July 6, 2015 Docket Operations, M-30 U.S. Department ofTransportation (DOT) DocketManagement System 1200 NewJersey Ave., SE Room W12-140, WestBuilding Ground Floor Washington, DC 20590-0001
Dear Sir or Madam: 

### Page 

## 11

Attached please find Photographic Solutions, Inc. (Photographic Solutions) request, as a member ofthe Professional Aerial Photographers Association, International (PAPA), for an exemption from the listed Federal Aviation Regulations to allow commercial operation of its Small Unmanned Aircraft Systems ("sUAS") for aerial imaging to include video and still photography. This exemption request is initially for the use ofthe Phantom II sUAS manufactured byDJI, an established sUAS company and in accordance with the sUAS training and certification program as administered by PAPA Also attached to this letter is the equipment "Photographic Solutions Flight Manual" (Manual), which outlines the operating requirements, limitations, and technical specifications for the DJI System as used by Photographic Solutions. Photographic Solutions has reviewed this Manual and has found it to be acceptable for sUAS operations. Applicant submits this manual as a Confidential document under 14 CFR 11.35 (b) as the entire Manual contains proprietary information that the applicant has not and will not share with others. The Manual contains operating conditions and procedures that are not available to the public and are protected from release underthe Freedom ofInformationAct 5 USC 552 et. seq. Thank you for yourtime and consideration, and please let me know ifyou have any questions.

Stan Macbean AllenMacbean Photographic Solutions Corporate Officers


### ProfessionalAerialPhotographers Association-InternationalSection333 Doc 15-001July 6, 2015 Docket Operations, M-30 U.S. Department ofTransportation (DOT) DocketManagement System 1200 NewJersey Ave., SE Room W12-140, WestBuilding Ground Floor Washington, DC 20590-0001 

### Pagel2

Re: Exemption Request Section 333 ofthe FAA Reform Act and Part 11 ofthe Federal Aviation Regulations from 14 CFR 61.113 (a) & (b); 91.103(b); 91.119;91.121; 9.151(a); 91.405 (a) (1); 91.409 (a) (2); 91.417 (a) & (b). Dear Sir or Madam: Pursuant to Section 333 ofthe FAA Modernization and Reform Act of2012 (the Reform Act) and 14 C.F.R. Part 11, Photographic Solutions Inc. (Photographic Solutions), an aerial photography and digital imaging company, on behalf of itself and its related affiliates under common ownership and control, hereby applies for an exemption from the listed Federal Aviation Regulations ("FARs") to allow commercial operation ofits Small Unmanned Aircraft Systems ("sUAS") for aerial imaging for video and still photography, so long as such operations are conducted within and under the conditions outlined herein or as may be established by the FAA as requiredby Section 333. As detailed in this document and the attached

**Fli~ht** Manual, the requested exemption would pennit the operation of sUAS under controlled conditions in airspace that is 1) limited 2) predetermined 3) controlled as to access and 4) would provide safety enhancements to the already best practices safety protocols followed by Photographic Solutions during aerial photography operations in accordance with the training and certification provided by the Professional Aerial Photographers Association, International (PAPA). Photographic Solutions is a member ofthe Professional Aerial Photographers Association-International (PAPA) and has a demonstrated record of safe operations in the National Airspace System (NAS). Principal employees have received ground school training and have logged well over 25 hours of sUAS flight operations. The Pilot/s In Command (PIC) proposed by Photographic Solutions are both FAA licensed pilots with years ofsafe and successful aerial photography operations. Approval ofthis exemption would thereby enhance safety and fultill the Secretary ofTransportation's (the FAA Administrator's) responsibilities to "
...establish requirements for the safe operation ofsuch aircraft systems in theNational Airspace System." Section 333(c) ofthe Reform Act.



### ProfessionalAerialPhotographersAssociation-InternationalSection333 Doc 15-001The name and address ofthe applicant is: Photographic Solutions, Inc. 1347N. State Street Orem, UT 84057 PIC-StanMacbean, FAA LicensedPilot (Commercial) PIC-AllenMacbean, FAALicensedPilot (Commercial) PH: 801-224-6446 Email: info@utahbyair.com Regulations from whichthe exemption is requested: 14 C.P.R. Part21


## . . .. ' 14 C.P.R. 45.23(b) 14 C.P.R. 61.113 (a) & (b) 14 C.P.R. 91.7 (a) 14 C.P.R. 91.9 (b) (2) 14 C.P.R. 91.103 14 C.P.R. 109 14 C.P.R. 119 14 C.P.R. 121 14 C.P.R. 91.151 (a) 14 C.P.R. 91.203 (a) & (b) 14 C.P.R. 91.405 (a) 14 C.P.R. 407 (a) (1) 14 C.P.R. 409 (a) (2) 14 C.P.R. 417 (a) & (b)
L STATUTORYAUTHORITYFOREXEMPTIONS 

### Page 

## 13

The Federal Aviation Act expressly grants the FAA authority to issue exemptions. This statutory authority includes exempting civil aircraft, as the term is defined under §40101 of the Act, including sUASs, from the requirement that all civil aircraft must have a current airworthiness certificate. The Administrator may grant an exemption from a requirement ofa regulation prescribed under subsection (a) or (b) ofthis section or any sections 44702-44716 ofthis title ifthe Administrator finds the exemption in the public interest. 49 U.S.C. §44701(f) See also 49 US.C §44711(a); 49 USC §44704; [4 CFR §91.203(a) (1). Section 333(b) of the Reform Act assists the Secretary in determining whether sUAS may operate in the National Airspace System (NAS) without creating a hazard to the user, the public, or a threatto national security. In makingthis determination, the Secretary must consider:
• The sUAS's size, weight, speed, and operational capability; 

### Professional AerialPhotographers Association-InternationalSection333 Doc 15-001

### Page 

## 14

• Whetherthe sUAS operates within the visual line ofsight ofthe operator • Whetherthe sUAS operates outside ofhighly populated areas and away from close proximity to airports Reform Act §333(a). Ifthe Secretary determines that a sUAS "may operate safely in the national airspace system, the Secretary shall establish requirements for the safe operation ofsuch aircraft in the national airspace system." Id. §333(c) Photographic Solutions' sUAS are multirotor vehicles, weighing 20 or fewer lbs. including payload. They operate under normal conditions at a speed ofno more than 70 knots and have the capability to hover, and move in the vertical and horizontal plane simultaneously. The sUAS will operate only in the Pilot's visual line of sight at all times and will operate only within the controlled "Area of Operations" described in the Confidential Photographic Solutions Flight Manual (Manual), attached as Exhibit 1 (hereinafter "Manual"). Such operations will ensure that the sUAS will "not create a hazard to users of the National Airspace System or the public." Reform Act Section 333 (b). Given the small size ofthe sUAS involved and the restricted and controlled environment within which they will operate, our application falls squarely within the zone of safety (an equivalent level of safety) in which Congress envisioned that the FAA must, by exemption, allow commercial operations of sUAS to commence immediately. Also, due to the small size ofthe sUAS, altitudes, and controlled areas in which the sUAS will operate, approval ofthe application presents no national security issue. Given the clear direction in Section 333 ofthe Reform Act, the authority contained inthe Federal Aviation Act, as amended; the strong equivalent level of safety surrounding the proposed operations, and the significant public benefit, including enhanced safety, the grant of the requested exemptions is in the public interest. Accordingly, Photographic Solutions respectfully requests that the FAA grantthe requested exemption without delay.
II. PUBLIC INTEREST This exemption application is expressly submitted to fulfill Congress' goal in passing Section 333(a) through (c) of the Reform Act. This law directs the Secretary of Transportation to consider whether certain unmanned aircraft systems may operate safely in the NAS before completion ofthe rulemaking required under Section 332 ofthe Reform Act. By granting an exemption the FAA will fulfill Congress's intent of allowing UAS to operate with significant safety precautions in low risk environments. The use. of sUAS on aerial photography operations can significantly reduce the risk to photographers and participants. sUAS can inspect, photograph, and collect data on hard to get to areas that otherwise would require direct access or manned aircraft. Additionally, sUAS could replace the use ofhelicopters and small aircraft to produce imagery for various purposes. The sUAS we propose to fly in this application are less than 20 pounds, Professional AerialPhotographersAssociation-InternationalSection333 Doc 15-001

### PagelS and carry no combustible material on board, as opposed to the much larger conventionally powered small aircraft. Shifting to sUAS from manned aircraft presents a marked safety increase for our workers andthe public. Lastly, sUAS reduce the environmental impact by dramatically decreasing the energy used for aerial imaging and data collection. The sUAS used by Photographic Solutions use rechargeable lithium ion batteries, as opposed to fossil fuels burned in operation of small aircraft that are many hundreds oftimes heavier. lll. EQUIVALENT LEVEL OF SAFETYAND SECURITY Photographic Solutions proposes that the exemption requested herein apply to sUAS that have the characteristics and that operate with the limitations listed herein. These limitations provide for at least an equivalent or even higher level ofsafety to operations under the current regulatory structure because the proposed operations represent a safety enhancement to the already safe protocols followed on imaging and photography operations conducted with conventional aircraft. Photographic Solutions will be bound by the following limitations when conducting its sUAS operations under anFAA issued exemption: 1. The sUAS will be less than 20 pounds. 2. Flights will be operated within visual line ofsight ofa pilot. 3. Maximumtotal

**fli~ht** time for each operational

**fli~ht** will he 20 minutes. The operator calculates battery reserve, and will returnthe sUAS to the "Designated Safety Zone" with at least 20% battery powerreserve should that occur priorto the 20 minute limit. 4. Flights will normallybe operated at an altitude ofnot more than 400 feet AGL, but never in controlled airspace without prior coordination and approval ofATC. 5. Flights will not be conducted within the surface area ofcontrolled airport airspace without prior coordination and approval ofATC. 6. Flights will not be conducted within 5 miles ofany uncontrolled airport withoutprior coordination and approval ofthe airport authority. 7. Crew for each operation will consist ofthe sUAS Operator who will keep the sUAS within his visual line ofsight at all times and a qualified Observer. 8. The sUAS operator will betrained inflight, operations, and safety procedures as detailed in the FlightManual. 9. The sUAS will only operate within a confined "Area ofOperations" as defined in the Manual, includingbutnot limited to evaluation ofthe airspace byreference to a current 1:500,000 scale FAA Sectional Aeronautical Chart. The Manual also requires the establishment ofa "Designated Safety Zone" for the flight operations area. 10. A briefing will be conducted regarding the planned sUAS operations prior to each day's production activities. Itwill be mandatory that all personnel who will be performing duties within the boundaries ofthe Designated SafetyZone be present for this briefing. 11. All onsite personnel will consent to the UAS flyover on site bywaiver, and the Operatorwill obtain additional verbal or written consent ofall persons who will be allowed within 100 feet ofthe flight operation.


### Professional AerialPhotographers Association-InternationalSection333 Doc 15-001

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## 16 12. Operator will have beentrained in operation ofUAS generally and will have received up-todate information onthe particular sUAS to be operated as requiredbythe Photographic Solutions Manual. 13. Necessary written and/or oral permission from the relevant propertyholders will be obtained. 14. All required permissions andpermits will be obtained from territorial, state, country, or city jurisdictions, including local law enforcement, fire, or other appropriate government agencies. 15. Ifthe sUAS loses communications or loses its GPS signal, itwill have the capability to enter "loitermode'' and hover, reestablish satellite connection, and return to a predetermined location within the "Designated Safety Zone" and land. 16. Photographic Solutions personnel will be easily identifiedby law enforcementpersonnel and the Public through wearing a green fluorescent orblaze orange vestwith Section 333 Grant and PAPA credentials prominently displayed within a weatherproofcontainer onthe persons back. IV. DESCRIPTION OF SPECIFIC REGULATIONS 14 CFR61.113 (a) & (b): Private pilot privileges and limitations: Pilot in command Sections 61.113 (a) & (b) limit private pilots to non-commercial operations. Because the sUAS will not carry a pilot or passengers, the proposed operations can achieve the equivalent level of safety ofcurrent operations by requiring the Operator operating the aircraft to have completed a sUAS flight training course of25 hours before flying a sUAS (See the Photographic Solutions Manual for details) or meeting any FAA pilot licensing requirement. Unlike a conventional aircraft that carries the pilot and passengers, the sUAS is remotely controlled with no living thing or cargo on board. Tli'e area of operation is controlled and restricted per prior planning and necessary coordination with the local FSDO if applicable, and all flights are planned and coordinated in advance as set forth inthe Photographic Solutions Manual. The sUAS to be operated hereunder is less than 20 lbs. fully loaded, carries neither a pilot nor passenger, carries no explosive materials or flammable liquid fuels, and operates exclusively within a controlled Area of Operation as set out in the Photographic Solutions Manual. Like other civil aircraft, operations under this exemption will be tightly controlled and monitored by the Operator, pursuant to the Photographic Solutions Manual requirements, and under the requirements and in compliance with local public safety requirements, to provide security for the Area of Operation as is currently done on aerial photography operations. The FAA will have advance notice ofall operations as required. The risks associated with the operation ofthe sUAS are therefore diminished from the level of risk associated with commercial operations contemplated by Part 61 when drafted, and allowing operations ofthe sUAS as requested, with an operator who has met the minimum requirements stated in the Photographic Solutions Manual, achieves the level of safety contemplated by 14 C.F.R. §61.113 (a) & (b).

