Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 1 of 10 

January 9, 2015

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 of the Federal Aviation Regulations from 14

C.F.R. 45.23(b); 14 C.F.R. Part 21; 14 C.F.R. 61.113(a)&(b); 91.7(a); 91.9(b) (2); 91.103(b); 91.109;

119.121; 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,

 I, Bruce Pogosaew, am writing pursuant to the FAA Modernization and Reform Act of

2012 and the procedures contained within 14 C.F.R. 11, to request that I, Bruce 

Pogosaew,

an owner and operator of small unmanned aircraft, be exempted from the Federal 

Aviation Regulations (“FARs”) listed below so that I, Bruce Pogosaew, may operate my 

small ultra lightweight unmanned aircraft system (“UAS”) in commercially regulated 

airspace by the Federal Aviation Administration (“FAA”).

As described herein I, Bruce Pogosaew, have experience in flying hobby helicopters 

and planes for recreational purposes for the past eighteen (18) years. I have flown small 

and large remote control (RC) gas and electric aircraft models for those eighteen (18) 

years without incident and pledge my continued commitment to safety on all future 

flights.

Following exemption and approval by the FAA, I, Bruce Pogosaew, will primarily use my 

hobby grade quad-copter1 and fixed wing2 UAS equipped with cameras for the 

following applications: aerial videography/cinematography to enhance academic 

community awareness for individuals and companies unfamiliar with the geographical 

layout of the metro Tucson and surrounding areas; augmentation of real estate listing 

videos; and the creation of visual and topography layout videos for Search and Rescue 

(SAR) missions for state and local agency’s, education, agricultural inspections and 

building and construction zone inspections.

1

 Appendix A - Bixler 2 Operator Manual 2 Appendix B - Quad-Copter Operator Manual
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 2 of 10

My, Bruce Pogosaew’s, exemption request would permit the operation of ultra 

lightweight, unmanned (i.e. piloted by remote control) UAS’s for the development of 

community and government use videos, permissible within property boundaries for 

individual homeowners and within in tightly controlled, limited airspaces predetermined 

in areas away from the general public, airports, heliports and vehicular traffic. Currently, 

similar lightweight, remote controlled UAS's are legally operated by unmonitored 

amateur hobbyists with no safety plan or controls in place to prevent catastrophe. With 

that in mind, I, Bruce Pogoaew, have personally installed safety protocols and controls6

to avoid and prevent public hazard, as well as any catastrophic manned aircraft 

hazard. Furthermore, it is my intent to assist future FAA safety protocols and 

regulations exclusive to lightweight UAS's for specific video and photography usage by 

sharing information with the FAA as I, Bruce Pogosaew, record flight data and other 

pertinent information gained through permitted flight operations.

In addition, granting my, Bruce Pogosaew’s, exemption request will comply with the 

Secretary of Transportation’s (FAA Administrator’s) instructions to not only integrate 

UAS's into the national airspace system, but to “...establish requirements for the safe 

operation of such aircraft systems [UAS's] in the national airspace system” under 

Section 333(c) of the Reform Act specific to the use of UAS's for real estate/Realtor 

purposes, educational videos, Search and Rescue, land/trusts inspections, and 

structure inspections, to aid state and local agency’s. Further I, Bruce Pogosaew, will 

conduct my operations in compliance with the protocols described herein or as 

otherwise established by the FAA.

For the reasons stated below, I, Bruce Pogosaew, respectfully request the grant of an

exemption allowing me to operate ultra lightweight, remote controlled UAS’s to aid

academic community awareness, to benefit/stimulate attraction to the metro Tucson

area and to enhance personal and public video feeds. A grant that will ultimately allow 

UAS’s to play a more positive role in our local community by increasing employment 

opportunities, heightening security measures and decreasing government expenditures 

by reducing the need for heavier manned aircraft, containing costly, combustible fuel- a 

potential public hazard in and of itself.

6 Appendix F - Personal Protocols and Controls 
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 3 of 10 

I. Contact Information:

Bruce Pogosaew

FPV CATALOG, LLC 

7432 E Placita Del Espiritu

Tucson, AZ 85715

Office: (520) 495-4674

Mobile: (520) 271-9630

Email: service@FPVCATALOG.com

II. The Specific Sections of Title 14 of the Code of Federal Regulations From

Which Bruce Pogosaew Requests Exemption are:

14 CFR 21;

14 C.F.R. 45.23(b);

14 CFR 61.113 (a) & (b);

14 C.F.R. 91, et seq.;

14 CFR 407 (a) (1);

14 CFR 409 (a) (2); and,

14 CFR 417 (a) & (b). 

III. The Extent of relief Bruce Pogosaew Seeks and the Reason He Seeks Such

Relief:

I, Bruce Pogosaew, submit this application in accordance with the Reform Act, 112 P.L.

95 §§ 331-334, seeking relief from any currently applicable FARs operating to prevent

me, Bruce Pogosaew, contemplated commercial cinematic, academic and other flight

operations within the national airspace system. The Reform Act in Section 332 provides

for such integration of civil unmanned aircraft systems into our national airspace system

as it is in the public’s interest to do so. My, Bruce Pogosaew’s, ultra lightweight UAS

meets the definition of “small unmanned aircraft” as defined in Section 331 and

therefore the integration of my ultra light weight UAS is expressly contemplated by the

Reform Act. I would like to operate my ultra lightweight UAS prior to the time period by

which the Reform Act requires the FAA to promulgate rules governing such craft.

Thereby, providing direct experience and valuable information for formal regulation that

can be administered uniformly to all related UAS aerial video and

photography. The Reform Act guides the Secretary in determining the types of UAS's

that may operate safely in our national airspace system. Considerations include: The

weight, size, speed and overall capabilities of the UAS's; Whether the UAS will be

operated near airports or heavily populated areas; and, Whether the UAS will be

operated by line of sight. 112 P.L. 95 § 333 (a). 
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 4 of 10 

Each of these items reflect in favor of an exemption for me, Bruce Pogosaew.

