paragraph (c) of this section, no person may operate an

aircraft

unless, within the preceding 12 calendar months, it has had—

(1) An annual inspection in accordance with part 43 of this chapter and has been approved

for return to service by a person authorized by § 43.7 of this chapter; or

(2) An inspection for the issuance of an airworthiness certificate in accordance with part

21 of this chapter.

*****

(.417) (a) Except for work performed in accordance with §§ 91.411 and 91.413, each

registered

owner or operator shall keep the following records for the periods specified in paragraph

(b) of this section:

(1) Records of the maintenance, preventive maintenance, and alteration and records of the

100-hour, annual, progressive, and other required or approved inspections, as appropriate,

for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance

of an aircraft. The records must include—

(i) A description (or reference to data acceptable to the Administrator) of the work

performed; and

(ii) The date of completion of the work performed; and

(iii) The signature, and certificate number of the person approving the aircraft for return to

service.

(2) Records containing the following information:
(i) The total time in service of the airframe, each engine, each propeller, and each rotor.

(ii) The current status of life-limited parts of each airframe, engine, propeller, rotor, and

appliance.

(iii) The time since last overhaul of all items installed on the aircraft which are required to

be overhauled on a specified time basis.

(iv) The current inspection status of the aircraft, including the time since the last

inspection required by the inspection program under which the aircraft and its appliances

are maintained.

(v) The current status of applicable airworthiness directives (AD) and safety directives

including, for each, the method of compliance, the AD or safety directive number and

revision date. If the AD or safety directive involves recurring action, the time and date

when the next action is required.

(vi) Copies of the forms prescribed by § 43.9(a) of this chapter for each major alteration

to the airframe and currently installed engines, rotors, propellers, and appliances.

(.417) (b) The owner or operator shall retain the following records for the periods

prescribed:

(1) The records specified in paragraph (a)(1) of this section shall be retained until the

work is repeated or superseded by other work or for 1 year after the work is performed.

(2) The records specified in paragraph (a)(2) of this section shall be retained and

transferred with the aircraft at the time the aircraft is sold.

(3) A list of defects furnished to a registered owner or operator under § 43.11 of this

chapter shall be retained until the defects are repaired and the aircraft is approved for

return to service.

Reason for Exemption: These sections reference the procedures and protocols under 14

CFR Part 43, which applies only to aircraft with an airworthiness certificate. Given that

the sUAS will not have an airworthiness certificate, these sections will not apply to the

applicant.

Mitigation Basis: Maintenance (including routine maintenance and repair to correct

functionality issues) will be conducted by the operator. Any sUAS maintenance or

alterations that affect operations or flight characteristics (e.g., replacement of a motor or

electronic speed controller, but not replacement of the battery), will undergo a functional
flight test before being returned to service. Such maintenance, inspection, or alterations

will be noted in the aircraft logbook, to include total flight hours, description of work, and

the signature of the person returning the sUAS to service. As required in §91.7(b), the PIC

also completes a pre-flight checklist to ensure the sUAS is safe for flight before every

flight. An equivalent level of safety is therefore achieved by documentation of any

maintenance or repair work done on the sUAS, functional flight tests after certain

maintenance, and pre-flight checkouts to ensure all systems are safe for flight.

Relief from §91.405(a), §91.407(a)(1), §91.409(a)(1) & (2), and §91.417(a) & (b) has

previously been granted to similar petitions, for example Exemption 11062 (Astraeus

Aerial), Exemption 11138 (Douglas Trudeau), and Exemption 11110 (Trimble Navigation

Ltd).

[3] RELATING TO PILOT IN COMMAND

[3.1] OVERVIEW AND SUPPORTING INFORMATION

The applicant, Jesse Slesar, would be the pilot-in-command (PIC) for all sUASs

operations under this exemption request. Jesse Slesar’s commitment to safety, technical

expertise in aerospace systems, flight training and certification, and experience with

similar systems all enable operation of the sUASs while meeting or exceeding the safety

levels currently seen in manned platforms that perform similar missions.

Technical Expertise. The PIC, Jesse Slesar, works in the electronics industry and has been

a hobbyist for several years. Furthermore Jesse Slesar has the technical background and

knowledge to fundamentally understand the capabilities, and limitations, of the sUAS and

to perform any required maintenance to keep the sUAS in safe, working order.