Professional AerialPhotographers Association-InternationalSection333 Doc 15-001

### Pagel7 14 C.F.R. 91.103: Preflight Action 

### This regulation requires that each Operator in Command take certain actions before flight to ensure the safety offlight. An exemption is needed from this requirement as the Pilot will take separate preflight actions, including checking for weather conditions, checking flight battery requirements, checking takeoff and landing distances, and all other actions in the Preflight Checklist in the Photographic Solutions Manual. These actions will provide an equivalent level ofsafety. 14 C.F. R. 91.119: Minimum/Maximum SafeAltitudes 

### Section 91.119 establishes safe altitudes for operation ofcivil aircraft. Section 91.119 (d) allows helicopters to be operated at less than the minimums prescribed, provided the person operating the helicopter complies with any route or altitudes prescribed for helicopters by the FAA. This exemption is for a multirotor craft that flies similarly to a helicopter, with vertical takeoff and vertical landing, which will typically operate at altitudes ofless than 400 AGL, so an exemption may be needed to allow such operations. The sUAS will never operate at altitudes higher than the base ofcontrolled airspace without prior approval and coordination with ATC and will be in a Controlled Area with a "Designated Safety Zone", where buildings and people will not be exposed to operations without the specified pre-obtained consent. (See Photographic Solutions Manual for detailed procedures.) The equivalent level ofsafety will be achieved

**~iven** 

### the size,

**wei~ht,** 

### speedofthe sUAS as well as the location where it is operated. No flight will be taken withoutthe required permission ofthe property owner or local officials. Because ofthe advance notice to the property owner and any onsite personnel, as outlined in the Photographic Solutions Manual, all affected individuals will be aware of the planned flight operations. Unlike flight operations with aircraft or rotorcraft weighing far more than the maximum 20 lbs. proposed herein, our sUAS will not carry flammable fuel. In addition, the low-altitude operations of the sUAS will ensure separation between sUAS operations and the operations of conventional aircraft that must comply with Section 91.119. 14 C.F.R. 91.121: Altimeter Settings 

### This regulation requires each person operating an aircraft to maintain cruising altitude by reference to an altimeter that is set 11 •••

### to the elevation ofthe departure airport or an appropriate altimeter setting available before departure. 11 

### As the sUAS may not have a barometric altimeter, but instead a GPS altitude read out, an exemption may be needed. An equivalent level ofsafety will be achieved by the operator, pursuant to the Photographic Solutions Manual and Safety Check list, confirming the altitude ofthe launch site shown on the GPS altitude indicator before flight. 14 CFR91.151 (a): Fuel requirements for flight in VFRconditions 

### Section 91.151 (a) outlines fuel requirements for beginning a flight in VFR conditions. Our sUAS is limited to operations in controlled environments as outlined in the Photographic Professional AerialPhotographers Association-InternationalSection333 Doc 15-001

### Page 

## IS Solutions Manual, and has a limited range and flight time which require an exemption from 14 CFR 91.151 (a) The battery powering the sUAS provides approximately 20 minutes ofpowered flight. To meet the 30 minute reserve requirement in 14 CFR §91.151, sUAS flights would necessarily be impossible to conduct. Given the limitations on the sUAS's proposed flight area and the location of its proposed operations within a predetermined area, a shorter time frame (less than 30 minutes) for flight in daylight or night VFR conditions is reasonable. Photographic Solutions believes that an exemption from 14 CFR §91.151(a) falls within the scope of prior exemptions. See Exemption 10673 (allowing Lockheed Martin Corporation to operate without compliance with FAR91.151(a)). Operatingthe small sUAS, in a controlled area where only people and property owners or official representatives who have signed waivers will be allowed, with less than 30 minutes ofreserve fuel, does not engender the type ofrisks that Section 91.151(a) was intended to alleviate given the size and speed ofthe small UAS. An equivalent level ofsafety canbe achieved by limiting flights to 20 minutes, or enough battery reserve to ensure thatthe sUAS lands at the ground station with at least 20% ofbattery power (as determined by the onboard

**monitorin~** system and the operator), whichever happens first. This restriction would be more than adequate to return the sUAS to its planned landing zone from anywhere in its limited operating area. Similar exemptions havebeen granted to other operations, including Exemptions 2689F, 5745, 10673, and 10808. 14 CFR91.405 (a); 407 (a)(1); 409 (a)(2); 417 (a) & (b): Maintenance inspections These regulations require that an aircraft operator or owner "shall have that aircraft inspected as prescribed in the subpart E of this part and shall between required inspections, except as provided in paragraph (c) ofthis section, have discrepancies repaired as prescribed in part 43 of this chapter...," and others shall inspect ormaintainthe aircraft in compliance with Part 43. Given that these sections and Part 43 apply only to aircraft with an airworthiness certificate, these sections will not apply to Photographic Solutions. Maintenance will be accomplished by the operator and pursuant to the flight manual and operating handbook as referenced in the Photographic Solutions Manual. An equivalent level of safety will be achieved because these small sUAS are very limited in size and will carry a small payload and operate only in controlled areas for limited periods oftime. Ifmechanical issues arise, the sUAS can land immediately even ifoperating at a maximum of 1200 feet AGL. As provided in the Photographic Solutions Manual, the operator will ensure that the sUAS is in working order prior to initiating flight, perform required maintenance, and keep a log ofany maintenance performed. Moreover, the operator is the person most familiar with the aircraft and best suited to maintain the aircraft in an airworthy condition to provide the equivalent level ofsafety. Pursuant to C.P.R. Part 11, the following summary is provided for publication in the Federal Register, should 

### itbe determinedthatpublication is needed: Professional AerialPhotographers Association-InternationalSection333 Doc 15-001

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## 19
Applicant seeks an exemption from the following rules: 14 C.F.R. § 21, subpart H; 14 C.F.R. 45.23(b); 14 C.F.R. §§ 61.113(a) & (b); 91.7 (a); 91.9 (b) (2); 91.103(b); 91.109; 91.119; 91.121; 91.151(a); 91.203(a) and (b); 91.405 (a); 91.407 (a) (I); 91.409 (a) (2) and 91.417 (a) & (b) to operate commercially a small unmanned vehicle (55lbs orless) in aerial photography operations. Approval of exemptions allowing commercial operations of sUAS in the aerial photography industry enhances safety while reducing risk. Manned aircraft still photography and video may create a greater risk because the craft are much larger, have combustible fuel, and carry an onboard human pilot. In contrast, a sUAS weighing fewer than 20 lbs. and powered by batteries eliminates virtually all ofthat risk given the reduced mass and lack ofcombustible fuel carried on board. The sUAS will carry no passengers or crew and, therefore, will not expose them to the risks associated with manned aircraft flights. The operation of small sUAS, weighing less than 20 lbs., conducted in the strict conditions outlined above, will provide an equivalent level ofsafety supporting the grant ofthe exemptions requested herein, including exempting the applicant from the requirements of Part 21 and allowing commercial operations. These lightweight aircraft operate at slow speeds, close to the ground, and in a controlled environment and, as a result, are far safer than conventional operations conducted with manned aircraft operating in close proximityto the ground and people. Privacy All Flights will occur over private or public property with the property owner's prior consent and knowledge. Images taken will be of individuals who have also consented to being filmed or otherwise having agreedto be inthe areawhere aerial photography will take place. Satisfaction of the criteria provided in Section 333 ofthe Reform Act of 2012--size, weight, speed, operating capabilities, proximity to airports and populated areas and operation within visual line ofsight and national security

- provide more than adequatejustification for the grant of the requested exemptions allowing commercial operation of applicant's sUAS in the aerial photography industry pursuantto the Manual appended hereto.

StanMacbea Allen Macbean Photographic Solutions, Inc. Corporate Officers



### Professional AerialPhotographer-s Association-InternationalSection333 Doc 15-001

## www.utahbyair.com 

# sUAS Operations Manual Photographic Solutions, Inc.

06 July 2015

This manual contains standard operating procedures and guidelines for UAS operations.

# Photographic Solutions, Inc. sUAS Operations Manual TableofContents Purpose, Scope, and Mission Statement**································~····························5** Definitions

..........................................................................................................6 

### Personnel Responsibilities

..................................................................................8

Visual Observer

....................................................................................................8 PIC

.......................................................................................................................8 Flight Team Composition

.....................................................................................8 Qualification Requirements

.................................................................................8 

### Operating Limitations and Conditions.................................................................9 'Maintenance Procedures ..................................................................................10 Routine Maintenance

........................................................................................10 Full Flight Test

....................................................................................................11 Software Firmware Update Policy

......................................................................11 

### Logs and Records

..............................................................................................12 Pilot and Aircraft Hours

......................................................................................12 Battery Logbook

.................................................................................................12 

### Flight Planning ..................................................................................................13

Weather

.............................................................................................................13 Site Permissions

.................................................................................................13 Pre-Flight Inspections and Checks

......................................................................13 Documentation

..................................................................................................14 Pre-Flight Area and Personnel Checks

................................................................14 Closed Set Operations

........................................................................................15
2

### On-Site Procedures ............................................................................................16 Site Survey ..................................................................................................16 Selection ofOperating Areas and Alternatives............................................16 Boundaries..................................................................................................17 Anemometer Weather Check .....................................................................18 Crew Briefing

.....

**~**

### ........................................................................................18 Communications .........................................................................................19 Frequency Scans .........................................................................................19 Recharging and Battery Use (Fuel Management) ........................................19 Load-outs and Equipment ...........................................................................19 

### Flight Procedures ..............................................................................................21 Motor Start ........................................................................................................21 Take-Off.............................................................................................................21 ln-Fiight..............................................................................................................22 Let Down/Landing..............................................................................................23 Shutdown ..........................................................................................................23 

### Emergency Procedures......................................................................................24 MotorThrust Loss ..............................................................................................24 Battery Failure ...................................................................................................24 Battery Failure Failsafe ...............................................................................25 Transmitter/Controller Battery Failure .......................................................26 Controller Battery Failsafe ..........................................................................26 Loss of Control Frequency..................................................................................26 Loss of Frequent Failsafe....................................................................................26 Malicious or Accidental Interference with Control Frequency
...........................27 Pilot Incapacitation .....................................................................................27
3

### Aircraft Incursion

........................................................................................27 

### Fly Away 

### Procedure

..........................................................................................28 Crash 

### & Incident Response

................................................................................28 

### Appendix A- Checklists.....................................................................................29 Pre-Flight Start-Up Checklist

..............................................................................30 Pre-Flight Inspection Checklist

...........................................................................32 ln-Fiight

..............................................................................................................33 landing Checklist

...............................................................................................34 

### Appendix B

.......................................................................................................35 Maintenance logbook

.......................................................................................36 

### Appendix C

.......................................................................................................37 Incident/Accident logbook

................................................................................38 

### Appendix D.......................................................................................................39 Flight Record logbook

.......................................................................................40 

### Appendix E ........................................................................................................41 Phantom II User Manual

....................................................................................41

4

## PURPOSE, SCOPE, AND MISSION STATEMENT Photographic Solutions, Inc. (Photographic SolutionsL a member of the Professional Aerial Photographers Association, International (PAPA} intends as the Operator to promote safe operation of sUAS in the National Airspace System (NAS) in a manner that is consistent with a long history of safe and professional flight operations in close cooperation with the Federal Aviation Administration (FAA). The Operators are experienced licensed pilots. The sUAS Pilots In Command (PIC) that will operate systems according to the approach outlined in this Manual of Procedures (Manual) are trained in accordance with this Manual and FAA regulations and have decades of successful experience on Aerial Photographic flight missions. The intent ofthe Manual is to provide the outline of a system to conduct safe and successful sUAS operations in accordance with the applicable FAA regulations and consistent with the section 333 waiver that this Manual is based upon. It is expected that the Operator will continue to apply the skills and experience they have employed in manned aircraft operations under FAA regulations. This combination of prior successful flight experience and sound sUAS flight operational procedures is intended to promote the highest levels of professionalism in safe aerial photographic flight missions.

5

### DEFINITIONS The following definitions of words and terms apply to the information contained in this Manual and are specific to procedures and operations that are outlined herein. In the case of a conflict with an official FAA definition, the FAA definition will be the rule.
Anemometer- An instrument to measure the velocity ofthe wind in the Area of Operations. Area ofOperations- Defined as the area where sUAS operations will be carried out for a specific flight or series offlights on a given mission. Checklists- Procedural checklists used by the PIC to verify proper and safe procedures during all phases ofsUAS operations. Designated Safety Zone- Defined and marked area of ground operations used for safe takeoffs and landings ofthe sUAS at a given Area ofOperations. Flight Control Systems- The combination oftelemetry, PIC operated controls, and onboard control mechanisms that are employed to control the flight ofthe sUAS. Frequency Analyzer- A device used to scan the Area of Operations for possible interference from radio waves. GPS- Global Positioning System. Handheld Radio- A radio transceiver capable of communication with other Pilots or FAA personnel in the Area ofOperations. Loiter Mode- A default recovery mode the sUAS goes into when communications are lost from the PIC. Maintenance Recommendations- Periodic maintenance recommendations for each ofthe sUAS components that have a usable life.

6

### Manual- 

### This flight manual that combines the Operator specific procedures with the sUAS manufacturers' manual. Manufacturers Recommendations
- 

### Written recommendations provided by the manufacturers ofthe various components ofthe sUAS. NAS- National Airspace System. Non Participants- 

### Persons who have not agreed to participate in sUAS operations. Operator- 

### The entity submitting as the applicant on this waiver request to the FAA who will be responsible for all sUAS operations and procedures. PAPA- 

### Professional Aerial Photographers Association, International. Participants- 

### Persons who have agreed to participate in sUAS operations. Pilot In Command
- 

### Person who will fly the UA during sUAS operations and who is responsible for all safety related or operational decisions under the direction of the Operator in accordance with this Manual and FAA requirements. SOP- 

### Standard Operating Procedures. sUAS- Small Unmanned Aerial Systems as contemplated underthe FAA guidelines, notto exceed 55 pounds in weight or 100 miles per hour in speed. Telemetry- 

### Electronically transmitted data that provides control and information transmissions to and from the PIC and the sUAS. UA- Unmanned Aircraft. Visual Observer- 

### An individual who is designated to observe flight operations and to maintain visual contact with the UA duringflight operations while maintaining communications and coordination with the PIC.

