# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com January 6, 2016 United States Department of Transportation Federal Aviation Administration Docket Operations 1200 New Avenue SE Washington DC 20590 Re: Petition for an exemption seeking relief from specific sections of Title 14 CFR under Section 333 of the FAA Modernization and Reform Act of 2012 (Public Law 112 - 95)

Dear Sir or Madam: Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 and 14 CFR Part 11, TrueONE Group LLC hereby seeks an exemption from the Federal Aviation Regulations as detailed below for the purpose of conducting commercial Unmanned Aerial System (UAS) operations in the National Airspace System (NAS).

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### TABLE OF CONTENTS Page GLOSSARY OF ABBREVIATIONS ................................................................................................................................................ .. 3 NAME AND ADDRESS OF THE PETITIONER...............................................................................................................................4 BACKGROUND AND OPERATING DESCRIPTION....................................... .......................................................................... ......5 SPECIFIC SECTIONS OF 14 CFR FROM WHICH TRUEONE GROUP LLC SE EKS EXEMPTION AND THE EXTENT OF RELIEF SOUGHT AND THE REASON THAT THE RELIEF IS SOUGHT......................................................... ................... ... ............ ..........9 THE REASONS WHY GRANTING THE REQUEST WOULD BE IN THE PUBLIC I NTEREST ......................................................11 THE REASONS WHY GRANTING THE REQUEST WOULD NOT ADVERSELY AFFECT SAFETY.............................................. 12 SUMMARY SUITABLE FOR THE PUBLIC REGISTER ........................ ..........................................................................................12 ADDITIONAL INFORMATION, VIEWS, AND ARGUMENTS AVAILABLE TO SUPPORT TRUEONE GROUP LLC’S REQUEST...................................................................................................................................................................................... 12 ADDENDUM................................................................................................................................................................................ 13  TrueONE Group LLC Preflight Safety Checklist  Link to DJI Phantom 2 Manual  Link to DJI Inpire 1 Pro Manual  Ground Control System  AMA Safety Code

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### GLOSSARY OF ABBREVIATIONS **AGL** Above Ground Level **ATC** Air Traffic Control **ATO** Air Traffic Organization **UAV** Unmanned Aerial Vehicle **CFR** Code of Federal Regulations **COA** Certificate of Authorization **FAA** Federal Aviation Administration **FAR** Federal Aviation Regulation **GCS** Ground Control System **GPS** Global Positioning System **L OL**  Loss of Link **NAS** National Airspace System **NOTAM** Notice to Airman **PIC** Pilot in Command **Section 333** FAA Modernization and Reform Act of 2012 Section 333 **SOP** Standard Operating Procedures **VFR** Visual Flight Rules **VLOS** Visual Line of Sight **VMC** Visual Meteorological Conditions **VO** Visual Observer **VTOL** Vertical Takeoff and Landing

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### NAME AND ADDRESS OF THE PETITIONER: The name and address of the petitioner is: TrueONE Group LLC Lawrence Monis, Founder 18410 36 th Ave W, Apt. A Lynnwood, WA 98037 (206) 330 - 7023 lawrencem@trueonegroup.com

