### DENNIS MONTGOMERY PHOTOGRAPHY 4845 Knollwood Drive Ogden, Utah 84403 801.479.8072, 801.391.1757 (C) U.S. Department ofTransportation Docket Management System 1200 New Jersey Ave, SE Washington, DC 20590 Re: Petition for FAA Section 333, 14 CFRPart 11 Exemption for Dennis Montgomery Photography (DMP) to Operate sUAS's for Commercial Purposes Dear Sir or Madam:

Pursuant to Section 333 ofthe Aviation Modernization and Reform Act of2012, Dennis Montgomery, doing business as Dennis Montgomery Photography (DMP), applies for an exemption from the Federal Aviation Regulations identified below, to allow operation of two small, unmanned system sUAS's, the DJI Inspire 1 (Registration NumberN5780M) and the Yuneec Q500 (Registration NumberNxxxxx) within the continental United States for commercial purposes as detailed in this petition. Both ofthese sUAS's weigh less than 55 pounds and have maximum speeds ofless than 55 KIAS.

The petition is organized as follows: Section A: Description ofPetitioner Section B: Types ofOperations to be Conducted Section C: Specific 14 CFR's Requested for Exemption, Extent ofRelief, Rationale for Requiring the Exemption, and How an Equivalent Level ofSafety will be Maintained Section D: Public Benefits for Granting the Exemption Section E: Federal Registry Summary Appendix A: DMP Operations and Maintenance Procedures and Checklists Appendix B: DJI Inspire 1 Specifications and Operations and Maintenance Manuals/Checklists Appendix C: Yuneec Q500 Specifications and Operations and Maintenance Manuals/Checklists SECTION A: DESCRIPTION OF PETITIONER
1 ..·-,n _:. <.iDennis Montgomery, operator and sole proprietor ofDennis Montgomery Photography (DMP) is a retired AirForce pilot with 26 years ofAir Force aviation experience in a variety ofaircraft, including aerial reconnaissance platforms. Heholds a Commercial Pilot Certificate, No. 1646837, with multi-engine, land and instrument ratings. He holds a Medical Certificate, Second Class, dated July 30, 2013. He has a Master's Degree in Engineering from the United States AirForce Institute ofTechnology and a Bachelors Degree from the United States AirForce Academy.

He has operated a freelance photographybusiness since 2007 with emphasis on sports, editorial and real estate photography. He has flown multi-rotor sUAS's, as a hobbyist, for the past year. He will be the chiefand onlypilot for the sUAS's operated by DMP under currentplans. The following sections describe how the requested waiver will allow him to use aerial photography/videography as an adjunct to his existing business services and benefit the community as a whole.

Contact Information:

Dennis W. Montgomery 4845 Knollwood Drive Ogden, UT 84403 Phone: 801.479.8072, 801.391.1757 (C) Email: 0 SECTION B: TYPES OF OPERATIONS TO BE CONDUCTED

All operations will be conducted subject to the conditions and limitations grantedby the FAA approval ofthis request for exemption andunderthe DMP operations procedures detailed inAppendix A. All the operations are adjuncts to the existing business conductedby Dennis Montgomery Photography (DMP). 1. Obtain still and video aerial imagery oflocal area eventvenues and other local places ofinterest for editorial purposes, advertising use and sale to private parties. 2. Obtain still and video aerial imagery ofconstruction sites during the construction process.. 3. Obtain still and video aerial imagery ofhigh-end real estate properties. 4. Obtain aerial photos ofaffinity group gatherings in appropriate settings.

SECTION C: SPECIFIC 14 CFR'S FORWHICH EXEMPTION IS REQUESTED, EXTENT OF RELIEF, RATIONALE AND MAINTENANCE OF AN EQUIVALENT LEVEL OF SAFETY

2This request for exemption is similar to the reliefgranted by FAA Exemptions No. 11638, 12483, and 12446 for the DJI Inspire 1 and to the reliefgranted by Exemption No. 12475 for the Yuneec Q500, with similarrationale for the requestedrelief. Regulations from which reliefis requested are: 14 CFR 91.7(a), 91.9(b)(2), 91.119(c), 91.151, 91.121, 91.203, 91.215, and CFR 14 Subpart E, 91-401 thru 417. 14 CFR, 91.7(a) Civil Aircraft Airworthiness

The regulation requires thatno person may operate a civil aircraft unless it is in airworthy condition. Since there is no airworthiness certificate nor an FAA regulatory standard issued for either ofthe sUAS 's operatedby DMP, this exemption should be granted. An equivalent level ofsafety will exist based onthe use ofapproved manufacturer's inspection and operations procedures, as well as those detailed inthe DMP operations and maintenance manuals. 14 CFR, 91.9(b)(2) Civil Aircraft flight Manual, Marking and Placard Requirements

This regulation states that no person may operate an aircraft unless a current, approved flight manual is inthe aircraft. Given the small size ofthe sUAS's and the fact that there is no pilot onboard, the regulation is not practical for these aircraft. An equivalent level ofsafety will be in effect bykeeping a current manufacturer's user manual and a DMP Operations Manual with the ground station and at thejob site where the pilot will have ready access to the manuals. 14 CFR, 91.119 Minimum Safe Altitudes, General

This regulation establishes safe altitudes for civil aircraft operations. Section 91.119(d) allows helicopters to be operated at less than the prescribed minimum altitudes ifthe operator complies with published helicopter routes and altitudes prescribed by the FAA. The sUAS's operatedby DMP are similar to helicopter operations in that they can ascend/descend vertically, as well as hover. Typical operations conductedby DMP photography will be accomplished at 200 feet AGL or lower, inmost instances, with occasional flights to an altitude not greater than 400 feet AGL to obtain photographic coverage oflarger areas.