7

## PERSONNEL RESPONSIBILITIES
VISUAL OBSERVER 

### All operations will utilize a Visual Observer. The main responsibilities ofthe Visual Observer will be to ensure thatthe UA is operated within the visual line of sight of both the PIC and Visual Observer at all times. The Visual Observer will maintain verbal communication with the PIC at all times. Prior to flight, the PIC will ensure that the Visual Observer understands and can perform all the duties required of the Visual Observer. PIC 

### Pilot in Command is responsible for the safe operation ofthe sUAS at all times in accordance with this Manual and the applicable FAA regulations. Pilot in Command will be responsible for: • All support personnel. • Performing all pre-flight, flight phase, and post flight inspections, air worthiness, diagnostics, and testing. • Manufacturer recommended maintenance operations. • Weather condition assessments and forecast reviews. FLIGHT TEAM COMPOSITION 

### The onsite flight team is composed of a Pilot in Command (PIC} and a Visual Observer (VO). The PIC is responsible for all flight operations and decisions to proceed. The VO is responsible to maintain visual contact with the UA and to provide constant communication with the PIC regarding aircraft status and surrounding conditions within the Area ofOperations. QUALIFICATION REQUIREMENTS 

### The PIC must be an FAA-licensed pilot and must have completed the PAPA sponsored ground school with at least 25 hours of sUAS flight time. The VO must have completed sUAS ground school training and must demonstrate experience with FAA procedures and the standard procedures ofthis Manual.

8

## OPERATING LIMITATIONS AND CONDITIONS Operational Ceiling- Maximum 1,200 ft AGL, typical 400ftAGL. Operational Endurance- 15 minutes. Maximum Speed- 100 MPH Maximum OperatingTemperature - 110 degrees F Minimum OperatingTemperature - 0 degrees F Maximum Operational Wind Speed -15 MPH (gusts to 20 MPH)

9

## MAINTENANCE PROCEDURES Only Photographic Solutions personnel or an appointed service technician may carry out maintenance on the sUAS aircraft systems described in this operations manual. In all cases a Maintenance Logbook (see Appendix B) is completed to reflect any work undertaken and a flight test, testing all functions (including the return-to-home failsafe facility), is subsequently carried out by the PIC. ROUTINE MAINTENANCE 

### The Pre-Flight and Post-Flight checklists shown in Appendix A are completed by the PIC every time a Photographic Solutions sUAS aircraft is operated. Every six months (or fifty hours of flight time - whichever comes first) the following inspection is carried out by the PIC. The inspection is recorded in the Maintenance Logbook along with any findings. Any issues identified are remedied and the aircraft undergoes a full flight-test before the aircraft is returned to Operational Status: • Inspection ofthe airframe for any damage, unusual marks and tightness of fixings; • Inspection ofthe motor mountings for correct tension; • Inspection ofthe propellers for condition, unusual marks, chips, cracks and tightness of fasteners; • Inspection of electrical wiring for condition, unusual marks or discoloration; • Inspection of electrical terminal fittings and plugs for secure attachment and general condition; • Inspection ofthe attachment of all fittings such as flight controller, GPS antennas etc. for secure attachment; • Inspection of payload attachment points for condition and security of payload; • Inspection ofthe condition and function ofall ancillary equipment such as transmitter etc. • Testing of all system battery packs for charge status and general condition. If any issues or problems are identified then the aircraft is not allowed to fly until the issue has been remedied. If minor problems (such as damaged propellers, faulty battery packs etc.} are identified and remedied, and the PIC believes the aircraft is suitable to return to Operational Status then the work completed is noted in the Maintenance Logbook. If major issues are identified (such as an 10

### unserviceable motor, damaged airframe etc.), then the aircraft undergoes a full flight test regime (as described below), once the identified fault has been remedied. FULL FLIGHT TEST 

### The system has all functions tested with a minimum offive minutes flight time by a qualified PIC recording any abnormalities in the Flight Record Logbook (Appendix D). Ifthe PIC deems the aircraft to be safe then he must sign the Flight Record Logbook as fit for Operational use. Systems with identified issues relating to firmware or software (see below) are grounded by Photographic Solutions until any problems are rectified. SOFTWARE AND FIRMWARE UPDATE POLICY 

### All new software and firmware are thoroughly assessed before installation. Particular attention is focused on relevance to operations, reason for release and any known issues. Multi-rotor and sUAS forums are consulted regularly for any reported issues with the release and only when the validity of the upgrade has been confirmed is the upgrade considered. In all circumstances the upgrade is performed by qualified Photographic Solutions personnel or appointed service providers. All upgrade information such as version numbers and new functions are recorded in the Maintenance Logbook. All Photographic Solutions PIC are made aware that the firmware or software has been upgraded before any flight operations are undertaken. Any upgraded system has all functions thoroughly tested with a minimum of five minutes flight time by a qualified Photographic Solutions PIC who records any abnormalities in the Flight Record Logbook. If the PIC deems the aircraft to be safe then the PIC signs the Flight Record Logbook as fit for Operational use. Ifany doubts exist as to the new upgrade the aircraft is downgraded to the previous firmware and the flight test procedure is repeated. Systems with identified issues relating to firmware or software are grounded until the problem can be rectified.

11

## LOGS AND RECORDS PILOT AND AIRCRAFT HOURS 

### Photographic Solutions PIC are required to keep a log of pilot and aircraft hours. To meet this requirement, Photographic Solutions holds and updates a spreadsheet-based Personal Flying log Book for Aircraft Operating Crew. This log book is a separate document which can be viewed on request (see sample page at Appendix D). BATTERY LOGBOOK 

### Photographic Solutions Personal Flying log Book (Appendix D) additionally records information about battery condition (charge) before and after each flight. The Battery logbook is accompanied by - and supported with - Photographic Solutions Incident logbook (Appendix 

### C) and Maintenance logbook (Appendix B).

12

## FLIGHT PLANNING WEATHER 

### Operator will require PIC to obtain all necessary weather information in order to plan and conduct safe flight operations according to and as referenced by any applicable UA Operator Manuals. If operating near an operating Automatic Terminal Information Service (ATIS}, the ATIS broadcast system will be consulted. If ATIS is not available, PIC will consult-alternative sources for a current weather forecast. The operating envelope for the Phantom 2 has been referred to earlier. It is emphasized that the PIC is to ensure the operating envelope environment meets or exceeds all safe and legal visibility, precipitation, humidity, and wind limitations for safe operation. SITE PERMISSIONS 

### • Secure permissions from property owner if required. • Secure permissions from participants. • Coordinate with local law enforcement if required. • Prior to operations, Operator receives permission for take-offand landing from the relevant land-owner. In most cases permission attainment is unproblematic as the landowner and the client are the same individual (or entity}. In the case of local authority owned land, the relevant authority is contacted in advance to secure permission for take-off and landing, and to find out about any operating restrictions or specific insurance requirements that might apply. PRE-FLIGHT INSPECTIONS AND CHECKS 

### Prior to each flight, the PIC will conduct a pre-flight inspection and determine if the sUA$ is in a condition for safe flight, and to account for all possible discrepancies or inoperable equipment. If the inspection reveals any condition that will affect the safe operation ofthe sUAS, the aircraft will be prohibited from operating until the necessary maintenance can be performed and the sUAS can be returned to safe flight. The preflight inspections will include the following components according to the recommended checklists in the DJI Phantom 2 operator manual, and in the Photographic Solutions checklist:

13

### D Airframe 

### D Battery 

### D Transmitters 

## D Camera and Gimbal 

## D Propulsion system including propellers In addition, with the battery attached and turned on in the sUAS, the PIC will oversee and monitorthe series of diagnostic tests to determine and verify proper voltage levels, control function, communication, and GPS satellite connectivity acquisition. PIC will utilize the DJI Phantom 2 LED indicators as well as telemetry data to determine if the proper preflight diagnostics have been completed. The PIC will also perform and log a pre-flight compass calibration each time the sUAS is flown from a new location. DOCUMENTATION 

### PIC will ensure that all documents used by Photographic Solutions to ensure safe flight operations and any document required under 14 CFR 91.9 and 91.203 must be available at the Ground Control Station on site at any time the sUAS is operating, and ready to be made available to any law enforcement official upon request. If possible, these documents will be on the PIC's person at all times during flight operations, and accessible to law enforcement without interrupting the PIC while conducting flight operations (possibly in a pouch on the back ofthe vest). PRE-FLIGHT AREA AND PERSONNEL CHECKS 

### • Survey flight operations area for safety concerns and to verify conditions. • Examine all components ofthe sUAS to verify proper function in accordance with the applicable manuals and manufacturer's instructions. • Verify notification to all personnel on site. • Establish Designated Safety Zone and verify safe clearances. • PIC should wear the specified safety vest. • The ultimate responsibility for aircraft airworthiness and operational safety rests with the UAV pilot-in-command. For this, the PIC- as an aid- uses a Pre-Flight Checklist (see Appendix A). In summary, the Pre-Flight Checklist prompts examination ofthe following: 

### D The airframe (for condition and lack of damage); 

## 0 The battery (for level-of-charge and security ofattachment);
14

## D The transmitter (for level-of-charge and to check that switches are in the 'home' position); 

### D The camera (secured, on and operating). 0 Propulsion system
• In addition, when the flight battery is connected to the sUAS, the flight controller undertakes a series of diagnostic tests (while simultaneously locating the position ofGPS satellites). CLOSED SET OPERATIONS 

### Ifthis exemption permits operations for the purpose of closed-set motion picture and television filming and production, the following additional conditions and limitations apply: • The operator must have a Motion Picture and Television Operations Manual (MPTOM) as documented in this grant ofexemption. • At least 3 days before aerial filming, the operator ofthe UAS affected by this exemption must submit awritten Plan ofActivities to the local Flight Standards District Office (FSDO) with jurisdiction over the area of proposed filming. The

**3~day** 

### notification may be waived with the concurrence ofthe FSDO. The plan ofactivities must include at least the following: o Dates and times for all flights; o Name and phone number ofthe operator for the sUAS aerial filming conducted.underthis grant ofexemption; o Name and phone number ofthe person responsible for the onscene operation ofthe sUAS; o Make, model, and serial or N-Number of sUAS to be used; o Name and certificate number ofsUAS PICs involved in the aerial filming; o A statement that the operator has obtained permission from property owners and/or local officials to conduct the filming production event; the list ofthose who gave permission must be made available to the inspector upon request; o Signature ofexemption holder or representative; and o A description ofthe flight activity, including maps or diagrams ofany area, city, town, county, and/or state over which filming will be conducted and the altitudes essential to accomplish the operation.
15

### • Flight operations may be conducted closer than 500 feet from participating persons consenting to be involved and necessary for the filming production, as specified in the exemption holder's MPTOM. ON-SITE 

### PROCEDURES 

### The on-site procedures undertaken by Photographic Solutions are conducted in accordance with and controlled through an extensive use ofchecklists. For this reasonJ the following sections repeatedly refer to various checklists found in AppendixA ofthis Manual.
• Site Survey- In advance ofoperations, a survey is undertaken to review the site, its terrain, structures and surroundings- to check any assumptions made about the location priorto arrival and to adjust the operations plan accordingly. For this, an On-Site Survey Checklist is used (see Appendix A, page 25). The primary purpose ofthe site survey is to make avisua;l check ofthe operating area with the objective of identifying any potential hazards.


### • Selection of Operating Areas and Alternatives - In advance ofthe pre-flight On-Site Survey, Google maps will be consulted and- if possible- the local site will be visited beforehand. The site will be specifically checked in terms of: o Proximity to Airport Reference Points (ARP) as denoted in the Airport Facility Directory (AFD). Must operate outside 5 miles ofARP, unless otherwise agreed upon by virtue ofwritten letter of agreement with the airport's management or otherwise permitted by the COA issued to Photographic Solutions o Ability of PIC and VO to operate the sUAS clear of, and give way to, all manned aviation operations and activities at all times. o 500ft. clearance ofall non-participating persons, vessels, vehicles, and structures unless; 

### A. sufficiently protected in the event ofan accident, and the nonparticipating persons remain protected at all times during operations ofthe sUAS, and 

### B. The owners and controllers of any vessels, vehicles, or structures has granted permission forthe operating closer to
16

### those objects and the PIC has made a safety assessment ofthe risk ofoperating closer to those objects and determined that it does not present an undue hazard. o Ability of Photographic Solutions to conduct operations over private or controlled access propertywith permission from the owner/controller or representative ofsuch, and said permissions are granted. o Proximity to radio interferences o Prevailing weather conditions have been adequately assessed, including; high winds, convection, visibility, minimum cloud clearance (500ft below, and 2,000 ft horizontal clearance}, or when visibility is less than 3 miles from the PIC. The primary site for take-off and landing will be assessed (size, shape, surface, slope and surroundings} and an alternative site will be identified should the primary site become unavailable or unsuitable.


### • Boundaries
- Photographic Solutions requires that proper identifiers and signage will be in place in the operating area to alert people to the fact that aerial work is being conducted. The PIC will be responsible for cordoning to ensure safe distances from operations are observed. Cordoning procedures to be practiced include: o Take-off and Landing safety Area: PIC will determine the safe distances ofall people from the take-off and landing operation ofthe UAS. The PIC will also establish a cordoned area with clearly marked delineation the take-off and landing operations. o Signage and Identifying Clothing: The PIC will place signage at each entry point within the operations area alerting people to the following: A. Low altitude aerial work is being conducted B. Use ofany actual sensing equipment being used 

### C. A request asking people to not enterthe area without first notifying the PIC or Photographic Solutions designated on-site flight operations personnel D. PIC and VO will put on outerwear that will identifythem in their respective roles. Signage will be attached on their person that will instruct law-enforcement,
17

### observers, or any other people present that they are not to be interrupted un-necessarily while conducting flight operations.

• Anemometer Weather Check- 

### Beyond pre-site planning weather forecast checks, Photographic Solutions requires that the PIC conduct specific onsite weather checks. The PIC will utilize a hand-held or portable Anemometer to determine wind speed, direction, temperature, and humidity. Aerial operations will only be conducted within the specific recommended wind and humidity limitations of the sUAS manufacturer's operating manuals, or if not identified therein, only in conditions where wind speed is less than lSmph, gusting up to 20mph.
• Crew Briefing - 

### Photographic Solutions flight operations personnel will typically include the PIC, VO, and other possible ground crew. The operations personnel, in addition to any other parties that may be present, will be briefed priorto the start of operations. The briefing will include: o Introduction to the equipment being used including the sUAS and the ground station functions, with particular emphasis on moving parts including weight ofthe sUAS, and the harm or damage that could possibly be inflicted by coming into contact with those components (particularly the propellers, and hot surfaces} o Familiarization with the failsafe return-to-home systems and instruction on how to activate those systems ifthe PIC is unable to activate those systems o Expected flight plan, holding positions, flight duration, and overall flight boundaries. o Expected responsibilities and authority of each flight operations personnel o Identification and familiarization with the take-off and landing designated areas, and the requirements for remaining clear of those areas at all times. o The need for all present to alert the PIC ofany encroachments of people or objects into the airspace and ground boundaries o Importance of mitigating any possible distractions or unnecessary communication with the PIC during operations
18

### o Careful review of Lost Link and emergency procedures • Communications 

### Photographic Solutions uses channel-hopping technology on 2.4GHz to maintain communications with the UAV for the purposes of platform control. There is no communication rdownlink') from the UAV to the ground station. In the event of loss of or interference with the control frequency, the UAV is programmed to return to its take-off position and land autonomously ('return-to-home'). This failsafe procedure is described further under Emergency Procedures.

