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Indy Aerial Photography LLC

Andrew Hawes

2290 Willow Lakes East Blvd

Greenwood, Indiana 46143

indyaerialphoto@gmail.com

January 13, 2016

U. S. Department of Transportation

Docket Management System

1200 New Jersey Ave., SE 

Washington, DC 20590

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

Aviation Regulations from 14 C.F.R. 45.23(b);14 CFR Part 21;14 CFR 61.113 (a) 

& (b); 91.7 (a);91.9 (b) (2);91.103(b); 91.109;91.119; 91.121; 91.151(a);91.203(a) 

& (b);91.405 (a); 91.407(a) (1); 91.409 (a) (2);91.417 (a) & (b).

Dear Sir or Madam:

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

Act) and 14 C.F.R. Part 11, Indy Aerial Photography LLC, developer and operator of Small 

Unmanned Aircraft Systems (“sUASs”) equipped to conduct aerial electronic data collection c

and aerial photography for the commercial video industry, hereby applies for an exemption 

from the listed Federal Aviation Regulations (“FARs”) to allow commercial operation of its 

sUASs, 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.

As described more fully below, the requested exemption would permit the operation of 

small, unmanned and relatively inexpensive sUAS under controlled conditions in airspace that 

is 1) limited 2) predetermined 3) controlled as to access and 4) would provide safety 

enhancements to the already safe operations in the aerial filming and monitoring 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.” Section 333(c) of the Reform Act.

c Aerial Data Collection” which includes any remote sensing and measuring by an instrument(s) aboard the 

UA. Examples include imagery (photography, video, infrared, etc.), electronic measurement (precision surveying, RF 

analysis, etc.), chemical measurement (particulate measurement, etc.), or any other gathering of data by instruments 

aboard the UA
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The name and address of the applicant is:

Indy Aerial Photography LLC

Andrew Hawes

Ph: 317-560-0766

Email: indyaerialphoto@gmail.com

Address: 2290 Willow Lakes East Blvd, Greenwood, Indiana, 46143

Regulations from which the exemption is requested:

14 CFR Part 21

14 C.F.R. 45.23(b)

14 CFR 61.113 (a) & (b)

14 C.F.R. 91.7 (a)

14 CFR 91.9 (b) (2)

14 C.F.R. 91.103

14 C.F.R. 91.109

14 C.F. R. 91.119

14 C.F.R. 91.121

14 CFR 91.151 (a)

14 CFR 91.203 (a) & (b)

14 CFR 91.405 (a)

14 CFR 407 (a) (1)

14 CFR 409 (a) (2)

14 CFR 417 (a) & (b)

This exemption application is expressly submitted to fulfill Congress’ goal in passing Section 

333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to 

consider whether certain unmanned aircraft systems may operate safely in the national 

airspace system (NAS) before completion of the rulemaking required under Section 332 of the 

Reform Act. In making this determination, the Secretary is required to determine which types of 

sUASs do not create a hazard to users of the NAS or the public or pose a threat to national 

security in light of the following:

• The sUAS’s size, weight, speed, and operational capability;

• Operation of the sUAS in close proximity to airports and populated areas

• Operation of the sUAS within visual line of sight of the operator.

Reform Act § 333 (a). Lastly, if the Secretary determines that such vehicles “may operate 

safely in the national airspace system, the Secretary shall establish requirements for the safe 

operation of such aircraft in the national airspace system.” Id. §333(c) (emphasis added) A

_______________________________________________________________________

A Applicant interprets this provision to place the duty on the Administrator to not only process applications for 

exemptions under section 333, but for the Administrator to craft conditions for the safe operation of the sUAS, if it 

should be determined that the conditions set forth herein do not fulfill the statutory requirements for approval.
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The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This 

statutory authority by its terms includes exempting civil aircraft, as the term is defined under 

§40101 of the Act, that includes sUASs, from the requirement that all civil aircraft must have a 

current airworthiness certificate.

The Administrator may grant an exemption from a requirement of a regulation prescribed 

under subsection (a) or (b) of this section or any sections 44702-44716 of this title if the 

Administrator finds the exemption in the public interest. 49 U.S.C. §44701(f) See also 49 USC 

§44711(a); 49 USC §44704; 14 CFR §91.203 (a) (1).

Indy Aerial Photography LLC’s sUASs are rotorcraft, weighting 55 or fewer lbs. including 

payload. They operate, under normal conditions at a speed of no more than 50 knots and have 

the capability to hover, and move in the vertical and horizontal plane simultaneously. They will 

operate only in line of sight and will operate only within the sterile area described in the Flight 

Safety Manual, attached as Exhibit B (hereinafter “the Manual”). Such operations will insure 

that the sUAS will “not create a hazard to users of the national airspace system or the public.” B

Given the small size of the sUASs involved and the restricted sterile environment within which 

they will operate, the applicant falls squarely within that zone of safety (an equivalent level of 

safety) in which Congress envisioned that the FAA must, by exemption, allow commercial 

operations of UASs to commence immediately. Also due to the size of the sUASs and the 

restricted areas in which the relevant sUASs will operate, approval of the application presents 

no national security issue. Given the clear direction in Section 333 of the Reform Act, the 

authority contained in the Federal Aviation Act, as amended; the strong equivalent level of 

safety surrounding the proposed operations, and the significant public benefit, including 

enhanced safety, reduction in environmental impacts, including reduced emissions associated 

with allowing sUASs for commercial video operations, the grant of the requested exemptions is 

in the public interest. Accordingly, the applicant respectfully requests that the FAA grant the 

requested exemption without delay.

AIRCRAFT AND EQUIVALENT LEVEL OF SAFETY

The applicant proposes that the exemption requested herein apply to civil aircraft that 

have the characteristics and that operate with the limitations listed herein. These limitations 

provide for at least an equivalent or even higher level of safety to operations under the current 

regulatory structure because the proposed operations represent a safety enhancement to the 

already safe commercial video filming operations conducted with conventional aircraft.

__________________________________________________________________________

B Reform Act Section 333 (b).
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These limitations and conditions to which Indy Aerial Photography LLC agrees to be bound 

when conducting commercial operations under an FAA issued exemption include:

1. The sUAS will weigh less than 55 lbs.

2. Flights will be operated within line of sight of a pilot and/or observer.

3. Maximum total flight time for each operational flight will be 20 minutes. Flights will be 

terminated at 25% battery power reserve should that occur prior to the 20 minute limit.

4. Flights will be operated at an altitude of no more than 400 feet AGL or, not more than 200 

feet above an elevated platform from which filming is planned.

5. Minimum crew for each operation will consist of the sUAS Pilot and the Visual Observer.

6. sUAS pilot will be an FAA licensed airman with at least a sport or recreational certificate (or 

the minimum required certification at the time of the flight) and a valid driver’s license. The 

observer will also hold a valid driver’s license.

7. sUAS Pilot will be Pilot in Command (PIC). If a pilot certificate holder other than the sUAS 

Pilot, who possess the necessary PIC qualifications, is also present on set (i.e. the Aerial 

Coordinator), that person can also be designated as PIC.

