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- 1553 • www.HeliWatch.com • Twitter: @heli_watch U.S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590

May 10

, 2015

Dear Sir or Madam,

Heli Watch, Inc. (“Heli Watch”) is submitting this petition on its own behalf , without legal counsel or consultation, in accordance with the terms set forth in Section 333 of the FAA

Modernizatio n and Reform Act of 2012 (“Reform Act”) and 14 C.F.R. Part 11. Heli Watch requests an exemption from the Federal Aviation Regulations (“F ARs”) described below as they pertain to the operation of small Unmanned Aerial Systems (“UAS ”).

Heli Watch, Inc. is seeking said exemptions to commercially operate its small UAS within the National Airspace System (NAS) for the purpose of providing aeria l video graphy and photography services. All Heli Watch flight operations will be performed by a two

- person flight team and will be conducted in accordance with Section 333 of the Reform Act as set forth by the Federal Aviation Administration (“FAA”)

Pursuant to 14 C.F.R. § 11.81(f), Heli Watch is providing the following summary for publication in the Federal Register to be included at the discretion of the FAA:

Docket Number: No. FAA

- 2014

-

_____ Petitioner: Heli Watch, Inc. Seeking Exemptions from Sections of 14 C.F.R: 14 C.F.R. Part 21, 14 C.F.R. § 45.23(b), 14 C.F.R. § 61.113(a) and (b), 14 C.F.R. § 61.133(a), 14 C.F.R. § 91.109(a), 14 C.F.R. § 91.119, 14 C.F.R. § 91.121, 14 C.F.R. § 91.151(a), 14 C.F.R. § 91.203(a) and (b), 14 C.F.R. § 91.215, 14 C.F.R. § 91.401 through 91.417, 14 C.F.R. § 91.7(a) and (b). Description of Relief Sought: Heli Watch, Inc. is requesting an exemption from
sections of Title 14 of the Code of Federal Regulations to operate small (55 lbs. gross weight or less) unmanned ai rcraft systems under the control of licensed private pilots.

The Heli Watch petition is significantly similar in scope to the exemption granted to
Astraeus Aerial under Exemption No. 11062 (Regulatory Docket No. FAA

- 2014

- 0352) and the associated Summary G rants (Regulatory Docket Nos. FAA

- 2014

- 035 3, FAA

2014

- 0354, FAA

- 2014

- 0356, FAA

- 2014

- 0357 and FAA

- 2014

- 0358 ) . Where applicable,
Heli Watch will adhere to the terms set forth in the Astraeus exemption. When applicable, Heli Watch will also modify its trai ning, maintenance and operations procedures to comply with future regulations set forth by the FAA as UAS law is implemented.

Heli Watch has received several inquiries, and has had initial conversations, regarding its services from companies in Mexico and Canada and would like to request consideration to exercise the privileges of any exemption outside of the United States.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch The petitioner contact information for Heli Watch is: Heli Watch, Inc. 6444 E. Spring St. #324 Long Beach, CA 90815

- 1553 Attn: Ralp h Rebaya Phone: (562) 833

- 2817 Email: Ralph@heliwatch.com

Heli Watch is requesting exemptions from the following regulations:

• 14 C.F.R. Part 21

• 14 C.F.R. § 45.23(b)

• 14 C.F.R. § 61.113(a) and (b) and 14 C.F.R. § 61.133(a)

• 14 C.F.R. § 91.109(a)

• 14 C.F.R. § 91.119

• 14 C.F.R. § 91.121

• 14 C.F.R. § 91.151(a)

• 14 C.F.R. § 91.203(a) and (b)

• 14 C.F.R. § 91.215

• 14 C.F.R. § 91.401 through 91.417

• 14 C.F.R. § 91.7(a) and (b)

G ENERAL R ESTRICTIONS AND A SSURANCES Using FAA Notice on National Policy N 8900.227, “ Unmanned Aircraft Systems (UAS) Operational Approval ” and Exemption No. 11062 as guidance, Heli Watch will document and implement policies and training to ensure compliance with N 8900.227 Section 14 “Operational Requirements for UAS” and including the following re strictions: (a.) All flight operations will be performed by a minimum of two (2) individuals: a Pilot in Command (PIC) and a Visual Observer (VO). (b.) PIC will conduct a pre