• Frequency Scans
- 

### Photographic Solutions will perform frequency scans to help identify possible conflict with radio communications. This will be performed via a hand-held or portable radio spectrum scanner by the PIC. These scans will include a full spectrum scan of the applicable frequency range ofthe sUAS. Possible sources of radio interference or conflict will be identified and evaluated to determine if flight operations can be safely continued.

• Recharging and Battery Use (Fuel Management)
- 

### The DJI Phantom 2 utilizes a 5,200mah 11.1V LiPo (/intelligent" battery. Batteries are charged at base prior to flight operations. The number of batteries that will be transported to the flight operations area will be based on the specific needs of the flight operations or mission. The battery capacity will be tested utilizing the internal proprietary tester on the battery, and will also be checked utilizing the proprietary DJI software, as well as any internally sensed telemetry software and hardware attached to the sUAS. A battery charge log will be kept via the proprietary DJI Phantom 2 software and will be completed prior to every flight. Any battery found to be less than fullycharged, damaged, displays insufficient voltage, or otherwise defective will not be used.

• Load-outs and Equipment
- 

### The Phantom 2 is a simple quad-copter UAS with limited capability for loads and equipment. Removable equipment includes the battery, gimbal, camera, telemetry hardware, antenna, and imaging transmitter. The battery is held in place via proprietary fittings. The gimbal is attached via screws into the airframe. The camera is attached to the gimbal using screws and a proprietary harness. All other equipment is attached using nylon fittings, Velcro, or adhesives. Total takeoff weight
19

### with these components will not exceed the maximum recommended takeoff weight identified in the Phantom 2 Users/operators Manual of 1300 grams, with a total payload weight not to exceed 300 grams. Payload security is tested prior to any operations both visually and by vigorous tactile testing. All attachment points will be inspected and tested weekly.

20

## FLIGHT PROCEDURES Photographic Solutions will utilize checklists to direct the flight operations personnel in flight procedures. The following section will continually refer to the several checklists presented in the Appendix.
• Motor Start- 

### All of the various preflight checks will have been performed priorto motor start and will include: o PIC and VO will put on identifying outerwear. o Pre-flight compass calibration, GPS verification, and voltage diagnostics completed. o Take-off position and location is checked to ensure it is clear of obstacles, debris, potential hazards, and people. o Transmitter switches are placed in the proper configuration, including the home switch and GPS mode switch. o Transmitter is on and properly charged with voltage confirmed. o Battery is secured, on, and properly seated. o Camera and gimbal is armed, responding to commands, and stabilized. o sUAS is placed in the proper takeoff position. o LED flight mode indicator, and telemetry-read-out shows adequate GPS connectivity according to the DJI Phantom 2 User/operators Manual. o LED flight mode indicators and telemetry read-outs show the proper flight mode is selected DJI Phantom 2 User/operators Manual. o Camera is switched on. o All flight operations personnel are in their proper position and atthe ready. o Start motors, and establish functional pre-take-off power setting.

• Take-Off
- 

### Once motors have been started, the PIC will verify that the pretake-off checklist has been completed. Once this has been verified, the PIC will follow the following take-off procedure: 1. Apply power for a controlled ascent to a safe low-level test altitude overthe take-off area, and then hold. 2. After in hold, PIC performs check of all control stick response including rudder, aileron, elevator, and throttle to ensure proper 21

### response to commands. 3. PIC confirms with VO that the flight operations area is free of obstructions or other manned or unmanned air traffic. 4. PIC confirms with all flight operations personnel that they are ready to proceed with flight operations as planned.


### • In-Flight - Photographic Solutions requires that the PIC is free to concentrate on positioning, scanning, and monitoring systems and the flight operations area without un-necessary distraction, and to ensure the flight is compliant with remaining 500 ft clear of all non-participating persons, vessels, vehicles, or structures unless proper permissions have been obtained as described in the previous section addressing the selection ofsites. Throughout the flight, PIC will take particular care to remain within the established operating permissions and envelope by executing the following practices: o Verify through verbal communication with the VO that they are alerted to any manned or unmanned aircraft within the flight area. o Verify through verbal communication with the VO that obstacles are being identified and avoided. o Interval monitoring ofvoltage and communication with sUAS to ensure adequate voltage according to the DJI Phantom 2 User/operating Manual for safe return and landing. o Monitortime since motors were started to ensure a minimum of 3 minutes of battery fuel is available for return and landing of sUAS. o A safety margin ofa minimum of 3 minutes of battery life is maintained at all times. o Maintain visual contact withflight systems/mode and battery LED light indicators at all times. o Maintain situational awareness of changes in weather, visibility, or cloud avoidance at all times. o Maintain operation speeds less than lOOmph. o Maintain visual contact with sUAS at all times. o Ensure VO has visual contact with the sUAS in flight at all times. Establish a position hold until VO re-establishes visual contact with the sUAS if contact is lost.

22• Let-Down/Landing
- 

### To execute a safe recovery and landing of the sUAS, the PIC will ensure that the following practices are followed: o Establish and guide the sUAS through a safe route to directly above the cordoned take-off and landing area. o Maintain a safe descent rate and follows all procedures and techniques to avoid vortex state or settling with power. o Verify that a minimum of 3 minutes of battery life is available, as mentioned above, to ensure a holding position ifthe landing area is not cleared. o Verify that the landing area is clear ofdebris, obstacles, people, or hazards that would preclude a safe landing.

• Shutdown
- 

### Upon landing, the throttle is returned to the home position causing the rotors to stop spinning. Operations then proceed as follows: 1. The sUAS battery is switched offor disconnected. 2. The camera is stopped and is then switched off. 3. The sUAS is removed from the landing area and is checked for any abnormalities or damage. 4. The transmitter is switched off. 5. The sUAS battery is removed, 

### tested, and then the battery is safely secured and stored.

23

## EMERGENCY PROCEDURES The emergency procedures described below address the following, safety-critical question: 

### In the event ofa malfunction,failure or other in-flight emergency, how is the sUAS going to safely land without creating a hazard to other airspace users orpersons orproperty on the ground? MOTOR THRUST LOSS 

### As a quad copter, The Phantom 2 has no 'rotor redundancy'. Loss of power to a motor on a quad copter will result in a crash. For this reason, Photographic Solutions takes specific preventative steps to ensure that loss of power to a motor will not occur: • Wiring integrity is checked visually priorto any flight operations. • A pre-flight battery check is undertaken to test the charge ofthe cells. • Upon take-off, the sUAS is lifted into atemporary, low-altitude holding position and the throttle/ rudder and aileron/elevator control sticks are moved to check that sUAS is responding as expected. If there is a loss ofthrust to a motor, any residual control left available to the PIC will be used to guide the sUAS away from people and objects to avoid injury or damage to property and people. Every effort will be made to restrict the crash site to the safest possible position. sUAS BATTERY FAILURE 

### As has been addressed in above previous sections, Photographic Solutions has procedures and practices in place designed to prevent sUAS batter failure or malfunction, and they include: • The batteries are physically inspected and tested through all phases of preflight and post flight for damage or swelling • The Battery performance and condition is tested prior to each flight to ensure they are fully charged, and the proprietary DJI Phantom 2 software charge track/log is checked to ensure the battery meets the minimum safe requirements as specified by DJI in operating manual and firmware specs. • Throughout all phases offlight, the batteryvoltage, percentage of charge remaining, and time in operation is constantly monitored via the telemetry transmission to the ground station to ensure there is the proper minimum voltage and time to return and land is achieved and maintained.
24

### • The PIC will immediately land the UAV in the nearest possible landing area iftelemetry indicates the minimum voltage, time in operation, or percentage of charge are not met. 

### BATTERY FAILURE FAILSAFE As a preventative measure to keep the sUAS from a forced landing or crash due to battery failure, the DJI Phantom 2 flight controller has several levels of low voltage protections incorporated as specified in the attached User/Operator's Manual, triggering an automated Failsafe Return to Home and Landing command as follows: • The low battery capacity warning alerts users when the battery is close to depletion duringflight. When it appears, users should promptlyfly back and land to avoid accidental damage. The Phantom 2 has two levels of low battery capacity warning. The first appears when the battery has less than 30% power and the second appears when it has less than 15% power. The following list details the battery power warnings:

.. o When battery power drops below 30% the LED indicator will blink red slowly. o At lowerthan 15%, the LED indicator will blink red rapidly. The Phantom 2 will also begin to descend and land automatically. After it has landed, keep the throttle stick at its lowest point or execute the combination stick command (CSC) to shut off motors. o There is a hidden third low batterythreshold in addition to the 1st and 2nd level warnings. This uses 10.65V as its threshold. Both this voltage threshold and the 2nd Level Low Battery Warning will trigger auto-landing. • Altitude can be maintained if necessary by pushing up on the Throttle stick. 

# [•

# .... l -----------



# •••••• 11st Level Low Battery Capa_c_ity_W

__

a_rn_in_g
________



# ~ 2nd Level Low Battery Capacity Warning 1 

# ••• Not Stationary orSensor Bias is too big j 

### Errors &Aircraftcannotfly.*



## ~ 

# ICompass data abnormal because offerro-magneticj J 

### interference or the compass needs calibration.

**----------------~----** 25

### TRANSMITTER/CONTROLLER BATTERY FAILURE 

### As has been mentioned previously, through the extensive use of checklist procedures, Photographic Solutions requires that the PIC ensure the DJI Phantom 2 controller (ground station} will be fully charged prior to any aerial operation. Any monitors being used to display telemetry will also be fully charged. CONTROLLER BATTERY FAILSAFE 

### Photographic Solutions will use The DJI Phantom 2 flight control system that incorporates an automated failsafe system which commands the sUAS to return to home and land ifthere is a loss offrequency due to battery failure. The PIC will reference the below LED lighting system to monitorthe controller charge; Remote Controller Power LED Indicator Status Power LED Sound Remote Controller Status None Normal 

# •••••• 8-8-8
...... 

### Lowvoltage (at 4V-4.3V). Replace the batteries immediately



## --

# •••• 8-8--8
...... 

### Alertwill sound after 15 minutes ofinactivity. Itwill stop once you start using the remote controller.

The remote controller will power off automatically when battery voltage drops below 4V. Land and 

### A, change batteties as soon as possible when the low voltage alert occurs to avoid loss of control during flight. 

### LOSS OF CONTROL FREQUENCY (and/or Ground Station Failure) 

### To help prevent a loss of control frequency, Photographic Solutions requires that the PIC ensure flight operations only occur within un-aided visual line of site VLOS at all times. Doing so will keep the sUAS well within the required minimum range ofthe DJI Phantom 2 controller/transmitter. LOSS OF CONTROL FREQUENCY FAILSAFE 

### If the control frequency signal is lost for more than 3 seconds (sUAS out of range, ground station failure etc.} the DJI Phantom 2 Flight Controller has been programmed to switch the UAS into failsafe mode and it will 1

### return to· home' (RTH} and also land: • Ifthe failsafe occurs while in GPS mode according to the parameters of the DJI Phantom 2 User/Operator Manual, the sUAS will return to the
26

### take-off and landing area and auto-land. • Ifthe fail location occurs while in ATTI mode according to the parameters ofthe DJI Phantom 2 User/Operator Manual, the sUAS will auto-land. • The RTH failsafe mechanism works by the sUAS Flight Controller saving the home (take-off} point automatically when the throttle stick is moved for the first time (after 6 or more GPS satellites have been acquireddenoted by a single red pulse from the LED or a series ofcontinuous green pulses). The RTH failsafe function on the sUAS is tested on aweekly basis by Photographic Solutions by switching the transmitter offduring atest flight session. MALICIOUS OR ACCIDENTAL INTERFERENCE WITH CONTROL FREQUENCY 

### As was mentioned in previous sections, through the extensive use of checklists, Photographic Solutions requires that the PIC utilize a Spectrum Scanner to ensure there is no accidental or malicious radio interference. In the unlikely event that this should 

## occur, the PIC will initiate the failsafe procedure mentioned in the previous section

• Pilot Incapacitation
- 

### If the pilot-in-command becomes incapacitated to the extent that control ofthe sUAS becomes unviable, the sUAS will hover in a stationery position until the battery's second level low-voltage protection is triggered. At this point, the sUAS will descend and land in a steady, controlled manner. If an observer is present, they will have been briefed on the sUAS's failsafe (return-to-home) mode and its activation (see Section on "Crew Briefing").

• Aircraft Incursion
- 

### If another aircraft should enter or appears to be entering the Visual Line of Sight Operating Envelope VLOS, PIC will operate the sUAS to immediately maintain safe visual separation, and give way to any manned flight operation.