The equivalent level ofsafety will be effectedby carefully selecting the launch/recovery sites, establishing a safety perimeter around the launch/recovery site, avoiding direct overflight ofprivate property unless sufficient notice ofoperations has been given and not flying in close proximity (500 feet) to non-participating individuals or animals. Additionally, the maneuverability, built in safety features ofthe sUAV's andthe operating procedures ofDMP greatly reduce the chances ofuncontrolled flight or landings. 14 CFR, 121 ALTIMETER SETTINGS



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### _The regulation requires the pilot to maintain cruising altitude by reference to an appropriately set, current altimeter setting obtained thru the proper agencies. Because there is no pilot onboard and there is no altimeter on the sUAS's, an exemption to this regulation is requested.

The equivalent level ofsafety is effectedby use ofthe GPS, visual sensors (DJI Inspire I only) and barometric sensors onboard the sUAS's. Readouts are displayed to the pilot on the ground control device in terms ofaltitude above the ground. The pilot constantly monitors this readout to comply with the altitude restrictions imposed on sUAS operations. 14 CFR 91.151, FUEL REQUIREMENTS FORFLIGHT IN VFR CONDITIONS _This regulation sets the fuel reserves required for a flight under VFR conditions specifically requiring a minimum of30 minutes ofreserve fuel. Because both sUAS's operated by DMP are poweredby LiPo batteries, the current battery technology does not allow for a 30 minute reserve. Under sea level, controlled conditions both sUAS's have an advertised, useful flight time ofno more than 25 minutes and considerably less at higher altitudes and under windy conditions. Forthat reason, compliance with this regulation is impossible.

Under DMP procedures, flight times will be set by using the "remaining battery" indicator on the respective ground stations. Flights will be terminated when the onboard aircraft battery has 25% battery charge remaining. Under windy conditions or for longer range flights, the return to home will be initiated even earlier ifconditions dictate. Setting flight lengths byusing a time standard is not practical given the variance in MSL altitudes the sUAS's will be operating at inthe mountainous area that exists inthe DMP area ofoperations, as well as variable wind conditions which accompany the area weather patterns
.. Using the remaining battery indicator as the fuel reserve standard creates the safest, most meaningful method ofmaintaining a safe fuel reserve as intended bythe regulation.

Because the operations will be conducted with while maintaining a Visual Line ofSight (VLOS) under daylight conditions and because battery health is carefully monitored using the manufacturer's published procedures, an equivalent level ofsafety will exist. Additionally, because the batteries are electric, there is no possibility offuel contamination or carburetor icing that can occur with liquid aircraft fuels, resulting in even safer flights compared to manned aircraft. 14 CFR, 91.203, Carrying Civil Aircraft Certification and Registration

This regulation provides, inpart, that no person may operate a civil aircraft unless it has an appropriate and current airworthiness certificate and that certificate is displayed at the cabin or cockpit entrance. Because both sUAS's operated by DMP weigh less than 25 pounds and there is no onboardpilot, there is no place to display the documents on the aircraft. An 

### equivalent level ofsafety will be maintained by keeping these documents



### 4

### with the Pilot in Command (PIC) who is operating the sUAS where anyone requiring access to these documents will have them readily available. 14 CFR 91.215, ATC TRANSPONDER EQUIPMENT AND USE

This section requires operable transponder equipment for certain operations conducted within FAA airspace. Because ofthe small size oftoday's sUAS, there is no known transponder equipment available that would be compatible with these aircraft. Further, the sUAS's will not be operated within 5 miles ofan airport nor within controlled airspace without specific authorization ofthe controlling FAA airspace manager and even then, it wouldbe under VFR conditions only and under 400 feet AGL. All operations currently foreseen would take place in Class G airspace under VFR conditions.

Given these restrictions and limits , an equivalent level ofsafety exists without requiring the sUAS to have an operable transponder which would only add to the workload ofthe controlling agency inmanaging air traffic. 14 CFR 91-405 9(a) AND (d), MAINTENANCE REQUIRED

This regulation requires, in part, that aircraft be inspected according to current FAA directed requirements and records be kept ofthe inspections and ofany parts replaced or maintenance work accomplished. Because the standards for manned vehicles differ from those for an unmanned vehicle without an airworthiness certificate, direct compliance with the existing regulation is impractical.

An equivalent level ofsafety will be maintained by adhering to the published DJI and Yuneec maintenance and inspection requirements detailed in Sections B and C ofthis petition. Additionally, the DMP procedures outlined in Section A will insure that the intent ofthe regulation regarding safety and record keeping will be as high orhigher than the existing regulation requires. All records will be kept at the site ofthe ground station so they are available to the PIC prior to flight and appropriate authorities who may require access to the records 14 CFR 91.407, OPERATIONS AFTERMAINTENANCE, REBUILDING OR ALTERATION This regulation requires that an aircraft that has undergone maintenance, preventative maintenance, rebuilding or alterationbe approved for return to service by persons authorized to perform such service under FAA rules.