Experience with Similar Systems. Skills specific to particular equipment operations (e.g.,

handling of controls, specific airspeeds, etc.) offer less of a parallel from traditional

commercial aircraft to sUAS due to the great difference in responsiveness, control, and

agility of these smaller systems. However, the PIC, Jesse Slesar, has been flying small,

electric RC helicopters and other small, unmanned aircraft systems recreationally for over

8 years. Bernard Malouin Jr has over 50 hours of flight time on small, electric rotorcraft

in recreational settings. Moreover, Jesse Slesar has over 40 hours of flight time on multirotor sUAS, and well over the 5 hours of logged flight time on the exact makes and

models of this exemption.

[3.2] REQUESTED EXEMPTION FROM 14 CFR 61.113(a)

Text of Cited Regulation:
(a) Except as provided in paragraphs (b) through (h) of this section, no person who holds

a private pilot certificate may act as pilot in command of an aircraft that is carrying

passengers or property for compensation or hire; nor may that person, for compensation

or hire, act as pilot in command of an aircraft.

Reason for Exemption: Regulation §61.113(a) limits operators with a private pilot

certificate to non- commercial operations. While the sUASs will not be carrying

passengers or transporting property for hire, the operator will be the pilot in command of

an aircrafts being used in a compensated activity. Therefore, an exemption from

§61.113(a) is requested.

Mitigation Basis: Because the sUASs 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 sUASs to have a private pilot certificate rather than a commercial

pilot’s license. Further, as explained in [3.1], the applicant is exceptionally well qualified

to operate such systems with years of recreational experience with like systems. The

combination of these relevant skills reduces the risk to the public and the national airspace

to levels below what would be found with knowledge acquired from a commercial pilot

license alone. To maintain a level of currency, within the previous 90 days the PIC will

also conduct at least 3 take offs and landings with the sUASs before commencing a

commercial flight as noted in the SOP. The size (cf., [2.1]), speed (cf., [2.1]), and

operating limitations (cf., [4] and SOP) found herein exceed the level of safety that would

otherwise be found with a commercial pilot operating a conventional helicopter.

Relief from §61.113(a) has previously been granted to similar petitions, for example

Exemption 11062 (Astraeus Aerial), Exemption 11138 (Douglas Trudeau), and

Exemption 11110 (Trimble Navigation Ltd).

[4] RELATING TO THE sUAS OPERATIONS

[4.1] OVERVIEW AND SUPPORTING INFORMATION

The sUAS under this petition is equipped with an imaging sensor (e.g., GoPro video

camera, and larger SLR type cameras on the Syndrone) and is to be operated for aerial

imaging, photography, and videography of property and events in a limited and welldefined boundary. The intention is to capture video of properties or events with the owner

or coordinators permission. Examples would be events such as weddings or similar

events, private athletic competitions, or shooting photos and videos of real estate locations

with the owners consent. 
The proposed operations serve many needs of homeowners, Realtors, and others in a way

that is more cost effective and safer than traditional approaches. One example pertains to

a homeowner or Realtor who wishes to have an aerial view of a property for advertising,

marketing, or reasons of general interest. Traditional methods include the use of a

helicopter, posing additional risks due to the persons onboard the platforms, significant

weight (several tons), carriage of combustible Jet A fuel (over 100 gallons), and the

relative lack of maneuverability/agility of such platforms. This is all compounded by

additional harmful impacts to nearby persons who are then exposed to additional noise

pollution in excess of 100 dB, causing non-active participant safety concerns. Conducting

this operation with the sUASs greatly reduces (or in some cases, eliminates) these risks.

Safe operation of the sUAS will be ensured by a thorough set of Standard Operating

Procedures. A separate document has been attached to this petition with the fully detailed

SOP; however, these topically include:

 Operation limited to visual, line-of-sight (VLOS)

 Operation limited to daytime activities; or night activities provided there is adequate

lighting.