My UAS’s utilize four (4) or less rotating propellers

for balance, control and stability.

My UAS’s are equipped with the following via video and data telemetry :

 1)Altimeter

 2) Attitude indicator

 3) Ground Speed indicator

 4) Magnetic compass

 5) Heading indicator

 6) Vertical speed indicator

 7) Course deviation indicator

 8) Radio magnetic indicator

 9) GPS location

 10) Fuel consumption and Fuel Left with approximate time.

 11) Loiter and circle mode.

 12) Auto safety or RTL ( Return To Launch)

 13) Auto landing technology.

Each UAS weighing less than seven (7) pounds (far below the maximum 55 pound 

limit);

Including camera(s) with or without gimbal (a camera stabilizer).

I, Bruce Pogosaew, considers safety as foremost with each flight. My small unmanned

aircraft is designed to hover in place, circle in a specific place or loiter( figure 8 flight) via 

GPS and can be operated in winds up to 17.379 knots (20mph) wind. For safety, 

stability and fear of financial loss I will not fly in winds exceeding 13 knots (15 mph). 

Built in safety systems include a GPS mode that allows my UAS to hover/circle in place 

or land when radio controls are released.

With six (6) modes to choose from, I will fly with the modes safest to complete the 

videos

for aerial videography/photography and have the ability to choose the safest, most

reliable and stable mode to prevent accident and hazard. When pilot communication is

lost, UAS is designed slowly descend to point of takeoff and or to land at point of 

launch.

With an onboard flight controller - APM2.5, it has the capabilities of geofencing4 which 

will prevent the craft from exceeding a set altitude or distance. No matter 

what causes the craft to breach those boundaries - the craft is forced back within the 

boundary limits via the on board controller and will take over the craft to keep it within 

those set boundary lines and allow the pilot to regain control once the craft is within 

those boundaries.

 I, Bruce Pogosaew, will not operate my UAS near airports, hospitals nor police 

heliports, and do not operate near areas where general public is within fifty to one 

hundred (50-100) yards depending on location, conditions and weather. I am constantly 

on alert for any manned aircraft (police/medical helicopters, etc.) and prepared to 

land/abort immediately to the nearest and safest ground point should a manned aircraft 

approach my location or I suspect manned aircraft may

4

 Appendix D - Computerized Control Boards
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 5 of 10 

approach near my location. My UAS’s are capable of vertical and horizontal operations, and is 

flown only within my line of sight, as the remote control pilot. Utilizing battery power rather than 

combustible

I, Bruce Pogosaew, will not operate my UAS near airports, hospitals nor police heliports, and do 

not operate near areas where general public is within fifty to one hundred (50-100) yards 

depending on location, conditions and weather. I am constantly on alert for any manned aircraft 

(police/medical helicopters, etc.) and prepared to land/abort immediately to the nearest and 

safest ground point should a manned aircraft approach my location or I suspect manned aircraft 

may approach near my location. My UAS’s are capable of vertical and horizontal operations, 

and is flown only within my line of sight, as the remote control pilot. Utilizing battery power rather 

than combustible fuels, flights generally last between three (3) to fifteen (15) minutes, with an 

altitude under one hundred fifty (150) feet. Six (6 )Smart Mode includes safe circle for operation, 

position hold, self-leveling, altitude command, GPS, return home feature, and safety control to 

return home or land in the event of communication interruption between RC transmitter and 

UAS.See Appendix A, and C -Operator Manual. 

 I, Bruce Pogosaew, utilize a fresh fully charged battery with each flight as a safety 

precaution; full flight time limit for each battery is eight (8) to twelve (30) minutes as tested. I do 

not operate my UAS at or below manufacture recommend minimum charge levels for

operation; preferring to remain well within a safe operating range to insure adequate

communication between radio control and UAS to eliminate potential for crash, loss of

control or hazard. Reserve batteries are at hand with each exercise to insure

replacement for sufficient safe level of operation. I do not believe in taking risk that may

cause a crash, that could create hazard to the public/property/manned aircraft, and

have no desire to lose an investment. I have clocked numerous practice flights in

remote areas as a hobbyist simulating flights for future commercial use to gain

familiarization with the characteristics of this specific UAS's performance under different

temperature and weather conditions. I also practice computerized simulated flights to

maintain adequate skills and response reflex time. All for the sake of safety. I, Bruce Pogosaew, 

am extremely cautious when operating of my UAS/ultra light weight unmanned aircraft and will 

not “create a hazard to users of the national airspace system or the public.” 112 P.L. 95 § 333 

(b). Given the small size and weight of my UAS it falls well within Congress’s contemplated 

safety zone when it promulgated the Reform Act and the corresponding directive to integrate 

UAS's into the national airspace system. Bruce Pogosaew’s UAS, used in hobby flight, has a 

demonstrable safety record and does not pose any threat to the general public or national 

security.

IV. How Bruce Pogosaew’s Request Will Benefit the Public As A Whole:

Aerial videography for geographical awareness, education, search and rescue, land 

management, structure inspections and for real estate marketing has been around for a long 

time through manned fixed wing aircraft and helicopters. For small budget companies, average 

homeowners and property owners the expense of such aerial videography is cost prohibitive. 

Only large companies and high end Realtors or luxury homeowners can afford to absorb such 

expense. Depriving non-luxury owners and lower budget companies from a valuable marketing 

tool. Manned aircraft pose a threat to the public through potential catastrophic crash that the 

Tucson community has experienced in the past with military aircraft and medical helicopter 

crashes within the city of Tucson. Each resulting in loss of life.