Because ofthe inherent vehicle characteristics and the lack ofcertified repair facilities, other than the manufacturers themselves, it is notpractical to totally comply with this regulation. The operator ofDMP will conduct all inspections as specified in the manufacturer's manuals and do routine serving for the batteries, props and aircraft basic systems. This work will be documented inthe maintenance logs. After any maintenance procedure and after any firmware update for either the aircraft and/or the controller, a



### 5

### Functional Check Flight (FCF) will be accomplished to verify the integrity ofthe repair and proper operation ofthe aircraft. The aircraft will then be "signed off' before any commercial flights are undertaken. Rebuilds or alterations to the basic aircraft or its systems, otherthan firmware updates, will be done by the manufacturer, thus meeting the intent ofthe regulation and providing an equivalent level ofsafety. 14 CFR 91.417, MAINTENANCE RECORDS This regulation requires specific records to be kept for all maintenance accomplished on the aircraft, but is intended for manned aircraft having an airworthiness certificate. For these reasons, it is not directly applicable to the sUAS's operated by DMP. The intent of the regulation will be met by the detailed records kept for each sUAS, their ground stations, propellers, and batteries. These records will be reviewed priorto each flight by the PIC and will be available on site to appropriate authorities. For these reasons, an equivalent level ofsafety will exist. SECTION D: PUBLIC BENEFITS OF GRANTING THE EXEMPTION

The granting ofthe petition for exemption to FAA Section 333 for Dennis Montgomery Photography (DMP) is in the public interest since it increases the level ofsafety for aerial photography operations as compared to operating a manned aircraft. The reduced size and weight ofthe vehicle, absence ofcombustible fuel, as well as not having people in the vehicle, limit the damage and impact ifsomething does go wrong during flight. The built in safety, fail-safe systems built into both sUAS's operated by DMP also greatly reduce the possibility ofpilot error should something go wrong.

The exemption would also provide both media and business customers with a safe, reliable FAA approved method ofobtaining aerial imagery without buying a sUAS themselves orhiring a "hobbyist" who would might operate an sUAS without the proper training and without implementing the proper safety procedures. Furthermore, it allows business customers, media and individuals to obtain still and video recordings that benefit their businesses at a much lower cost than current alternatives.

For construction companies, the benefits ofhaving an aerial image quickly available can show defects intheir construction work and potential safety problems involved inthe construction process. It 

### also allows them to obtain the information and visual documentation ofthe construction process without inserting a photographer or videographer into the potentially dangerous construction environment. Furthermore, it provides a visual record ifimagery is needed inthe event oflitigation regarding their projects.

SECTION E: FEDERAL REGISTRY SUMMARY



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### Pursuantto 14 CFRPart 11, the following summary is provided for publication in the Federal Registry, ifrequired:

Dennis Montgomery Photography (DMP) based in Ogden Utah, seeks an exemption from the following regulations: 14 CFR 91.7(a), 91.9(b)(2), 91.119(c), 91.151, 91.121, 91.203, 91.215, and CFR 14 Subpart E, 91-401 thru 417 for the operation oftwo Small, Unmanned Aerial Systems (sUAS) for aerial photography and videography for commercial purposes. The approval ofthe DJI Inspire I and Yuneec Q500 sUAV's to operate commercially for these purposes enhances safety and reduces risk compared to obtaining the imagery through othermeans. These sUAV's weigh less than 25 pounds, contain no combustible fuel and do not carry a pilot or other crewmember thus reducing risk. Because they are operated within visual line ofsight and under visual conditions and do not operate offan airfield, they do not burden the air traffic control system orrisk conflicts with manned aircraft. The restrictions and limitations on the exemption ensure that there is no compromise of safety regarding the qualification ofthe operator (s), the maintenance ofthe vehicles and the safe operation ofthe vehicles. Privacy: All flights will occur overpublic property for which no federal, state or local restriction exits and over private property only when permission from the property owner has been obtained. Images ofany recognizable individuals in the imagery will require a signed model release before being used for commercial purposes. Pursuant to Section 33 ofthe FAA Modernization and Reform Act of2012, and 14 CFR Part 11, request an exemption to the Federal Aviation Regulations identified in this petition. Respectfully,

DENNIS W. MONTGOMERY Dennis Montgomery Photography (DMP) Owner

7

### DENNIS MONTGOMERY PHOTOGRAPHY (DMP) OPERATIONS AND MAINTENANCE MANUALS/PROCEDURES

The following procedures will be reviewed and accomplished as indicated when operating the DMP DJI Inspire 1 orthe Yuneec Q500 for commercial purposes. Operator Training

The pilot in command must have a minimum ofthree flights inthe month prior to any commercial shoot. Ifcommercial flights have not been accomplished, training flights will be scheduled. Training flights will include: takeoffand landing procedures, GPS assisted flight, loss ofGPS signals to a safe recovery, loss ofvideo to a safe recovery and camera operation without the use ofa visual observer. (i.e. the PIC is also the visual observer) All training flights will be documented in the pilot's training folder with any deficiencies noted and retraining required. Preflight Procedures

The day prior to the commercial flight:

_ Review the proposed commercial contract requirements to insure they are compatible with the aircraft capability, FAA Conditions and Limitations inthe FAA Section 333 Exemption. _Checkthe NOT AMS for TFR's or otherrestrictions that might impact the scheduled flight. _Checkthe forecast weather for the area ofthe proposed flight to make a preliminary assessment as to whether the flight is feasible. (this does NOT suffice for the weather checkmade the day ofthe flight) _Visitthe proposed site ofthe shoot and walkthe area. Look for the best takeoff/landing area, wires, buildings, trees, cell phone towers and bird concentrations which might affect the flight and adjust the planned flight path ifnecessary. Notify any private land owners that might be close to the flight orwhich might have to be overflown and obtain theirpermission for the flight. --Notify any agency for which a Letter ofAgreement (LOA) has been negotiated regarding any flight within their area ofoperation and obtain their approval for the flight. Ifdirect contact is required during the flight, the appropriate procedures will be agreed upon. LOA's will be established with the Ogden Airport (KOGD) tower, the Life Flight Medical helicopter operation at McKay-Dee Hospital and the University ofUtah, Air Medhelicopter operation at Ogden Regional Hospital. Special attention will be given to the standard arrival and departure procedures used by the medical helicopters.

1The day ofthe commercial flight: _Recheckthe NOTAMS for possible changes. Obtainthe current and forecast weather for the time ofthe flight ---Review the aircraft maintenance records to insure all scheduled maintenance actions have been accomplished. _Make a handheld anemometerreading at the site to insure the winds are within limits and to make a decision onthe optimal flight length depending on the wind direction. _Walkthejob site again to insure nothing has changed from the walk around accomplished the day priorto the flight. _Markthe takeoffand landing area and insure it is kept clear ofanyone other than the PIC and the visual observer (ifone is used}. Use the DMP vest to make bystanders aware that the pilot is operating an sUAS and should notbe disturbed while flying. _Notify any agency for which LOA procedures have been established ofthe takeoff /landing times andproposed flight path/altitude. _Accomplish the aircraft preflight detailed in the UserManual and checklists for either the DJI Inspire 1 or Yuneec Q500, depending on which is beingused for the flight. Particular attention will be given to insure the aircraft and controllerbatteries are 100% chargedbefore takeoff. _Activate the aircraft camera one time to insure the camera is working properly and an image is recorded prior to takeoff. Flight Procedures Commercial flights will be flown ONLY in the GPS mode. Ifthere are insufficient GPS satellites to fly in GPS mode, the commercial flight will notbe attempted.

_ Accomplish a Compass Calibrationpriorto takeoff. _Takeoffandplace the aircraft in a stable hover, 6-10 feet AGL to verify stability and the proper operation ofthe controls before proceeding onthe planned flight path. Ifthe aircraft is not stable inhover, the aircraft willbe landed immediately and the flight aborted. _Climb to the planned altitude for the flight as soon as practical to minimize noise and to obtain a safe operating altitude.

2

### _Maintain visual line ofsight ofthe sUAS at all times, to include aircraft orientation. Do NOT rely onthe visual display on the tablet oriPhone app for maintaining visual contact and orientation.

_Monitorthe aircraft battery status as shown on the controller display continually. The controller will be set to warn when 25% battery remains, but a earlier recovery may be needed ifthe flight has to return with any significant headwind component. _Ifvisual orientation ofthe aircraft is lost, the Return to Home (R TH) feature will be activated. When visual acquisition and orientation is regained, the flight may be continued on GPS mode ifsufficient battery powerremains. Ifvideo to the controller is lost, the RTH feature will also be activated until regaining the video feed. _Land immediately, in a safe area, ifthe aircraft appears to be unstable. _Return to the planned landing area ifanyone in authority questions the operation. After landing, any potential issues will be discussed and settled before proceeding with the planned shoot. _Descents to landing will NOT be done at the maximum rate ofdescent for the vehicle and the descent flight path will NOT be directly vertical in order to minimize potential Vortex Ring State (VRS) problems. _Accomplish the aircraft postflightprocedures detailed in the respective User Manual after landing. Any discrepancies or abnormal performance ofthe aircraft, controller orbatteries should be noted in both the flight log and maintenance records. _Contact any agency that was notified ofthe flight under LOA procedures to inform them that the flight is complete. Maintenance Procedures

All maintenance procedures will be in accordance with the respective Maintenance Manuals for each type aircraft. All inspections, procedures and work accomplished will be documented in the aircraft maintenance records. Particular attention will be paid to the proper calibration, charging, discharging and inspection ofthe LiPo batteries, to include recording all actions in the battery log for each individual battery.

All LiPo batteries will be charged in a sterile, safe environmentusing a fire proof LiPo bags. Batteries will be transported in a safe carrying case for each aircraft. If transporting the batteries on a commercial airline flight, the terminal will be taped, the batteries discharged to less than 50% capacity and all DOT regulations will be followed. A LiPo battery which "swells" or leaks will NOT be used and will be disposed of according to current EPA guidelines.



### 3

### Aircraft propellers will be balancedprior to their initial use on the aircraft using a DuBro balancer. If

### post flight inspection reveals chips or cracks on any propeller, it will discarded and notbe mounted on the aircraft.

