## Petition for Exemption / COA **Request**
**Petitioner :**  **Mid Island A ir Service,**  **Inc**

**.**

Gail Mancuso, Owner, VP , and GM LI MacArthur Airport 101 Hering Dr Ronkonkoma, NY 11779 [Ph one ] 631 588

- 5400 [F a x] 63 1 588

- 8841 [Email] info@midislandair.com www.midislandair.com 

## U.S. Department of Transportation, Docket Operations We st Building, Ground Floor, Room W 12

- 140 1200 New Jersey Avenue, SE Wa shington, 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 l aw enforcement, first responders, and search and rescue. **Exemption Request Pursuant to Section 333 of the FAA Reform A** **ct and Part 11 of the Federal A**  **viation 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:**  3/1 1 /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 Sect ion 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 orga nizations 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 we ll as for the protection of the persons and property. An awareness training sy llabus will also be offered to the hobbyist to promote general public safety, responsibility, and privacy. [1]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 activ ities. 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 provi de 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 Inst ruction 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) Ma intena nce Inspections 14 CFR 91.407 (a) (1) Ma intenance Inspections 14 CFR 91.409 (a) (1) (2) Ma intenance Inspections 14 CFR 91.417 (a) & (b) Ma intenance Inspections **Mid Island A ir Service, Inc** 

**. will**  **operate the following aircraft**s 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 a pproval 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 g rant 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

-

5.8G Hz. 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 Hub san 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 ® Inductrix TM 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 1 kg . 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 1 5 m/s or 3 3 m/h, with a flight time of 25 minutes. **The DJI Phantom 3 for further training and operations** 

. The DJI Phantom 3 dime ns ions, 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 h as 4 motors powered by 15.2v4480mAh LiPo 4S battery for approximately 23 min utes flight time , with GPS mode GPS/GLONASS.
**The Blade**  **Chroma CG03 for further training and operations** . The Blade Chroma dimension s 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

. 1 kg , and travels at a max speed of 18m/h. The Typhoon has 4 m otors 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 438 mm [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 L i

- Po battery

. There are 4 propellers, model DJI 1345, in use. [3]**AI RCRA**  **FT AN**  **D EQUIVA LENT LEVEL OF SA** **FETY**

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 l bs. 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 fi rst. 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, th e 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 m ust 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 und er the guidance of the local FAA. 1 1 . 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 estimat ed flight time, flight duration, elevation of flight and other pertinent information. Airport common traffic frequency or control tower frequency will be monitored during operations. 1 2 . The operator will file FAA Form 7711

- 1, or its equivalent, as modifie d 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. 1 3 . 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

. W ith advanced permission of the FSDO, operations at closer range may be approved. 1 4 . The PIC and VO will have been trained in o peration of UAS and receive up

-to

- date information for the particular UAS to be operated. 1 5 . The PIC and VO will be able to communicate by voice, radio, and/or text at all times. 1 6

. Written and/or verbal permission and permits as appropriate will be obta ined from territorial, state, county or city jurisdictions, including law enforcement, fire or other appropriate governmental agencies. [4]1 7 . If the UAS loses communications with the remote controller or loses GPS signal, the UAS

will have the capabil ity to return to a pre

- determined location within a designated location and land autonomously. 1 8 . 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: A irw**  **orthiness 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 as sociated 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 Sect ion 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 particula r 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 (f ixed 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 material s 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 complia nce 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 certific ates 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 ma terials or flammable liquid fuels, and inability to carry a substantial external load. **14 C.F.R. § 45.23 (b). Marking of the A ircraft**  The regulation requires: Wh en marks include only the Roman capital letter "N" and the registration number is displayed o n 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 cab in, 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 P rivileges 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 l evels 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 i s 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 A ircraft A** **irw orthiness.** 
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 determin ing 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 A ircraft Flight Manual in the A** **ircraft.** Section 91.9 (b) (2) provides: No person may operate a U.S.

- registered civil aircraft ... (2) For wh ich 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 Fl ight 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 bec ause 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 w ill have immediate access. **14 C.F.R. § 91. 103: Preflight A** **ction.** 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 PI C 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.** S ection 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 [6]without fully functional dual control s 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. §9 1.119: Minimum Safe A** **ltitudes.** 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 filmi ng 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 excee ds 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. Com

pared to flight operations with aircraft or rotorcraft weighting far more than the maximum 5 5lbs. 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 en sure separation between these UAS operations and the operations of conventional aircraft that must comply with Section 91.119. **14 C.F.R. §91.121 A ltimeter 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 poi nt 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 prede termined 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 s peed 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

— wh ichever 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): Carry ing Civil A** **ircraft Certification and Re gistration**  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 l oaded 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 th ese 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 re gulations 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 pre scribed 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 appli cant. 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 restricte d 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 mai ntenance, 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]**Ad ditional 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 (FSAN A). Her true desire is to educate the public as to the safe, responsible and respectful practices involved in the operation of UAS s

. Satisfaction of criteria provided in Section 333 of the Reform Act of 2012 provide more than adequate justification for th e 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

[9]