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### BACKGROUND AND OPERATING DESCRIPTION TrueONE Group LLC seeks exemption from the requirements of 14 CFR FAR Parts 91.7 (a), 91.9 (b) 2, 91.119, 91.121, 91.151 (a), 91.405 (a), 91.407 (a)1, 91.409 (a) 1 and 2, 91.417 (a) and (b) pursuant to Section 333 of the FAA Modernization and Reform Act of 2012. Th is exemption will permit TrueONE Group LLC to obtain an appropriate Certificate of Authorization to operate the described UAV aircraft below within the NAS for the commercial purpose of collecting aerial photo and video assets. TrueONE Group LLC was form ed in 2015 by Lawrence C Monis. Mr. Monis has been flying RC aircraft recreationally with just over a year of experience operating the type of UAVs that will be flown under the desired exemption. Mr. Monis will be attending flight courses to obtain his spo rt pilot license. In the meantime, once the Section 333 exemption is obtained, TrueONE Group LLC will hire FAA certified pilots with UAV flying experience to act as the PIC . TrueONE Group LLC seeks to provide aerial photo and video services for a variety of clients to include residential/commercial real estate brokers, ins urance companies, and roofing/construction contractors. As set forth in this petition, TrueONE Group LLC seeks to commercia lly operate it s UAVs with the highest lev el of safety and professionalism . **Description of the UAV aircraft s**  **and ground control station (GCS): DJI Phantom 2:**  The DJI Phantom 2 is a small quadcopter that takes off and lands vertically (VTOL) and is powered by 4 brushless electr ic motors and a 5200mAh lithium polyme r battery pack. It has a ready-to -fly gross weight of 2.2 pounds a nd can fly a mission of an estim ated 25 minutes on a fully charged battery, and has a maximum airspeed of approximately 29 knots (33mph) . It has a sophisticated onboard flight controller with GPS integration that provides stabilized flight and extremely precise control from the portable Ground Control Station (GCS). There is a flight telemetry system that delivers flight data from the onboard flight computer to the GCS including altitude AGL, horizontal and vertical speed, battery voltage, compass direction of flight and direction back t o the takeoff point. The flight controller also has many built - in safety features that will command the Phantom 2 to return to the takeoff point in the event of a Loss of Link (LOL). There is a low battery voltage indication at 20% battery power remaining, and a “hard” warning at 15% remaining that will be gin a slow descent for landing. The user can define maximum flight parameters such as altitude and/or lateral distance from the GCS. The Phantom 2 has a 3 - axis gimbal that provides stabilization for a sm all dig ital camera allowing for smooth and accurate photo and video acquisition. The Phantom 2 carries a low power Video Transmitter that transm its live video feed data to a 7 - inch LCD screen that displays live video data to the operator and/or Visual Obs erver (VO). In the Addendum below is the DJI Phantom 2 User Manual . **DJI Inspire 1 Pro:** The DJI Inspire 1 Pro is a small quadcopter that takes off and lands vertically (VTOL) and is powered by 4 brushless electr ic motors and a 45 00mAh lithium polymer battery pack. It has a ready-to -fly gross weight of 7.5 pounds a nd can fly a mission of an estimated 18 minutes on a fully charged battery, and has a maxi mum airspeed of approximately 35 knots (40 mph) . It has a sophisticated onboard flig ht controller with GPS integration that provides stabilized flight and extremely precise control from the portable Ground Control Station (GCS). There is a

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com flight telemetry system that delivers flight data from the onboard flight computer to the GCS includ ing altitude AGL, horizontal and vertical speed, battery voltage, compass direction of flight and direction back to the takeoff point. The flight controller also has many built - in safety features that will command the Inspire 1 Pro to return to the takeoff point in the event of a Loss of Link (LOL). There is a low battery voltage indication at 20% battery power remaining, and a “hard” warning at 15% remaining that will be gin a slow descent for landing. The user can define maximum flight parameters such as altitude and/or lateral distance from the GCS. The DJI Inspire 1 Pro has a 3 - axis gimbal that provides stabilization for a small dig ital camera allowing for smooth and accurate photo and v ideo acquisition. The Inspire 1 Pro uses the DJI Go App (mobile ap p) which transm its live video feed data to either a smart phone/tablet screen that displays live video data to the operator and/or Visual Observer (VO). In the Addendum below is the DJI Inspire 1 Pro User Manual . **Ground Control Station (GCS):** The GCS consists simply of a hand - held RC transmitte r used to pilot the UAV and a 7 - inch LCD screen attached to the RC transmitter to view the live image of the on board camera. This makes the GCS very portable and allows for flexibility and ease of use. It is al so very non - intrusive for observers and non - participants. The RC tran smitter transmits on the 2.4 GHz band at a power of 100mW and requires no FCC license to operate. The 7 - inch LCD screen receives and displays the video signal b eing transmitted from the 5.8 GHz 400mW video transmitter on board the UAV. This system does require an Amate ur Radio License from the FCC. The DJI Inspire 1 Pro uses a communicates with its native mobile app (DJI Go App) and displays the video signal to either a smart phone or a tablet. **Pilot in Command:** Once the requ ired Section 333 exemption are obtained, TrueONE Group LLC will contract out the requested wo rk to FAA certified pilots with UAV experience to act as the PIC. As the founder and owner of TrueONE Group LLC, Lawrence C Monis also will be seeking to acquire his sport pilot license so that he, too, can act as the PIC and op erator of the UAVs being flown. He has fl own RC aircraft for a little more than a year and will start taking courses to obtain his sport pilot license. He is also a member of the Academy of Model Aeronautics (AMA # 108 8525 ). He is fully capable and familiar with the various operating procedures, limitations, and safety features of the equipment to be utilized as described in detail above and referenced in the applicable manufacturer manuals (see attached manufacturer manuals in the Addendum). Once Mr. Monis acquires his sport pilot license, Mr. Monis’ qualifications and experience will allow him to maintain a safe and efficient operation that will preserve public safety and provide a useful and valuable service to both the clients of TrueONE Group LLC and the general public. **Visual Observer (VO):** TrueONE Group LLC will utilize a VO consistent with FAA and AMA established best practices.  Al l operations will utilize a VO  The PIC and VO will be able to comm unicate by voice at all times  The PIC will brief the VO and others concerning the hazards unique to each flight  The VO may not operate the aircraft  The UAV will be operated in VLOS o f the PIC and VO at all times  The PIC will be aware of the sight limitations of the VO an d plan the flight accordingly