Any substantial damage to the airframe or failure ofthe either the aircraft systems or controller will require returning the sUAS to the original aircraft manufacturer, or a manufacturer certifiedrepair station, for service. DMP is not a qualified repair facility forsUAS's. Record Keeping

The following records will be kept by DMP. (* indicates the record will be kept at the job site and be available to the PIC): 1. Pilot FlightLog. Includes flight times for individual flights, cumulative flight time, type ofsUAS flown, and training accomplished. 2. Visual Observer Log. Will document training received to qualify an individual as a visual observer with emphasis on proper recognition ofthe sUAS's light signals for orientationpurposes. Each individual flight that used a separate visual observer will be logged. 3. Aircraft Flight Logs. Flight ldata/logs for the DJI Inspire 1will be downloaded from the iOS Pilot App after each flight and will be kept in a separate binder for minimum ofone year. Flight data for the Yuneec Q500 will be entered manually in the aircraft log bookby the PIC after each flight and cumulative information will be kept regarding airframe, motor, and battery use. At some point, a Flytrex Live 3G data logger may be installed on the Yuneec Q500 which will provide the same type offlight data the DJI Inspire 1now provides through the PilotApp. When that occurs, the manual flight logging for the Yuneec Q500 will be discontinued. Flight logs will be kept a minimum ofone year and a record ofthe cumulative data will be kept for the life ofeach sUAS. 3. *Airframe Maintenance Records. Will include current status ofall firmware, aircraft inspections, aircraft maintenance accomplished, controller maintenance, and battery maintenance. All Functional Check Flights (FCF's) done as a result ofaircraft maintenance will also be documented and proper operation ofthe sUAS will be signed offprior to using the sUAS for commercial purposes. Each sUAS operated by DMP will have a separate maintenance record. 4. Contracts/Agreements for each commercial shoot completedby DMP to include flight path requirements, private property overflight notifications (ifrequired) and model releases (ifrequired) will be kept in a separate binder and in a backed up computer file.

4Additionally, the aircraft user manuals for the type sUAS used for a commercial flight will be available at the ground site, as will the aircraft registration and a copy ofthe FAA Section 333 Exemption.



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1. Check tiW battery for damage and delormiliu. If

there are any signs of damage 1o the battery, stop using it and disctwge lh6 battery 1o 10% or below for cispossl. Do not disassemble the battery for any

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erasar if any residue is observed. This will hfilp to ensure a ITIOI'a reliable connaclion. 3. Check the metal battery power connectors lor

damage. If the coonectors app8llf bum!, try lo cteer them. This can be done by inserting a piece of sandpaper (1mm thick) inio the conneciDrs 1o polish the metal. 4. Check the conlad pins in the bail&ry c:ornpartrnenl 1o

ensure lhai tiW pins are clear. They shoold be able to establish easy COi'1lt!!ct with lh6 battery connectors and shouldnotbebflllt. 5. Check !he elllC!rOO&s on !he battery. If they**~**

bumt, polish them wilh sandpaper. 11 there is serious 8f06ioo, sendthe ballary in for repai's. 6. Check the plastic**~** of the loailefy bracket

to see it is in good conditioo and !hat all screws are secure. This prewnts the battery from becoming loose duringfit1ll 7. Check !he power cables between the arms and the

center pla!e, if lh6 cables are worn, contact DJI to arrange ll!palrs. 8. For long term Sltlrage, please raiar to !he "Intelligent

Flight Battery Safety Guidelines• and check the battery once a l1'llll1th ID pi'ffll!lflt the bailery caR from being darnsged. 9. Run the DJI Pilot App to confirm that all battery cells

IVI'I ai simii!IYvoliage levels and stayailhlilsame 181181 when the !laitely is fully charged. If all cells maintain voltage IIM!Is above 3.7V bti any eel is 0.2V higher or 11Ji1118flhan the olhers, CCIIltact OJI lor analysis. You can also checkthe baltay cell warning hisiory. Ifany warning are 1'8pClfted, conlad DJI.**Ill.©~~~~** 1. Check the S8fiiOI110IDr cmles lorwear. Also confirm

11181the conneclion points arestill in good condition. 2. Check the lead screws and contact DJI Support

to arrange repairs if any bending or damage is discol!ered. Clean the lead SCil.'IIIIIS with INI).40spray if theyshow**~s** of rust 3. Ustan to the SIIMlfi10iors during !he lransformaiioo,

if there is abnormal noise, it may indicate thai the SMIIllliOiorsworn. 4. After the landing gMr rises, check the lead screws

and bearings. If any dirt or dust is fould, clean md IJI8&SEI thebearings. 5. Check the lead screws. If there is any scrslches,

dents, or plastic particles undemealh them, CCJI'rtact DJI Supporttol!rfli'I"ISl8 repairs.

1. Confirm that all the screws are still adequately

lighlened. 2. Check the aircraft for braaks or damage. If there is M'Jreason to beli8'11& 11181 cletectsiole damage might a11act flight safety,consul! with DJI Support. 3. Checkthecaroon lubesof !hearmsfor damage. 4. Checkthe olarr!pers on the lmc:ling gears. Ifthey sre

loose, secure themwith 502gluB. 5. Ensure lhai there sre no olosial::lils on or around the

GPS module or aroond !heantennas on the landing gear.**Re~T~C~~e** any obstacles (such u tapes with conduclive material) thai might affllC! or block the signal. 6. Checkthaithe right md left landrng gear res! ai the

sametill angle.