1 Appendix A - Bixler 2 Operator Manual 2 Appendix B - Quad-Copter Operator Manual 3 Appendix C - Transmitter Controller Manual
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 

6 of 10

Each with combustible fuel that exploded and burned on impact. Police helicopters have 

made emergency hard landings within city limits. My, Bruce Pogosaew's, UAS poses no 

such threat since size and lack of combustible fuel alleviates any potential threat to the 

public. Congress has already proclaimed that it is in the public’s interest to integrate 

commercially flown UAS's into the national airspace system, hence the passing of the 

Reform Act. Granting my, Bruce Pogosaew’s, exemption request furthers the public interest 

through academic/visual awareness of the geographical benefits in and around the metro 

Tucson area. My ultra light weight UAS is battery powered and creates no emissions that 

can harm the environment. The consequence of my ultra light weight UAS crashing is far 

less than a full size helicopter or fixed wing aircraft; which are heavy, contain combustible 

fuel and can cause catastrophic devastation to the public. The public’s interest is furthered 

by minimizing ecological and crash threat by permitting aerial video/photo capture through 

my battery operated ultra lightweight UAS's.

Permitting me, Bruce Pogosaew, to immediately fly within national air space furthers 

economic growth. Granting my exemption request substantially furthers the economic 

impact for the metro Tucson and surrounding community for companies looking to relocate 

or build around the Tucson metro area as well as individuals looking to relocate for career 

advancement through academic and geographical awareness. Both of which serve as a 

stimulus to the community.

V. Reasons Why Bruce Pogosaew’s Exemption Will Not Adversely Affect Safety

Or How The Exemption Will Provide a Level of Safety At Least Equal To Existing

Rule:

My, Bruce Pogosaew’s, exemption will not adversely affect safety. Quite the contrary,

for the reasons stated permitting me, Bruce Pogosaew, to log more flight time in FAA

controlled airspace, with communication with the FAA, will allow me to contribute to the

innovation and implementation of new and novel, as of yet undiscovered safety protocols for 

Realtors, land and structured owners. For development in cooperation with the FAA.

In addition I, Bruce Pogosaew, submit the following representations of enhancements to 

current aerial videography and photography:

My UAS’s weigh less than seven (7) pounds complete with a small ultra-light weight high

quality GoPro 3+ Black camera; Mobius camera or similar;

I only operate my UAS below 200 feet (well within the 400 foot permissible

ceiling set by the FAA Modernization and Reform Act of 2012);

My UAS only operate for 3-15 minutes per flight;

I land my UAS prior to manufacturer recommended minimum level of battery

power;

I pilot my UAS through remote control only by line of sight; and have live video feed for a 

secondary pilot to monitor video recording; 
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 7 of 10

My UAS’s have a GPS controlled main frame- a flight safety feature whereby it hovers 

or circles and then lands at the GPS takeoff point if communication with the remote 

control pilot is lost;

I actively record and analyze flight data through the APM main frame and other sources 

of information to constantly

update and enhance safety protocols;

I only operate in reasonably safe environment that are strictly controlled, are

away from power lines, elevated lights, airports and actively populated areas;

I conduct extensive preflight inspections and protocol, during which safety

carries primary importance;

I always obtain all necessary permissions prior to operation; and,

I have procedures in place to abort flights in the event of safety breaches or

potential danger.

My, Bruce Pogosaew’s, safety protocols provide a level of safety equal to or exceeding

existing rules. It is important to note that absent the integration of commercial UAS into

our national airspace system, helicopters are the primary means of aerial video and

photography for community awareness real estate, structured inspections, land 

management and search and rescue While the safety record of such helicopters is 

remarkably astounding, there has been local incident involving loss of life as well as 

extensive property damage; it is far safer to operate a battery powered ultra lightweight 

UAS. First, the potential loss of life is diminished because UAS's carry no people on 

board and I only operates my UAS in specific areas away from mass populations. 

Second, there is no fuel on board a UAS and thus the potential for fire or explosions is 

greatly diminished. Third, the small size and extreme maneuverability of my UAS allow 

me to remotely pilot away from and avoid hazards quickly and safely. Lastly, given its 

small size and weight, even when close enough to capture

amazing images, my UAS need not be so close to the objects they are focused on 

through the technology and use of post editing software allowing pan and zoom.

Accordingly, my UAS has been experimentally operated for familiarization/competency 

and will continue to operate at and above current safety levels.

VI. A Summary The FAA May Publish in the Federal Register:

A. 14 C.F.R. 21 and 14 C.F.R. 91: Airworthiness Certificates, Manuals and The Like.

14 C.F.R. 21, Subpart H, entitled Airworthiness Certificates, sets forth requirements for 

procurement of necessary airworthiness certificates in relation to FAR §91.203(a)(1). 

The size, weight and enclosed operational area of my, Bruce Pogosaew’s, UAS permits 

exemption from Part 21 because my UAS meets (and exceeds) an equivalent level of 

safety pursuant to Section 333 of the Reform Act.

The FAA is authorized to exempt aircraft from the airworthiness certificate requirement 

under both the Act (49 U.S.C. § 44701 (f)) and Section 333 of the Reform Act. Both 

pieces of legislation permit the FAA to exempt UAS's from the airworthiness certificate 

requirement in consideration of the weight, size, speed, maneuverability and proximity 

to areas such as airports and dense populations. My, Bruce Pogosaew’s, current and 

projected UAS's meet or exceed each of the elements.
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 8 of 10

14 C.F.R. 91.7(a) prohibits the operation of an aircraft without an airworthiness

certificate. As no such certificate will be applicable in the form contemplated by the

FARs, this Regulation is inapplicable. 

14 C.F.R. § 91.9 (b) (2) requires an aircraft flight manual in the aircraft. As there are

no on board pilots or passengers, and given the size of the UAS's, this Regulation is

inapplicable. An equivalent level of safety will be achieved by maintaining a

safety/flight manual delineating areas of where safety can be defined.

The FAA has previously issued exemptions to this regulation in Exemption Nos. 8607, 8737,

8738, 9299, 9299A, 9565, 9565B, 10167, 10167A, 10602, 10700 and 32827.

14 C.F.R. § 91.121 regarding altimeter settings is inapplicable insofar as my UAS utilizes

electronic global positioning systems with a barometric sensor or controled GPS “geofencing”

14 C.F.R. § 91.203 (a) and (b) provides for the carrying of civil aircraft certifications and

registrations. They are inapplicable for the same reasons described above. The equivalent

level of safety will be achieved by maintaining any such required certifications and

registrations by me, Bruce Pogosaew.