27

### FLY AWAY PROCEDURE 

### A "fly away" is defined as the loss of control transmission link where the PIC no longer has control or the ability to command the sUAS to remain within the bounds of the intended operation area. In the unlikely event that this should occur, the PIC will observe and record the direction of flight heading, speed, and altitude ofthe sUAS, and then follow the Incident Response Procedure as outlined below: • Crash & Incident Response 

### While Photographic Solutions takes extreme caution in its flight procedures to prevent a loss of control or crash, any incident, accident, or operation that transgresses the lateral or vertical boundaries as defined by the applicable COA issued must be reported to the FAA UAS Integration Office (AFS 80} within 24 hours. The following procedures will also be ensured by the PIC: o PIC will have on their person a copy ofthe local emergency response contact information, including fire, law enforcement, medical response, and the UAS Integration Office contact information

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## www.utahbyair.com 

# Appendix

# A Checklists

29

### PRE-FLIGHT START-UP CHECKUST: o Verify all transmitter, on-board aircraft and camera batteries are fully charged (confirm voltages}. o Ensure no frequency conflicts with video and transmitter

## I receiver. o Check all control surfaces for signs ofdamage, loose hinges, and overall condition. Inspect the wings 

## I rotors to ensure they are in good structural condition and properly secured. o Check motor

## I engine and mounting attachments to the airframe. o Inspect propeHers 

## I mounting hardware (tight} 

## I rotor blades for chips and deformation. o Check the landing gear for damage and function. o Test electrical connections (plugged in and secure}. o Ensure photo 

## I video equipment mounting system is secure and operational. o Check location of GPS equipment controlling the autopilot. o Check the IMU movements in the ground control software. o UAV in stabilization mode, ensure control response move toward the correct positions. o UAV 

## I Drone is in a level location safe fortakeoff. o FPV 

## I Power up ground station. o FPV 

## I Power up Video receiver. o If using Video recorder, turn on camera system. o Camera settings are correct (still images, video, frame rate}. o SD camera memory clear and inserted into the camera. o Action 

## I Start filming. o All transmitter controls move freely in all directions. o All transmittertrims in neutral position. o All transmitter switches in correct position (typically away}. o Transmitter throttle to zero. o Radio transmitter on. o Connect 

## I power on batteryto airframe. o Ensure led indicators and audible tones are correct. o Timer on (if applicable}. o FPV, confirm video is in monitor

## I goggles. o Scan for nearby cars 

## I people 

## I animals. o Say {(CLEAR!". o Arm flight controller.
30

### o Increase throttle slightly listening for any abnormalities. o Short 20-30 second hover at 3-5 feet (listen for vibrations 

## I loose items). o Confirm Voltage levels are correct.

31

### PRE;.FUGHT INSPECTION CHECKLIST: D Perform initial walk-around. 

### D Inspect UAV for cracks in joints and structural members. 

### D Inspect UAV for loose or damaged screws, ties, fasteners, straps. 

### D Inspect UAVfor loose or damaged wiring. 

### D Inspect UAV for loose or damaged connections (solder, plugs, etc.). 

### D Inspect prop mounts and screws and apply slight counter pressure on arms to check for loosened components. 

### D Ensure antennas and masts are secure. 

### D Inspect 

## I clean FPV Camera and Lens and insure it is secured and connections are firmly attached. 

### D Ensure camera settings are correct (still images, video, frame rate}. 

### D Ensure FPV Transmitters are secure and operational. 

### D Ensure batteries are fully charged, properly seated and secured. 

### D Ensure the following fail-safe equipment is functioning: 

### D RTH (return to home}. 

## 0 Recovery Command Response (toggle test}. 0 Firmware Airport Proximity Detection. 

### D Ensure props are smooth and free ofdamage 

## I defect (check blade, surface and hub}. 

### D Ensure prop adapters are tight 

## I secure. 

### D Ensure voltage alarm is connected. 

### D Ensure arming 

## I idle timeout is properly configured. 

### D Ensure correct model is selected in transmitter (if applicable}. 

### D Check RC transmitter for the correct range and centering for all sticks. 

### D Perform range test.

32

### IN-FLIGHT CHECKLIST: 

## 0 Basics: Ifflying manually, always keep your fingers on the controller/transmitter. 0 Never let the UAV out ofyour sight even for a second. 0 Climb to a safe altitude awayfrom potential hazards and to reduce noise pollution. 0 Keep aircraft at a safe operating distance from people, electric utility lines and buildings. 0 Ifthe UAV must be flown over buildings or people, use a lightweight UAV and maintain a safe altitude for recovery and make every effortto minimize exposure. 0 Spotter: Use a spotter whenever possible and appropriate, especially when flying by First Person View (FPV}. 0 Do notfly UAVs within distance defined by local laws of any private/commercial airport/helipad. 0 Do notfly around a pre-existing UAV flying site without afrequencymanagement agreement. 0 Do not interfere with operations and traffic patterns at any airport.

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### LANDING CHECKLIST: D Regardless ofwhether ofa manual or automated UAV landing, scan landing area for potential obstruction hazards. D Announce out loud {(Preparing to Land". D Use a safe descent rate and follow correct procedures to avoid avortex state or settling. D Carefully land the aircraft away from obstructions and people. D Turn the power offto the aircraft and/or disconnect the batteries. D Turn offthe transmitter. D Turn the power offto the photo equipment. D Visually check aircraft for signs of damage and/or excessive wear. D Remove the unused fuel ifapplicable. Secure the aircraft. D Check pictures: Verify that the UAV camera actually took the pictures. 

### D LOG FLIGHT.

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## www.utahbyair.com 

# Appendix B Maintenance Logbook

35

### MAINTENANCE LOGBOOK Date Component Maintenance Maintenance Comments Activity Time

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## www.utahbyair.com 

# Appendix C ·incident/ AccidentLogbook

37

### INCIDENT/ ACCIDENT LOGBOOK Date of Time of NameofInjured Incident/ Accident ActionTaken Notes Incident/ Incident/ Details Accident Accident

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## www.utahbyair.com 

# Appendix D FlightRecord Logbook

39

### FLIGHT RECORD LOGBOOK (Sample Page) Date Location Activity FlyingTime Battery Battery Comments Before After

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### www.utahbyair.com 

# AppendixE Phantom II User Manual

41Congratulationson purchasingyournewDJI product Pleasethoroughlyreadtheentirecontents ofthismanualto fullyuseandunderstandtheproduct

It is advised that you regularly check the PHANTOM 2's product page atwww.dji.com which is updated on a regular basis. This will provide services such as product information, technical updates and manual corrections. Due toany unforeseenchangesorproductupgrades,the information containedwithinthismanual issubjecttochange without notice. OJIand PHANTOM2are registeredtrademarksofDJI. Namesofproduct, brand, etc., appearing inthis manualare trademarks or registered trademarks oftheir respective owner companies. This product and manual are copy righted by OJ Iwith all rights reserved. lfyouhaveanyquestionsorconcemsregardingyourproduct, pleasecontactyourdealerorDJICustomerService. 

### 21Content CONTENT.............................................................................................................•..........2 IN THE BOX.....................................................................................................................4 REQUIRED ITEMS............................................•...............................................................4 SYMBOLLEGEND ............................................................................................................4

1. PHANTOM 2 AIRCRAFT .............................................................................................5

1.1 BUILT-IN FLIGHT CONTROL SYSTEM INSTRUCTIONS

...............................................................S 1.2 CONNECTIONS WITH OTHER DJI PRODUCTS

........................................................................5 Important Notes ofUsing with Other OJ/Products

........................................................6 Connections with Other OJ/Products

.............................................................................7 1.3 LED FLIGHT INDICATORS DESCRIPTION

.............................................................................10 1.4 NOTES FOR PHANTOM 2 USING WITH OTHER DJI PRODUCTS

..............................................11 2 PROPELLERS

............................................................................................................12

2.1 AssEMBLY

........................................................................................................................ 12 2.2 DISASSEMBLY

..............................................................................................................12 2.3 NOTES

.......................................................................................................................12 3 REMOTE CONTROLLER.............................................................................................13

3.1 POWER ON THE REMOTE CONTROLLER

.............................................................................13 3.2 REMOTE CONTROLLER POWER LED INDICATOR5TATUS

..............................................................13 3.3 ANTENNA ORIENTATION

.................................................................................................... 14 3.4 REMOTE CONTROLLER OPERATION

..................................................................................14 3.5 LINKING THE REMOTE CONTROLLER& BUILT-IN RECEIVER

......................................................16 4 INTELLIGENT BATTERY..................................................................................................17

4.1 CHARGING PROCEDURES

...............................................................................................17 4.2 INSTALL THE BATTERY

........................................................................................................ 18 4.3 BATTERY USAGE

...........................................................................................................18 4.4 DESCRIPTION OF THE BATTERY LEVEL INDICATOR

................................................................... 19 4.5 CORRECT BATTERY USAGE NOTES

...................................................................................20 5 CALIBRATING THE COMPASS ...................................................................................21

5.1 CALIBRATION WARNINGS

..............................................................................................21 ©2013 OJ! Innovations. All Rights ReseNed. 2(5.2 CALIBRATION PROCEDURES ..•.............•.•...•.••..•..•.•...•.....••.•...•...•..•......•.......••••.••......••..•..21 5.3 WHEN RECALIBRATION IS REQUIRED .••••.•.....••..••.....•....•••••••.••••.•.•••••..•......••......•••..•..•.....•21 6 FLIGHT.....................................................................................................................22

6.1 FLYING ENVIRONMENT REQUIREMENTS .•..••...•.••.•••.•.....•.•......•..•..•..•••....••.....••..••.•..•.•.......22 6.2 STARTING THE MOTORS·····································································································22 6.3 TAKEOFF/lANDING PROCEDURES .••.••..•....••.•..••..•.••..•.....••••....•....•.•..........•••..•.••••.•.••....•...22 6.4 FAILSAFE FUNCTION .•••••.....•.......•.........•...............•...•.•••.••.••••.•.......••..••..•......•..........••..23 6.5 LOW BATTERY CAPACITY WARNING FUNCTION •••.•.......•...•..•..•.••.•.•.....•.••.•......•..••....•...•.•....24 6.6 FLIGHT LIMITS FUNCTION .................•..•••.•••.........•.....•.....•.•..••••..•.••.•.••.•.•••..•.••.......••....•25 Max Height & Radius Limits.........................................................................................25 6.7 FLIGHT LIMITS OF SPECIALAREAS ....................................................................................26 6.8 CONDITIONS OF FLIGHT LIMITS .......................................................................................27 Disclaimer....................................................................................................................28 7 ASSISTANT SOFTWARE INSTAllATION AND CONFIGURATION
.................................29

7.11NSTALLING DRIVER AND PHANTOM 2 ASSISTANT SOFTWARE
............................................29 7.2 USING THE PHANTOM 2 ASSISTANT SOFTWARE ON APC..................................................30 7.3 FIRMWARE UPGRADE OF PHANTOM 2 ...........................................................................31 7.4 PHANTOM RC ASSISTANT SOFTWARE DESCRIPTION .........................................................32 8 APPENDIX................................................................................................................33

8.1 SPECIFICATIONS ...........................................................................................................33 8.2 LED FLIGHT INDICATORS DESCRIPTION .............................................................................33In the Box**·-··-----~----·---·---** ---·-------- ----- PHANTOM 2 2.4GHz Remote Controller Propeller Pair

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# . -· Intelligent Battery Charger**~a** 

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Screwdriver AssistantWrench 

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©2013-2014 OJI Innovations. All Rights Reserved. 3 I '

Cables

Accessories Box

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## €4 Reference1. PHANTOM 2 Aircraft [1] '

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### m· [8]'''. ·•···. [11] Figure 1-1 Figure 1-2 [1]Propeller [2]Motor [3]Front Side [4]Front LEOs [5]Micro-USB Port [6]Landing Gear [?]Receiver Antenna [8]CAN-Bus Connector [9]LED Flight Indicators [1 O]DJI Intelligent Battery[11]Compass 1.1 Built-in Flight Control System Instructions The built-in flight control system is used to control the entire aircraft's functions in flight such as Pitch (forwards and backwards), Roll (left and right), Elevator (up and down) and Yaw (tum left or right). The flight controller contains the MC (Main Controller), IMU, GPS, compass, receiver. The IMU (Inertial Measurement Unit) has a built-in inertial sensorand a barometric altimeterthat measures both attitude and altitude. The compass reads geomagnetic information which assists the GPS (Global Position System) toaccurately calculatetheaircrafts position and heightin orderto locktheaircraft in astable hover. The receiveris used to communicate with the remote controller and the MC acts as the brains ofthe complete flight control system connecting and controlling all the modulestogether. The PHANTOM 2 can be configured in the Assistant Software, by choosing Naza-M mode or Phantom 

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2 mode. This manual is for Phantom 2 mode. Please refer to the Naza-M V2 Quick Start Manual for 

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more information.

. ___ ! 1.2 Connections with Other DJIProducts PHANTOM2 iscompatiblewith otherDJI products, includingZENMUSEH3-2D and H3-3Dgimbal , iOSD mini , iOSD Mark II. Beloware connectionsforthese products and wirelessvideo transmission module.

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### ~:m~a~~u::**:s:o~** ]Mountthe H3-2D/H3-3D lgimbal using 4 screws. I L
________ t Figure 1-3 ©2013-2014 OJ! Innovations. All Rights Reserved. 3 I r------1 1 I

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## ·1~·~. **~------1** ----, I Compass 1 : Ulll I I I. I L---"'ImportantNotes ofUsingwithOther DJI Products ( 1 ) The video cable can provide powerforthe wireless video transmission module with a batteryvoltage (11.1V-12.6V)and amaximum current2A ( 2 ) Make suretheworking currentofthewireless videotransmission module you connect can workwith an operationalvoltage between 11.1V-12.6Vandthetotalworking currentofthe iOSDand wirelessvideo transmission module is under 2A, as an overcurrent will damage the central board's components. Ifthe total current exceeds 2A, please be sure to provide power supplied from aseparate power source forthe wireless video transmission module. ( 3) PHANTOM 2 uses a2.4GHz RC system. To avoid communication interference, it's not recommended to use other2.4GHz devices (including 2.4Gwifi or2.4Gwireless videotransmission module) exceptthe 2.4G Bluetooth and 2.4GDatalink. ( 4 ) Besuretokeepthewirelessvideotransmission moduleand othercommunicating devicesawayfromthe compass during installation and connection to avoid interference. ( 5 ) To improvethe compatibilitywith ZENMUSE gimbals, the latest factory deliveries of PHANTOM 2 has updated totheVersion 2shown below. H3-2D/H3-3D gimbal can be directly installed forthe Version 2 whileforVersion 1,aH3-3Dadapterkit(coming soon) is requiredto installtheH3-3Dgimbal.

Figure 1·4 ( 6) When using the H3-3D gimbal, please connectthe 8-Pin cable ofPHANTOM 2tothe G8 portofH3-3D shown below.