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com

 Electronic messaging, texting, or any other distracting activity shall not be permi tted during flight operations  The PIC shall be responsible t o ensure that the VO is fully capable of performing the required duties **Operating Procedures:** UAV operations will be conducted for the purpose of collecting photo and video footage that will be used for assisting real estate brokers in advertising real property for sale, assisting construction and roofing contractors with detailed site inspection and project progress, and capturing other photo and video footage that would be either impractical or impossible using full size aircraft. The proposed operati ons would be conducted as follows:  Before and after each flight, a Preflight Safety Checklist will be completed to ensure UAV and GSC airworthiness and status, as well as the consistency of condition that checklist usage provides instead of reliance on mem ory (see detailed Preflight S afety Checklist in Addendum)  All aircraft will be maintained as part of the Preflight Safety Checklist, which mandates that before flight the UAV, GSC, and its separate components must be updated with the latest firmware version from the manufacturer as spelled out in the applicable O perating Manual. Aircraft will be checked before flight for overall condition, nicks or cracks in propellers, security of all fasteners, and for proper LED status light indications. Flight battery packs will not be used beyond the manufacturers recommen de d maximum number of cycles  Aircraft flights will terminate with not less than 20% useable battery life, or 3 min utes of flight time remaining  Aircraft will be flown at a maximum altitude of 400 AGL and not more than 0.5 mile s lateral distance from the PIC and VO to ensure VLOS at all times. Most flight missions require much less than these maximum distance values. These vertical and horizontal distance limits shall be monitored in real time by the telemetry data displayed on the GSC and will be set within the DJI Flight Controller as manual limits per the DJI Operator Manua ls.  Aircraft will be flown at a maximum airspeed of 30 knots (35 MPH)  The minimum flight visibility for operations shall be 3 statute miles, and a minimum distance from clouds will be ma intained (500 ft be low and 2000 ft horizontally)  Aircraft will never be flown via First Person View (FPV) by either the PIC or VO  No flight operations will be conducted at n ight as defined by 14 CFR 1.1  No flight operations shall be conducted closer than 5 nautical miles from any airport denoted on a current FAA published aeronautical chart unless a letter of agreement with that airport’s management is obtained, and the operation is conducted in accordance with a NOTAM as re quired by the operator’s COA.  Th e UAV will remain clear and yield the right - of-way to all m anned aircraft at all times  The UAV will not be operated closer than 500 feet to any nonparticipating persons, vehicles, or vessels unless there is a structure or barrier to protect such persons or property from the UAV or debris in the event of an accident, or unless the owner of such vehicles/vessels has granted permission and the PIC has made a safety assessment of risk of operating closer to those objects and determined that it does not present an undue hazard, and that operations nearer to the PIC, VO, operator trainees or other essential persons do not present an undue hazard to th ose persons per FAR 91.119(a)  The UAV will not be operated over any conge sted or densely populated areas  All provis ions of the AMA Safety Code (see Addendum) will be adhered to as part of a best practices strategy **Maintenance:**