B. 14 C.F.R. § 45.23: Marking of The Aircraft.

Applicable Codes of Federal Regulation require aircraft to be marked according to

certain specifications. My UAS are, by definition, unmanned. They therefore do not

have a cabin, cockpit or pilot station on which to mark certain words or phrases. Further,

two-inch lettering is difficult to place on such small aircraft with dimensions smaller that

minimal lettering requirement. Regardless, I will mark its UASs in the largest possible

lettering by placing the word “EXPERIMENTAL” on its fuselage as required by 14 C.F.R.

§45.29 (f) so that I the pilot, or anyone assisting me as a spotter with the UAV will see

the markings. The FAA has previously issued exemptions to this regulation through

Exemptions Nos. 8738, 10167, 10167A and 10700.

C. 14 C.F.R. § 61.113: Private Pilot Privileges and Limitations: PIC.

Pursuant to 14 C.F.R. §§ 61.113 (a) & (b), private pilots are limited to non-commercial

operations. I, Bruce Pogosaew, can achieve an equivalent level of safety as achieved by

current Regulations because my UAS does not carry any pilots or passengers. Further,

while helpful, a pilot license will not ensure remote control piloting skills. The risks

attended to the operation of my UAS is far less than the risk levels inherent in the

commercial activities outlined in 14 C.F.R. § 61, et seq. Thus, allowing me, Douglas

Trudeau, to operate my UAS meet and exceed current safety levels in relation to 14

C.F.R. §61.113 (a) & (b). 

D. 14 C.F.R. 91.119: Minimum Safe Altitudes.

14 C.F.R. § 91.119 prescribes safe altitudes for the operation of civil aircraft. It allows

helicopters to be operated at lower altitudes in certain conditions. My UAS will never

operate at an altitude greater than 200 AGL; safely below the standard of 400 AGL. I,

Bruce Pogosaew, will however operate my UAS in safe areas away from public and

traffic, providing a level of safety at least equivalent to or below those in relation to

minimum safe altitudes. Given the size, weight, maneuverability and speed of my UAS,

an equivalent or higher level of safety will be achieved.
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 9 of 10

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

 10 Appendix E - Safety/Flight Manual 

The above-cited Regulations require, amongst other things, aircraft owners and operators to 

“have [the] 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. . . .”These Regulations only 

apply to aircraft with an airworthiness certificate. They will not, therefore, apply to my, Bruce 

Pogosaew's, UAS. However, as a safety precaution I inspect my UAS before and after each 

flight.

 A Summary The FAA May Publish in the Federal Register: A. 14 C.F.R. 21 and 14

C.F.R. 91: Airworthiness Certificates, Manuals and The Like. 14 C.F.R. 21, Subpart H,

entitled Airworthiness Certificates, sets forth requirements for procurement of necessary

airworthiness certificates in relation to FAR § 91.203(a)(1). The size, weight and

enclosed operational area of my UAS permits exemption from Part 21 because my,

Bruce Pogosaew’s, UAS meets an equivalent level of safety pursuant to Section 333 of

the Reform Act. The FAA is authorized to exempt aircraft from the airworthiness

certificate requirement under both the Act (49 U.S.C. § 44701 (f)) and Section 333 of

the Reform Act. Both pieces of legislation permit the FAA to exempt UAS's from the

airworthiness certificate requirement in consideration of the weight, size, speed,

maneuverability and proximity to areas such as airports and dense populations. My

UAS meets or exceeds each of the elements. 14 C.F.R. 91.7(a) prohibits the operation

of an aircraft without an airworthiness certificate. As no such certificate will be

applicable in the form contemplated by the FARs, this Regulation is inapplicable. 14

C.F.R. § 91.9 (b) (2) requires an aircraft flight manual in the aircraft. As there are no

pilots or passengers, and given the size of the UAS's, this Regulation is inapplicable. An

equivalent level of safety will be achieved by maintaining a manual. The FAA has

previously issued exemptions to this regulation in Exemption Nos. 8607, 8737, 8738,

9299, 9299A, 9565, 9565B, 10167, maintenance program that involves regular software

updates and curative measures for any damaged hardware. Therefore, an equivalent

level of safety will be achieved.

In summary, Bruce Pogosaew seeks an exemption from the following

Regulations:14 C.F.R. 21, subpart H; 14 C.F.R. 45.23(b); 14 C.F.R. §§ 61.113 (a) & (b); 14 

C.F.R. §91.7 (a); 14 C.F.R. § 91.9 (b)(2); 14 C.F.R. § 91.103(b); 14 C.F.R. § 91.109; 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. § 91.405 (a); 14 C.F.R. § 91.407 (a)(1); 14 C.F.R. § 91.409 (a)(2); 14 C.F.R. §

91.409 (a ) (2); and, 14 C.F.R. §§ 91.417 (a) & (b) 

to commercially operate my, Bruce Pogosaew's, small unmanned vehicle/lightweight 

unmanned aircraft vehicle in community awareness, education, structural inspection land 

management, search and rescue and real estate operations, and to develop economic 

platforms for the aforementioned to 
Bruce Pogosaew, Tucson AZ - Section 333 Exemption Petition page 10 of 10

enhance the experience of those seeking to relocate, rebuild, reevaluate and to find in the 

metro Tucson area.

Currently, the aforementioned aerial videography/photography relies primarily on the use of 

larger aircraft running on combustible fuel. Posing potential risk to the public. Granting my, 

Bruce Pogosaew’s, request for exemption will reduce current risk levels and thereby 

enhance safety. My UAS craft do not contain potentially explosive fuel, is smaller, lighter 

and more maneuverable than conventional video and photographic aircraft with much less 

flight time.