8. The sUAS will only operate within a confined “Sterile Area” as defined in the Manual. 

Section C of the Manual requires the establishment of a “Safety Perimeter” for the flight 

operations area.

9. A briefing will be conducted in regard to the planned sUAS operations prior to each day’s 

production activities. It will be mandatory that all personnel who will be performing duties within 

the boundaries of the safety perimeter be present for this briefing.

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

requested exemption, with the appropriate Flight Standards District Office.

11. The operator will obtain the consent of all persons involved in the filming and ensure that 

only consenting persons will be allowed within 100 feet of the flight operation, and this radius 

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

by Section F of the Manual. With the advanced permission of the relevant FSDO, operations at 

closer range can be approved. (See Section B in the Manual Appendix B)

12. The operator will submit a written Plan of Activities to the local FSDO with jurisdiction over 

the area of proposed filming. The three-day notification may be waived with the concurrence of 

the FSDO.

13. Pilot and observer will have been trained in operation of sUAS generally and received upto-date information on the particular sUAS to be operated as required.

14. Observer and pilot will at all times be able to communicate by voice.

15. Written and/or oral permission from the relevant property holders will be obtained.

16. All required permissions and permits will be obtained from territorial, state, county or city 

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

17. If the sUAS loses communications or loses its GPS signal, the sUAS will have capability to 

return to a pre-determined location within the Security Perimeter and land.

18. The sUAS will have the capability to abort a flight in case of unpredicted obstacles or 

emergencies.
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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 sUAS. In all cases, an 

analysis of these criteria demonstrates that the sUAS 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 sUAS 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 area as set out in the Manual. Unlike other civil aircraft, operations under this 

exemption will be tightly controlled and monitored by both the operator, pursuant to the 

Manual’s requirements, and under the requirements and in compliance with local public safety 

requirements, to provide security for the area of operation as is now done with conventional 

filming. The FAA will have advance notice of all operations. These safety enhancements, which 

already apply to civil aircraft operated in connection with motion picture and television 

production, 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 sUAS, 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 sUAS will have no airworthiness certificate, an exemption may be 

needed as the sUAS will have no entrance to the cabin, cockpit or pilot station on which the 

word “Experimental” can be placed. Given the size of the sUAV, two-inch lettering will be 
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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 sUAV marked on its 

fuselage as required by §45.29 (f) where the pilot, observer and others working with the sUAV 

will see the identification of the sUAS as “Experimental.” The FAA has issued the following 

exemptions to this regulation to Exemptions Nos. 10700, 8738, 10167 and 10167A.

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

Sections 61.113 (a) & (b) limit private pilots to non-commercial operations. Because the sUAS 

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 aircraft to have a private pilot’s 

license rather than a commercial pilot’s license to operate this small sUAS. Unlike a 

conventional aircraft that carries the pilot and passengers, the sUAS is remotely controlled with 

no living thing on board. The area of operation is controlled and restricted, and all flights are 

planned and coordinated in advance as set forth in the Manual. The level of safety provided by 

the requirements included in the Manual exceeds that provided by a single individual holding a 

commercial pilot’s certificate operating a conventional aircraft. The risks associated with the 

operation of the sUAS are so diminished from the level of risk associated with commercial 

operations contemplated by Part 61 when drafted, that allowing operations of the sUAS as 

requested with a private pilot as the PIC exceeds the present level of safety achieved by 14 

C.F.R. §61.113 (a) & (b).

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 and the requirements contained in the Manual for maintenance 

and use of safety check lists prior to each flight, as set forth in Sections C & D, 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.
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The sUAS, 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 sUAS will have immediate access to it. The FAA has 

issued the following exemptions to this regulation: Exemption Nos. 8607, 8737, 8738, 9299, 

9299A, 9565, 9565B, 10167, 10167A, 10602, 32827, and 10700.

14 C.F.R. § 91.103(b): 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. An equivalent level of safety will be provided as set forth 

in the Manual. The PIC will take all actions including 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.

sUASs and remotely piloted aircraft, by their design do not have fully functional dual controls. 

Flight control is accomplished through the use of a control box that communicates with the 

aircraft via radio communications. The FAA has approved exemptions for flight training without 

fully functional dual controls for a number of aircraft and for flight instruction in experimental 

aircraft. See Exemption Nos.5778K & 9862A. 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.

Safe simulation and practice flight will be carried out in controlled environments. All 

simulations will be carried out on a computer using the drone controls. Any practice flying will 

take place in a safe environment, with no risk to human life below.

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 sUAS 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 sUAS will never operate at higher than 400 AGL. It will however be operated in a 
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restricted area with safety 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 sUAS 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 as set forth in the Manual. Compared to flight operations with aircraft or rotorcraft 

weighing 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 the movie industry. In addition, the lowaltitude operations of the sUAS will ensure separation between these small-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 sUAS 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 Manual and Safety Checklist, 

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 sUAS provides approximately 25 minutes of powered flight. To meet 

the 30 minute reserve requirement in 14 CFR §91.151, sUAS flights would be limited to 

approximately 20 minutes in length. Given the limitations on the sUAS’s proposed flight area 

and the location of its proposed operations within a predetermined area, a longer time frame for 

flight in daylight or night VFR conditions is reasonable.

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

exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without 

compliance with FAR 91.151 (a)). Operating the small sUAS, 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 sUAS. 

Additionally, limiting sUAS flights to 20 minutes would greatly reduce the utility for which the 

exemption will be granted.
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Applicant believes that an equivalent level of safety can be achieved by limiting flights to 20

minutes or 25% of battery power whichever happens first. This restriction would be more than 

adequate to return the sUAS to its planned landing zone from anywhere in its limited operating 

area.

Similar exemptions have been granted to other operations, including Exemptions 2689F, 

5745, 10673, and 10808.

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 sUAS 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 sUAS.

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

control point where the pilot flying the sUAS will have immediate access to them, to the extent 

they are applicable to the sUAS. The FAA has issued numerous exemptions to this regulation. 

A representative sample of other exceptions includes Exemption Nos. 9565, 9665, 9789, 

9789A, 9797, 9797A, 9816A, and 10700.

14 C.F.R. §91.405 (a); 407 (a) (1); 409 (a) (2); 417(a) & (b): Maintenance Inspections

These regulations require that an aircraft operator or owner “shall have that aircraft inspected 

as prescribed in subpart E of this part and shall between required inspections, except as 

provided in paragraph (c) of this section, have discrepancies repaired as prescribed in part 43 

of this chapter...,” and others shall inspect or maintain the aircraft in compliance with Part 43.

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

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

operator pursuant to the flight manual and operating handbook as referenced in the 

Manual.(See Sections B, D and G) An equivalent level of safety will be achieved because 

these small sUASs are very limited in size and will carry a small payload and operate only in 

restricted areas for limited periods of time. If mechanical issues arise the sUAS can land 
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immediately and will be operating from no higher than 400 feet AGL. As provided in the 

Manual, the operator will ensure that the sUAS 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.

