Petition for Exemption / COA Request

Petitioner: Mid Island Air Service, Inc.

Gail Mancuso, Owner, VP, and GM

LI MacArthur Airport

101 Hering Dr

Ronkonkoma, NY 11779

[Phone] 631 588-5400

[Fax] 631 588-8841

[Email] info@midislandair.com

www.midislandair.com

U.S. Department of Transportation, Docket Operations

West Building, Ground Floor, Room W12-140

1200 New Jersey Avenue, SE

Washington, DC 20590

Description of Relief Sought:

The petitioner is seeking an exemption to commercially operate its unmanned aircraft in UAS

compliance training for the public, aerial photography or television operations, to conduct its 

own research and to develop economic platforms for law enforcement, first responders, and 

search and rescue.

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: 3/11/16

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

and 14 CFR Part 11, Mid Island Air Service, Inc., Gail Mancuso, 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:

1. 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. An awareness training syllabus will also

be offered to the hobbyist to promote general public safety, responsibility, and privacy.

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2. 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.

3. Aerial photography and/or video for public and/or private use including real estate,

architecture, land surveying, engineering and other related professional activities.

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

events, cinematography and news gathering.

5. Aerial inspection/photography of residential/commercial utility infrastructure including but

not limited to electrical power lines, wind turbines and cell towers.

.

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.”

Regulations from which the exemption is requested:

14 CFR Part 21 subpart H Airworthiness Certificates

14 CFR 45.23 (b) Marking of the Aircraft

14 CFR 61.113 (a) & (b) Private Pilot Privileges and Limitations: Pilot in Command

14 CFR 91.7 (a) Civil Aircraft Airworthiness

14 CFR 91.9 (b) (2) Civil Aircraft Flight Manual in the Aircraft

14 CFR 91.103 Preflight Actions

14 CFR 91.109 Flight Instruction

14 CFR 91.119 (c) Minimum Safe Altitudes

14 CFR 91.121 Altimeter Settings

14 CFR 91.151 (a) Fuel Requirements for Flight in VFR Conditions

14 CFR 91.203 (a) & (b) Carrying Civil Aircraft Certification and Registration

14 CFR 91.405 (a) Maintenance Inspections

14 CFR 91.407 (a) (1) Maintenance Inspections

14 CFR 91.409 (a) (1)(2) Maintenance Inspections

14 CFR 91.417 (a) & (b) Maintenance Inspections

Mid Island Air Service, Inc. will operate the following aircrafts as either initial trainers in a 

closed off predetermined area owned/operated by the representative within line of sight, or as 

further training and operations in similar 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.

[2]
The following UAV remote controls will use an operating frequency 10-channel 2.4GHz -

5.8GHz. Any live video feed will have an operating frequency of 5.728 GHz – 5.850 GHz. 

Hubsan X4 micro drone as an initial trainer craft. The Hubsan X4 is 8cm x 8cm (3.1in). 

Under still air the max speed is 10 m/s or 22mph, flight time 9 minutes. The Hubsan X4 has r 

coreless motors, powered by 3.7 V 380 mAh Li-Po battery, with precision 2.4Ghz Control.

Horizon Blade Inductrix RTF micro drone [BLH8700] as an initial trainer craft. The Blade®

InductrixTM drone is an ultra micro machine weighing .67oz [19g], 3.3in x 3.3in [83mm] by 1” high 

with significant durability and less noise. It has small pitch and roll angle limits with 

electronic self-leveling to help you stay in control. Durable rotor housings inherently prevent 

damage. It has a 150mAh 1S 3.7V 25C Li-Po flight battery, 2.4GHz technology, and has 6-8 

minutes of flying time on a charge, and with safe technology a good trainer anyone can fly with 

little effort, and anywhere inside or outside. Actual speed not specified by manufacturer.

The DJI Inspire 1 model T600 for further training and operations. The DJI Inspire 1 

dimensions are 438mm [17in] x 451mm [18in] x 301mm [12in] and has a weight of 6.5lbs 

[2.9kg]. Under still air the maximum speed of 22 m/s or 49 mph with a cruising speed of 11 m/s 

or 25 mph, and flight time of 18 min. The Inspire 1 has 4 motors, model DJI 3510, powered by a 

6 cell 4500 mAh or 5700 mAh Li-Po battery. There are 4 propellers, model DJI 1345, in use. 

The DJI Phantom 2 for further training and operations. The Phantom 2 dimensions are 

29cm x 29cm [11in] weighing 2.2lb or 1kg. Under still air the maximum sir speed is 10m/s or 

22.5 mph. DJI Phantom 2 has 4 motors powered by 11.1 V, 5200 mAh3 S Li-Po battery, and 

travels at a max speed of 15m/s or 33m/h, with a flight time of 25 minutes.