Figure 1·5
©2013-2014 DJIInnovations.AII Rights Reserved. 31Connectionswith OtherDJI Products ( 1 ) Connectingthe H3-2Dand H3-3Dgimbalandwirelessvideotransmissionmodule,thefigurebelowuses H3-2D asan example. i-wireless-

- Battl video Batt+ transmission I module VIDEO GND !Transmitter VIDEOL '------·---·-·j r**D.;,;;ripfu,~it"he"Vid:**i;bl.;

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**r~ommend ~onnecti-ng-th_e_V_Ba-t+_p_o_rt_o_f.the**  video cable. to the two BATT+ ports of the AVLsal

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( 4 ) Connectingthe H3-2Dand H3-3Dgimbal, iOSD MarkIIandWirelessvideotransmissionmodule, thefigure belowuses H3-2D asan example.

**r-~-------""** IWireless video transmission t module Transm!ttet sJJecified by ; J OJI(AVLSB) · t l OR

**!~------~~** IDeS'cri'Ptimi ci'fthe'Vide;"cabJe" - - , 1 (sequence by color} I VIDEO I I - VIDEOGND I t----1 - Vs.u I L -=:_G!:!D I i Other wireless video transmission

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# -r--c;,,;;;;.;;;: I Jllll I I·-. I I ,,: c I l..------- ©2013-2014 DJIInnovations.AII Rights Reserved. 31l I Figure 1-9 The diagram below illustrates the conneciton between the iOSD Mark II and the wireless video transmission module.
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### ! BATT+ Batt+ transmission module**~** I**BATT+~Batt+** • !IOSD Mark II UART ! ! Transmitter ! f UART I l ',· I AV-GND l------JVJDEOGND '**L~---** 

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Use the 8-Pin cable in the iOSD Markk II package when connecting to the DJI specified wireless video transmission module AVL58. ( 5) UsingtheiPadGroundStation
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©2013-2014 OJ! Innovations. All Rights Reserved. 3 I iPad Ground StationConnect the Air End of2.4G Bluetooth Datalinkto aspared CAN-Bus port of iOSD ifan

©2013-2014 OJI Innovations. All Rights Reserved. 3 I( 6) UsingthePCGroundStation

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Figure 1·11 1.3 LED Flight Indicators Description 1. LED ftigr>t indicators are used to show the aircraft's current status. Once powered on, the indicators will light up.

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Warnings and errors ·········--······-········-···········--···------·-·······' Remote Controller Signal Lost

.................... 

# ••••• 151 Level Low Battery Capacity Warning ©2013-2014 OJI Innovations. All Rights Reserved. 3 I**~--~---**

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**~--·-'"··----------------------··--·· "''"'''"'~'"''""'""-""''t'""'''''----~----------·~------**  ..**~----------------------- -------------------~-**  "'"""""'"'""'"'"""' i i Compass data abnormal because offerro-magnetic interference or i 

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## -~ ( 1 ) The LED indicators diagram above are for Phantom 2 mode. In Naza-M mode, LED indicators will work according to the Naza-M flight control system. ( 2 ) Connect to the PHANTOM 2 Assistant Software for detailed information about warnings and errors. 2. ThefrontlEDsarefor indicatingwhere the noseoftheaircraft is. They lightup solid red onlyafterthe motors have spooled up.
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1.4 Notes for PHANTOM 2 using with otherOJI products Before using PHANTOM 2with other DJI products, users should connecting the products correctly and upgrade the firmware as requirements below. Items to upgrade Firmware versions required P330CB (built-in V1.0.1.19 orabove

iOSD Mark II ••C
...........+-·····-·--·· ..- iQSD mini *TheiOSDAssistantSoftwareisappliedto both iOSD MarkII and iOSDmini.

©2013-2014 OJ! Innovations. All Rights Reserved. 3 I2 Propellers PHANTOM 2 uses the original9-inch propellers which are classified bythe colorof each central nut. Damaged propellers should be replaced by purchasing new ones ifnecessary.

Attach to the motor thread that has a black dot. Lock: Tighten the propeller in this direction. • Unlock: Remove the propeller in this direction. 2.1 Assembly

1. ( Figure 2-1 ) Remove the four warning cards from the motors after you've read them. 2. ( Figure 2-2 ) Prepare the two grey nut propellers and two black nut propellers. Make sure to match the black nut propellers with the correctly marked black dot motors. Tighten the propellers according to the fastening instructions.

Figure 2·1 Figure 2-2 Figure2-3 2.2 Disassembly

( Figure 2-3 ) Keep the motor deadlocked in place with the assistant wrench (or one hand) and remove the propeller acoording to the un-fastening instructions. 2.3 Notes

1. Propellers are self tightening during flight. DO NOT use any thread locker on the threads. 2. Make sure to match the propeller nut colors with the corresponding motors. 3. It is advised to wear protective gloves during propeller assembly and removal. 4. Check that the propellers and motors are installed correctly and firmly before every flight. 5. Check that all propellers are in good condition before flight. DO NOT use any ageing, chipped, or broken propellers. 6. To avoid injury, STAND CLEAR ofand DO NOT touch the propellers or motors when they are spinning. 7. ONLY use original DJI propellers for abetter and saferflight experience. ©2013-2014 DJIInnovations. All Rights Reserved. 3 I3 Remote Controller The PHANTOM2 remote controllercan be configured inthe PHANTOM RCAssistantSoftware. The sticks mode is Mode2on delivery.

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... Figure 3-1 " 

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Figure 3-2 [12]

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[1]Antenna [2]Carrying Handle [3]3-Position Switch S1 [4]3-Position Switch S2 [5]Joystick1(J1;J2) [6]Joystick2(J3;J4) [7]Neck Strap Attachment [8]Power Switch [9]Power Indicator [10]Battery Compartment [11]Micro-USB Port [12]Siide Lever [13]Potentiometer 3.1 Power on the RemoteController

1. Install the four AA Batteries (not included) into the battery compartment on the back of the remote controller according to the negative and positive poles. 2. Set the 81 and 82 switches to the upper most position and all sticks are at mid-point before switching on the powerswitch. 3. Push the power switch to the right to power on the remote controller. Ifthe power LED indicator is solid on, the remote controller is functioning normally. ( 1 ) Please make sure the batteries have enough capacity before use. If the low voltage warning alert sounds (refer to the <Remote Controller Power Indicator Status Information>), please replace batteries as soon as possible. ( 2 ) Using the correct type ofbatterywill prevent risk ofdamage or malfunction. ( 3 ) For long term storage, be sure to remove the batteries from the remote controller.
3.2 Remote controller PowerLED Indicator Status Sound Remote Controller Status None B-8-B
...... B-8-B
...... ©2013-2014 DJIInnovations.AII Rights Reserved. 31The remote controller will power off automatically when battery voltage drops below 4V. land and 

### ,A change batteries as soon as possible when the low voltage alert occurs to avoid loss ofcontrol during Hight 3.3 Antenna Orientation The remote controller's antenna should point skywardswithout obstructions for maximum communication range during flight.

Figure 3-3 3.4 Remote ControllerOperation

The operations ofremote controller are based on mode 2 stick oontiguration. Definitions The "stick neutral' positions and "stick released' mean the control sticks ofthe remote oontroller are placed at the central position. To "move the stick' means that the stick ofremote controller is pushed away from the central position. Slide lever is used forthe pitch control ofthe H3-2D and H3-3D gimbal.
Aircraft ( • 81 nosedirection )

Pushthestickup andtheaircraftwill rise. Pullthestickdown andthe aircraftwill descend. The aircraftwill automatically hoverand hold its altitudeifthesticksarecentered. Pushing the throttle stick above the centered (neutral) position will result in theaircrafttaking i off. We suggestthat you push the throttle stick

slowly to prevent the aircraft from sudden and

-**~--·** ---· -·**~** ... ___}**~::~n!]<J?~~e~.?t:!l.~.!:.**..•.. ©2013-2014 OJ! Innovations.All Rights ReseNed. 3 I.

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©2013-2014 DJIInnovations.AII Rights Reserved. 31 Theyawstickcontrolstheaircraftrudder. Push the stick left and the aircraft will counterclock-wise. Push the stick right and the aircraft will rotate clock-wise. Ifthe stick is centered, the aircraft willalwaysfly inthesamedirection. Thecommandstickcontrolstherotating angular velocity ofthe aircraft. Increasing movementof the command stick results in faster aircraft
The pitch stick controls the aircraft's front & backtilt. Push the stick up and the aircraft will tilt and fly forward. Pull the stick down and the aircraft will tilt and fly backward. The aircraft will keep level and straightifthestick is centered. Increasing movementofthe command stickwill result in a largertiltangle (maximum is 35") and The roll stick controls the aircraft left & right tilt. Push the stick leftand the aircraftwill tiltand fly left. Push the stick right and the aircraft will tilt and fly right. The aircraft will keep level and straightifthestick is centered. Increasing movementofthecommand stickwill result in a largertiltangle (maximum is 35°) and

switch from position-1 to position-3 and backto position-1, 5times ormoretoenterintocompass calibration mode. Users can configure position 3(bottom position) ofthe 81 switch to trigger the Failsafe in the Assistant Software. 82 is the IOC mode switch. IOC (Intelligent Orientation Control) function can be enabled in the Assistant Software when in Naza-M mode. Only use the IOC function afteryou arefamiliar withflying.

**"-~~<···~-~---·-** -----------Slide Lever controls the pitch ofthe H3-2D and H3-3D gimbal. The position of slide lever determines the pitch angle relative to the horizontallevel. Slide the lever left to make the gimbal pitch down upto a-90° position. Slide the lever right to pitch up to +0° position resulting in gimbal being at a horizontally level orientation. ( 1) For ·Ready to Fly' the aircraftwill hoverwhen all sticks are released. ( 2 ) For •Ready to Fly (non-GPS)' the aircraftwill only keep the altitude when all sticks are released. 3.5 Linking the remote controller& built-in receiver PHANTOM 2 has abuilt-in receiver, the linkbutton and indicatorlocated on the bottom ofthe aircraftas illustrated inthe Figure3-4. The link between the remote controller and aircraft is already established for you so you can initially skip this procedure.lfyoueverreplacetheremotecontroller, re-establishingthe linkisrequired. ' /

Linking procedures \.

Figure3-4 / linkbutton& Unkindicator

1. Power on the PHANTOM 2. 2. Turn on the remote controller and place it 0.5m-1m away from the aircraft. 3. Push the link button with athin object and hold it until the Link indicator blinks red, then release it 4. When the Link indicatorturns solid green, the link between the remote controller and the built-in receiver has been successfully established. Link Indicator Status The remote controller is linked with the receiver successfully.**~·····~--~-~-·-··-·-~··~--~······~···~·~·~-~~-~~-~·····~** The remote controlleristumed offandthere is no2.4GHzsignalaround, pleaseturn

©2013-2014 OJ! Innovations. All Rights Reserved. 31please carry outthe linking procedures. 4 Intelligent

**Batiery~,"~~,,~-,,~,-~~"'m~.o~·~···-···········,~·,···**..

**~------·-···········** The intelligent battery is specially designed forthe PHANTOM 2, with a battery capacity of5200mAh, voltage of 11.1Vand charge-discharge managementfunctionality. The battery should only be chargedwiththe OJI charger.

IntelligentBattery Charger DJIJntelligent Battery Functions ( 1 ) Balance Charging ( 2 ) Capacity Display ( 3 ) Communicating ( 4 ) Overcharging Protection ( 5 ) OverDischarging Protection ( 6 ) ShortCircuit Protection ( 7 ) Sleep Protection ( 8 ) Charging Temperature Detection Automatically balance the voltage of each battery cell during charging. Displaythecurrentbattery level. The main controller communicateswith the battery via communication ports forbatteryvoltage, capacity, currentand otherinformation. Charging stops automatically when the battery voltage reaches 12.8Vto prevent overchargingdamage. Discharging stops automaticallywhen the battery voltage reaches 8.4Vto preventoverdischarging damage. Automaticallycuts offthe powersupplywhen ashortcircuit isdetected. The batterywillentersleep modeafter 10 minutes ofinactivitytosave power. Thestatic current is 1OnA in sleep modewhenthe batteryis powered onwithoutconnectingtootherdevices. The batterywill chargeonlywhen itstemperature iswithinooc-55°C. Ifthe
1 batterytemperature isoutofthis range, the batterywill stopcharging. ( 1 ) Before use, please read and follow the user manual, disclaimer, and the warnings on the battery. Users take full responsibility for all operations and usage. ( 2 ) The battery should only be charged wilih the charger provided by DJI. DJI does not take any responsibility for operation ofany chargerfrom athird party. 4.1 Charging Procedures

1. Connect the charger to awall socket (Use the plug set ifnecessary). 2 Connect the batteryto the charger. Ifthe current capacity ofthe battery is over 75%, you should power on the battery to begin charging. 3. The Battery Level indicators display current capacity level as the battery charges. Please refer to battery level indicator description for details.
©2013-2014 OJ! Innovations. All Rights Reserved. 314. The battery is fully charged when the Battery Level indicator lights are off. Please disconnectthe charger and battery when the charging is completed. 

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4.2 Install the Battery Push the battery into the battery compartment correctly as the following diagram shows. Make sure to push the battery into the compartment until you hear a ·click' sound.

Figure 4-1 An incorrectly inserted battery may cause one ofthe following to occur: (1) Bad contact. (2) Unavailable battery information. (3) Unsafe for flight. (4) Unable to take off. 4.3 Battery Usage

LED2 LEDl Battery Level Indicator

Figure 4-2 

## • H·LED3 LED4 "·"Battery Power Button

(Built-in Battery Power Indicator)
(1) Checking the battery level: When the battery is powered off; pressing the battery power button once will indicatethe current battery level. Referto< Battery Level Indicator Description> for details. (2) Powering on:Whenthe battery is powered off; pressthe battery powerbutton once andthen press and hold for 2 seconds to turn on the intelligent battery. (3) Powering off: Whenthe batteryis powered on; pressthe battery powerbutton once and then press and hold for 2 seconds to turn offthe intelligent battery. (4) Checking the battery life: When the battery is powered off; press and hold the battery power button for 5 seconds to checkthe battery life. The battery level indicatorswill showthe life and the battery power indicator ©2013-2014 DJIInnovations. All Rights Reserved. 3 Iwill blink for 10seconds, then all LEOs will light out and the intelligent battery will tum off. Referto < Battery Level Indicator Description> for details. 