Pursuant to 14 C.F.R. 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 C.F.R. §21, subpart H; 14 C.F.R 45.23(b);14 C.F.R. §§ 61.113( a) 

& (b);91.7 (a); 91.9 (b) (2);91.103(b);91.109; 91.119; 91.121; 

91.151(a);91.203(a) and (b); 91.405 (a); 91.407 (a) (1); 91.409 (a) (2); 

91.409 (a) (2) and 91.417 (a) & (b) to operate commercially a small 

unmanned vehicle (55lbs or less) in motion picture and television 

operations.

Approval of exemptions allowing commercial operations of sUASs in the film industry will 

enhance safety by reducing risk. Conventional film operations, using jet or piston power 

aircraft, operate at extremely low altitudes just feet from the subject being filmed and in 

extreme proximity to people and structures; and present the risks associated with vehicles that 

weigh in the neighborhood of 4,000lbs., carrying large amounts of jet A or other fuel. Such 

aircraft must fly to and from the film location. In contrast, a sUAS weighing fewer than 55 lbs. 

and powered by batteries eliminates virtually all of that risk given the reduced mass and lack of 

combustible fuel carried on board. The sUAS is carried to the film set and not flown. The sUAS 

will carry no passengers or crew and, therefore, will not expose them to the risks associated 

with manned aircraft flights.

The operation of small sUASs, weighting less than 55 lbs., conducted in the strict conditions 

outlined above, will provide an equivalent level of safety supporting the grant of the exemptions 

requested herein, including exempting the applicant from the requirements of Part 21 and 

allowing commercial operations. These lightweight aircraft operate at slow speeds, close to the 

ground, and in a sterile environment and, as a result, are far safer than conventional operations 

conducted with turbine helicopters operating in close proximity to the ground and people.

sUASs Details: See Appendix C

Safety Features:

● Emergency “Return-To-Home”

○ At the beginning of each flight a home point is set. This home 

point is set in accordance with the manual to allow for a safe takeoff and return. Should the pilot’s control lose signal with the sUAS 
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or manually request a return, the sUAS will return to the starting 

point. 

Privacy

All flights will occur over private or controlled access property with the property owner’s prior 

consent and knowledge. Filming will be of people who have also consented to being filmed or 

otherwise have agreed to be in the area where filming will take place.

Satisfaction of the criteria provided in Section 333 of the Reform Act of 2012--size, weight, 

speed, operating capabilities, proximity to airports and populated areas and operation within 

visual line of sight and national security – provides more than adequate justification for the 

grant of the requested exemptions allowing commercial operation of applicant’s sUAS in the 

commercial video production industry pursuant to the Manual appended hereto.

Sincerely

Indy Aerial Photography 

LLC

Andrew Hawes
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Appendix A: No-Fly Zones

Indy Aerial Photography LLC’s Pilots will not be operating within 5 nautical miles of any 

airport.

As a safety precaution, Indy Aerial Photography LLC’s pilots will not be operating within 5 

nautical miles of any airport similar to the permission granted in Exemption No. 11153 -

Regulatory Docket No. FAA20140519, page 25, "20. The UA may not operate within 5 nautical 

miles of an airport reference point as denoted on a current FAA-published aeronautical chart 

unless a letter of agreement with that airports management is obtained, and the operation is 

conducted in accordance with a NOTAM as required by the operators COA. The letter of 

agreement with the airport management must be made available to the Administrator upon 

request."

As well as in Exemption No. 11195 - Regulatory Docket No. FAA20140884, page 12, "19. The 

UA may not operate within 5 nautical miles of an airport reference point as denoted on a 

current FAA-published aeronautical chart unless a letter of agreement with that airports 

management is obtained, and the operation is conducted in accordance with a Notice to 

Airmen (NOTAM), as required by the operators Certificate of Waiver or Authorization (COA). 

The letter of agreement with the airport management must be made available to the 

Administrator upon request."

Indy Aerial Photography LLC requests the same flexibility as exemptions 11153 and 11195 for 

acquiring agreement with the airports' management should operations fall within 5 nautical 

miles of an airport. 
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Appendix B: Safety Manual

A. Maintenance 

a. The sUAS must be inspected by a trained technician every 10 flight hours. All 

maintenance records will be maintained for inspection as set forth in Section B. 

b. If any maintenance is undergone, the sUAS must pass a flight test with both a 

pilot and a manufacturer trained technician before flight. 

B. Record Keeping

a. A digital record will be kept for all flights, flight times, and maintenance records. 

C. Securing Flight Site

a. FSDO Submissions

i. The sUAS operator will file a FAA Form 7711-1, or its equivalent, as 

modified in light of the requested exemption, with the appropriate Flight 

Standards District Office.

b. Safety Parameter

i. Before filming occurs, a 100 yard perimeter from the planned flight path 

will be identified in order to set a “sterile” environment for the operation.

1. Indy Aerial Photography LLC must obtain written or oral 

permission from all landowners in sterile environment. 

2. 48 hours before filming, all residents or businesses within 100 

yards of the filming will be notified with printed flyers.

a. Flyers will contain date of flight, time of flight, and contact 

information.

3. Streets and sidewalks that cross into the sterile environment will 

be marked with “Warning Low flying Aircraft - Stay Back 150ft” 

signs to warn the public.

4. At all times Indy Aerial Photography LLC will carry $1mm in 

general liability insurance in case of any damage to property or 

persons within the safety parameter

c. Identify potential obstacles 

i. Before each flight, an inventory will be taken for all potential obstacles 

that must be avoided while in flight. Including:

1. Powerlines

2. Cell Phone Towers

3. Trees

4. Flocks of birds that may take flight

5. Heavily traveled roadways

6. Utility wires

7. Elevated structures

8. At least 5 nautical miles from the nearest airport or helipad.

D. Pre-Flight Checklist

a. Take Off Location/ “Home”
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i. The sUAS will mark its take off location as a safe area to return to should 

the sUAS lose signal with the control or if the pilot signals the craft to 

return to its “home” location.

1. Take off location will be in an area with a 25ft radius with no 

obstructions, maintaining said radius vertically 200ft.

2. The sUAS will take off and land in the same location.

3. GPS Altimeter will be marked as 0’ elevation

b. Flight Canceling Events

i. All flights will be cancelled for a minimum of 2 hours if any of the below 

occur:

1. Police activity in the area

2. Low flying aircraft in the area

3. Medical/News Helicopters active in the area

4. Wind exceeding 10 mph

5. Any emergency requiring emergency services occurs within the 

sterile environment

6. PIC is unable to complete flight without losing visual of the sUAS

7. Any precipitation 

8. Heavy bird presence in the area that could cause a mid-air 

collision.

9. Any defects or damage found during preflight exam

c. Physical Inspection

i. Before each flight the sUAS will be checked to ensure that it is safe for 

flight.

1. Battery voltage will be checked to ensure it is >75%

2. Blades will be inspected to ensure they are tightened and free of 

damage

3. Camera mount and gimbal will be inspected to ensure it is fully 

attached and operating.