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com

 All UAV and GSC equipment will be maintained by checked for manufacturer Firmware updates and Safety Bulletins  No alterations or modifications will be performed unless such action will not pose any degradation in safety of performance, and a functional flight test will be performed to verify functionality and safe ty of the affected equipment  Any maintenance, repair, or alteration wi ll be r ecorded in an aircraft logbook. PIC performed maintenance will be limited to replacing faulty/worn out components and updating Firmware pe r manufacturers specifications. Any other maintenance will be performed by the applicable manufacturer or thei r approved repa ir facility  Total flight time of the UAV and GSC shall be recor ded in the aircraft logbook  Lithium polymer batteries shall not be used beyond the recommended service life or number of cycles as specified by the manufacturer The petitioner believes that the described operating procedures and limitations, maintenance plan, combined with the low weight, speed, and limited area of operation described for the intended missions will ensure a measure of safety equal to or greater than a full - size aircraft, and that the public will not be subject to any undue hazard.

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### SPECIFIC **SECTIONS OF 14 CFR FROM WHICH TRUEONE GROUP LLC SEEKS EXEMPTION AND**  **THE EXTENT OF RELIEF SOUGHT AND THE REASON THAT THE RELIEF IS SOUGHT** The petitioner believes that as per Section 333 of PL 112 - 95, and in consideration o f the size, weight, speed and limited operating area asso ciated with the aircraft and it s operation, that relief from 14 CFR Part 21 Subpart H regarding Airworthiness Certificates is not necessary and the refore relief is not sought. **FAR Part 91.7(a)** prescribes that –

No person may operate a civil aircraft unless it is in an airworthy condition . Relief is requested to maintain an airworthy condition by compliance with the operating procedures, checklist s, and documents prescribed in this petition prior to every flight. **Far Part 91.9 (b) 2** prescribes that –

(b) No person may operate a U.S. -registered civil aircraft — (1) For which an Airplane or Rotorcraft Flight Manual is required by § 21.5 of this chapter unless there is available in the aircraft a current, approved Airplane or Rotorcraft Flight Manual or the manual provided for in § 121.141(b); and (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. Relief is requested to comply by keeping all relevant company operating procedure s, limitations, logbooks, and checklists in a location accessible to the PIC. **Far Part 91.119** prescribes in part that –

Except when necessary for takeoff or landing, no person may operate an aircraft below the following altitudes: (c) Over other than congested areas. An altitude o f 500 feet above the surface, except over open water or sparsely populated areas. In those cases, the aircraft may not be operated closer than 500 feet to any person, vessel, vehicle or structure. Relief is sought for FAR 91. 119 (c) because that UAV aircraft will be operated below 400 feet AGL and would not be able to comply with this subparagraph. Petitioner would operate in accordance with the limitations described in this petition or by any other limitations the FAA deems necessary. **Far Part 91.121** prescribes in part that –

(a) Each person operating an aircraft shall maintain the cruising altitude or flight level of that aircraft, as the case may be, by reference to an altimeter that is set, when operating — (1) Below 18,000 feet MSL, to —

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com (i) The current reported altimeter setting of a statio n along the route and within 100 nautical miles of the aircraft; (ii) If there is no station within the area prescribed in paragraph (a)(1)(i) of this section, the current reported altimeter setting of an appropriate available s tation; or (iii) In the case of an aircraft not equipped with a radio, the elevation of the departure airport or an appropriate altimeter setting available before departure; or (2) At or above 18,000 feet MSL, to 29.92 ʺ Hg. Relief is sought because the UAV aircraft does not have a typical barometric altimeter on board, and all reported altitudes will be reported in feet AGL . **Far Part 91.151(a)** prescribes that –

(a) No person may begin a flight in an airplane under VFR conditions unless (considering wind and forecast weather conditions) th ere 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; o r (2) At night, to fly after that for at least 45 minutes. (b) No person may begin a flight in a rotorcraft under VFR conditions unless (considering wind and forecast weather conditions) th ere is enough fuel to fly to the first point of intended landing an d, assuming n ormal cruising speed, to fly after that for at least 20 minutes. Relief is sought to operate at less than the prescribed minimums because UAV w ill never be flown more than 0.5 mile s from the point of intended landing, and that safety will be maintained by monitoring the elapsed time in flight, real time battery voltage condition, and the 2 level low battery warnings detailed above in the UAV description. The PIC will never begin a f light unless there is enough power to fly to the intended point of landing at normal cruising speed and still land with 20% battery power remaining. **Far Part 91.405 (a), 91.407 (a) 1, 91.409 (a) 1 and 2,**  **91.417 (a) and (b)** prescribe that –