C 2015 OJL All Righls RIIOleM!d. i1. Check the rotors to confirm that they have not become k:x:!Sa. 2. Datach the propellers and start the motors. Listen

c!l.fefully. If there is any abnormal noise, please replace the motors. This may be a sign that the bearings havebeenworn out. 3. Detach the propellers and start lhe moklrs. Carefully

tro)ffline the edge of !he roior and confirm thai the shaft is perfectly centered on the motor. Check for any abnormal or excessive vibration. If any problems 8ffldetected, contacl DJI Supportloorder replacementmotors. 4. Check for deformities by confirming that the gap

between the motor and motor base is even. If not contacl DJI Support toorder replacement motors. 5. Ensure that the screws used to secure the motor

base are tight and the plaslic components aroond the motors are in good condition. If not please tighten lhe screws and contact DJI to repair any broken plasliccomponents.

1. Check the propellers. If there is any banding,

I:.Jreakage orcracking on a propellar, donot use it 2. Aliach lila propeller lothe motor, tum on lila aircraft, and place iton the gromd. Stand 1 meter 8fNa'1 from the aircraft and obsaMtthe rotating propellers. If you can sea two distinct propeller outline layers, when looking at a spinning propeller from the side, this propeller is damagedand should not beused.**m.~illlll!lliJ!J** 1. Open DJI Pilotappto checkthe condilion ofthe IMU

and perform an advanced IMU calibration. Please place the aircraft in a cool environment and on a flat, stable surlace (if the landing gear is damaged, support the aircraft with four objects of equal heigttt). Do not touch thecraft dulingthe calibmlion. 2. Tum on the aircraft and listen for any abnormal noise

or vibration from the fan located on the front of the aircraft. If any irregularity is d8tactad, replace the fm.

1. Checkthe4 antennas onthe landing geartoensure

that they are secure. Also check for any benamg or damage. 2. Check the antennas of the remote controller for

damage 3. Checkthe neckstrap for damage orwear, replace

if necessary. 1. The quick-mount connector for the camera is a particularly vulnerable component. If the gimbal fails lo initialize when turned on, fails lo work after initialization, or fails to transmit video to the app (while OSD data is displayed), the quick-mount connector may be worn. In this case, replace lila rubber mat, circuit board, and/or connactoron the gimbal qtliek-moont 2. Check the metal contacts on the quick mount

connector board, if any contact is bent, replace lhe quick-mount connector. 3. Check the contact pins on the quick-mount

connector board, if there is any dirt, rub it clean with an eraser. If any contact pins are worn rut it should bereplaced. 4. Confirm thai the gimbal is abl& 1o jiJ£(Ipllffy stabiriZe itself. If ils stabilizing performance deteriorates, contact DJIID arrange repairs. 5. Listen fur any abnormal noise from the fan when

the gimbal is hmed on. This may indicate unusu!ll vibration and the fan should bereplaced.

1. Check the lens of the camera. If any dirt Of resiWa

is detected, gently clean the lens. 2. Check for and fiJITlDI!8 objects thai might block the

sensors. 3. Ensurethat the V.sion Positioning System is securely installed on the aircraft. 4. Detach lila propellers and tum on lhe aircralt. Hold

the aircraft 1·2 meters above a surface with rich patterns. under good lighting conditions. Change the Flight Mode switch to P Mode on lhe controller and check the DJI Pilot app. If the app displays m altitude value and indicates that P-OPTI mode is active, the VISion Positioning System should function normally.**$M~~~In1o:** 

### http://WWW.dji.com/support

The conten1 is subject lochange.**~tlial~~tmm iri!ip~.~~~** 

@ 2015 OJI. All Righls Rassr.oed.**~**

# INTELLIGENT FLIGHT BATTERY Safety Guidelines

(V1.0) 2014.12o Do not leave the battery near heat sources such as a furnace or heater. Donot leave the batteries inside of the vehicle on hot days. The ideal storage temperature is 22"C-28"C.

o Keep the battery dry. Never drop the battery into

water.

e Do not drop, strike, impale, or manually shortcircuitthe battery.

o Keep the battery away from metal objects such

as necklaces and hairpins.

o Discharge the battery to 30%-50% ofthe battery

level if it will not be used for 7 days or rrx:Jre. This can greatly extend the battery life.

o Battery discharges automatically to below 65%

when it is idle for more than 10 days to prevent the batteryfrom swelling. Ittakes around 2 days to discharge the battery to 65%, It is normal that you may feel moderate heat emits from the battery during the discharge process. Set the discharging thresholds in the OJI Pilot app.
o The battery will enter hibernation mode if

depleted and stored for a long period. When in hibernation mode, if you try to power on the battery, the battery power LED will show a solid red light and the battery level LEOs will all be off. You cannot manually turn off the battery power LED in this state. Leave the battery unattended for 5 minutes, and then it will power off. Recharge the battery to bring it out of hibernation.

o Remove batteries from the aircraft when stored

for an extended period. Battery Disposal

o Dispose of the battery into specific recycling

boxes only after a complete discharge. Do oot place the battery into regular rubbish bins. Strictly follow your local disposal and recycling regulations of batteries.

o If the power on/off button of the Intelligent Flight

Battery is disabled and the battery cannot be fully discharged, please contact a professional battery disposal/recycling agent for further assistance. Notice
o Before carrying the Intelligent Flight Battery on a

airline flight, it must first be fully discharged. This can be done by using it in your Inspire 1 or by connecting your remote controller to the battery using the Remote Controller Charging Cable. Only dischargethe battery in afireproof location. o Store Intelligent Flight Batteries in a ventilated location.

o Should you require to carry the battery onto the

plane, it is recommend to discharge the battery to the range between 10% and 20% in order to ensure the safety ofthe battery.