 Use of a visual observer (VO) for all flights, who is in direct verbal contact with PIC

 Operation limited to a maximum altitude of 400 feet AGL

 Operational minimum standoff distances for nonparticipating persons

 Operational minimum standoff distances for nonparticipating vehicles/structures

 Operation with minimum standoff distances to clouds

 No sUAS operations within 5 miles of a Class B, C, or D airport without ATC consent

 Comprehensive Pre-Flight inspection by the PIC to determine safe-for-flight

 Flight duration limited to 20 minutes in length or 30% battery remaining

Each of the above are listed in the attached SOP and are further elaborated upon in

subsequent sections that discuss relief to specific FARs and how the portion of the SOP

mitigates any risk that may be encountered by exemption from that particular FAR.

[4.2] REQUESTED EXEMPTION FROM 14 CFR §91.105

Text of Cited Regulation:
(a) During takeoff and landing, and while en route, each required flight crewmember

shall—

(1) Be at the crewmember station unless the absence is necessary to perform duties in

connection with the operation of the aircraft or in connection with physiological needs;

and (2) Keep the safety belt fastened while at the crewmember station.

(b) Each required flight crewmember of a U.S.-registered civil aircraft shall, during

takeoff and landing, keep his or her shoulder harness fastened while at his or her assigned

duty station. This paragraph does not apply if—

(1) The seat at the crewmember's station is not equipped with a shoulder harness; or (2)

The crewmember would be unable to perform required duties with the shoulder harness

fastened.

Reason for Exemption: The regulation requires crew members (which may include the

PIC and VO) to keep a safety belt fastened while at their crewmember stations. As the

sUAS has no occupants, this regulation is not applicable as it would be detrimental to

flight safety to require the operator and visual observer on the ground to remain with a

safety belt fastened. Therefore, exemption from §90.105 is requested.

Mitigation Basis: Due to the unusual nature of the sUAS operation (remotely from

ground, with no onboard crew), the safety of the general public, pilot in command, visual

observer, and national airspace system is adversely affected under the interpretation of

this requirement that the pilot in command and the visual observer on the ground must

have a safety belt fastened at a designated station.

[4.3] REQUESTED EXEMPTION FROM 14 CFR §91.119(c)

Text of Cited Regulation:

Except when necessary for takeoff or landing, no person may operate an aircraft below

the following altitudes:

(a) [omitted as not relevant to request for relief]

(b) [omitted as not relevant to request for relief]

(c) Over other than congested areas. An altitude of 500 feet above the surface, except over

open water or sparsely populated areas. In those cases, the aircraft may not be operated

closer than 500 feet to any person, vessel, vehicle, or structure.
(d) Helicopters. Helicopters may be operated at less than the minimums prescribed in

paragraph (b) or (c) of this section if the operation is conducted without hazard to persons

or property on the surface. In addition, each person operating a helicopter shall comply

with any routes or altitudes specifically prescribed for helicopters by the Administrator.

Reason for Exemption: The regulation requires minimum standoff distances to persons

and objects (in other than congested areas) of no less than 500 feet. Due to the altitude

limitation of the sUASs (of 400 feet maximum) as well as the intended mission of aerial

imaging/photography/videography, it will be necessary to operate closer than 500 feet to

essential persons, structures, vehicles, and vessels. Therefore, an exemption is requested.

Mitigation Basis: The applicant has no intentions to operate the sUAS over congested

areas. However, there is no clear definition as to what metrics constitute a congested area

(as expressed in Exemption 11110). While “yellow” areas on sectional charts are a good

means to alerting operators to potentially congested areas, these alone only indicate the

general area is populated and is not sufficient to prescribe congestion (consistent with the

findings of Exemption 11138), nor should they be used for such. The level of congestion

should seemingly be determined relative to the aircraft being operated in the candidate

Area of Operation. To ensure safety in the event of an emergency, the aircraft would

ideally be afforded sufficient space to land without collision due to the density of nearby

persons or structures. Clearly, the characteristic length scale (and, therefore, allowable

density) for safe landing would vary substantially between an aircraft requiring hundreds

of feet to make an emergency landing versus a sUAS that requires only several feet. The

pilot in command will therefore use best judgment on whether a particular sUAS Area of

Operation, which is spatially limited, is congested before commencing any flight

activities. Such a judgment will take into consideration:

 The candidate Area of Operation will not be found acceptable if it includes an open air

assembly of persons

 The candidate Area of Operation will be judged based on the expected flight

boundaries. That is, a large open space in a heavily settled area would be judged based on

the open space and not the surrounding area if operations are to be limited to safely within

the open space.