4. sUAS will be checked for any damage that may have taken place 

in transit.

5. The sUAS will be tested at a low altitude to ensure all controls are 

responding correctly.

6. Battery checked for damage that could affect its charge

ii. If any party of the inspecting shows a damaged part or parts, the sUAS is 

deemed non-usable and must be inspected by a trained technician. 

d. Post Flight Inspections/Checklist

i. After each flight, the the sUAS will be thoroughly inspected for any 

damage that occurred in flight. 

1. Body inspected for any damage

2. Blades visually checked for any damage at all

3. Battery checked for damage

E. Mid-Air Safety Protocol

a. Max Speed
15

i. Ascent

1. 10m/s

ii. Descent

1. 4m/s

iii. Flight Speed

1. The sUAS is never to exceed 10m/s

b. Altitude

i. The sUAS is never to exceed 400ft

c. Emergency

i. If it appears that the sUAS, any property or humans are at risk, the sUAS 

will be grounded immediately to a safe location.

d. Sight

i. The pilot must keep the sUAS within eyesight at all times unassisted by 

any technology. 

F. Participation by non-pilot staff

a. All staff involved in the production or filming using the sUAS will consent to 

maintain a safe distance of at least 30 ft during the filming.

G. Pilot/Spotter Training

a. Before flying, both the Pilot and spotter will receive updated information on the 

sUAS and its firmware. 

i. The controller allows for a simulator training, both the pilot and spotter are 

allowed to run through the simulator training 
16

Appendix C 

UAS #1: DJI 

See Appendix D for user manual

Model: Inspire 1 Pro

UAS #2: Turbo Ace

See Appendix E for UAS Info

Model: Matrix-E
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Appendix D: User Manual
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Appendix E: UAS Information

MATRIX-E SPECIFICATIONS

x Dimensions Wingspan (including propellers): Diagonal=1160mm, Front=1040mm, 

Back=980mm

x Dimensions Operating Position (including propellers): W=840mm, L=790mm, 

H=130mm

x Dimensions Folded Position (including propellers): W=295mm, L=830mm, H=110mm

x Dimensions Motor to Motor: Diagonal=780mm

x Maximum Payload Capacity: Gimbal+Camera+Accessories=3.5LB, 

Gimbal+Camera+Accessories+8000mah Battery=6.2LB

x Maximum Optimal Payload Capacity: Gimbal+Camera+Asscessories=2.5LB, 

Gimbal+Camera+Accessories+8000mah Battery=5.2LB

x Matrix Weight without Payload/Battery: 4.8LB

x Typical Operating Weight with Hero3: Matrix+Gyrox-3+VTX& Power (5.33LB)+ Hero3 

(.17LB) +VTX+8,000mah Battery (2.5LB) = 8LB

x Typical Operating Weight with Sony NEX 5R: Matrix-E+Gyrox-5R+VTX&Power 

(5.5LB) + NEX-5R+Lense (1LB), 8,000mah Battery (2.5LB) = Total: 10LB

x Motors: Diameter=42mm, Height=35mm

x ESC: 40amp

x Propellers: 2xCW & 2xCCW, 15" Extra Robust Carbon Fiber Constructions, Dual 

Position Mount

x Battery Recommended: 8,000mah 6S (22.2V) 25C

x Flight Time: Matrix + 10,000mah Battery = 35min

x Flight Time: Matrix + 8,000mah Battery + Vibration Isolation Carbon Plates + Hero3 = 

30min

x Flight Time: Matrix-S + 8,000mah Battery + Brushless Gyrox3 Gimbal + Hero3 = 22-

25min

x Flight Time: Matrix-E + 8,000mah Battery + Brushless Gyrox5R Gimbal & Sony NEX5R = 12-15min

x Transmitter & Receiver Recommendation: 2.4GHz, Minimum 6-Channels, Optimal 7-

Channels or more

x Standard Distance Operations: 300 to 500 feet (Using Walkera Devo 10 & Most Other 

Name Brand Transmitters)

x Long Distance Operations: 4,224 feet (.8miles) to 6,336 feet (1.2miles) (Using 

Spektrum DX8/DX18 & Futaba 14SG)

x FPV Recommendation: 5.8GHz Video Transmitter & Video Receiver + Monitor or 

Goggles

x Wind Tolerance: Class 5

x Aluminum Case Dimensions: L=935mm, W=410mm, H=145mm
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MATRIX PACKAGE FEATURES & OPTIONS

x Triple Deck Carbon Fiber Architecture

x C4 Vibration Isolation Deck to eliminate jello effect on videos

x Foldable Arms that locks into portable or operating positions

x Naza-M Lite, Naza-M V2 & WooKong Flight Controller Selection

x GPS & Compass Functions include GPS-Lock, Home-Lock, Course-Lock & Return-toHome

x Brushless Gimbal for gyro based auto-stabilization or Hard Mount with Vibration Isolation 

Options

x Centrally Located Rotation for camera & gimbal auto-stabilization eliminates the 

pendulum effect

x 42mm Brushless Motors dynamically balanced to minimize vibrations

x 40amp ESCs with Cooling Algorithm overspecced to support extended high torque 

operations 

x 15inch Extra Heavy Duty Carbon Fiber Propellers to resist flexing and warping under 

heavier payloads

x 2.4GHz Standard & Long Range Walkera, Spektrum & Futaba Transmitters, Receivers 

& Telemetry

x Multiple Battery Mounting Positions on both top or bottom of main frame

x Single 8,000 & 10,000mah 6S (22.2V) LiPo Battery Options

x B601 or Quattro Professional Wall Charger Options

x Adjustable Landing Skid for a variety of surfaces

x Foldable GPS Compass with Locking Bracket for consistent alignment

x Adjustable Arms Mounting Position for aggressive forward sports flight

x FPV Live Feed Video available for a selection of cameras

x Flash Memory with detailed instructions

x Heavy Duty Aluminum Carrying Case will be available to fit Matrix, transmitter, gimbal & 

more.

x Training Package Options including small crash resistant quadcopters & flight simulators

CULMINATION OF INNOVATION, EXPERIENCE & EXECUTION

Leapfrogging quadcopter records with ease, the sporty new Matrix is crushing all competitions 

with its super sized wingspan. Yet, it folds down nicely to fit in a professional aluminum case 

along with the transmitter radio. Matrix's super efficient 6-cell system powers 4 muscular 42mm 

brushless motors driving 15" carbon fiber propellers for unparalleled lifting capacity and stability. 

Conceptualized by master FPV pilots, Matrix is a quadcopter designed for rather than adapted 

to carrying cameras. To satisfy an almost insurmountable list of high expectations, Turbo Ace 

engineers set out on a journey of innovation and discovery. Applying more than 85 years of 

combined helicopter and multi-rotor expertise between our master pilot group, engineers and 

designers, the Matrix represents an ultimate breakthrough in quadcopter engineering and 

optimization. To search for the ultimate mix of performance and durability, Turbo Ace 
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developers matched up countless motors, ESCs and propellers combinations followed by series 

of unrelenting updates and test flights. From planning and implementing the best components 

on a foldable structure, setting and meeting new milestones in flight time and payload, to 

executing crucial requirements for flight and camera stabilization, the Turbo Ace Matrix is truly a 

quadcopter beyond its time. 