Further, I operate at lower altitudes and in controlled airspace eliminating potential public 

risk flying to and from established airfields. I, Bruce Pogosaew, have been informally 

analyzing and recording flight

information and will compile safety protocols and the implementation of a flight

operations manual for usage that exceeds currently accepted means and

methods for safe flight. Formal collection of information shared with the FAA will

enhance the FAA's internal efforts to establish protocols for complying with the FAA

Modernization and Reform Act of 2012. There are no personnel on board my, Bruce

Pogosaew’s, UAS and therefore the likelihood of death or serious bodily injury is

significantly diminished. My, Bruce Pogosaew’s, operation of my UAS, weighing less

than seven (7) pounds and travelling at lower speeds within limited areas will provide an

equivalent level of safety as that achieved under current FARs. Accordingly I, Bruce 

Pogosaew, respectfully request that the FAA grant my exemption request and am willing

to cooperate in sharing information to benefit the FAA, safety of manned aircraft, and

the general public at large.

Respectfully submitted,

Bruce Pogosaew

FPV Catalog, LLC

7432 E Placita Del Espiritu

Tucson, AZ 85715
Appendix A

Bixler 2 Operator Manual
INSTRUCTIONS

Thank you for purchasing a 3DR Plane!

CONTENTS 1 Fuselage

2 Right wing

3 Left wing

4 Horizontal stabilizer

5 Vertical stabilizer

6 Carbon fiber bar

6

3DR Plane 

1

2

3

4

5
1 Audio/video (AV) cable

2 AV receiver power cable

3 AV receiver antenna

4 AV receiver

5 AV transmitter battery (air)

6 AV receiver battery (ground)

7 Telemetry module (ground)

8 Telemetry antenna (ground)

 9 Propeller

10 Servo horn screws

11 Ailerons Y cable

12 Micro-USB cable

13 USB extension cable

14 Wing screws

15 Main battery

16 Adhesive Velcro squares

1 Telemetry (air)

2 Power module

3 AV transmitter 

4 Camera

5 GPS module

 6 Air speed sensor

 7 AV transmitter power connector

 8 On-screen display board

 9 APM

10 Input connectors

1 2

3

5

6

7 8

10 11

12

13

14

15

9

4

16

1

2

5

6

7

9

10

3

4

8
Bixler Assembly Manual

Please refer to the assembly manual included with your 

plane to install main wings, stabilizers, and other parts of 

the plane’s frame. Use the Y-cable to connect the aileron 

cables from the left and right wings.

WIRING APM OUTPUTS

Connect the servo and electronic speed controller (ESC) wires to APM’s 

outputs pins in the order indicated below. Connect the white wire to the 

S pin (top row), the red wire to the + pin (center row), and the black wire 

to the - pin (bottom row).

Elevator

Ailerons

Throttle

Rudder

Connect the wires from the APM inputs to 

the signal pins on your RC receiver. The 

wires are labeled with the channel they 

should connect to.

Connect the black wire to a ground pin on 

the receiver, and connect the red wire to a 

power (five volts) pin on the receiver.

CONNECT RC RECEIVER

APM inputs wires

Connect inputs wires to RC receiver

Servo cables are labelled by type.

Connect them to APM’s output 

pins as shown.
Your plane is now fully assembled. 

For software downloads and flying 

instructions, please visit 

plane.ardupilot.com. Happy flying!

POWER WIRING Connect the power module’s yellow 

XT60 connectors to the motor and 

main battery connectors. Connect 

the AV transmitter battery to the 

red connector on the transmitter.

AV transmitter battery

Main battery

Motor power 

connector

Power module and 

transmitter power connector

BALANCING THE PLANE

Your plane’s center of gravity should 

be 71 mm from the leading edge. 

Please balance the plane 

at this point before flying, 

and move the main battery 

as necessary to achieve the correct center of gravity,

MOUNT TELEMETRY AIR MODULE

Use the adhesive Velcro squares to mount 

the telemetry radio air module to the side 

of the fuselage where it has a clear view 

of the sky.
Mission Planner is free, open-source software providing multiplatform 

configuration and full-featured waypoint mission scripting for 

autonomous vehicles.

To install Mission Planner on your ground station computer (Windows 

only), visit ardupilot.com/downloads, select Mission Planner, and select 

sort by date (short link: goo.gl/Si5grC). Select the most recent (top) 

MissionPlanner - MSI (Microsoft installer package).

INSTALL SOFTWARE

After selecting the most recent MSI, read 

the safety information and select Download:

Download

Open the downloaded file to run the Mission Planner Setup Wizard. 

Select the option to proceed if prompted with a security warning.

Mission Planner 

Setup Wizard will 

automatically install 

the correct device 

drivers.

Device Driver Installation Wizard

Mission Planner Downloads Screen

Mission Planner (6) « Downloads

Sort by: Title | Hits | Date

■ MissionPlanner - ZIP - 1.2.62

■ MissionPlanner - MSI - 1.2.62

■ MissionPlanner - ZIP - 1.2.60

■ MissionPlanner - MSI - 1.2.60

■ MissionPlanner - ZIP - 1.2.61

■ MissionPlanner - MSI - 1.2.61

Sort by date.

Select top MSI to 

download most 

recent version.
Mission Planner Setup Wizard

Mission Planner: Flight Data Screen

Launch Mission 

Planner to explore 

the capabilities of 

your autonomous 

vehicle! 

Mission Planner will 

notify you when an 

update is available; 

please always run 

the most current 

version of Mission 

Planner.

CALIBRATE RADIO CONTROL

Mission Planner’s RC calibration utility teaches APM to work with your 

RC transmitter.

For more information on using Mission Planner or troubleshooting 

your installation, please visit planner.ardupilot.com.
Open Mission Planner. Connect APM to your 

computer using the provided micro-USB cable.

Windows will automatically install the correct 

drivers for APM. In Mission Planner, select the 

COM port for Arduino Mega, set the Baud rate 

to 115200, and select Connect.

Turn on your transmitter, and ensure it is set to airplane mode (not 

helicopter mode). In Mission Planner, navigate to Initial Setup, 

Mandatory Hardware, and Radio Calibration. Select Calibrate Radio. 