 The candidate Area of Operation must provide sufficient free space away from persons

and structures to allow typical takeoff, landing, and flight without presenting an undue

hazard to nearby persons or structures.
 The candidate Area of Operation must provide sufficient free space to allow emergency

landing procedures without presenting an undue hazard to nearby persons or structures.

 The candidate Area of Operation must allow the flight operations to adhere to the

minimum standoff distances that would otherwise be required of an area other than a

congested area.

If the Area of Operation is determined by the pilot in command to be congested, no flight

operations shall occur. If the Area of Operation is determined by the pilot in command to

be other than a congested area, the following limitations on flight operations will be

imposed, based on the light weight of the sUASs (under30 lbs) and the findings of

previous FAA analyses:

 Minimum standoff distances to non-participating persons is nominally 500 feet.

 If barriers or structures are present that can sufficiently protect non-participating

persons

from the sUAS or debris in the event of an accident, then the sUAS may operate closer

than 500 feet to non-participating persons afforded such protection.

o If a situation arises where non-participating persons leave such protection and are within

500 feet of the sUAS, flight operations must cease as soon as is practicable and in a

manner to ensure the safety of the non-participating person as the primary concern.

 Minimum standoff distances may be less than 500 feet to vessels, vehicles, and

structures when the owner/controller of any such vessel, vehicle, or structure grants

permission and the PIC makes a safety assessment of the risk of operating closer to those

objects and determines that it does not present an undue hazard.

 Minimum distance to clouds will be 500 feet below any clouds and 2000 feet

horizontally from any clouds to ensure the PIC and VO have VLOS with the sUAS

throughout the flight.

It is noted that, currently, full-scale helicopters are permitted under §91.119(d) to operate

in similar missions with potentially less restrictive requirements. It is believed that the

proposed limitations will maintain the safety of the general public on the ground at levels

that exceed current safety levels of conventional helicopters performing similar missions.

Relief from §91.119(c) has previously been granted to similar petitions, for example

Exemption 11138 (Douglas Trudeau) and Exemption 11110 (Trimble Navigation Ltd).
[4.4] REQUESTED EXEMPTION FROM 14 CFR §91.151(a)(1)

Text of Cited Regulation:

(a) No person may begin 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

Reason for Exemption: The sUASs in this petition does not carry any fuel and, therefore,

this regulation is not well-posed for these sUASs. The sUASs are battery powered with a

total flight duration that is limited to approximately 20 minutes. Therefore, requiring

enough battery power to fly to the first destination plus an additional 20 minutes is not

feasible.

Mitigation Basis: The proposed operations of the sUAS are limited to a defined area,

typically a single property, with the property owner/controller’s consent. Due to this, it is

believed that not being able to fly for an additional 30 minutes does not engender the

types of risks that §91.151(a)(1) was intended to alleviate given the sUAS is small,

relatively low speed, and will not be flown over non-participating structures. An

equivalent level of safety can be achieved by limiting flights to 20 minutes or 30%

remaining battery power (manufacturer-recommended low battery limit), whichever

occurs first. This is more than adequate to return the sUASs to the intended landing area

and execute a normal landing procedure.

Relief from §91.151(a)(1) has previously been granted to similar petitions, for example

Exemption 11062 (Astraeus Aerial), Exemption 11138 (Douglas Trudeau), and

Exemption 11110 (Trimble Navigation Ltd).

[4.5] PROPOSED MODIFICATION OF TYPICAL SECTION 333 EXEMPTION

CONDITION - NOTAMS

Text of Cited Typical Exemption Condition:

The operator must obtain an Air Traffic Organization (ATO) issued Certificate of Waiver

or Authorization (COA) prior to conducting any operations under this grant of exemption.

This COA will also require the operator to request a Notice to Airman (NOTAM) not

more than 72 hours in advance, but not less than 48 hours prior to the operation.

Feedback on Condition: Due to the nature of the assignments/missions, the starting

day/time of the sUAS operations in this petition may not always be known three days in
advance, and it would not be unexpected to be asked to support missions the next day

(within 24 hours). Furthermore, weather conditions in the Northeast are variable with

meteorological forecasts often changing when made several days in advance. It is

therefore respectfully requested that the above typical exemption condition be modified to

require the operator to request a NOTAM not more than 72 hours in advance, but not less

than 12 hours prior to the operation.