- flight briefing with VO and client or their designee to review flight profile, safety consi derations and emergency procedures. (c.) PIC will perform a pre

- flight inspection of the UAS that includes : the communications link between the UA and ground control station, remaining battery charge, condition of airframe, propellers and wiring. (d.) During flight, PIC and VO will maintain direct communications and terminate flight operations if they are no longer able to communicate with each other. (e.) Unmanned Aircraft (UA) shall not exceed 55 pounds gross vehicle weight (including any attached cameras, gimbals or ot her equipment). (f.) All flight operations will take place in Class G airspace no further than 3⁄4 nm from the PIC, below 400 feet AGL and at airspeeds less than 25 kts. (g.) All flight operations will take place under VFR conditions within visual line of sight (VLOS) of the PIC. No flight operations will take place at night. (h.) Flight operations will not be conducted over densely populated areas, heavily trafficked roads, at an air show or other environment that may include other low

flying aircraft, or within 5 nm of a n airport or heliport. (i.) No flight operations will be conducted over an open

- air assembly of people unless a comprehensive safety plan can be implemented to mitigate risk of injury to individuals or damage to property. (j.) Flight operations will be terminated wh en the UA battery reaches a remaining charge of 2 0 %

.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch Additional information regarding General Flight Operations, PIC and VO qualifications may be found in Appendix B: Heli Watch Equipment and Flight Operations Overview

B ENEFIT TO THE P UBLIC

Th e requested exemptions will allow Heli Watch to operate its UASs to provide commercial photography and videog raphy services to its clients

. In addition to advancing the “safe and expedient integration of UAS into the NAS” as mandated by the FAA

Modernization and Reform Act of 2012, Public Law 112

- 95 (P.L. 112

- 95), g ranting the requested exemption is in the public interest as:
1. A UAS generates less pollution from exhaust, has a lower noise signature and requires a substantially smaller to footprint from which to operate

, making it more cost

- effective and environmentally friendly than full size , manned fixed

- wing aircraft and helicopters.

2. A UAS uses either a n electric power source or a significantly smaller amount of
flammable fuel than a manned aircraft , making it a safer platform than its manned counterparts . The UAS described herein are also more maneuverable and provide a greater safety margin at the speeds and altitudes required for aerial cinematography than full size fixed

- or rotary

- wing aircraft

. 3. When p roperly operated within the regulations set forth by the FAA, a UAS can be less disruptive to the NAS t han its full

- sized counterparts because it does not require airports/runways, fueling apparatus or other infrastructure required by
manned aircraft.

Tha nk you for your review and consideration of this petition. Please contact us if you require any additional information to process this request.

Sincerely,

Ralph Rebaya, Owner and Chief Pilot Heli Watch, Inc.

Attachments: Appendix A: Exemption Request and Equivalent Safety Assurance Appendix B: Heli Watch Equipment and Flight Operations Overview

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch APPENDIX A:

E XEMPTION R EQUEST AND E QUIVALENT S AFETY A SSURANCE

Heli Watch respectfully requests an exemption from the following regulations for the unmanned aircraft systems (UAS) in its inventory.

14 C.F.R. Part 21 , Airworthiness Certificates This part prescribes, in significant part, the requirements for issuing or modifying design approvals, production approvals, airworthiness certificates and airworthiness approvals. It also establishes the rules governing applicants for and holders of cert ificates specified

above.

Heli Watch requests an exemption from 14 C.F.R. Part 21 due to the size, construction materials and operational restrictions under which the UAS will operate. Additionally, the UAS will carry neither passengers nor flammable fuel, which will make it inherently safer than other aircraft holding an standard or experimental certif ication and performing the same operations under similar or less restrictive regulations.

If an exemption is not granted , Heli Watch intends to apply f or an FAA airworthiness certification in the experimental category under 14 C.F.R. § 21.191.

14 C.F.R. § 45.23(b) , Display of Marks; general (a) Each operator of an aircraft must display on that aircraft marks consisting of the Roman capital letter “N” (d enoting United States registration) followed by the registration number of the aircraft. Each suffix letter used in the marks displayed must also be a Roman capital letter.

(b) When marks include only the Roman capital letter “N” and the registration number is displayed on limited, restricted or light

- sport category aircraft or experimental or provisionally certificated aircraft, the operator must also display on that aircraft near each entrance to the cabin, cockpit, or pilot station, in letters not l ess than 2 inches nor more than 6 inches high, the words “limited,” “restricted,” “light

- sport,” “experimental,” or “provisional,” as applicable.