# e. More battery information is available in the battery tab ofthe PHANTOM 2 Assistant Software. 4.4 Description ofthe BatteryLevel Indicator The battery level indicatorswill showthecurrent battery levelduring both thecharging and discharging process as wellas batterylife. Thefollowing is adescriptionofthe indicators

. • :TheLEDissolidon • :TheLEDwillblinkregularly :TheLED is

0%-25% 25%-50% 50%-75% 75%-100% Full charged

62.5%-75% 50%-62.5% 37.5%-50% 25%-37.5%

90%-100% 80%-90% 

# • 

# • 70%-80% 

# • • 60%-70% 

# • • 50%-60%
©2013-2014 OJI Innovations. All Rights Reserved. 3 I4.5 Correct Battery Usage Notes 1. Never plug or unplug the battery intothe aircraftwhen it is powered on. 2. The battery should be charged in an environment that is between o·cto 40"C, and be discharged in an environmentthat is between -20"C to 5o•c. Both charging and discharging should be in an environment wherethe relative humidity is lowerthan 80%. 3. It's recommended to charge and discharge the battery thoroughly once every 20 charge/discharge cycles. Users should dischargethe battery untilthere is less than 8% power leftor until the battery can no longer be tumed on. Users should then fully recharge the battery to maximum capacity. This power cycling procedurewill ensurethe batteryisworking atitsoptimal level. 4. For long term storage please placethe batterywith only a40-50%capacity in astrong battery box securely.We recommend dischargingand chargingthe batterycompletelyonceevery3 monthsto keep it in good condition. The capacity should be varied in such acycle (40%-50%)-0%-100%-(40%-50%). 5. It's suggested you purchase a new battery after you have discharged your current battery over 300 times. Please completely discharge abattery priorto disposal. 6. It'ssuggested that you purchase anew battery ifthe current battery is swollen or damaged in any way. 7. Nevertryto recharge orflywith a batterythat is swollen ordamaged in any way. B. Neverchargethe battery unattended. Always chargethe battery on a non-flammable surface such as concrete and nevernearanyflammable materials. 9. Safety is extremely important and users can get more information in the DISCLAIMER.

©2013-2014 DJIInnovations.All Rights Reserved. 3 I5 Calibrating the Compass IMPORTANT: Makesureto performthe CompassCalibration procedures priortothefirstflight. The compass isverysensitiveto electromagnetic interferencewhich causes abnormal compass data and leadsto poorflightperformance orevenflightfailure. Regularcalibrationofthecompass enablesthe compassto performat its optimal level. 5.1 Calibration Warnings ( 1) DO NOT calibrate your compass where there is a possibility for the existence of strong magnetic interference such as magnetite, parking structures, and steel reinforcement underground. 

# 0 { 2) DO NOT carry ferromagnetic materials with you during calibration such as keys or cellular phones. ( 3) Compass Calibration is very important; otherwise the flight control system will work abnormally. 5.2 Calibration Procedures Please carry outthe calibrating procedures intheflightfield before flight. Pleasewatch the quickstartvideo ofthe PHANTOM 2for more compass calibration details.

Start cali Quickly flip the switch St

Position-1

**:,~)**

**'\-~**..

**~-** l.t--;"", Position-3 •J.!lb

........... Position-1->Position-3->Position-t

Flip no less than 5 times

LED Flight Indicator
Start horizontal calibration 360° Rotate the aircraft horizontally

LED Flight Indicator
Start vertical calibration Position-1

# :,iiiP,)

...\.Y:



# Position-3{(~

**Position-t->Positi~~-~Position-1** Flip once 5.3 When Recalibration is Required 360°Rotatetheaircraft vertically(Nose downward)



# t I LED Flight Indicator Normal LED 

# • 

# •

Succeed Fail
Re-calibrate

( 1 ) When Compass Data isabnormal,the LEDflight indicatorwillblinkalternatingbetween red andyellow. ( 2 ) Lastcompasscalibrationwas performedatacompletelydifferentflyingfield/location. ( 3 ) The mechanical structure ofthe aircraft has changed, i.e. changed mounting position ofthe compass. ( 4 ) Evident drifting occurs in flight, i.e. the aircraft doesn'tfly in straight lines. ©2013-2014 DJilnnovations.AII Rights Reserved. 316 Flight 6.1 Flying EnvironmentRequirements ( 1 ) Before your first flight, please allow yourself some flight training (Using a flight simulator to practice flying, getting instruction from an experienced person, etc.). ( 2 ) DO NOT fly in bad weather, such as rain orwind (more than moderate breeze) or fog. ( 3 ) The flying field should be open and void oftall buildings or other obstacles; the steel structure within buildings may interfere with the compass. 

# A ( 4 ) Keep the aircraft away from obstacles, crowds, power lines, trees, lakes and rivers etc. ( 5 ) Try to avoid interference between the remote controller and other wireless equipment. (No base stations or cell towers around) ( 6 ) The flight control system will not work properly at the South Pole or North Pole. ( 7 ) Never use the aircraft in a manner that infringes upon or contravenes international or domestic lays and regulations. 6.2 Starting the Motors ACombination StickCommand (CSC) is neededtostartthe motors. Pushthesticks accordingtoone oftheoptions belowto start motors. Oncethe motors have spun up, release both sticks simultaneously. The same command is usedtostopthe motors.

# ··~

.

# . --

# .. '

# . •

A B 

### c D Figure 6-1 6.3 Takeoff/Landing Procedures

1. Start by placing the PHANTOM 2 on the ground with the battery level indicators facing you. 2. Turn on the remote controller. 3. Power on the aircraft byturning on the intelligent battery. 4. When LED flight indicator blinks green/yellow, the PHANTOM 2 is entering Ready to Fly/Ready to Fly (non-GPS) mode. Start the motors with the esc command. 5. Push the throttle stick up slowly to liftthe aircraft offthe ground. Refer to <Remote Controller Operation> for more details. 6. Be sure you are hovering over alevel surface. Pull down on the throttle stick gentlyto descend and land. ©2013-2014 DJIInnovations. All Rights Reserved. 3 I7. After landing the aircraft on the ground, keep the throttle stick at its lowest position for about 3 to 5 seconds which will automatically stop the motors. 

## 0 You SHOULD NOT execute the esc during normal flight! This will stop the motors and cause the aircrafttodescend rapidlyand dropwithoutanytypeofcontrol. ( 1 ) When the LED flight indicator blinks yellow rapidly during flight, the aircraft has entered into Failsafe mode, referto <Failsafe Function> fordetails. 

## ,6, (2 ) A low battery capacity warning is indicated by the LED flight indicator blinking red slowly or rapidlyduringflight. Refertothe<LowBatteryCapacityWarningFunction>fordetaiIs. ( 3 ) Watch the quickstartvideo aboutflightformoreflight information. 6.4 Failsafe Function The aircraft will enter Failsafe mode when the connection from the remote controller is lost. The flight control systemwill automaticallycontrolthe aircraftto return to home and land to reduce injuries ordamage. The following situationswould maketheaircraftfailto receiveasignalfromthe remote controllerandenterFailsafe mode: ( 1 } The remote controlleris powered off. ( 2 ) The remote controller is powered on butthe 81 is toggled in the position triggering the Failsafe (this must have been configured in the PHANTOM 2Assistant Software). ( 3 ) The aircrafthas flown outoftheeffectivecommunication range ofthe remote controller. ( 4 ) There is an obstacle obstructing the signal between the remote controller and the aircraft, essentially reducing the distance the signal can travel. ( 5 ) There is interferencecausingasignal problemwiththe remote controller.
Failsafe works differently depending on the mode the aircraft is in when Failsafe mode is initiated whether it is in the Ready to Fly or Readyto Fly (non-GPS) mode. Readyto Fly (non-GPS) -Automaticlanding

The ftight control system will try to keep the aircraft level during descent and landing. Note that the aircraft may be drifting during the descent and landing process. ReadytoFly--Automaticgo horneand land

The ftight control system will automatically control the aircraft to fty back to the home point and land.
Home Point

When the aircraft is initializing the Ready to Fly status, the aircraft will record the current GPS coordinates as the home point. It is recommended to lift offonly after Ready to Fly status is confirmed for the safety ofbeing able to fty backto home point successfully in case the Failsafe mode is initiated.
©2013-2014 OJIInnovations.AII Rights Reserved. 31

## j
I Go Home Procedures 1Record Home Point. 2 Flying. 3 Remote controller signal lost
.

.**·---~*****-~** ... >• -- ;,_.,; ,. LED Flight Indicator**0~ ~t**  LED Flight Indicator 8 0 e •• LED Flight Indicato_r 4 Signal lost lasts3s, begin to go home. 5 Fly backto home point 6 Landing after hovering 15s. 

# w '
. 

## ..,.,.-**~~~~~~~~t:~~~:: ~:eight**  over home

### point~2om lED Flight Indicator;:;_, (J· ·,(' -:;,;,**-~'":·** Z' Figure 6-2 ( 1 ) In aFailsafe situation, if less than 6 GPS satellites are found for more than 20 seconds, the aircraft will descend automatically. In Phantom 2 mode, users can set a new home point manually when the aircraft is in "Ready to fly" status as long as a home point has been recorded automatically. Quickly flipping the S2 switch ofthe remote controller from upper most to lower most positions 5times or more will reset the current aircraft position as a new home point of PHANTOM 2. When successfully reset, you will see aseries of rapid green blinks on the LED Flight Indicator. The definition of"home point" is: ( 1 ) The home point is the place PHANTOM 2 returns to when the control signal is lost, which is recorded last time. ( 2 ) The home point is used to calculate the horizontal distance between you and the aircraft, the distance will be displayed as 

### 12.. ifusing iOSD module. Regaining Control during Failsafe Procedure**~----m---~-~~--~~,l~~.~.-~"~·~-~~-~~~·-~~~~--·~""~~;;?·:.:'~-~¥~'"-~·-···~~~--·~~~-~--r-·~-;;=·~~~;~··--N-~~"·~-~-~;7:=-~~---~~---~~~l** ' I**{~** I 

### ·<¥. I**·~** 

### ; ! Position (**\,~....** 

### i l.. ......./ t '.._.. ( 

### i · I l ! Position-3 ,

# t-::=~~~~t~J:':~::'~~;5;::~:-r:;::,::::~~=:~~~·~J-i ' control 

# I regain control. Ifremote controller's signal is 

# I recovered. '------**-----------~~£overed, ~-~~.l~!:.':~ur**  __**~':~-~-ac_l< ~o~~~-Pi~o~**  ___!__ ···--------------------------------- . 6.5 Low BatteryCapacityWarning Function The low batterycapacitywarning alerts userswhen the battery is closeto depletion during flight. When it appears, users should promptlyflybackand landtoavoid accidental dama_ge. The PHANTOM2 hal?two levels oflowbattery capacitywarning.Thefirstappearswhenthe battery has lessthan 30% powerandthesecond appearswhen it has ©2013-2014 DJIInnovations. All Rights Reserved. 3 Ilessthan 15%power. ( 1 ) When batterypowerdrops below30%and LED indicatorwill blinkredslowly. ( 2) At lowerthan 15%the LED indicatorwill blink red rapidly, the PHANTOM 2will also begin to descend and

land automatically.Afterithas landed, keepthethrottlestickat its lowestpoint orexecuteesc. ( 3 ) There is ahidden third lowbatterythreshold in addition tothe 1 stand2nd level warnings. This uses 10.65V as its threshold. Both thisvoltage threshold and the 2nd Level Low BatteryWarning will trigger auto-landing. Altitudecan be maintained ifnecessarybypushing uponthethrottlestick. ( 1 ) Rememberto fly your PHANTOM 2 backas soon as you see alow battery capacity warning. ( 2 ) Keeping the battery contact needles and pads clean is very important. Any dirt and dust may cause acommunication failure.
6.6 Flight Limits Function All UAV (unmanned aerial vehicle) operators should abide by all regulations from such organizations at ICAO (International CivilAviation Organization) and percountryairspace regulations. Forsafety reasons, theflight limits function is enabled by defaultto help users use this product safely and legally. The flight limits function includes height, distancelimits. In Ready to Fly status,

**heigh~** distance limits works together to restrict the flight. In Ready to Fly (non-GPS) status, only height limitworks and the flying height restricted to be not over 120m. (1) The default parameters in the Assistant Software is compliant within the definitions of class G ruled by ICAO. (Refer to Airspace Classification to get more details). As each country has its

**~** own rules, make sure to configure the parameters to comply with these rules too, before using the PHANTOM 2. (2) Users in Mainland China can refer to

**~ffl&t~l!itMif.}$.** Max Height & Radius Limits The Max Height & Radius restricts the flying height and distance. Configuration can be done in the PHANTOM 2 Assistant. Oncecomplete, youraircraftwillflyinarestricted cylinder.

**~l'<H}•Cl** ,._

**~** 't:

**[\~ :&~;** 

0 A

ispoweredon Figure 6-3 Figure6-4 ©2013-2014 DJIInnovations.AII Rights ReseNed. 31Ground Station flight height is restricted to fly Warning: Height limit reached. Warning: Distance limit reached.

Ground Station Rear LED flight indicator
None.

close to the Max radius limit

Rear LED flight indicator Warning: Height limit reached. None.

Not limited, no warnings or LED indicators.**'···-·----------~---------------------·--··-·-** ---··---·---·-···--·-...--------·---·-- (1) Ifthe aircraft flies out ofthe limits, you can still control your aircraft except to fly itfurther away. (2) If the aircraft is flying out of the max radius in Ready to Fly (non-GPS) status, it will fly back within the limits range automatically if6 or more GPS satellites have been found.
6.7 Flight Limits of SpecialAreas Special areas include airports worldwide. All special areas are listed on the OJI official website. Please referto htto:/lwww.dji.comlfly-safe/category-mcfordetails. These areas have been divided into category Aand category B. 8100m

10.5m CategoryA

©2013-2014 OJ! Innovations. All Rights Reserved. 3 I Category B Center of Special Area

Airspace: A,C,D Boundary:**~** g,.