Move the transmitter’s sticks and mode switches to all available 

positions until the red bars are set at the extremes for each control. 

Select Click when Done to complete RC calibration.

APM USB port

Connect APM to Mission Planner:

1 Select Arduino Mega.

2 Select 115200.

3 Select Connect.

1 2

3

1

2

3

4

5

6

1 Select Hardware.

2 Select Mandatory Hardware.

3 Select Radio Calibration.

4 Select Calibrate Radio.

5 Move transmitter sticks and switches to all positions.

6 Select Click when Done.

Left Stick:

Right Stick:

To learn about utilizing your plane’s autonomous flight modes, 

designing missions, troubleshooting, multicopter safety, and 

more, please visit plane.ardupilot.com.

Mission Planner: Radio Calibration Screen
Appendix B

Quad‐Copter Operator Manual
Bumb lebee -S Manua l

使用前请仔细阅读此说明书。

Read the manual carefully before usin.g it
∅550mm

展开状态:

参数 特点 F e a t h u r s:

折叠状态:

305mm

191mm

571mm

158mm

空机重量( : g

起飞重量( A l l W e i g h t ):1200g 

建议飞行载重量( P a y l o a d C a p a b i l i t y ):200~500g

最大安全起飞重量( ):1700g

电池要求 (Cell Chemistry):11.1V 3S 2200uma/h~5500uma/h

 Li_poly 电池放电能力(Instant Discharge Capacity)>20C

飞行时间(Flight Time):>10分钟

轴距(wheelbase):550mm

整机高度 (height):306mm

折叠后长度( Length Of After F o l d):784mm

折叠后高度( H e i g h t Of After F o l d):100mm

桨Propeller:1038*2pcs,1038P*2pcs

3512无刷电机( B r u s h l e s s M o t o r ):

重量( W e i g h t ):75g

KV:930rpm/V

空载电流( N o _ l o a d C u r r e n t ):0.7A/11.1V

无刷电子调速器 ( B r u s h l e s s E S C ):20A * 4pcs

Empty Frame Weight) 450

M a x i m u m G r o s s T a k e - O f f W e i g h t

兼容所有模型遥控器和接收机,建议使用6通道以上的遥控器和接收机。

可折叠设计,方便携带和运输。

C o m p a t i b l e w i t h a l l t h e R C d e v i c e s , w e r e c o m m e n d y o u t o u s e 

R C d e v i c e w i t h 6 c h a n n e l s o r m o r e f o r e x p a n s i o n .

-1-
-5-

 B e f o r e F l i g h t :

DISCLAIMER OF LIABILITY

1.Using the company products within the limits permitted by local laws and 

regulations. the company is not responsible for any illegal activities.

2.The Bumblebee is an aeromodelling product only. Please strictly follow the 

aeromodelling safe function rules, the company does not hold responsible for 

any control over its operation or usage. 

3.Model aircraft are not toys! Fly under professional guidance and strictly 

follow instruction rules in this document. the company is not responsible for 

consequences caused by improper install, wrong setting or operation.

SAFETY CAUTIONS

1. Familiarize yourself with fly environment and any obstacles. Identify any 

potential hazards such as power lines, cars, people, etc. 

2.Do not fly the aircraft when fatigued, drunk or your mental state has been 

compromised which may cause an accident.

3.Stay away from wet areas. Do not fly in the rain or wet environments which 

can cause device failure and probably lead to danger. Do not fly at night or 

in windy conditions.

5. Do not fly alone during your preliminary flights. If you need help, please 

enlist the aid of an experienced pilot before flying for the first time.

6. Prepare rescue tools such as cell phones or other communication devices 

which should you need to call for help.

7. Please fly under safe take-off weight, do not overload the aircraft which can 

lead to danger.

8. Ensure all the equipment operates correctly before flight and that there is 

no transmitter interference or conflicts.

9. Do not touch any moving or powered parts. Do not try to catch the 

quadcopter which has rotating motors or blades for example. Keep loose 

clothing away from moving parts as they may get caught and could cause 

physical harm.

10. Always throttle down to minimum before fly.

11. Remove the propellers when testing the remote device or motors operation. 

Attach the propellers after you have tested that everything is working good 

to prevent an accident.

12. Assemble the aircraft with accessories the company provides. the company is not 

responsible for any consequence resulted from assembly with other 

accessories or modifications.

4. Stay away from any fire resulting in damage of the electronic parts or others 

such as the flight battery.
INSPECTIONS BEFORE FLIGHT

PLEASE PAY ATTENTION TO THE AGING AND WORN PARTS, AND FLY WHEN THEY ALL 

WORK WELL. PLEASE DO CHECK EVERY ASSEMBLY CAREFULLY BEFORE FLIGHT, 

especially lapses in these parts will easily cause DANGER.

1. Check that the propellers are secured properly.

2. Check that the receiver is receiving a stable signal.

3. Check that the battery is secured tightly and the battery is fully charged.

4. Check that the receiver is attached correctly.

5. Check the antenna is assembled tightly enough.

6. Check that the brushless motor and brushless ESC are secured to the 

 airframe.

Before flight, please assemble receiver or connect ESC to FC as the company factory 

defaults, if not, please DO CHECK the operations of Remote Control channels and 

consistence of motor reactions.

FLIGHT CONTROL INSTRUCTION

1. Start: Set the throttle stick to the lowest then turn on the transmitter. 

Connect the flight battery then slowly apply the throttle until all motors 

begin to run. 

2. Stop: Move the throttle stick to the minimum. All motors should stop to 

work in about one second. First cut off the Bumblebee then the RC powers 

off.

3. Any emergency occurs when taking off or landing, please move the throttle 

stick to the lowest position immediately to keep safe.

4. Flight control to the front, back, left and right is similar to the traditional RC 

helicopters but each motion is controlled by a separate channel. Do not use 

any channel mixing in your RC transmitter such as v-tail or swashplate 

mixing etc.