Heli Watch aircraft are unmanned and do not have a cockpit/entrance . Further, the size
of the aircraft do no t allow for 2 inch lettering. Heli Watch would display the word “Experimental” in a prominent location on the top of the UAS in as large a size as is practical to be prominent, but not interfere with operating the UA. Heli Watch would also

include the wo rd “Experimental” on the UAS ground control station from which the Pilot in Command (PIC) operates the aircraft.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch 14 C.F.R. § 61.113(a) and (b) and 14 C.F.R. § 61.133 (a), Private pilot privileges and limitations, Pilot in command ; Commercial pilot privil eges and limitations 14 C.F.R. § 61.113 states , in significant part, that a person holding a private pilot license is prohibited from acting as a PIC of an aircraft for compensation or hire, nor may that person, for compensation or hire, act as a PIC of an aircraft. Sub

- part (b) prescribes, in significant part, exceptions for scenarios in which a PIC may be compensated. 14 C.F.R. § 61.113 prescribes, in significant part, when a person holding a commercial pilot license my act as a PIC of an aircraft for hire and the scenarios in which they may not act as a PIC for compensation.

Heli Watch UA s are unable to carry passengers or any cargo other than Heli Watch still and/or video cameras. Heli Watch requires that a PIC holds a private pilot license,

which d emonstrates an understanding of both the rules and best practices for maintaining safe ty and de

- conflicting UAS operation from other users of the NAS. As there is not currently UAS pilot licensing or certification, the requirements to obtain a private pil ot license and the additional qualifications required by Heli Watch establish an equivalent level of safety. UAS limitations are adequately addressed in the FARs addressing min/max altitude, prohibition of night flying and the requirement of operating

onl y within visual line of sight (VLOS) of the UA.

14 C.F.R. § 91.109(a)

, Flight instruction; Simulated instrument flight and certain test flights This section states, in significant part, that a civil aircraft being used for training or flight

instruction must have either dual controls or a “throwover control wheel.”

The UAS ground control station is a single control radio transmitter that does not accommodate a second set of controls. Any training of new PICs will be done in such a way that the trainer has positive, hands

- on control of the UA should there be a need to take control from the trainee. Further, all training activities will take place in a location that adds to the equivalent level of safety intended by 14 C.F.R. § 91.109(a).

14 C.F.R. § 91 .119

, Minimum Safe Altitudes: General (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, v essel, vehicle, or structure.

Heli Watch anticipates operating UASs to film movie scenes, special events or other missions that will require operating below 500 feet and within 500 feet of people,

vehicles or structures. Additionally, in accordance with FAA regulations for small UAS operation, maximum altitude for such operations is restricted to below 400 feet AGL.

Heli Watch will provide an equivalent level of safety by operating over authorized and participating individuals, vehicles or structures who are accounted for during the pre

flight planning and review process . Heli Watch will define divert areas to be used in the event that an emergency landing is required and will also operate at low enough altitudes so as to minimize risk to people and prop erty on the ground.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch 14 C.F.R. § 91.121

, Altimeter Settings This section states, in sub

- section (a)(1) , that the PIC must maintain a cruising altitude via the use of an altimeter that is set to either the reported altimeter setting of a station along the route and within 100 nm of the aircraft, if unavailable, the PIC will use the reported altimeter setting of an appropriate available station.

Heli Watch UAS have instrumentation that report s Altitude, Airspeed, Temperature, and Voltage to the ground stat ion.

Because the Heli Watch UA will operate well below 18,000 feet MSL , sub

- section 2 is not relevant to this petition.

14 C.F.R. § 91.151(a)

, Fuel Requirements for flight in VFR conditions (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;

Heli Watch UAs oper ate on electrical battery, but the implied intent of this section is to ensure that adequate flight time is available to accommodate any delays in landing. For purposes of this petition, remaining battery charge is equivalent to remaining fuel.

The pre

- f light check performed by the PIC will ensure that the UA has a full charge prior to takeoff, which will provide a minimum of 30 minutes of flying time. Landing procedures will be initiated with 20% charge remaining, or approximately 6 minutes of flight ti me. This margin will allow adequate time to ensure that the landing area is clear and safely land the UA, thereby providing an equivalent level of safety to the requirements set forth in 14 C.F.R. § 91.151(a).