QLimits Motors will not start. A Ifthe Phantomflies intoaspecial area in Readyto Fly (non-GPS) mode and Ready to Fly mode activates, itwill automatically descend and land then stop its motors. lfthe Phantomflies intoaspecialarea in Readyto Fly (non-GPS)modeand Readyto Flymodeactivates, itwill descendto airspaceCand hover5meters belowedgefl..

····-

## ____,_,_,___....,, No restrictions offlight, butthe Phantomwill notenter CategoryA, the aircraftcan flyfree, but itwill notenter Airspace Bthrough Boundaryb&d. Around Category Bsites, the phantomcan flyfreely, but itwill notenterintoAirspaceAthrough Boundary§.. No restrictions. 

# ......

None.

Semi-automaticdescent: All stickcommands are available exceptthethrottle stick command during thedescentand landingprocess. Motorswill stopautomaticallyafterlanding. Users musttoggletheS1 switchtoregaincontrol. Thisisthesameas regaining controlduring Failsafe. Please referto Regaining Control During Failsafe Procedure (Page23). (1) When flying in the airspace (AlB/C) of restricted special area, LED flight indicators will blink red

...... quickly and continue for 3 seconds, then switch to indicate current flying statusand continuefor5 seconds atwhich point itwill switch backto red blinking. (2) Forsafety reasons, please do notfly closeto airports, highways, railway stations, railway lines, citycentersandotherspecialareas.Trytoensuretheaircraftisvisible. 6.8 Conditions of Flight Limits In different working modes and flight modes, flight limits will differ according to number ofGPS satellites found. The following table demonstratesall the cases(·V: available; x:unavailable). All flights are restricted by height, distance and special areas simultaneously. The Failsafe and Ground Station operations are not restricted to flight limits, but if Ground Station function is used, the flight will be restricted the specialarea limits builtinto Ground Station. RefertotheGround Stationmanualfordetails.
©2013-2014 DJIInnovations.All Rights Reserved. 3 I! Phantom mode I Flight Status Limits of SpecialArea Max Height Max Radius 

## i r--------·Ready to Fly 

### v v v

Readyto Fly (non-GPS) X ..J X 

## !Naza-M mode

Control Mode number of GPSfound Limits of SpecialArea Max Height Max Radius )!6 

### v v 

# " GPS 

## i <6 X 

### v X 

### I )!6 

### v v X ATTl. ······- <6 X 

# " X

.... 

# .l··- <!6 X X X Manual <6 X X X I

-··- Disclaimer Please ensure thatyou are keptuptopate:vv!th**lnter,nation~L<j~dD,otl1e~~i9}W-:iPace** rules and regulations before usingthis product. By**usingthfspr9.(jlict.y,ptLherE!byagre~tothis ciisclal~~r~n.:clsignifythat** you have readthisfully. You agreethatyou are**responsli:>l¢fory~~rown'·~~l)~~ct**and contentwhileus[ngthis product, and foranydirect or indirect consequences**causedby~dtfolloWingthis tft~n~af,viei(.lte**  ordisregard any other applicable local laws,

. ·. _,·· :. ' - . administrative rules and social.habitsthereof.

©2013-2014 OJ! Innovations. All Rights Reserved. 3 I7 AssistantSoftware Installation and Configuration 7.1 Installing Driverand PHANTOM 2 Assistant Software

**r-----·---~-~-------~---~--"~'""--"-~----·-.......-----~-~-··----------·n**..**-------~--A0~»·-··-~--~-----··---** ..

**··~----~'-·-·-"'"-1** i Installing and running on Windows

1. Download driver installer and Assistant Software installer in EXE format from the download page of PHANTOM 2 on the DJI website. 2. Connectthe PHANTOM 2 to a PC via a Micro-USB cable. 3. Run the driver installerand followthe prompts to finish installation. 4. Next, run theAssistant Software installer and followthe promptstofinish installation. 5. Double clickthe PHANTOM 2 icon on yourWindows desktopto launch the software.

**A!~"** The installer in EXE format only supports Windows operating systems (Win XP, Win7, WinS (32 or 64 bit)). lnstallingand running on MacOS X 1. Download theAssistant Software installer in DMGformatfrom the download page ofPHANTOM 2 on the DJI website. 2. Run the installer and follow the prompts to finish installation.

3. When launching forthefirs.ttime ifuseLaunchpadto runthe PHANTOM2AssistantSoftware, Launchpad won' tallowaccess because the software has notbeen reviewed by MacApp Store.

? **~aAtom" can~**  beopened beu:useIt Is ftotn an unidenllfted de-veto-per.

4. Locatethe PHANTOM 2 icon in the Finder, pressthe Control key and then clickthe PHANTOM 2 icon (orright-clickthe PHANTOM 2 icon using amouse). ChooseOpenfromthe shortcutmenu, clickopen in the prompt dialog box and then software will launch. 5. Afterthefirstsuccessful launch, directly launching ofthesoftware can be achieved bydouble-clicking thePHANTOM2 icon intheFinderorusing Launchpad. ©2013-2014 DJIInnovations.AII Rights Reserved. 31**M>Wl'lti~** t'3PSLoetdiOI\ X Dom "'"' 

### "'"' A•>l!iMI:**&.h~t~** Tyee Ouad.fOt(Y. X

Yow "'""

......................... 1000
....................... ""

..... ""'""'"""'"" 1000 -tE!Jit "''"'"''"''"'''i 1000

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## .............................**~1(1-1** Mob!' Idle Spaod; RetommendOO ruon**1~** lrltettgent**f,~** Fadufot Melt!Ods: Go-f-kxne snd lar!ding**lO~** !ntelig(Jnl Qr;ootaflon Coolrd**O~F G~Swileh:** **S~I!I"..T\1** CU!reni'Voltage**Culuont~y:** F'wst**t.~** Warning: S$cond Lave! WartJing ON

12400mV 

### ""' """


## ....

Usage of PHANTOM 2 Assistant Software on Mac OS X and Windows are exactly the same. The Assistant Software pages appear in other places ofthis manual are on the Windows for example. 7.2 Using the PHANTOM 2 Assistant Software on a PC

1. Start up the PC, power on the PHANTOM 2, then connect the PHANTOM 2 to the PC with a Micro-USB cable. DO NOT disconnect until configuration is finished. 2. Run the PHANTOM 2_Assistant.**So~t~re** and**wai~** for the PHANTOM 2 to i::orinect to the Assistant Software. Observe the indicatcirs· •• on the oottdm ofthid;creen. When connected successfully, the connection indicator is E1> and communication indicator is blinkingG 3. Choose [Basic] or [Advanced] configuration pages. 4. View and checkthe current configuration in the [View] page.

PHANTOM2 f'tw ::!**~~.** r**~** - Viewconfigurations

___ c/' !1' ;,; @· L ·-----·---·--·--

..**~ "~'** **~** j**~** .._, ••• FunctionsWitch ofPhantom 2 and Naza-M mode**~** Language swap Account, software version

f",F':j**~~"M::.~** RC, Gain •.

# 1 _ : Gimbal,**Batter;~** , ..**·~.~""'~-** ........**~,..-~:.J** · Firmware upgrade**'·~·····O:::~~i""'·~...,;·"":i~···-··'l,'i;f,,.,;,~,,..**...**-,"""""'':i<~·+** IMU calibration

Communication indicator Connection indicator ). tr;,..; Y OWl l**~:,.** :t**~** ":>,J.:h


# _ ..........**-:.:~·~.~ -::.::~:::::.:..::** 
...**~ :.::.::_~** 

# . ..::::._:: "'This image is for reference only. Please refer tothe**f:!.4~.=-..** •••••••••••••••••••••••••• actual userinterface.
©2013-2014 OJI Innovations. All Rights Reserved. 3 I( 1 ) Users should not enable the Naza-M function before finishing Advanced Flight Maneuvers procedure in the " PHANTOM Pilot Training Guide". Ifthe Naza-M mode is enabled, users can switch the control mode between ATTI. Mode, GPS Mode or Manual Mode, and access the advanced settings (e.g. IOC). In addition, the LED located on the rear frame arms will display Naza-M flight status indications instead of the PHANTOM 2's indicators. Do not enable the Naza-M mode unless you are an experienced user or guided by aprofessional. ( 2 ) You can change to the Phantom 2 mode by clicking the same button used to turn on the Naza-M mode. This operation will disable the Naza-M mode and enable Phantom 2 mode. All parameters will be returned to factory settings. 7.3 Firmware upgrade of PHANTOM 2 Please referto the PHANTOM 2Assistant Software to install driverand PHANTOM RC Assistant Software, and then followthe procedures belowto upgrade the software and firmware; otherwise the PHANTOM 2 might not work properly.

1. An internet connection is required to upgrade PHANTOM 2'sfirmware. 2. Click the [Upgrade] icon to check the current firmware version and whether the installed firmware is the latest version. Ifnot, clickthe relative links to upgrade. 3. Be sure to wait until the Assistant Software shows "finished". Click OK and power cycle the PHANTOM 2 after 5 seconds. Once completed, the firmware is up to date.
PHAMTOM2 Pl.e.l;:l!l'1 "'•' b¥ - X

**~~** ./"

**(f~ ~**  i

.. ' "· J.

**~** dt

**~** ' ' j' Firmware upgradable items

Currentfirmw-areversion Upgrade link

"This imageis forrelerence only. Please refertothe •••••••••••••••••••••••• actual user interface.
(1) DO NOT power offuntil the upgrade is finished. (2) If the firmware upgrade failed, the main controller will enter a waiting for firmware upgrade status automatically. Ifthis happens, repeat the above procedures. 

# e. Firmware upgradable items: (1) Main Controller (2) P330CB(Main Board) (3) Receiver (4) Gimbal CMU (5) GimbaiiMU .(6) Battery ·'
©2013-2014 OJ! Innovations. All Rights Reserved. 317.4 PHANTOM RC Assistant SoftwareDescription Pleasefollowthe procedurestofinishthe configurationoftheremote controller.

1. Turn offthe remote controller and find the Micro-USB port on the bottom ofit. 2. Start up the PC, power on the remote controller, and then Connect the remote controller to the PC with a Micro-USB cable. DO NOT disconnect until the configuration is finished. 3. Run the PHANTOM RC Assistant Software and wait for the remote controller to connect to the Assistant Software. Observe the indicators •• on the bottom left ofthe screen. When connected successfully, the connection indicator is 0 and communication indicator is blinking 0
. 4. Finish configuration in the [Main] page. 5. Finish upgrade in the [Info] page ifnecessary.

•• 'I}!J!i < •

Main page ofthe2.4GHzremote controller

Main

Communicationindicator :; 

### i 

# .•---· 

# ..**/ijji~.:fi:i,**

I!!!B

J'M.Pr•:•f·lilm R::**~Blf!i)l1($-'oii'..,!,J~t~ ~sUb** **::o~ll~ur• ITill~91"~~** **IT.~[;,\ Ptl~l'l'.ct-'Remo:M:::~r:r~l~t** **S..~r.** 50C,H;**~PI!;'.I.(;.-.:1 ~**  'I '
...

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Firmware upgrade Account, software version**-=:o:~;;.** 

### -a:;:....,..__**,_~**

- ..........,.......... ' --· ._.--1--"- '"

- '""""'i""'"'" ' -11-"-----'--'-**-~c.:.:.;:,**

Connection indicate(, ••••••••••••••••••••••••• "This image is for reference only. Please referto the actual user interface.

©2013-2014 OJI Innovations. All Rights Reserved. 3 I8Appendix ,8:_1

**~p~_<;!fi_~_!!~_ll_!;** ________..---- ------·-

**----~----------** ·····-· --- --------------------------- --------------· Aircraft Operating environmenttemperature Power consumption Supported Battery Weight(includingthe battery) Recommend payload Maximum payload Hovering Accuracy (Ready to Fly) Max Yaw AngularVelocity Max Tiltable Ar]gle MaxAscent/DescentSpeed Max Flight Speed Wheelbase 2.4GHz Remote Controller Operating Frequency Communication Distance (open area) Receiver Sensitivity (1 %PER) Working Current/Voltage Battery OJIIntelligent Type Capacity Charging EnvironmentRange Discharging EnvironmentRange -1oac to 50°C 5.6W OJIIntelligent battery 1000g

**~1300g** 1350g Vertical: 0.8m; Horizontal: 2.5m 200°/S
.. ·.· · 35" '. Ascent 6m/s; Descent: 2m/s 15m/s(NotRecommended) 350mm
2.4GHziSM 1000m -97dBm 100mA@6V

3S LiPo Battery 5200mAh, 11.1V 0°Cto40"C -20"C to 50"C

Power On Warming Up&Aircraftcannottakeoffduring warming up Ready to Fly
···-·----------------•- -·-·· ·- -------------------------------· Readyto Fly(non-GPS)

-·------------------ Aircraft in abnormal status Warnings and errors Remote Controller Signal Lost ©2013-2014 OJ! Innovations. All Rights Reserved. 31,-..**~"'···~· ·-~'** **·~~--~"··~ ··-~·** ·- ! 

### ee e eee 

## !2"d Level Low Battery Capacity Warning j**••.--~-,-~-,~·-~~J**..**~•~v~•~,~~-~,.~~·-~-~-·~-~=~~-~~·---j~•·~--~·~•--~~-·~-··~"~ •••••-~·~** **'"'~'--"~ '''~~~~-~~•-'---"!**  

### rT-

•.••**~-·"·~·~-~=~~--~--·-,-~--·--·~-~~---** 

### i NotStationaryorSensorBiasistoobig ' i 1 Errors&Aircraftcannotfly* 1**r-----------------------------------------t-------------------------------------------------------------------------------------------~** i I Compass data abnormal because offerro-magnetic interference or i 

# i.

. . i : i 

### ! thecompassneedscalibration. 1

.------------------------------------------ _____L ------------------------------------------------ --------------------------------------------- ____J i

*Userscan connecttothe PHANTOM2AssistantSoftwaretogetdetailed informationaboutwarningsanderrors.

©2013-2014 OJ! Innovations.All Rights Reserved. 3 I