## l_l

--



# Gl5CC TYPHCCn

- INSTRUCTION MANUALVersion 2.1

# YUnc.c.~ ELECTRIC AVIATION

### SPECIFICATIONS Q500 Height 210mm {8.3 in) Length (without rotor blades): 420mm (16.5 in) Width {without rotor blades): 420mm (16.5 in) Diameter (without rotor blades): 565mm {22.2 in) Propeller/Rotor Blade Diameter: 330mm (13.0 in) Weight (without battery and payload): 1130g (40.0 oz) Takeoff Weight (with battery and CG02-GB): 1700g {60.0oz) Battery: 5400mAh 35 11.1V LiPo (included) Charger: DC 3S 11.1 V LiPo balancing and AC adapter (included) Transmitter: ST10 to-channel 2.4GHz with 5.8GHz video link (included) FlightTime: 2Q-25 minutes CG02·GB Height 115mm (4.5 in) Width: 75mm {2.9 in) Depth: 135mm {1.4 in) Weight 185g{6.5 oz) Video Resolution: 1080p 60. 50 or48fps Photo Resolution: 12 megapixels Transmission Distance/Range: Up to 600m (1970 ft) dependingon receiving device Transmission Band: 5.8GHz Storage (memory): mi<:roSD Class 10 up to 128GB 

### suo Numberof Channels: 10 RC Band: 2.4GHz RC Modulation: Yuneec Video Downlink Band: 5.8GHz Telemetry/OSD: Yes SD Card Compatible: Yes LCD Screen Size: 4.5" Touchscreen: Yes

### Conduct mission**planning~** 

### weather**check~** 

### airspace check ofarea of**operations~** 

### COA current as needed, ATC notified if**necessary~** 

### no tam issued as required, observerbriefing oonductcd, notice to non-participating persons completed 

### 24 hours**prior~** 

### QSOO TIM, Quick Start guide appropriate docs onhand.

Motor Support structure-- LED Covers-- Motors-- Rotor Blade mounts/drive shaft threads-- 0-R.ings--

Rotor Blades/props--

Install Rotor Blades--

Landing Gear--

Battery Compartment--

Camera/Gimbal-- Check Condition and security. Check Condition and security. Check Condition and security. Check ordamage, Free ofgalling, clean as necessary. Check**condition~** 

### security replace as needed. Check**condition~** 

### no nicks OK' 

### damage, iffound markblades and discard, clean as necessary, check threads. Checkproperly seated, motor and blades tum 

### freely, nobinding or grinding. Check condition and security, no cracks OK' 

### damage. Condition and security. Checkbattery compartment door for oondition and security, opens and latches properly. Remove Cameracover, check oondition and security ofgimbal mount attachment points and connecting plugs-insert SD card.Compass Calibration--

Condition--

Charge level Install battery--
Battery compartment door--

Ovcmll Condition--

Checkbattery--

Position Aircmft for flight--

Blade Covers-- §TlO-- QSOO--

Observe--

CheckDisplay-- Check andpcrfom1 as necessary.

Visually inspect, casing for cracks,**~welling** orbulging condition of**£Qn~.** Iffound orquestionableDo not uscbattery. Check fully charged. Insure battery installedinbattery £2mnartment. contacts seated. Door shut and secure.

Check, control positions. switch £Qndition, check display screen £Qndition, clean as necessary. Condition and security. oompartment closed and**s~me~** Check fully charged.

Position at safe distance perQSOO TIM/Quick start Guide. Removed and stored.

Power switch on after, §TlO Initialized. Display, QSOO LED status indications, solid illumination. solid as per flight mode. (Green), §mart mode, (Purple) Angle mode. GPS- Satellites, §TlO at least 6.Cycle Camera Gimbal §lider--

Position Proportional Control Sider-- CheckControl Position--

Pilot/Observer--

§tart §witch--

Clcrur Area Check--

LED §tams--

§TlO-- Acquired, QSOO at least 6 Acquired Gl?§-Indicatcs (ready), Check all Warning, alerts out, Camera Connected, telemetry displayed, altitude, distant, groundspeed displayed appropriately. Status ready, Mode displayed according to mode switchposition. Observe for proper camera mOV§!ment.

Yaw, Power and Pitch and RollCentered. Attach strap, place inposition on Pilot

Obtain/maintain a safe distance From aircraft Visually check Clear**are~** verbally announce-Clear for**cngin~** start Engage start switch for 3 seconds Observe for smooth operation, simultaneous blade movement, all blades at idle rpm.