Because the Heli Watch UA will operate only during daylight hours, sub

- section (a)(2) is not relevant to this petition.

14 C.F.R. § 91.203(a) and (b)

, Civil aircraft: Certification required. This section states, in significant part, an aircraft may not be operated without an

airworthiness certificate and that furthermore, it may not be operated “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 Heli Watch UA s are unable to carry passengers or crew, do not have an entrance, cabin or cockpit and, due to their size, are too small to carry the documentation referenced in 14 C.F.R. § 91.203(a) and (b). In lieu of affixing the certificate to the UA,

Heli Watch will display the registration number, the word “Experimental” and Heli Watch contact information on the UA. Additionally, the airworthiness certificate (if applicable

– see request regarding 14 C.F.R. 91.7 below) and registration certificate will be on file

a nd available for inspection at the control station.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch 14 C.F.R. Subpart E ( 91.401 through 91.417 ), Maintenance, Preventative
Maintenance and Alterations This regulation prescribes the responsibility for maintaining aircraft, requirements for returning an aircraft to service a fter maintenance or alterations, maintenance schedules

and required documentation

.

As compared to full

- size, manned aircraft, the UAS operated by Heli Watch are relatively straightforward for trained individuals to inspect and maintain. PICs will inspect the major components including the air

- ground communications, power plant, rotors/p ropellers, electrical connections and ensur e that camera and gimbal equipment

are firmly attached to the UA. Detailed inspections and preventative maintenance procedures that include partial tear

- down of the UA will be performed after every 20 flight

hour s.

PICs will be able to perform basic maintenance such as tightening connections, repairing cracks that do not compromise airframe integrity, replacing components such as propellers or switching camera equipment. Upon completion of the basic maintenance,
PICs will be authorized to re

- inspect the UA, verify that it is airworthy and return it to

service.

The Heli Watch Chief Pilot will perform any i ntermediate repairs or modifications, such as updating firmware or software or replacing general airframe. A ny advanced repairs or rebuilding of components will by performed by the component manufacturer or their designated agent.

The PIC and Chief Pilot will be responsible for documenting all repairs or modifications performed on the UA.

The implementation of a maintenance schedule, thorough pre

- flight inspections and the hierarchy assigned to the type of repair and which Heli Watch team member is authorized to perform the maintenance ensures an equivalent level of safety to the requirements set forth in 14 C.F.R. Subpart E (91.401 through 91.417).

14 C.F.R. § 91.7(a) and (b) Civil Aircraft Worthiness (a) No person may operate a civil aircraft unless it is in an airworthy condition.

(b) The pilot in command of a civil aircraft is responsible for determining whether that aircraft is in condition for safe flight. The pilot in command shall discontinue the flight when unairworthy mechanical, electrical, or structural conditions occur.

A certificate as described in 14 C.F.R. 91.7 may not be available or applica ble in the case of UAS and Heli Watch therefore requests an exemption to 14 C.F.R. § 91.7(a) and (b). However, the pre

- flight check that the Heli Watch PIC will conduct prior to each flight cycle and the in

- flight practices performed by the PIC and VO dur ing flight operations will provide equivalent safety to this regulation.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch APPENDIX B:

H ELI W ATCH E QUIPMENT AND F LIGHT O PERATIONS O VERVIEW

Heli Watch Unmanned Aircraft Systems ( UAS ) The Heli Watch fleet includes a variety of small, Unmanned Aircraft (“UA”) that are built

on

- site by an expert who has experience building manned experimental aircraft, large commercial aircraft and remotely

- operated aircraft, or UAs. The various UA designs allow Heli Watch to employ equipment that best fits within a proje ct’s requirements and is least disruptive to the NAS and surrounding environment. The following small UAs and related components/equipment make up the Heli Watch fleet:

Quadcopter

– Dji Phantom

Weight (Battery & Propellers included) = 1000g

Hover Accurac y (Ready to Fly)

• Vertical: 0.8m;

• Horizontal: 2.5m Max Yaw Angular Velocity = 200°/s Max Tilt Angle = 35° Max Ascent / Descent Speed = Ascent: 6m/s; Descent: 2m/s Max Flight Speed = 15m/s(Not Recommended) Diagonal Length = 350mm Flight Time = 25mins
Take