Mitigation Basis: It is believed that this will not adversely affect national airspace safety

as NOTAMs are checked before flights and may be checked during flights. Allowing

NOTAMs to be requested closer to the actual flight operations (when weather conditions

are more accurately predicted) will greatly increase the fidelity of the NOTAM process

and airman awareness by producing fewer false-alarms, and, as a consequence, leading to

greater vigilance to those receiving the NOTAM.

[5] PUBLIC INTEREST

The proposed exemption under Section 333 of the FAA Modernization and Reform Act of

2012 is within the public interest. This petition for imaging, photography, and

videography of property and events would allow access to aerial imaging to those who

would previously have been excluded from the market by the cost of using a larger,

manned aircraft. The impact to the public is multifaceted, including greater access to

aerial capabilities, increased levels of safety over conventional manned systems to

perform the same duty, and reduced impact to nearby persons or ecological sites due to

noise or burned hydrocarbon emissions.

One example is a homeowner who suspects possible roof damage, perhaps as a result of a

recent storm. To determine if damage has occurred, the homeowner may wish to inspect

the roof before calling a carpenter or repairperson. This may lead to an unprepared

homeowner in peril on an icy or slippery roof. By comparison, the sUAS can quickly be

used to image the suspect area and those images can subsequently be visually inspected

by the homeowner, greatly reducing the risk to persons.

A second example pertains to a homeowner or Realtor who wishes to have an aerial view

of a property for advertising, marketing, or reasons of general interest. Traditional

methods include the use of a helicopter, posing additional risks due to the persons

onboard the platforms, significant weight (several tons), carriage of combustible Jet A

fuel (over 100 gallons), and the relative lack of maneuverability/agility of such platforms.

This is all compounded by additional harmful impacts to nearby persons who are then

exposed to additional noise pollution. Typical decibel noise level for a Bell helicopter at
100 feet is approximately 100 dB. By contrast, the sUAS at less than 10 feet is

approximately 80 dB, leading to a 4X reduction in noise pollution, even when 10X closer.

[6] SUMMARY FOR PUBLICATION IN THE FEDERAL REGISTER, IF NEEDED

Pursuant to 14 CFR Part 11, 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 rules:

14 CFR Part 21, Subpart H; 14 CFR §61.113(a); 14 CFR §91.7(a); 14 CFR §91.9(b)(2);

14 CFR §91.105; 14 CFR §91.119(c); 14 CFR §91.121; 14 CFR §91.151(a)(1); 14 CFR

§91.203(a)(1); 14 CFR §91.203(b); 14 CFR §91.405(a); 14 CFR §91.407(a)(1); 14 CFR

§91.409(a)(1); 14 CFR §91.409(a)(2); 14 CFR §91.417(a); 14 CFR §91.417(b) to operate

two small, unmanned aircraft systems (sUASs) weighing less than 30 lbs in commercial

aerial imaging, photography, and videography operations.

[7] CONCLUDING REMARKS

It is believed that the criteria presented in this petition, including size, weight, operational

parameters, pilot qualifications and training, and Standard Operating Procedures, provide

a very high level of safety, at or above current levels, during the proposed sUAS use. This

level of safety, the interest to the public, and the commission of the FAA to integrate

sUAS into the national airspace provide more than adequate justification for the grant of

the requested exemptions allowing commercial operation of the applicant’s sUAS.

Below are links to the manufacturers of the flight controllers for both frames, they should

include Standard Operating Procedures, and Pre-Flight Checklists.

http://download.djiinnovations.com/downloads/phantom_2/en/PHANTOM2_User_Manual_v1.2_en.pdf

http://wiki.mikrokopter.de/en/FlightCtrlManual

The applicant is very passionate and active in the field of sUAS. Should any supplemental

information be helpful in the adjudication of this exemption petition, please do not

hesitate to get in contact. Moreover, if it provides any value now or in the future, the

applicant would be pleased to offer feedback on the exemption process or offer input

(either procedural or technical) on future implementations to satisfy Sections 332 or 334

of the FMRA.

Respectfully submitted,
Jesse Slesar

Sky Definition Photography