91.405 (a) Each owner or operator of an aircraft — (a) 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; 91.407 (a) 1 (a) No person may operate any aircraft that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless — (1) It has been approved for return to service by a p erson authorized under §43.7 of this chapter; and 91.409 (a) 1 and 2 (a) Except as provided in paragraph (c) of this section, no person may operate an aircraft unless, within the preceding 12 calendar months, it has had — (1) An annual inspection in accordance with part 43 of this chapter and has been approved for return to service by a person authorized by §43.7 of this chapter; or (2) An inspection for the issuance of an airworthiness certificate in accordance with part 21 of this chapter.

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 91.417 (a) and (b) (a) Except for work performed in accordance with §§91.411 and 91.413, each registered owner or operator shall keep the follo wing records for the periods specified in paragraph (b) of this section: (1) Records of the maintenance, preventive maintenance, and alteration and records of the 100-hour, annual, progressive, an d other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. The records must include — (i ) A description (or reference to data acceptable to the Administrator) of the work performed; and (ii) The date of completion of the work performed; and (iii) The signature, and certificate number of the person approving the aircraft for return to service (2) Records containing the following information: (i) The total time in service of the airframe, each eng ine, each propeller, and each rotor. (ii) The current status of life -limited parts of each airframe, engine, propeller, rotor and appliance. (iii) The time since last overhaul of all items installed on the aircraft which are required to be overhauled on a specified time basis. (iv) The current inspection status of the aircraft, including the time since the last inspection required by the inspection program under which the aircraft and its appliances are maintained. (v) The current status of applicable airworthiness directives (AD) and safety directives including, for each, the method of compliance, the AD or safety directive number and revision date. If the AD o r safety directive involves recurring action, the time and date when the next action is required. (vi) Copies of the forms prescribed by §43.9(d) of this chapter for each major alteration to the airframe and currently installed engines, ro tors, propellers, and appliances. (b) The owner or operator shall retain the follo wing records for the periods prescribed: (1) The records specified in paragraph (a)(1) of this se ction shall be retained until the work is repeated or superseded by other wor k or for 1 year after the work is performed. (2) The records specified in paragraph (a)(2) of this section shall be retained and transferred with the aircraft at the time the aircraft is sold. (3) A list of defects furnished to a registered owner or operator under §43.11 of this chapter shall be retained until the defects are repaired and the aircraft is approved for return to service. Relief from these sections is sought because it is our intention to perform any maintenance and inspections as d escribed above and that this will ensure a high level of safety. As provided in the Preflight Safety Checklist (see Addendum) the PIC will be responsible for ensuring that the aircraft is in airworthy condition prior to every flight. The PIC will documen t any work performed as detailed above in the aircraft logbook as well as cumulative flight time. 

### THE REASONS WHY GRANTING THE REQUEST WOULD BE IN THE PUBLIC INTEREST Granting the present Petition would benefit the public interest by allowing TrueONE G roup LLC to safely, efficiently, and economically provide commercial aerial photo and video services for a variety of clients. These services will allow our clients and end users to experience these photo and video assets thus enhancing their own business es and creating economic opportunities for everyone involved. In addition, it is our desire to play a role of constructive public education on the benefits and uses of civil UAV systems by being an example of what is possible when this new technology is used in a safe and useful manner.

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com The public would benefit as well from the decrease in the air pollution, noise, and potential danger of using large manned aircraft with flammable fuel on board and an internal combustion engine to accomplish what our UAV aircraft can do using small, quiet electric motors and a small battery pack. 

### THE REASONS WHY GRANTING THE REQUEST WOULD NOT ADVERSELY AFFECT SAFETY Because of the speed, weight, size, and limited operating area associated with the proposed UAV aircraft operations, the Petitioner submits that our proposed flights would not create a hazard to other users of the NAS or to the public, or otherwise pose a threat to the national security. We also submit that TrueONE Group LLC can safely operate in the NAS p ursuant to FMRA Section 333 because: 1. We have detailed the operating characteristics of the UAV system. 2. We will hire experienced PICs to control the UAV system. 3. We will operate pursuant to the detailed set of operating limitations and procedures as set forth in this Petition to ensure the highest level of safety to ourselves, our clients and the public.