- of f Weight ≤ 1300g Operating Temperature =

- 10°C ~ 50°C Supported Battery = DJI Smart Battery DJI Smart Battery

• 3S LiPo

• Capacity: 5200mAh, 11.1V

• Charging Environment Range: 0  to 40 

• Discharging Environment Range:

- 20  to 50 

2.4GHz Remote Control

• Operating Frequency: 2.4GHz ISM

• Communication Distance (open area): 1000m

• Receiver Sensitivity (1%PER):

- 97dBm

• Working Current/Voltage: 120 mA@3.7V

• Built

- in LiPo Battery Working Current/Capacity: 3.7V, 2000mAh

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Diagonal Wheelbase: 900mm Frame Arm Length : 358mm Frame Arm Weight (Including Motor, ESC, Propeller ) : 316g
Center Frame Diameter : 272mm Center Frame Weight (with Landing Gear Mounting Base, Servos) : 1185g Landing Gear Size : 460mm(Length) × 450mm(Wi dth) × 360mm(Height)

Motor

• Stator Size : 41 × 14mm

• KV : 400rpm/V

• Max Power : 500W

• Weight(with Cooling Fan) : 158g

ESC

• Working Current : 40A

• Working Voltage : 6S LiPo

• Signal Frequency : 30Hz ~ 450Hz

• Drive PWM Frequency : 8KHz

• Weight(with Radiators) : 35g

• Foldable Propeller (1552/1552R)

Material

• High strength performance engineered plastics

• Size : 15 × 5.2inch

• Weight: 13g

Flight Parameters

• Takeoff Weight

• 4.7Kg ~ 8.2Kg

• Total Weight : 3.3Kg

Power Battery : LiPo (6S

10000mAh~15000mAh

15C(Min))

• Max Power Consumption : 3000W

• Hover Power Consumption : 1000W (@6.8Kg Takeoff Weight)

• Hover Time : 18min (@12000mAh& 6.8Kg Takeoff Weight)

• Working Environment Temperature :

- 10 °C ~ +40 °C

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch Heli Watch Flight Team Members The Heli Watch flight team will include the following individuals for all events:

1. A Pilot in Command (PIC), whose primary responsibility will be the safe operation
of the UAS in accordance with the FARs. The PIC will hold a minimum of an FAA Private Pilot License and the corresponding medical cer tificates to maintain

said license.

2. A Visual Observer (VO), who will be responsible for ensuring that the UAS is being operated within the restrictions set forth in the FARs and to provide a second pair of eyes to mitigate any hazards to safe operations. If not a licensed pilot, the VO will receive orientation on the FAR and training on the responsibilities of an observer such as, but not limited to, flight team communications, properly monitoring the airspace and identifying hazards.

3. (Optional

– if requir ed and on a project

- by

- project basis) A Camera Operator

, (CO) who will operate any still or video camera included in the UAS. The CO is not considered a part of the flight team, but will be used when a project requires a moving camera instead of one that it locked in a fixed position, or if terrain, proximity to non

- Class G airspace or other environmental factors make the
addition of a third team member prudent.

Heli Watch Flight Team Qualifications and Responsibilities

Each member of the Heli Watch flight team will meet a minimum set of qualifications,

includ ing FAA licenses and UAS operation training to ensure team and public safety. During operations, flight team members will be responsible for specific tasks to divide the workload and enhance safety.

Pilot in Command (PIC) The PIC holds the proper licen ses/certifications to conduct the flight and has final authority over all operations (regardless if UA is in the air at the time) and responsibility for safely operating the UA. A PIC will be designated prior to flight operations and only one person will be the designated PIC at any time.

At minimum, the PIC will possess the following:

• FAA Private Pilot License and required medical certifications

• The PIC will be qualified to operate the UA by possessing a minimum of 100 flight cycles and 25 hours of total time as a UA rotorcraft pilot and at least ten hours logged as a UA pilot with a similar UA type.

• Successful completion of Heli Watch training on the proper pre

- flight inspection of UAs

.

The PIC’s duties include:

• Evaluating the environment for hazards

• Performing pre

- flight checks and briefings

• Safely operating the UA within the FARs

• Coordinating with the VO to evaluate the operating area for safety

• Terminating flight operations and landing the UA as soon as practical and
safe to do so if unsafe condi tions arise.