The DJI Phantom 3 for further training and operations. The DJI Phantom 3 dimensions, 

diagonal size [including propellers] 590mm or 23.2 inches, has a weight of 2.8lbs or 1.2kg, and 

travels at a max speed of 16m/s or 35m/h. The Phantom 3 has 4 motors powered by 

15.2v4480mAh LiPo 4S battery for approximately 23 minutes flight time, with GPS mode 

GPS/GLONASS.

The Blade Chroma CG03 for further training and operations. The Blade Chroma 

dimensions are 9.50 in (242mm) x 15.7 in (400mm) motor to motor. Has a weight of 2.9lbs or 

1.3kg, and travels at a max speed of 17.9m/s or 40m/h. The Chroma has 4 motors powered by 

11.1V 3S 5400mAh Li-Po battery for approximately 30 min flight time. Comes with a 3-axis 

Gimbal for GoPro or a fixed GoPro mount, with GPS mode GPS/GLONASS.

The Yuneec Typhoon Q500 for further training and operations. The Typhoon dimensions 

are 16.54in [420mm] x 22.2in [565mm], with a weight without battery 2.5lbs or 1.1kg, and 

travels at a max speed of 18m/h. The Typhoon has 4 motors powered by 5400mAh 3S 11.1V 

LiPo battery for approximately 22 minutes flight time, with GPS mode GPS/GLONASS.

The DJI Inspire 1 Raw Quadcopter for further training and operations. The DJI Inspire One 

Pro Raw, with two controllers, dimensions are 438mm [17.2”] x 451mm [17.8”] x 301mm [11.9”] 

and has a weight 8.5 lbs [3.9kg] with camera and battery. Under still air the maximum speed is 

22 m/s or 49 mph with a flying time of 18 minutes. The Inspire 1 Raw has 4 motors, model DJI 

3510, powered by a TB47 6 cell 4500 mAh Li-Po battery. There are 4 propellers, model DJI 

1345, in use. 

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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 include:

1. The UAS will weigh less than 55 lbs.

2. The UAS will have a maximum operating speed of no more than 50mph.

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

Observer (VO). The applicant will operate the UAS in line of sight within a closed off and

predetermined area owned and/operated by the property representative.

4. Maximum flight time for each operational flight will be 30 minutes. Flights will be terminated

at 25% battery power reserve or 30 minutes of flight time whichever occurs first.

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

and not more than 200 feet above an elevated platform from which filming is planned.

6. 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.

7. The UAS pilot will be a designated Pilot in Command (PIC) and must hold either an airline

transport, commercial, private, recreational, or sport pilot certificate. The PIC must also 

hold a current FAA airman medical certificate or a valid U.S. driver's license issued by a 

state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal 

government. The PIC must also meet the flight review requirements specified in 14 CFR

§ 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

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

flight consisting of all the days’ production activities.

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

10. The flight will occur no closer than a 5 mile radius of the geographic center/Airport 

Reference Point (ARP) of a tower controlled or uncontrolled airport or under the 

guidance of the local FAA.

11. 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. Airport common traffic frequency or control tower 

frequency will be monitored during operations.

12. 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.

13. 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. With advanced permission of the FSDO, operations at closer range may 

be approved.

14. 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.

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

16. Written and/or verbal permission and permits as appropriate will be obtained from

territorial, state, county or city jurisdictions, including law enforcement, fire or other

appropriate governmental agencies.

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17. 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.

18. 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. 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 may 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.”

[5]
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. Mid Island Air Service Inc., Gail Mancuso may achieve an equivalent level of safety as 

achieved by current Regulations because the applicant’s UAS do not carry any pilots or 

passengers nor property. The risks attendant to the operation of UAS is far less than the risk

levels inherent in the commercial activities outlined in 14 CFR 61. The PIC of the UAS will hold 

either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC 

must also hold a current FAA airman medical certificate or a valid U.S. driver's license issued by 

a state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal 

government. The PIC must also meet the flight review requirements specified in 14 CFR

§ 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate exceeding the

current safety levels in relation to 14 CFR 61.113 (a) & (b). I feel the operation and limitations

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 the aircraft, not 

only because there is no pilot on board, but because there is no room or capacity to carry such 

an item on the aircraft. The equivalent level of safety will be maintained by keeping the flight 

manual at the ground control point where the pilot flying the UAS will have immediate access.

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 under Normal Procedures 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

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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 it is 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 30 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.

[7]
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 30 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) (1)&(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. The operator will ensure

that the UAS is in working order prior to initiating flight and perform required maintenance as

needed.

[8]
Additional Information

The applicant, Mid Island Air Service, Inc./ Gail Mancuso, has been involved in the

flight training business over 20 years. Ms. Mancuso is also an active member of the

“The Flight School Association of North America (FSANA). Her true desire is to

educate the public as to the safe, responsible and respectful practices involved in the operation

of UASs.

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.

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, professional and private user education, 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.

Sincerely,

Gail Mancuso

Mid Island Air Service, Inc.

Owner, VP, & General Manager

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