### SUMMARY SUITABLE FOR THE PUBLIC REGISTER TrueONE Group LLC seeks exemption from the requirem ents of 14 CFR Parts 91.7 (a), 91.9 (b) 2, 91.119, 91.121, 91.151 (a), 91.405 (a), 91.407 (a) 1, 91.409 (a) 1 and 2, 91.417 (a) and (b). This exemption will permit TrueONE Group LLC to commercially operate a UAV aircraft for the purpose of collecting aeri al photo and video assets for a variety of clients . 

### ADDITIONAL INFORMATION, VIEWS, AND ARGUMENTS AVAILABLE TO SUPPORT **TRUEONE GROUP LLC** **’S REQUEST** This Petition is made pursuant to the FAA Moder n ization and Reform Act of 2012 Section 333. As stated abo ve, TrueONE Group LLC will operate safely in the NAS without creating an undue haz ard to other users of the NAS, the general public, or by posing a threat to national security. TrueONE Group LLC operation will also provide a benefit to the public interest as detailed in this petition .

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### TRUEONE GROUP LLC PREFLIGHT **SAFETY CHECKLIST**  PREFLIGHT  Check weather status  Check solar activity (geomagnetic fields and solar rays)  Make sure that a ll firmware updates are installed  Charge necessary UAV/GSC Batteries to 100%  Secure a ll fasteners/wiring/connectors  Balance, secure, and inspect all propellers  Complete flight briefing PRIOR TO TAKE - OFF  Make sure GSC is powered on  Make sure UAV is powered on  Makes sure camera is powered on  Check for correct status of LED lights  Perform compass calibration  Perform final visual check of AOA DURING FLIGHT  Warn bystanders of imminent takeoff  Test controls within close distance to landing area to make sure there are no issues during flight  Monitor battery and signal strength during flight  Maintain VLOS AFTER LANDING  Turn UAV power off  Turn GSC power off  Turn camera power off  Perform inspection of battery and motor temperature

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

### LINK TO **MANUALS FOR DJI PHANTOM 2 AND DJI INSPIRE 1 PRO**  **DJI Phantom 2 Manual:** http://dl.djicdn.com/downloads/phantom_2/en/PHANTOM2_User_Manual_v1.4_en.pdf **DJI Inspire 1 Pro Manual:** http://dl.djicdn.com/downloads/inspire_1_pro/en/Inspire_1_Pro_User_Manual_en_v1.0_1201.pdf 

### GROUND CONTROL SYSTEMS

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 

## Academy of Model Aeronautics National Model Aircraft Safety Code Effective January 1, 2014 A. **GENERAL** : A model aircraft is a non - human -carrying aircraft capable of sustained flight in the atmosphere. It may not exceed limitations of this code and is intended exclusively for sport, recreation , education and/or competition. All model fligh ts must be conducted in accordance with this safety code and any additional rules specific to the flying site. 1. Model aircraft will not be flown: (a) In a careless or reckless manner. (b) At a location where model aircraft activities are prohibited. 2. Model aircraft pilots will: (a) Yield the right of way to all human -carrying aircraft. (b) See and avoid all aircraft and a spotter must be used when appropriate. (AMA Document #540 - D.) (c) Not fly higher than approximately 400 feet above ground level within three (3) miles of an airport without notifying the airport operator. (d) Not interfere with operations and traffic patterns at any airport, heliport or seaplane base except where there is a mixed use agreement. (e) Not exceed a takeoff weight, including fuel, of 55 pounds unles s in compliance with the AMA Large Model Airplane program. (AMA Document 520 -A.) (f) Ensure the aircraft is identified with the name and address or AMA number of the owner on the inside or affixed to the outside of the model aircraft. (This does not apply to model aircraft flown indoors.) (g) Not operate aircraft with metal - blade propellers or with gaseous boosts except for helicopters operated under the provisions of AMA Document #555. (h) Not operate model aircraft while under the influence of alcohol or while usi ng any drug that could adversely affect the pilot’s ability to safely control the model. (i) Not operate model aircraft carrying pyrotechnic devices that explode or burn, or any device which propels a projectile or drops any object that creates a hazard to pe rsons or property. Exceptions:

• Free Flight fuses or devices that burn producing smoke and are securely attached to the model aircraft during flight. • Rocket motors (using solid propellant) up to a G -series size may be used provided they remain attached to the model during flight. Model rockets may be flown in accordance with the National Model Rocketry Safety Code but may not be launched from model airc raft. • Officially designated AMA Air Show Teams (AST) are authorized to use devices and practices as defined within the Team AMA Program Document. (AMA Document #718.) (j) Not operate a turbine - powered aircraft, unless in compliance with the AMA turbine regu lations. (AMA Document #510 -A.) 3. Model aircraft will not be flown in AMA sanctioned events, air shows or model demonstrations unless: (a) The aircraft, control system and pilot skills have successfully demonstrated all maneuvers intended or anticipated prior to the specific event. (b) An inexperienced pilot is assisted by an experienced pilot. 4. Wh en and where required by rule, helmets must be properly worn and fastened. They must be OSHA, DOT, ANSI, SNELL or NOCSAE approved or comply with comparable standards. B. **RADIO CONTROL (RC)** 1. All pilots shall avoid flying directly over unprotected people, vessels, vehicles or structures and shall avoid endangerment of life and property of others. 2. A successful radio equipment ground - range check in accordance with manufa cturer’s recommendations will be completed before the first flight of a new or repaired model aircraft.

# TrueONE Group 18410 36 th Ave W, Apt A Lynnwood, WA 98037 206 - 330- 7023 lawrencem@trueonegroup.com 3. At all flying sites a safety line(s) must be established in front of which all flying takes place. (AMA Document #706.) (a) Only personnel associated with flying the model aircraft are allowed at or in front of the safety line. (b) At air shows or demonstrations, a straight safety line must be established. (c) An area away from the safety line must be maintained for spectators. (d) Intentional flying behind the safety line is prohibited. 4. RC model aircraft must use the radio -control frequencies currently allowed by the Federal Communications Commission (FCC). Only individuals properly licensed by the FCC are authorized to operate e quipment on Amateur Band frequencies. 5. RC model aircraft will not knowingly operate within three (3) miles of any pre -existing flying site without a frequency- management agreement. (AMA Documents #922 and #923.) 6. Wi th the exception of events flown under official AMA Competition Regulations, excluding takeoff and landing, no powered model may be flown outdoors closer than 25 feet to any individual, except for the pilot and the pilot's helper(s) located at the flightline. 7. Under no circumstances may a pilot or other person touch an outdoor model aircraft in flight while it is still under power, except to divert it from striking an individual. 8. RC night flying requires a lighting system providing the pilot with a cle ar view of the model’s attitude and orientation at all times. Hand - held illumination systems are inadequate for night flying operations. 9. The pilot of an RC model aircraft shall: (a) Maintain control during the entire flight, maintaining visual contact withou t enhancement other than by corrective lenses prescribed for the pilot. (b) Fly using the assistance of a camera or First- Person View (FPV) only in accordance with the procedures outlined in AMA Document #550. (c) Fly using the assistance of autopilot or stab ilization system only in accordance with the procedures outlined in AMA Document #560. C. **FREE FLIGHT** 1. Must be at least 100 feet downwind of spectators and automobile parking when the model aircraft is launched. 2. Launch area must be clear of all indivi duals except mechanics, officials, and other fliers. 3. An effective device will be used to extinguish any fuse on the model aircraft after the fuse has completed its function. D. **CONTROL LINE** 1. The complete control system (including the safety thong where applicable) must have an inspection and pull test prior to flying. 2. The pull test will be in accordance with the current Competition Regulations for the applicable model aircraft category. 3. Mo del aircraft not fitting a specific category shall use those pull -test requirements as indicated for Control Line Precision Aerobatics. 4. The flying area must be clear of all utility wires or poles and a model aircraft will not be flown closer than 50 feet to any above -ground electric utility lines. 5. The flying area must be clear of all nonessential participants and spectators before the engine is started.