UNPRECEDENTED PAYLOAD & FLIGHT TIME

Matrix's big breakthrough is a 25-minute flight time carrying the #1 selling GoPro Hero3 

stabilized on the ultra fast 2-axis brushless Gyrox3 gimbal. Cutting out the gimbal but keeping 

the Hero3 on a vibration isolation plate will extend Matrix flight time beyond the amazing 30min 

threshold. Despite many unrealistic claims, the closest competition offers less than half the flight 

time. At about 3 times the size of a mid-sized quadcopter, heavier payloads exert 

disproportionatelly less impact on Matrix flight time than smaller quadcopter flight time. Without 

exception, even the top selling mid-sized quadcopters with 8" to 10" propellers will max out at 5-

6 minutes with Hero3 and gimbal onboard. It's common for both vendors and end users to 

exaggerate or manipulate payload and flight time by gutting critical components inside 

quadcopters and cameras.

 

IDEAL UNOBSTRUCTED AUTO-STABILIZED CAMERA/GIMBAL LOCATION

Tired of propellers and landing skids framing your video? The Matrix's nose offers an ideal 

location with unobstructed view - no propellers even in wide angle videos, no skid landing when 

pointed down and no more annoying propellers shadows on the lenses. Although these are 

nagging issues, there are even more crucial factors in achieving stability. Because traditionally 

mounted cameras are about 8 inches below the main hub, a quadcopter's roll causes the 

camera to swing like a pendulum. Although a good gimbal is able to compensate for the roll axis 

movement, it's unable to address the horizontal movement that causes a video to shift from side 

to side as if a skater is holding the camera. By moving the gimbal and camera up to the level of 

the propellers, the Matrix design has basically eliminated the pendulum effect. Last but not 

least, gimbals are only as stable as the foundation they are mounted on. Bypassing the weight 

and slack of unstable undermounted gimbal platforms, Matrix's gimbal is mounted directly on 

the main frame to prevent oscillation from surfacing. 

TRIPLE CARBON FIBER DECK FOR COMPREHENSIVE & VERSATILE INTEGRATION

In housing and supporting an extensive list of stock and upgrade components on a super-scaled 

quadcopter, Matrix's triple decked carbon fiber structure is extremely strong and versatile. Four 

foldable arms which double as supporting beams are securely sandwiched between the lower 

decks along with multiple ventilated ESC positions. The middle deck houses and protects all 

critical electronic components such as the flight controller, the GPS, LED and other optional 

systems. Versatile Battery and ESC mounting positions allows the operator to shift CG (center 

of gravity) upward, downward, forward and backward to accommodate a wide variety of 

payloads and flight characteristics. Mount the battery below the lower deck for more stable 

flights or move the battery to the upper deck to increase maneuverability. And to counter 

balance different camera payloads, you can shift the battery, ESCs and arms into optimal 

positions for proper CG.
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ADDITIONAL C4 VIBRATION ISOLATION DECK TO ELIMINATE JELLO EFFECTS ON 

VIDEOS

High frequency vibration on cameras is the principal cause of jello effects on videos. 

Implemented on a vast scale, Matrix's C4 vibration isolation deck offers a comprehensive antivibration solution for gimbal, camera and flight controller. In contrast to skimpy isolation plates, 

rubber bands or balls, Matrix's C4 vibration roadblock encompasses the entire surface and 

mass of the upper decks including the weight of a top mounted battery to neutralize vibrations. 

By including an extra layer of vibration dampening for the flight controller, Matrix is also 

preserving a common practice amongst professional pilots. A flight controller's sensitive gyro 

system can often misinterpretate vibrations as part of an aircraft movement, leading to 

adjustments and counter adjustments that generates more vibrations. By addressing the cause 

and effect of vibrations, the Matrix platform offers the epitome of production quality videos 

without the risk and disappointment of software stabilization.

FOLDS AND FITS NEATLY INTO A CARRY-ON SIZED ALUMINUM CASE

No more awkward quadcopter with protruding arms and propellers to lug around. Unlike typical 

folding mechanisms, the Matrix's arms and landing skids are designed to lock into folded or 

operating positions so you don't have to sacrifice structural integrity for portability. 

Implementations of slotted tracks enable fast and secured transitions without the risk losing any 

hardware. For a day out in the park or a hiking trip, you can retract the arms and skids to reduce 

the footprint. And for traveling, foldable antenna enable the Matrix and the transmitter to slip 

comfortably into a professional aluminum case without dismounting the propellers and gimbal. 

Upon arrival at the flight location the operator can adjust the landing skid height to 

accommodate rougher terrain. An optional aluminum case even includes cutouts for transmitter, 

batteries, spare parts & tools. Who knows, you might have a trip planned for Europe and the 

very versatile Matrix can make a great companion as a carry-on. 

DYNAMICALLY BALANCED MOTORS & OVER-SPECCED ESCS 

For exceptionally smooth flights, Matrix super muscular 42mm brushless motors are dynamical 

balanced. Since brushless motors are hand wound, the mass center is usually not in alignment 

with the mechanical center. Using advanced electronic balancing instruments, our factory spins 

up each motor then make proper adjustment to bring the mass center into alignment. Then to 

control and power the motors, Matrix 40A ESCs feature advanced multi-rotor algorithms which 

offers better performance and reliability than generic helicopter algorithms. Over-specced to 

sustain unrestrained amperage in higher torque for acceleration, extreme maneuvers and bigger 

payloads, Matrix is engineered to operating below capacity, so mechanical and electronic 

components stay relatively cooler even with consecutive flights. 

STIFFER & THICKER DOUBLE-POINT MOUNTED 15" CARBON PROPELLERS

No propellers are created equal. 15" Matrix robust carbon fiber propellers are sculpted with 

extra thick mid-section to resists flex then tapers to efficient blades to cut through the air with 

minimal resistance. Traditional circular mounts are accidents waiting to happen because the 

force of rotating propellers will eventually unscrew the crown nuts during flight. Integrated 
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double point mounts on Matrix motors and propellers eliminate this possibility and at the same 

time improve tracking precision because the propellers are forced to sit flat against the top of 

the motors. Another benefit of a flat mount is that there are no vulnerable protruding motor 

shafts. Slight deviations in traditional circular mounting holes or protruding motor shafts are 

extremely difficult to detect which magnify pitch and tracking variances, a major cause of 

vibrations and unstable flights. Since end-users are often required to purchase and mount 

propellers, Matrix's new hassle free mounting configuration is implemented to prevent vibration 

issues from surfacing. 

SELECTABLE MANUAL, ATTITUDE & GPS FLIGHT MODES

A 3-positioned switch is setup on Matrix' transmitter for pilot to select between 3 different flight 

modes. (1) With Manual Flight Mode, the absence of Gyro assisted flight makes it very difficult 

for the Pilot to stabilize and maneuver the quadcopter. (2) For 3-axis gyro auto-stabilized flight, 

the Attitude Flight Mode will automatically keep the Matrix in a leveled and sustainable flight 

thus enabling the pilot to focus on maneuvering the quadcopter. (3) Finally, the GPS Flight 

Mode is the most often used mode because it combines the benefit of 3-axis gyro autostabilized flight with 4 advanced GPS based functions described below.

GPS-LOCK & RETURN-TO-HOME

Under GPS Flight Mode, (1) one of the most utilized GPS based functions is the GPS-Lock 

function. Simply release the cyclic stick and allow it to spring to the middle of the control and the 

Matrix will be locked into a fixed GPS location (longitude-lock and latitude-lock) with a tolerance 

of 3 to 5 feet radius. Another similar function from the Matrix flight controller, the BarometricLock can be activated by moving the throttle stick to the middle of the control and the Matrix will 

be locked into a fixed elevation (altitude-lock). A hands-free hover modes is established when 

the pilot activates both the GPS-Lock and the Barometric-Lock simultaneously and the flight 

controller takes over. Either lock may also be used independently to hover in a fixed GPS 

coordinate with pilot controlled elevation or the longitude/latitude. By relinquishing controls to 

these auto-hover modes, the pilot can better focus on monitoring the video and controlling the 

camera. (2) Another popular GPS function is the Return-to-Home feature, a preprogrammed 

failsafe function that's automatically triggered by lose of remote control signals. Upon activation, 

the quadcopter will hover in place for a couple of seconds before elevating to a preprogrammed 

height and return to the home position for an automated landing sequence. 

GPS BASED COURSE-LOCK & HOME-LOCK

Under GPS Flight Mode, there is dedicated 3-positioned carefree mode switch set up to access 

(3) Course-Lock, a compass based carefree mode that remembers the initial take-off direction 

of the flight which is used to consistently orient the quadcopter. Under Course-Lock, the 

transmitter radio must remain in the initial take-off direction until it's reset or until the quadcopter 

lands. For example, with the transmitter pointed in the eastward direction, a quadcopter takes 

off in eastward heading orientation then turns towards a northward heading. Without CourseLock, a transmitter cyclic (directional) stick moved up towards the east will cause the 

quadcopter to head northward. Under Course-Lock, a cyclic stick moved up towards the east 

will cause the quadcopter to head eastward which is consistent with the initial take-off direction. 
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In fact, by keeping the transmitter pointed in the initial eastward take-off direction, the cyclic 

stick direction will always correspond to the direction of the quadcopter no matter how the 

heading has changed. At any time the pilot may reset the initial direction by flipping the Carefree 

Mode Switch in and out of Course-Lock. (4) Lastly, there is another similar carefree mode with a 

twist. Home-Lock, a home coordinate based carefree mode is very similar to Course-Lock. The 

difference is that Home-Lock uses the home location as the consistent tail-in orientation for the 

entire flight. While this allows the pilot to constantly turn and follow the quadcopter, the pilot 

should not move away from the home location. And because GPS has a tolerance of 3-5 feet, 

Home-Lock is less precise than Course-Lock. However, as the quadcopter gains more distance 

from the home position the precision improves dramatically. This is why Home-Lock will not and 

cannot be activated within a 30-feet circle from the home position. To use Home-Lock, the pilot 

usually maintains a tail-in orientation until the quadcopter is well beyond the 30-feet circle before 

assuming that Home-Lock has activated. At this point the pilot can constantly turn and point the 

transmitter at the quadcopter and the cyclic stick will always correspond directly to the 

quadcopter's direction. To bring the quadcopter back, the pilot simply pulls the cyclic towards 

himself - basically a manual controlled return-to-home function. Special caution is required when 

the quadcopter approaches the 30-feet circle because Home-Lock will automatically switch to 

Course-Lock. If the quadcopter enters the 30-feet circle from the initial take-off direction so that 

Home-Lock is equal to Course-Lock the pilot can assume that the quadcopter is under CourseLock until the quadcopter lands. In summary, an experienced pilot uses the "Normal" flight 

mode because no help is required from GPS. Both Course-Lock & Home-Lock carefree flight 

modes enable the operator to pilot the quadcopter without keeping track of the quadcopter's tail 

position. This is especially useful if a less experienced pilot is rotating the quadcopter to pan the 

video. There is much less confusion for beginner pilots to stick with either "Normal" mode or use 

GPS assisted Course-Lock. Home-Lock is usually reserved for longer distance within-the-lineof-sight flight because it's a bit confusing to operate when it approaches the home position.

ULTRA DURABLE & MAINTENANCE FRIENDLY

All Matrix material and components are selected and built for reliability and durability. Premium 

carbon fiber is utilized in the main frame for its rigidity and light-weight properties. Wear 

resistant CNC aluminum is utilized in screw-mounted joints, brackets and posts. Tough 

Japanese bearings are implemented to guard against higher temperatures. Then for continued 

maintenance, Matrix is based on a modularized design with strategically placed high tensile 

strength connectors so it's extremely easy and cost effective to maintain and operate. With 

minimal disassembly, components can be independently removed and replaced to diagnose 

and repair problems. As with all Turbo Ace production models, well stocked Matrix parts and 

upgrades are manufactured in larger volumes and savings are passed on to end-users. 

Operators are encouraged to keep some backup parts such as spare propellers, screws and 

batteries for replacement. Complimentary Turbo Ace videos are available online to assist

operators in maintaining and upgrading the Matrix. 

EXPANDABILITY WITH OPEN ARCHITECTURE & UPDATABLE ONLINE FIRMWARE

Catering to research professionals and avid hobbyists, the Matrix welcomes a full spectrum of 

specialized modifications. An open architecture supports unparalleled flexibility for arm and 
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frame extensions, variable motor mount options and ample space for peripheral integration. To 

get a head start on more advanced integrations, you can get an upgrade from the DJI Naza-M 

Lite to either the Naza-M V2 or WooKong flight controllers that are all supported with continued 

online updatable firmware. Multiple adjustable mounting positions are pre-drilled to 

accommodate third party gimbal integration. 

FLIGHT CONTROLLER OPTIONS & SPECIFICATION

DJI NAZA-M LITE MULTI-ROTOR STABILIZATION CONTROLLER

Support Multi-Rotor: Quad-Rotor I4, X4/ Hex-Rotor I6, X6, IY6, Y6

Supported ESC Output: 400Hz Refresh Frequency

Recommended Transmitter: PCM or 2.4GHz with minimum 4 channels

Working Voltage Range: MC: 4.8V~5.5V

Power Consumption: MAX 1.5W (0.3A@5V), Normal: 0.6W (0.12A@5V)

Operating Temperature: -10 ~ 50 degree Celsius

Assistant Software System Requirement: Windows XP sp3 / Windows 7 / Windows 8

Maximum Yaw Angular Velocity: 200 Degree/Sec

Maximum Tilt Angle: 45 Degree

Ascent / Descent: +-6m/Sec

MC: 25g

GPS/Compass: 21.3g

VU: 20g

Dimensions: MC: 45.5mm x 31.5mm x 18.5mm, GPS/Compass 46mm (diameter) x 9mm, VU 

32.2mm x 21.1mm x 7.7mm

Built-in Functions: Three Modes Auto-pilot, Enhanced Failsafe, Low Voltage Protection, S-Bus 

Receiver Support, PPM Receiver Support, 2-Axis Gimbal Support

DJI NAZA-M V2 MULTI-ROTOR STABILIZATION CONTROLLER

Support Multi-Rotor: Quad-Rotor I4, X4/ Hex-Rotor I6, X6, IY6, Y6/

Octo-rotor I8,V8,X8

Supported ESC Output: 400Hz Refresh Frequency

Recommended Transmitter: PCM or 2.4GHz with minimum 4 channels

Working Voltage Range: MC: 4.8V~5.5V

Working Voltage Range: PMU input: 7.4V to 26.0V (recommend 2S to 6S Lipo)

Power Consumption: MAX 3.15W (0.25A@12.6V), Normal: 1.638W (0.13A@12.6V)

Operating Temperature: -10 ~ 50 degree Celsius

Assistant Software System Requirement: Windows XP sp3 / Windows 7 / Windows 8

Maximum Yaw Angular Velocity: 200/s

Maximum Tilt Angle: 45

Ascent / Descent: +-6m/s

MC: 27g

GPS/Compass: 27g

PMU: 28g
89

LED: 13g

Dimensions: MC: 45.5mm x 32.5mm x 18.5mm, GPS/Compass 46mm (diameter) x 10mm, PMU 

39.5mm x 27.5mm x 10.0mm, LED 25mm x 25mm x 7.0mm

Built-in Functions: Three Modes Auto-pilot, Enhanced Failsafe, Low Voltage Protection, S-Bus 

Receiver Support, PPM Receiver Support, 2-Axis Gimbal Support

DJI A2 MULTI-ROTOR STABILIZATION CONTROLLER

Based on the technology and design philosophy of DJI’s Ace series of high-performance 

controllers, the A2 offers you a brand new flight experience. The A2 adopts a full metal case 

design and utilizes high quality components precisely calibrated with temperature compensation 

in all gyros and sensors, industry renowned flight algorithm in flight control and UAV field.

Peripherals

* Supported Multi-Rotor: Quad-Rotor: +4,x4; Hex-Rotor +6,x6,Y6,Rev Y6; Octo-Rotor +8,x8,V8

* Supported ESC Output: 400Hz refresh frequency

* Supported Transmitter for Built-in Receiver: Futaba FASST Series and DJI DESST Series

* Supported External Receiver: Futaba S-Bus, S-Bus2, DSM2

* Recommended Battery: 2S ~ 6S LiPo

* Operating Temperature: -5°C to +60°C

* Assistant Software System Requirement: Windows XP SP3 / 7 /8 (32 or 64 bit)

* Other DJI Products Supported: Z15,H3-2D,iOSD,2.4G Data Link,S800 EVO

Flight Performance

* Hovering Accuracy (In GPS Mode): Vertical: ± 0.5m; Horizontal: ± 1.5m

* Max Yaw Angular Velocity: 150 deg/s

* Max Tilt Angle: 35°

Electrical & Mechanical

* Power Consumption: MAX 5W (Typical Value: 0.3A@12.5V

* Built-In Functions: Built-in Receiver; Multiple Control Modes; 2-axis Gimbal Supported; Low 

Voltage Protection; PC & Bluetooth Ground Station

* Built-In Functions: External Receiver Supported; Intelligent Orientation Control; Sound Alarm; 

4 Configurable Output

* Total Weight: Total Weight: <= 224g(overall)

* Flight Controller Dimensions: 54mm x 39mm x 14.9mm

* IMU Dimensions: 41.3mm x 30.5mm x 26.3mm

* GPS-Compass Pro Dimensions: 62mm (diameter) x 14.3mm

* LED-BTU-I Dimensions: 30mm x 30mm x 7.9mm

* PMU Dimensions: 39.5mm x 27.6mm x 9.8mm

CAMERAS
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Aerial camera mounted under quadcopter serves two main purposes. (1) First and foremost, 

cameras are used for the purpose of recording videos or taking still photographs. Preferably, a 

DSLR camera is mounted on an auto-stabilized gyro based gimbal (camera mount) to stabilize 

the camera's horizon. (2) For more experienced pilots, a camera can be used for the purpose of 

piloting the quadcopter from the point of view of the camera aka FPV (first-person-view) piloting. 

If the camera is either mounted directly on the quadcopter without stabilization so the pilot can 

experience the tilt (pitch) & roll of the hexacopter. If the camera is auto-stabilized, OSD (onscreen-display) may be required to overlay artificial horizon and flight status on live feed video.

600TVL Camera

Super Compact at 1"x1"x1" Approximate Dimension

Extremely Light

Convenient 2-way Tape Mounting facilitates an easy way to change PFV location.

For FPV Piloting: 600TVL camera is hard mounted on the hexacopter's frame so pilot can see 

the video's tilt & roll action of the hexacopter.

For Framing Videos: 600TVL camera is mounted on the bottom of the brushless gimbal which is 

aligned with the Hero 3 on the gimbal.

GoPro Hero3

Adjustable Ultra Wide Angle Lenses

2X Faster Image Processor

2X Low Light Performance

12MP Image Sensor for high definition photos

HD Video from 1080p at 60 fps to 4K at 15 fps

Wi-Fi enables all camera function to be remotely controlled at up to 500 feet.

VIBRATION ISOLATION MOUNT & AUTO-STABILIZED CAMERA MOUNTS ON MATRIX

Employing vibration isolation mount for camera can significantly dampen high frequency 

vibrations to prevent rolling shutter & jello effects on videos. And for more professional 

applications, we can optionally add gyro based camera mounts to automatically stabilize 

cameras to accommodate quadcopter's tilt & roll movements to maintain a leveled video 

horizon. To control the camera's aim, a dial switch on the transmitter radio enables the pilot to 

tilt the camera up or down. With the freedom to maneuver and turn the quadcopter from 

different perspectives, heights and angles, one can achieve an endless variety of high quality 

shots and videos.

H3 Vibration Isolation Mount

Vibrations Dampening (for GoPro Hero2/3 & other small cameras)

GoPro Tripod Mount & Tripod Screw

Super Light Weight Configuration Enables Dual Battery Setup for Extended Flight Time 

Gyrox-3 Brushless 2-Axis Gimbal
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Super Fast Auto-Stabilized Roll-Axis

Super Fast Pilot Controlled & Auto-Stabilized Tilt-Axis

Expanded Tilt-Axis Angle Enables the Camera to Point Straight Down

Optimized Stabilization & Mounting for GoPro Hero3 Camera Only

Gyrox-5R Brushless 2-Axis Gimbal

Super Fast Auto-Stabilized Roll-Axis

Super Fast Pilot Controlled & Auto-Stabilized Tilt-Axis

Expanded Tilt-Axis Angle Enables the Camera to Point Straight Down

Optimized Stabilization & Mounting for Sony NEX-5R/5N/6/7 Cameras

FPV Live Feed Video

Live feed video enables the pilot or cameraman to see real time videos from the camera's point 

of view which is synonymous to FPV (first-person-view). In contrast to slower and shorter 

distanced WiFi video streaming on cameras, aerial FPV requires much longer distance 

transmission without visible delay. A video transmitter is usually attached to a camera's videoout port transmits the video signals. A matching video receiver located next to the pilot or 

cameraman receives the video signal that is then plugged into a monitor's video-in port for 

displaying the video. There are 2 main purposes for aerial FPV. (1) To enable pilot/cameraman 

to see and frame videos or still shots by adjusting the gimbal and/or the quadcopters location 

and orientation. (2) To enable pilot to see and fly from the point of view of the camera (view from 

the cockpit). If a camera is hard mounted without auto-stabilization, the video will reflect the tilt 

(pitch) and roll of the quadcopter. If a camera is auto-stabilized on a gimbal, an OSD (onscreen-display) may be implemented to overlay artificial horizon and flight data on the autostabilized video that does not reflect the tilt and roll of hexacopter.

FPV From 600TVL Camera

Lighter TVL camera is easy to set up and promotes longer flight time. 

Composite video output & standardized plug enable simple connection to video transmitter. 

Hard mounted on the Hexacopter, TVL camera can be used for FPV piloting & surveillance.

Mounted on under or above the gimbal, TVL camera can be aligned with DSLR camera for 

framing your videos and stills.

FPV From Hero3 or HD Camera

You can see exactly what the Hero3 or HD camera is capturing for framing your video and stills.

Special cable connector is provided for video transmitter to plug into the Hero3 or HD camera's 

video out port

Examples of cameras supported: Hero3 & Sony NEX 5N/6N/7N

STANDARD & LONG DISTANCE TRANSMITTERS FOR MATRIX

Due to safety and equipment concerns, transmitter reliability is crucial in professional 

quadcopter operations. Without an established standard of verification, it's common place for 

transmitter brands to overstate operating distance by discounting the importance of reliability. A 
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typical transmitter spec for 2,000 feet range may only be reliable 80% of the time and you can 

easily lost your equipment in several flights at 300 feet. Only extensive field testing over several 

months - not biased reviews based on several test flights - are true indicators of consistently 

reliable operating range.

Walkera F7 Transmitter

2.4GHz Transmitter with 7 Channels

RX701 Receiver with 7 Channels

Telemetry Installed for Updated Flight Battery Status to Trigger Low Battery Alarm

Standard Distance of 300-500 Feet

Build-in 3.5" Color LCD Screen for FPV Live Video Display

Compatible only with DV04 Camera 

Walkera Devo 10 Transmitter

2.4GHz Transmitter with 10 Channels

RX1002 Receiver with 10 Channels

Telemetry Installed for Updated Flight Battery Status to Trigger Low Battery Alarm

Standard Distance of 300-500 Feet

A Practical and Cost Effective Solution 

Spektrum DX8 Long Distance Transmitter

2.4GHz DSMX Transmitter with 8 Channels

AR8000 Receiver Package with 8 Channels

Main Receiver & Satellite Receiver Strategically Placed for Signal Path Diversity

TM1000 Telemetry Installed for Updated Flight Battery Status to Trigger Low Battery Alarm

Reliable Standard & Long Distance of 1 to 1.2 Mile

2013’s #1 Selling & User Friendly Transmitter

Spektrum DX9 Long Distance Transmitter

2.4GHz DSMX Transmitter with 9 Channels

AR9020 Receiver Package with 9 Channels

Main Receiver & 2x Satellite Receivers Strategically Placed for Signal Path Diversity

TM1000 Telemetry Installed for Updated Flight Battery Status to Trigger Low Battery Alarm

Reliable Standard & Long Distance of 1 to 1.2 Mile

Upgraded Robust Antenna

2014’s #1 Selling & User Friendly Transmitter
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Futaba 14SG Long Distance Transmitter

2.4GHz FASSTEST Transmitter with 14 Channels

R7800SB Bi-Directional Receiver with 8 Channels (Optional: R6106HFC Receiver for 6 

additional channels)

S.Bus2 Bi-Directional Protocol for Additional Servos, Telemetry & Other Auxiliary Functions

Telemetry Voltage Sensor Installed for Updated Flight Battery Status to Trigger Low Battery 

Alarm

Ultra Reliable Standard & Long Distance of 1 to 1.2 Mile (Upgradable to EZUHF for up to 25 

miles)

Overwhelmingly Recommended by Professional RC Pilot Groups

TRANSMITTER & RECEIVER OPERATING REQUIREMENTS

Standard remote control transmitters and receivers utilized with the Matrix quadcopter operate 

under FCC Part 15 (S29DEVO-10, BRWDAMTX11, AZPT14SG-24G, S29TX5803) in either 

legal 2.4GHz and/or 5.8GHz frequencies. In general, advanced quadcopters require a minimum 

of 7 channels under the 2.4GHz frequency range: 4 channels for piloting controls, 2 channels for 

the GPS and 1 channel for controlling the tilt-axis of the gimbal. Extended distance transmitters 

usually employ several methods to promote signal strength and reliability. (1) Frequencyhopping spread spectrum (FHSS) is a method of transmitting radio signals by rapidly switching 

between several frequencies to seek the least amount of traffic. (2) Dual paths diversity enable 

the signals to reach two receivers or antennas mounted in different locations on the quadcopter 

so the system can utilize the strongest signal path. Bi-directional communications between 

transmitter and receiver can also utilize feedback signal strength to traget the best frequencies 

in real time (3) In case of signal disruptions, algorithm for ultra fast signal recovery enables the

transmitter and receiver to quickly rebind for uninterrupted operations. Products using permitted 

frequencies without certification will require an amateur radio (ham) license. It is the operator's 

responsibilities to ensure the use of such products meet their individual countries' federal and 

local government's rules or regulations for RF devices. If you are unsure of your government's 

requirement or unable to comply with them, please do not purchase this product. Please do not 

alter the purchased product in violation of said rules and regulations because Wow Hobbies 

cannot be held liable for operator's misuse or modification of a legal product.

INTEGRATION, SET UP, FLIGHT TEST & SHIPPING

There is a myriad of Matrix options to satisfying specific applications. After installation, setup 

and inspection, our technicians will complete final adjustments plus a series of test flights. If 

your orders is placed for pick-up, we will redo a live flight-test when you arrive at our showroom. 

If your order is to be shipped, a test flight video for your specific Matrix order will be recorded, 

saved and shipped with the instructions in a flash drive. Our Matrix packages are designed to 
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retain all assembled components as a fully integrated system during shipping. To prevent 

damage, the Matrix quadcopter is suspended in the middle of a large corrugated shipping box.