START TO FLY

Power ON/OFF Operations: Before plugging in the quad you have to turn on the RC 

and set the throttle stick to the lowest position. When powering off, you have to cut 

off the aircraft first then the RC powers off. Disorder in the on and off procedure will 

cause an accident.

1. Place the aircraft on the ground. Put the throttle stick to the lowest position 

then turn on the transmitter.

2. Connect the battery to the ESC board.

3. Start the Quad by applying power slowly with the throttle stick. When all the 

motors rotate at a slow speed you can move the stick to check the X650 

Value actions according to your operation. 

4. If you can not calibrate the tilt on one side during your flight, please 

connect Bumblebee to the PC and use the company configuration software to do 

the calibration.

-6-

 B e f o r e F l i g h t :
机身臂安装 F r a m e A r m a s s e m b l y :

 Screw M 2 . 5 * 2 4

机身管固定座

A r m M o u n t

杯头内六角螺丝

 M2.5*22 Screw

M 2.5防松螺母

L o c k N u t M.25

碳 管 C a r b o n t u b e

垫片

Washer

M 2 . 5防松螺母L o c k N u t

电调线

wire of ESC

电调线

wi r e of ESC

安装M 2 . 5 * 2 4的螺丝时,请注意避开里面的电调线,

以免碰伤电调线致使电调损坏。

-8-
Identify the parts carefully 

before installing

机身下板

Fuselage Lowerr Plate

杯头内六角螺丝

S o c k e t S c r e w M 2 . 5 * 1 0

杯头内六角螺丝

S o c k e t S c r e w 

M 2 . 5 * 1 0

M 2 . 5防松螺母

L o c k N u t

M 2 . 5防松螺母

Lo c k N u t

M2.5防松螺母

Lock Nut

半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝

半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝

半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝

半圆

S o c k e t S c r e w M 2 . 5 * 6

杯头内六角螺丝 头内六角螺丝

S o c k e t S c r e w 

M 2 . 5 * 1 0

支撑管卡扣

T h e s u p p o r t 

p i p e b u c k l e

起落架固定块-左

Landing Gear Fixed block-left

起落架固定块-右

Landing Gear 

Fixed block-right

机身装配 M a i n F r a m e A s s e s b l y ( 1 ) :

机身上板

F u s e l a g e u p p e r P l a t e

机身下板

Fuselage Lower Plate

安装前请仔细辨认

-9-

起落架固定块-左

Landing Gear Fixed block-left

注意安装方向

N o t i c e f a c e .

起落架固定块-右

Landing Gear Fixed block-right
机身装配 M a i n F r a m e A s s e s b l y ( 2 ) :

-10-

半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝

杯头内六角螺丝

S o c k e t S c r e w M 3 * 2 8

半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝

杯头内六角螺丝

S o c k e t S c r e w M 3 * 2 8

机身上板

F u s e l a g e U p p e r P l a t e

直形卡扣

S t r a i g h t b u c k l e

弧形卡扣

C u r v e d b u c k l e

弧形卡扣

C u r v e d b u c k l e

尼龙垫片

Nylon washer

尼龙垫片

Nylon washer

尼龙垫片

Nylon washer

半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝 半圆

S o c k e t S c r e w M 2 . 5 * 6

头内六角螺丝

自锁螺母

Locker Nut
起落架安装 L a n d i n g G e a r A s s e m:b l y

3

5

6

7

1

2

1

4

3

5

6

7

7

4 4

1 起落架

2 起落架连接柱

3 圆头十字自攻螺丝 

4 支撑管

Landing Gear Connector 

S u p p o r t i n g Tu b e

Landing Gear

Screw PA 2.5×10

5

6

7

硅胶套

碳管胶塞

杯头内六角轴套螺丝 

Plugs 

Silicon gel- Slipcover

Screw M3×12 

-11-
1.先将单边起落架向侧面分开 First please separate landing gear to another side 

2.把电池板组件卡在另一边的支撑杆上 Fixing component of the battery board on another support rod

3.分开的起落架复位 Resetting the separated landing gear frame 

4.电池板组件另一边卡扣卡在另一支撑杆上 Fixing another component of the battery board on another 

 support rod

扎带

用扎带固定在电池板上

r i b b o n t i e d

fixing upon the battery 

board with a ribbon tied

电池battery

电池板组件Battery Assembly :

BatteryB oard

电池板

半圆头内六角螺丝

Screw M2 .5*12

半圆头内六角螺丝

Screw M2 .5*12

M 2 . 5防松螺母

L o c k N u t

电池板卡扣

B a t t e r y b u c k l e

电池板组件安装 Battery Mounting Assembly:

起落架横管安装The installation of landing gear cross tube:

硅胶套

silicon gel- Slipcover

起落架横管

landing gear cross tube

硅胶套

silicon gel- Slipcover

2

1

3

-12-
桨的安装 Propeller Installation:

S T 1 0 3 8

正桨2 p c s

S T 1 0 3 8 P

反桨2 p c s

螺旋桨有正反之分,安装前请仔细辨认!

M1、M3相同,M2、M4相同。

There are difference of pros and cons in the propeller, please 

identify it carefully before installation ! M1、M3 is the same, 

M2、M4 is the same too. 

桨 Propeller

桨夹 Propeller Locker

无刷电机

Brushless Motor

螺旋桨必须贴紧电机,以保证四个螺旋桨的

高度一致性。

Close to motor to make 

sure 4 blades in the same height.

Motor Blade

用螺丝刀穿过桨夹上的孔来拧紧桨夹。

We recommend you use the driver to poke through the hole on 

the locker for better tighten in case of any loose of the screw 

during your flight.