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch Visual Observer (VO)
The VO is responsible for overseeing the safety aspects of UAS operations on each project and enforcing all FAA regulation s set forth in the Reform Act.

At minimum, the VO will demonstrate knowledge of the requirement s defined in 14 C.F.R. including: operations near other aircraft, right

- of

- way and basic VFR, plus the proper use of pilot/air traffic control phraseology. VOs who are not licensed private pilots will also complete a comprehensive Heli Watch training prog ram to ensure that:

• The VO fully understands the FARs as they relate to the safe operation of a UAS and the importance of complying with them,

• The VO is familiar with crew resource management and clearly understand s his/her role as it relates to the PIC,

• The VO is able to accurately read and interpret aeronautical charts, NOTAMs, COAs, weather forecasts and any other information required to ensure safe operations,

• The VO is able to effectively communicate and coordinate with the PIC to ensure a safe opera ting environment

• The VO has the opportunity to gain hands

- on experience with a PIC, before participating on a paid project, to validate knowledge and address any questions or concerns in an environment that is dedicated solely to knowledge transfer betwee n Heli Watch crew.

In addition to PIC and VO qualifications, the Heli Watch Chief Pilot possesses an extensive set of qualifications and experience from which training and oversight of flight operations will benefit:

The Chief Pilot (CP) is responsible for the construction, maintenance and safe operation of the Heli Watch UAS fleet. The CP possesses the following:

• FAA Private Pilot License with more than 20 years of flying experience

• B.S. degree in Mechanical Engineer ing

• M.S. degree in Aeronautical Science

• 15 years experience in the testing, maintenance and repair of commercial aircraft, which includes FAA

- required documentation, while working for several major aircraft manufacturers

• 25 years experience building and maintaining manned experimental and
small unmanned aircraft

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- 1553 • www.HeliWatch.com • Twitter: @heli_watch Heli Watch Flight Operations

Pre

- flight The PIC and VO will conduct a pre

- flight briefing that includes:

• Review aeronautical charts to

o ensure that planned operating area is compliant wit h FARs

o identify known hazards to navigation

o determine safe divert areas (if applicable)

• Review weather forecasts

• Review all Notice to Airmen (NOTAM) that may be active in the operating area

• When required, obtain a Certificate of Waiver or Authorization (CO A) from the regional ATO

• When required, submit a notice of planned operations to the appropriate Flight Standards District Office (FSDO) a NOTAM between 72 and 48 hours prior to commencing operations

• Perform a pre

- flight maintenance check to ensure that th e UAS is functioning according to manufacturer specifications including the communications link between the UA and ground control station, remaining battery charge, condition of airframe, propellers and wiring.

• Inspect the UA to comply with maximum weight limitations of 55 lbs. gross weight

• Display a sign or other notice indicating that UAS operations are in progress in the area and identifying Heli Watch as the owner/operator of the UAS. The ground control station is a portable unit that is worn by the PIC to ensure freedom of movement should repositioning be required to maintain proper visual line of sight. As such, the notification sign will be placed within 10 feet of the PIC’s initial position and moved, as required, and never to exceed a distance o f 20 feet
from the PIC. Additionally, flight operations will primarily be conducted within a closed set environment or in an area where only authorized and consenting

individuals are allowed.

In

- flight The PIC will operate the UAS in accordance with the FARs and Heli Watch pre

- flight briefing described above to maintain public safety. During flight operations, the PIC will:

• Navigate the UAS within the operational area

• Monitor a ltitude and airspeed

• Maintain visual line of sight (VLOS) with the UA

• Monitor b attery charge/remaining flying time

The VO will:

• Monitor UAS operations to cross

- check PIC and ensure that the UA stays within
VLOS and within the required altitude and airspeed limitations,

• Monitor the airspace to ensure that aircraft, birds or other a irborne hazards remain out of the operating area,

• Monitor the general operating area to ensure that the UA maintains proper separation from hazards, restricted or unauthorized airspace and that no ground hazards, such as unauthorized persons or vehicle ent er, the operating area,

• Monitor weather conditions to ensure that wind, cloud ceiling or other factors do not exceed safe operating parameters,

• Immediately instruct the PIC to terminate flight operations and assist the PIC to safely land the UA if any unsafe conditions arise.