Pilot and observer conduct area Visual area check, free ofobstacles in intended flight path,**£Qmmuni~atc** all clear. No warnings, solid LED. 2 white 2 rod center, solid green orpurple**~cr** mode selected. GP§ 

### 12£.. GP§ ready, atleast 6 satellites acquired camera record**~necessary,** altitude,Power--

Mission--

Check Landing zone
Pic/Observer

Maneuver Land

Power lever--

QSOO Power Switch-- STlO-- gmundspeed, distant indicating with-in appropriatetolerances, 0-15, ngwarnings indicated

Smoothly increase until clear of Surface and 3 foot hover is Obtained, observe position stabili!)!, yaw, pitch androll Control-- normal- continue mission. nftmibJHlll1lJI1'll!Oltmll- reduce power and land, shut down motors. Checkparameters, stability and**~ntrol** ifnormal continue, 

### ifnot a:Qort mission.

CleaJr, free ofpersons, slope and**Qb~tacles.** Communicate, verbally announce landing zone cleaT. As necessary. Adjustcontrol as necessary for smooth landing.

Maintainpowerlever centered and 

### full down. Press and hold red start switch_. 3 seconds oruntil motors shut off. Off Off

### Propellers-- Landing Gear-- Airframe-- Battery-- Check for Excessive heat Check security? general condition and cleanliness Check security? general condition General condition Remove battery? check condition? excessive heatUA§ does notRespond appropriately

Indicated by vibration in §T10 and LED Orange**flash~** GP§ on display reads disabled.

Ifpotential hazard or conflictexists Mode switchto Home-- Ifrecovery made attempt noxmal control again ifcontrollill®ll'lmlla!!RContinuewithmission or abort and investigate cause. If**liD®~** li1l®ll'!illlla!!R-Mo9£ switch tQ Homea**cl~** landing area. Ifrecovery notmade-- Shut**offSTlO~** QSOO should rerum to take offsite. Clear Landing area. Ifstill no**response~** attempt to clear path and shut off Motors when over clear area.
Mode switchto §mart follow Qn(cn arrow on**dis,Rla~** to**rocov~r** until**Qri~nmtign rogainc~**  iflll!l!lli!!lbllle**~® ~~®V<ell"-**  Mode Switch to**Hom~~ Cle~**  Landingarea.

Land**ASAP~** Shutdown motors

Abort**mission~** land Immediately. Abort mission. land ASAP.

### Alii 

### m.mnntel!llanm will

### bepedol!"med il!llac«:cJrda\llll«:te withthe mmufutemrerlll reqmrem.el!llts, sme-oper.mting p:r.m«:tices 2l!lldlpe:ri.the ope:r.mm:r"s mamterum.ce proaedure§ as 

### de§aibedheJrem. TheMrcrnftleg §beetwill

### be dosedmid .mnewleg sheetateaJ.ttedaflte:r '1 

### d.mys el!llding at2400

### hours ol!ll 5lU!i1d.myol!ll a weeklyb.msis.**PK'~flight**

### Jil!llspectiol!ll perthe cperntro:r"§ «:hecklblstrequiredbefore eachfliglhltt. 

### The opernrorrequires aiD! 

### mspteOOCl!ll signoff; Ol!llCe dayOl!ll the daythatii:he aJ.ircrnft fts 

### illllttended m beflown prior

## mflight. 

### Discrepancies and deficiencies will

### benetted in the aircraftlogbook 

### mindude

### an Ittem li1Umbter, Datte andtime, Disterepancy, Pernolllls lil.mme alllld Certificate l!llumber. The mcraftwilllilctbe 

### ftcWllll Uli'!til

### the Disaepancyis oorrecttedand signed offby \the cpernmror**aru\thmi~ed** 

### rnpm

### perool!ll,**H~g**

### the Item number, Date amd Time, the «:orrective actiollllt.mllreJm alllld\the persol!ll's sipamreperformingi.tlhle corrective act:itDn. AlUI alilliiralmi!!, groundsmtiollll mdcomponeJmtlittems areperthe mmmacturer, onoonditi«m allmdtimelimits will

### be set.ms the l!llll!eded. As

### prevel!lltative malil!lltenmce the**~DpterntoJr**

### elects m time limitpropeller0-rililgs

## oo**a~** 

### ma.Jdmum of4 calendarwetelks ofinstallation. 0-rmgswmberemoved andreplaced atthattime interwll!llll' upl!lln cl!llntd!iti.Otn wii.tlhl an teitjjuiwllentorhlgher ltjjUalllty

### 0-ring tlhtam 

### thatoopplfted !by

### the mmurlactuwer

. .AJill fmu 

### 0-rings will bereplaced anytime a repli.mcement is

### pedol!"med. Alm 

### alpprOtpriate entrywlillbe made nl!llttlillllgtheflight

### time sililcelalStchangeaJ.Jmdi.tlhle installattli@n datemdtime. Weekly.beginniiDlg atthestartoifa newweekthe pmptellller shaftthreads will**ha~ve** 

### a smalll amo'!.ID.t @fanttli-seill::e appliedto the p!mpelllerh1lllb threads 

### ro preventgrullmg allmd pr(Qlptelllerseimlre. Propellerswill beiiDlstalled !by

### mmiiDlgi.the propellerin theproperdirection until**~is** 

### madewiththe 0-rililg, ii:hen l!llne full mda half

### rum winl be made m properlyseatthepr@pelllers ontb.e shaft. 1'lbJ.M; 

### is perthe mmufucmrers rec(QlmmendaJ.tiom.