桨夹必须拧紧,以免飞行时脱桨造成危险。建议 螺丝刀

Screw Driver

M2

M3 M4

M1

前

Fornt

-13-
无桨通电测试 P o w e r - o n T e s t w i t h o u t P r o p e l l e r s :

电路安装完成后,请勿安装螺旋桨,进行Bumblebee无桨通电测

试。

1 将遥控器油门收到最小后打开遥控器开关。

2 Bumblebee接通电源。

3 轻推油门。

4 观察四个电机启动是否顺畅,旋转方向是否正确。

a) 如果电机没有启动或启动不畅,则将油门收到最小,断开

Bumblebee的电源,检查电路和电机后重新测试,直到正

常。

b)如果旋转方向不正确,则将油门收到最小,断开Bumblebee

电源,对调任意两条电机线,直到电机旋转方向都正确。

5 推动各操纵杆,观察电机的转速是否有变化。

6 测试完成,将油门收到最小,断开Bumblebee的电源。

After electronic parts installation, DO N OT install the

propellers and follow in steps.

1 Lowest the RC throttle then turn on the transmitter.

2 Power on Bumblebee.

3 Apply the throttle slowly.

4 Note if four motors rotate sm oothly

a)If motor does not r otate or not sm oothly enough, 

please throttle down to the lowest t hen unplug

Bumblebee . Check on electronic circuit and motors 

to retest until it works fine.

b)If not in the right direction, lower the throttle to

m inim um and power off Bumblebee. Swap any motor

wire of three connecting to the holes until i t works in

the right way.

5 Poke all control sticks to observe motor rotation speed

changes or not.

6 Throttle back to lowest and power off Bumblebee.

-16-
折叠方式 F o l d i n g M e t h o d :

支臂的折叠 F o l d i n g A r m:

1.先取下电池板组件

First pletake of component

as battery board

2.沿箭头方向将起落架拉平

 Along the arrow direction to 

e v e n t h e l a n d i n g g e a r o u t

3.起落架和支臂折叠后

 A f t e r f o l d i n g o f l a n d i n g

 g e a r a n d r o t o r w i n g s

起落架的折叠 The folding of landing gear:

571mm

305mm 158mm

电池板组件 191mm

b a t t e r y b o a r d

 c o m p o n e n t

-17-
Appendix C

Transmitter Control Manual





Appendix D

Computerized Control Board



Appendix F

Personal Protocols and Controls
Protocols and Controls

Bruce Pogosaew ,  FPVCATALOG.llc, Tucson Arizona                                                     Page 1

Safety for public on the ground as well as manned aircraft above is an essential and utmost

consideration for aerial videos and photography. As such, safety protocols and controls must be

implemented through pre‐flight preparation and during flight.

Pre‐Flight Protocol:

Check batteries with voltage meter to insure fully charged and ready for use.

Inspect batteries for damage or leakage that may affect proper operation.

Inspect propellers for cracks, chips or damage that may cause sudden loss of propulsion or

unmanageable/uncontrolled flight.

Check all GPS and Telemetry connections prior to flight  

Check weather forecasts for wind advisory or other conditions that my impact flight.

Consult Sky Vector aeronautical Charts (Skyvector.com)for airport vicinity and flight paths of possible air

traffic.  

 Contact respective airport to advise of estimated flight time, estimated flight duration,

estimated elevation of flight, and any other pertinent information.

Inspect flight area for

 vicinity of public safety helipads/heliports

 vicinity of medical helipads/heliports

 vicinity of light poles

 vicinity or utility wires

 vicinity of trees

 flocks of birds that may cause interference and potential flight impact

 vicinity of any elevated obstructions that may pose potential flight hazard

 vicinity of roadways with moderate to heavy traffic that can be distracted

 public gatherings that may attract viewers

 optional point of control for best visual site of UAS while in flight

 Emergency landing areas

Takeoff and landing

 inspect area for best and safest point of takeoff and landing

 if in a subdivision or area that is within 150 feet of a residential street, post warning

sign(s)/stand(s) "Attention Aerial Photography In Progress ‐ Remain Back 150 Feet "
Flight Protocol:

takeoff and land from same location ( have alternate landing areas in case of emergencies)

remain alert to birds, sound or aircraft, curious public, and approaching vehicles

do not allow anyone to engage in conversation or distract the remote control pilot

restrict flight to minimal elevation sufficient to acquire desired results

remained prepared for emergency landing at all times

pay attention to flight time –  warning meter for low voltage.

 set voltage meter alarm for low voltage and flight timer as a safety alert

land UAS and shut down propulsion immediately following landing  –  priority of disconnecting batteries  

Post flight:

a) disconnect battery to prevent accidental activation of propulsion system

b) secure UAS in a safe location

c) remove all warning signs from public access areas

Emergency or Suspected Hazard:

Immediate land UAS at safest and closet ground location in the event

 manned aircraft is heard or seen in vicinity of flight

 there is a public gathering within established safety boundary wanting to observe flight

 pilot is being distracted from focusing on flight and safety

 sudden change in weather (wind bursts)

 sudden increase in vehicular traffic in vicinity of flight

 birds enter into proximity of flight

 any sudden unsafe event that can cause collision, distraction or interruption of control
Safety for public on the ground as well as manned aircraft above is an essential and utmost

consideration for aerial videos and photography.

Maintaining a record of safe flight for FAA request and for determining future UAS safety protocols is

imperative.

Date:____________________ Location: ___________________________________________________

pre‐flight Inspection:  

o Yes

o No  

Comment: _________________________________________________

Elements

Weather Good Fair Poor Comment :

Visibility Good   Fair   Poor Comment :

Wind Speed ___mph ___Gusts/MPH ___avg/MPH Comment :

Proximity to airport: _________________ (see attached map pinpointing approximate location of flight)

Airport notified   

o Yes

o No       Date:_______________ Time: ______________

Phone Number: _______________________ Contact Name: ___________________________________

Nearest major intersection: ______________________________________________________________

Proximity to medium traffic road: _________________________________________________________

Proximity to heavily traveled roadway road: _________________________________________________

Proximity to congested population: ________________________________________________________

Approx. Takeoff Time :                             GMT:

Approx. Landing Time:                              GMT:

Estimated Elevation Ground level:                                      sea level:

Safety Concerns:

Additional Comments: