### May 15 , 2015

Exemption No. 11599 Regulatory Docket No. FAA

–20 15

–0 506

Mr. Christopher Alan Frank Rotary Image Marketing 9206 Timber Knoll Dr. College Station, TX 77845
Dear Mr. Frank : This letter is to inform you that we have granted your request for exemption. It transmits our decision, explains its basis, and gives you the conditions and limitations of the exemption, including the date it ends. By letter dated February 2 2, 2015 , you petitioned the Federal Aviation Administration (FAA) on behalf of Rotary Image Marketing (hereinafter petitioner or operator) for an exemption

. The exemption would all ow the petitioner to operate an unmanned aircraft system (UAS) to conduct aerial videography and cinematography to develop community awareness for housing and business properties

. See Appendix A for the petition submitted to the FAA des cribing the proposed operations and the regulations that the petitioner seeks an exemption

. The FAA has determined that good cause exists for not publishing a summary of the petition in the Federal Register because the requested exemption would not set a precedent, and any delay in acting on this petition would be detrimental to the petitioner

. Airworthiness Certification The UAS proposed by the petitioner is a Phantom 2 Vision +

.

### 2

The petitioner requested relief from 14 CFR part 21, Certification procedures for products and parts, Subpart H

— Airworthiness Certificates

. In accordance with the statutory criteria provided in Section 333 of Public Law 112

−95 in reference to 49 U

. S

. C

. § 44704, and in consideration of the size, weight, speed, and limited operating area associated with the aircraft and its operation, the Secretary of Transportation has determined that this aircraft meets the conditions of Section 333. Therefore, the FAA finds that the requested relief from 14 CFR part 21 , Certification procedures for products and parts, Subpart H

— Airworthiness Certificates , and any associated noise certification and testing requirements of part 36, is not necessary. The Basis for Our Decision You have requested to use a UAS for aerial data collection

. The FAA has issued grants of exemption in circumstances similar in all material respects to those presented in your petition. In Grants of Exemption No s . 11062 to Astraeus Aerial (see Docket No. FAA−2014−0352), 11109 to Clayco, Inc. (see Docket No. FAA

−20 14

−0507), 11112 to VDOS Global, LLC (see Docket No. FAA−2014−0382), and 11213 to Aeryon Lab s , Inc. (see Docket No. FAA−2014−0642), the FAA found that the enhanced safety achieved using an unmanned aircraft (UA) with the specifications described by the peti tioner and carrying no passengers or crew, rather than a manned aircraft of significantly greater proportions, carrying crew in addition to flammable fuel, gives the FAA good cause to find that the UAS operation enabled by this exemption is in the public i nterest. Having reviewed your reasons for requesting an exemption, I find that

—

 They are similar in all material respects to relief previously requested in Grant of Exemption Nos. 11062, 11109, 11112, and 11213 ;  The reasons stated by the FAA for granting Exemption Nos. 11062, 11109, 11112, and 11213 also apply to the situation you present; and
 A grant of exemption is in the public interest. Our Decision In consideration of the foregoing, I find that a grant of exemption is in the public interest. Therefore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701, delegated to me by the Administrator, Rotary Image Marketing is granted an exemption from 14 CFR §§ 61.23(a) and ( c ), 61.101(e)(4 ) and (5), 61.113(a), 61.315(a) , 91.7(a), 91.119(c), 91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 91.417(a) and (b), to the extent necessary to allow the petitioner to operate a UAS to perform aerial data collection

. This exemption is subject to the conditions and limi tations listed below. Conditions and Limitations
In this grant of exemption, Rotary Image Marketing is hereafter referred to as the operator.

### 3

Failure to comply with any of the conditions and limitations of this grant of exemption will be grounds for the immediate suspension or rescission of this exemption. 1. Operations authorized by this grant of exemption are limited to the Phantom 2 Vision+ when weighing less than 55 pounds including payload. Proposed operations of any other aircraft will require a new petition or a petition to amend this exemption

. 2. Operations for the purpose of closed

- set motion picture and television filming are not permitted. 3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The exemption holder may use either groundspeed or calibrated airspeed to determine compliance with the 87 knot speed restriction. In no case will the UA be operated at airspeeds greater than the maximum UA operating airspeed recommended by the aircraft manufacturer. 4. The UA must be operated at an altitude of no more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL. 5. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. This requires the PIC to be able to use human vision unaided by any device other than corrective lenses, as specified on the PIC’s FAA

- issued airman medical certificate or U.S. driver’s license.
6. All operations must utilize a visual observer (VO). The UA must be operated within the visual line of sight (VLOS) of the PIC and VO at all times. The VO may be used to satisfy the VLOS requirement as long as the PIC always maintains VLOS capability. The VO and PIC must be able to communicate verbally at all times ; electronic messaging or texting is not permitted during flight operations. The PIC must be designated before the flight and cannot transfer his or her designation for the duration of the flight. The PIC must ensure that the VO can perform the duties required of the VO.
7. This exemption and all do cuments needed to operate the UAS and conduct its operations in accordance with the conditions and limitations stated in this grant of exemption, are hereinafter referred to as the operating documents. The operating documents must be accessible during UAS operations and made available to the Administrator upon request. If a discrepancy exists between the conditions and limitations in this exemption and the procedures outlined in the operating documents, the conditions and limitations herein take precedenc e and must be followed. Otherwise, the operator must follow the procedures as outlined in its operating documents. The operator may update or revise its operating documents. It is the operator’s responsibility to track such revisions and present updated and revised

### 4

documents to the Administrator or any law enforcement official upon request. The operator must also present updated and revised documents if it petitions for extension or amendment to this grant of exemption. If the operator determines that any update or revision would affect the basis upon which the FAA granted this exemption, then the operator must petition for an amendment to its grant of exemption. The FAA’s UAS Integration Office (AFS− 80) may be contacted if questions arise regarding up dates or revisions to the operating documents. 8. Any UAS that has undergone maintenance or alterations that affect the UAS operation or flight characteristics, e.g. , replacement of a flight critical component, must undergo a functional test flight prior to conducting further operations under this exemption. Functional test flights may only be conducted by a PIC with a VO and must remain at least 500 feet from other people. The functional test flight must be conducted in such a manner so as to not pose an undue hazard to persons and property. 9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is in a condition for safe operation. 10. Prior to each flight, the PIC must conduct a pre

- flight inspection and determine the UAS is in a condition for safe flight. The pre

- flight inspection must account for all potential discrepancies, e.g. , inoperable components, items, or equipment. If the inspection reveals a condition that affects the safe operation of the UAS, the aircraft is prohibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight. 11. The operator must follow the UAS manufacturer’s maintenance, overhaul, replacement, inspection, and life limit requirements for the aircraft and aircraft components. 12. Each UAS operated under this exemption must comply with all manufacturer safety bulletins. 13. Under this grant of exemption, a PIC must hold either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC must also hold a current FAA airman medical certificate or a valid U.S. driver’s license issued by a state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal government. The PIC must also meet the flight revi ew requirements specified in 14 CFR § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate. 14. The operator may not permit any PIC to operate unless the PIC demonstrates the ability to safely operate the UAS in a manner consistent with how the UAS will be operated under this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from persons, vessels, vehicles and structures. PIC qualification flight hours and currency must be logged in a manner consistent with

### 5

14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs (training, proficiency, and experience

-building) and determining the PIC’s ability to safely operate the UAS in a manner consistent with how the UAS will be operated under this exemption are permitted under the terms of this exemption. However, training operations may only be conducted during dedicated training sessions. During training, proficiency, and experience

-building flights, all persons not essential for flight operations are considered nonparticipants, and the PIC must operate the UA with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119. 15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All operations must be conducted under visual meteorological conditions (VMC). Flights under special visual flight rules (S VFR) are not authorized. 16. The UA may not operate within 5 nautical miles of an airport reference point (ARP) as denoted in the current FAA Airport/Facility Directory (AFD) or for airports not denoted with an ARP, the center of the airport symbo l as denoted on the current FAA

-published aeronautical chart, unless a letter of agreement with that airport’s management is obtained or otherwise permitted by a COA issued to the exemption holder. The letter of agreement with the airport management must be made avai lable to the Administrator or any law enforcement official upon request. 17. The UA may not be operated less than 500 feet below or less than 2,000 feet horizontally from a cloud or when visibility is less than 3 statute miles from the PIC. 18. If the UAS loses communications or loses its GPS sign al, the UA must return to a pre - determined location within the private or controlled

- access property. 19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies. 20. The PIC is prohibited from beginning a flight unless (considering wind and forecast weather conditions) there is enough available power for the UA to conduct the intended operation and to operate after that for at least five minutes or with the reserve power recommended by the manuf acturer if greater. 21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All operations shall be conducted in accordance with an ATO

- issued COA. The exemption holder may apply for a new or amended COA if it intends to conduct operations that cannot be conducted under the terms of the attached COA

. 22. All aircraft operated in accordance with this exemption must be identified by serial number, registered in accordance with 14 CFR part 47, and have identification (N−Number) markings in accordance with 14 CFR part 45, Subpart C. Markings must be as large as practicable.

### 6

23. Documents used by the operator to ensure the safe operation and flight of the UAS and any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the PIC at the Ground Control Station of the UAS any time the aircraft is operating. These documents must be made available to the Administrator or any law enforcement official upon request. 24. The UA must remain clear and give way to all manned aviation operations and activities at all times. 25. The UAS may not be operated by the PIC from any moving device or vehicle. 26. All Flight operations must be conducted at least 500 feet from all nonparticipating persons, vessels, v ehicles, and structures unless: a. Barriers or structures are present that sufficiently protect nonparticipating persons from the UA and/or debris in the event of an accident. The operator must ensure that nonparticipating persons remain under such protectio n. If a situation arises where nonparticipating persons leave such protection and are within 500 feet of the UA, flight operations must cease immediately in a manner ensuring the safety of nonparticipating persons ; and b. The owner/controller of any vessels, vehicles or structures has granted permission for operating closer to those objects and the PIC has made a safety assessment of the risk of operating closer to those objects and determined that it does not present an undue hazard. The PIC, VO, operator trainees or essential persons are not considered nonparticipating persons under this exemption. 27. All operations shall be conducted over private or control led

- access property with permission from the property owner/controller or authorized representative. Permission from property owner/controller or authorized representative will be obtained for each flight to be conducted. 28. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of the operational area as defined by the applicable COA must be reported to the FAA's UAS Integration Office (AFS− 80) within 24 hours. Accidents must be reported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

. If this exemption permits operations for the purpose of closed

- set motion picture and television filming and production, the following additional conditions and limitations apply. 29. The operator must have a motion picture and televisio n operations manual (MPTOM) as documented in this grant of exemption.

### 7

30. At least 3 days before aerial filming, the operator of the UAS affected by this exemption must submit a written Plan of Activities 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 of the FSDO. The plan of activities must include at least the following: a. Dates and times for all flights; b. Name and phone number of the operator for the UAS aerial filming conducted under this grant of exemption; c. Name and phone number of the person responsible for the on

- scene operation of the UAS; d. Make, model, and serial or N−Number of UAS to be used; e. Name and certificate number of UAS PICs invol ved in the aerial filming; f. A statement that the operator has obtained permission from property owners and/or local officials to conduct the filming production event; the list of those who gave permission must be made available to the inspector upon request ; g. Signature of exemption holder or representative; and h. A description of the flight activity, including maps or diagrams of any area, city, town, county, and/or state over which filming will be conducted and the altitudes essential to accomplish the operation. 31. 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. Unless otherwise specified in this grant of ex emption, the UAS, the UAS PIC, and the UAS operations must comply with all applicable parts of 14 CFR including, but not limited to, parts 45, 47, 61, and 91. This exemption terminates on May 31, 2017 , unless sooner superseded or rescinded. Sincerely,

/s/ John S. Duncan Director, Flight Standards Service

# Documents

• Petition of Exemption
• Acknowledgement Letter
• Phantom 2 Vision+ User Manual
• Phantom Pilot Training Guide
• Phantom 2 Vision + Quick Start Guide
• UAS Flight Log
• UAS Maintenance Test Flight Log
• UAS Maintenance Log
• Copy of Rotary Pilot Certificate

## PETITION OF EXEMPTION for Rotary Image Marketing

a) 

### Christopher Alan Frank 9206 Timber Knoll Dr. College Station, Texas 77845 (979) 820-3096 chrisfrank83 @yahoo.com
b) 

### Request exemption from part 21, subpart Hand Sections 45.23(b), 61.113(a) and (b), 91.7(a), 91.9(b )(2), 91.1 03(b ), 91.109, 91.119, 91.121, 91.151(a), 91.203(a) and (b), 91.405(a), 91.407(a)(l), 91.409(a)(2), and 91.417(a) and (b) ofTitle 14, Code ofFederal Regulations (14 CFR). c) This exemption would allow Rotary Image Marketing to operate the Phantom 2 vision 

## + quad copter unmanned aircraft system (UAS) to conduct aerial videography and cinematography to develop community awareness for those parents/students who are planning to attend Texas A&M University and individuals, companies that are unfamiliar of the geographical layout of the Bryan/College Station area for housing and business properties. This exemption would allow Rotary Image Marketing to enhance real estate, small or large business, and apartment/ condo marketing.
The extent of each relief requested will be as follows:
CFR 45.23(b) Display of marks; general


### I request the UAS not to be either a certificated aircraft or a certificated "experimental" aircraft. Exemption from display of marks is requested due to its size and airspace that it will operate in.
CFR 61.113(a) and (b) Private pilot privileges and limitations: Pilot in command


### As I Chris Frank, currently hold a private rotary certificate with a third-class airmen medical certificate and currently a UH-60L PIC for the US Army, I understand the importance to be knowledgeable of the National Airspace System (NAS). However, I request that a non certificated pilot be able to operate the UAS with direct and written discretion of a certificated pilot with proper ground, operation and airspace training that is established by that certificated pilot. This appointed pilot would be tested in aircraft operation, maintenance, emergency procedures and the NAS before assuming operation

### of the UAS. A proper training program will be in place with documentation and training logs.
CFR 91.7(a) Civil aircraft airworthiness
Given that the UAS will not require an airworthiness certificate in accordance with 14 CFR part 21, I request exemption. Also, there is no FAA regulatory standard for determining the airworthiness of an UAS. The manufacturers operating documents will be used by the operator to determine if the UAS is airworthy.
CFR 91.9(b)(2) Civil aircraft flight manual, marking, and placard requirements
Followed by exemption :from CFR 45.23(b). Manufacturers operating manual shall be used and kept by the operator on location ofUAS operations
CFR 91.103(b) Preflight action
While there is no approved airplane or rotorcraft flight manual available for the UAS the manufacturers operating manual is requested to be used for proper preflight. Runways and airports will not be used to deploy or recover the UAS excluding them :from the preflight/planning action.
CFR 91.109 Flight introduction; simulated instrument and certain flight tests Although the UAS does not allow operation with a dual set of controls, proper hands on training ofUAS operation will be given to any operational pilot by a certificated pilot who has sufficient UAS operation hours. Simulated training may be used for sufficient operational training. All pilots will be familiar with preflight actions, routine flight operations, and emergency procedures.
CFR 91.119 Minimum safe altitudes: general
Notification of all residing tenets on which property the UAS is intended to operate on will be coordinated in advance. Tenets will be aware of the exact time and area that the UAS will be operating in.
CFR 91.121 Altimeter settings
The UAS operator will maintain a GPS that will have derived altitude capabilities to report feet AGL. Altitudes to be flown will be reported to local ATC before flight.

### CFR 91.151(a) Fuel requirements for flight in VFR conditions
The UAS operator will land the UAS prior to the manufacturer's recommended minimum level of battery power of 30%. The UAS shows a low voltage warning when 30% battery life is remaining. This provides ample time for the UAS operator to land in an immediate safe area. Also, the UAS is equipped with an automated function that lands the aircraft immediately when a low battery is detected.
CFR 91.203(a) and (b) Civil aircraft: certification required Operations ofthe UAS prove to be above safety standards due to its size, weight, speed, and limited operating area that it will be operated in
CFR 91.405(a) Maintenance required
This only applies to aircraft with airworthiness certificates. Maintenance of the UAS will be performed by the operator if a discrepancy is found during pre- flight and recorded on a "Maintenance Log" for personal history records.
CFR 91.407(a)(l) Operation after maintenance, preventive maintenance, rebuilding, or alteration
This only applies to aircraft with airworthiness certificates. Maintenance test flights will be performed after each maintenance discrepancy is corrected as a safety precaution and recorded on a "Maintenance Test Flight Log" for personal history records.
CFR 91.409(a)(l) and (2) Inspections
This only applies to aircraft with airworthiness certificates. Pre- flight will be performed as a safety precaution by the operator using the outlined procedures in the operating documents.
CFR 91.417(a) and (b) Maintenance records
This only applies to aircraft with airworthiness certificates. Any maintenance performed on the UAS will be recorded on a "Maintenance Log" for personal history records

### d) The UAS operations would provide more detailed and adequate information to potential individuals, companies looking to relocate to the Bryan/College Station area and promote economic growth overall. Also, the aerial videography would allow small business owners a more feasible option for marketing and advertisement over the high cost of manned rotary/fixed wing aircraft as in the past. Further, the UAS operation increases the safety of patrons due to its small size and lack of combustible fuel over compared to a large manned aircraft and reduces the ambient noise level helping to prevent noise complaints. Lastly, the UAS proves to be more ecological by emitting no exhaust fumes and requires no fossil fuels for operations. e) UAS operations will not reduce the safety of other airborne pilots, operating pilots, or patrons that are in an area ofUAS operation. Conversely, the UAS increases safety as it reduces flight operations by rotary wing aircraft flying at low levels while conducting videography operations which are conducive to a pilot becoming over task saturated and not recognize other flight dangers enabling them into a dangerous situation. Additionally the UAS size, weight, and speed do not pose a threat to the public or users of the NAS. f) (1) 

### Rotary Image Marketing request exemption from the requirements of part 21, subpart Hand Sections 45.23(b), 61.113(a) and (b), 91.7(a), 91.9(b)(2), 91.103(b), 91.109, 91.119, 91.121, 91.151(a), 91.203(a) and (b), 91.405(a), 91.407(a)(1), 91.409(a)(2), and 91.417(a) and (b) ofTitle 14, Code ofFederal Regulations (14 CFR). (2) 

### This exemption will permit Rotary Image Marketing to operate an Unmanned Aircraft System (UAS) for the purpose of conducting real estate and business videography and cinematography throughout the Bryan/College Station area to provide a more feasible and safer option for real estate and small business owners advertising and marketing. g) Supporting operating documents are attached. 

# /)**z~;~<** VI-

-**_;--·-·~** 

# I / 

# I ChriStopher 

### .N.. Frallk F eMruary 22, 1 2015

### Rotary Image Marketing 22 Feb 2015

To whom it may concern,

We are submitting this Petition of Exemption for the purpose of allowing businesses the financial ability to use videography and cinematography as a marketing tool for their business, property, and or house. Also, to showcase land and housing options for newcomers to the Bryan/ College Station area who may be unfamiliar to its geography My wife Jeanie Frank, is currently a real estate agent in the Bryan/College Station, Texas area and understands the needs of the local businesses and people. She works for United Country Real Estate which works largely in auction homes, large plots ofland, and homes with land acreage attached. She has developed the knowledge of how to market homes from photography resources but clearly understands the effectiveness in the video marketing power that a drone can provide for properties and housing. I myself am working on acquiring my real estate license to better understand and serve the people with a great service. I also currently am employed as an Airport Operations Manager at Easterwood Airport which is located in College Station, Texas. In 

### my duties, it is my job to comply with FAA requirements as a Part 139 airport and be in compliance with all FAA procedures as well. I understand the notification process that drones need to take with the local airports and I currently issue NOTAMS for the airport and local airspace. Additionally, I currently serve in the United States Army Reserve as 153D UH-60A/L Blackhawk Pilot. I have served in the military for 13 years and as a pilot for the last 5 years. I have over 500hrs of multi-turbine engine rotary time and serve as a Pilot In 

### Command (PIC). I write this letter hoping to show that our experience allows us to realize, understand and respect the very issues that the FAA is facing with drones for commercial use. Our years of experience and knowledge make us more heightened and aware of the obstacles that lie ahead but make us respect the process. As aviation enthusiast, we look forward to developing the UAS into the marketing world.

# p T U 1\.A 1 1 

## v1sl ser 

# 1v1anua l

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# 2 ISION+( Q)o 

### Contents Important Safety Notice 2 5.2 Power on the Remote Controller 17 Using This Manual 5.3 Remote Controller Power LED Status Key 2 Information 17 Important 2 5.4 Battery Level Indicator 17 Before Flight 2 5.5 Antenna Orientation 17 Watch the Tutorial Videos 2 5.6 Remote Controller Operation 18 Download DJI VISION App 2 5.7 Linking the Remote Controller and Overview Receiver 19 1 In the Box 5 Linking Procedures 19 2 Introduction 6 Link Indicator 19 Assembly and Use 5.8 Compliance Version Configuration 19 1 Removing Gimbal Clamp 7 6 Preparing the Range Extender 20 2 Preparing the Battery 7 6.1 Introduction 20

2.1 DJI Smart Flight Battery 7 SYSTEM Indicator 20 2.2 Usages 8 POWER Indicator 20 2.3 Charging the Flight Battery 9 Binding Reset Button 20 2.4 Battery Installation 10 6.2 Using Range Extender 20 2.5 Correct Battery Usage Notes 10 Charging the Range Extender 20 3 Preparing the Phantom 2 Vision+ 11 Powering on the Range Extender 21

3.1 Introduction 11 Checking the Battery Level 21 3.2 Built-in Flight Control System 11 6.3 Rename Range Extender SSID 21 FC Assistant Port 11 6.4 Binding the Phantom 2 Vision+ and 3.3 LED Flight Indicator Descriptions 12 Range Extender 21 3.4 3-axial Stabilized Gimbal 12 7 Downloading and Installing the Anti-drop Kit 13 DJI VISION App 22 Micro-SO Slot 13 7.1 Download and Install 22 Gimbal Error Warnings 13 7.2 Register and Login 23 3.5 Camera 14 [1] Register 23 Lens cap removal 14 [2] Login 23 Camera Function Buttons 14 [3] Usage tips·· 23 Camera Data Port 14 8 Connecting theiCam'era 24 Camera LED Indicator 15 8.1 Connecting Procedures 24 4 Attaching the Propellers 15 Wi-Fi Computer Connection Status

4.1 Introduction 15 Description 24 4.2 Assembly 15 Flight 4.3 Removing the Propellers 16 Flight Environment Requirements 25 4.4 Notes 16 Preflight Checklist 25 5 Preparing the Remote Controller 16 1 Calibrating the Compass 25

5.1 The Remote Controller 17 1.1 Calibration Procedures 25 © 2015 DJI. All Rigt·ts Reserved. 3

### bverview The Phantom 2 Vision+ is the next evolution of the Phantom 2 Vision. It features the same App enabled First Person View (FPV), high performance camera, remote camera control and in-flight content sharing, but adds to it a high performance 3- axial camera stabilization system. It is ideal for aerial creativity whether photo or video. In addition, it provides ground station function which allows users to plan the flight mission and enables aircraft to flight automatically. EJ:§ FPV: First Person View, see the world from the perspective of the craft and feel a true flying experience.

Check that all of the following items have been included in your package before use. If anything is missing, please contact your local dealer.

NO. Name

2

3

4

5

6

7

8

9

10

11

12

13 Aircraft

Propeller Pairs

Micro-SO Card

Lens Cap

Gimbal Clamp
Prop Wrench

Remote Controller

AA Batteries

OJI Smart Flight Battery

Charger

Power Cables

Plug Adaptors

Micro-USB Cable Picture

### ~**~**

# ~G 

# 0 0**~**

# ~ Qty.

4

4

2

2 Remarks

Integrated gimbal and camera

4 with black nut, 4 with grey

Inserted in aircraft Micro-SO slot

Fixed to camera lens

Attached to the gimbal

In maintenance packet

Includes attached Phone Holder and Range Extender

For Remote Controller

Inside aircraft

110-240V Adaptive

GB&CE

SAA&BS
For range extender charging and firmware upgrade

© 2015 OJI All Rights Reserved. 5 :::; ::;. (1) rn 0 XAssembly and Use 

### '\j: Choose between Phantom and Naza-M working modes using Phantom 2 Vision+ Assistant. If using Naza-M mode, please refer to the NAZA-M V2 Quick Start Manual for related instructions.

• Phantom: Flight settings will be selected automatically depending on whether 6 or more satellites have been found. This mode allows users to configure the Remote Controller and gain values, and use Failsafe and battery level warnings. • Naza-M: Flight settings will be identical to the Naza-M V2. Users can choose between GPS, Attitude, or Manual

mode. They can also access advanced settings including Intelligent Orientation Control (IOC). Rear LED Flight Indicators will display the flight status according to the Naza-M indicator. • Ready to Fly: When 6 or more GPS satellites have been found, the Flight Control System will lock its home point

and Rear LED Flight Indicators will blink a slow green (-:!g::·· ·····).This mode is ideal for beginners. • Ready to Fly (non-GPS): When less than 6 GPS satellites have been found, the Flight Control System will stabilize itself less than in full Ready to Fly rnode and will require more skilled flying. Rear LED Flight Indicators will blink a slow yellow 

### ('($· · · · ··-). 

### Assembly and Use Follow the below instructions to prepare for flight.

Pull gimbal clamp in the direction indicated to remove.

Figure 2 

### 0 To avoid damage to the gimbal, remove Gimbal Clamp before powering up the Phantom. 

### '\j: Attach the Gimbal Clamp during transportation or long terrn storage to avoid damage.

Ensure all related devices are fully charged before flying the Phantom 2 Vision+.

Devicec Remote Controller Range Extender
Aircraft (including gimbal and camera) Mobile Device
2.1 DJI Smart Flight Battery Power supply 2000mAh rechargeable LiPo battery Charge fully through Micro-USB slot. See Charging the Range Extender (Page 20) for details.

DJI Smart Flight Battery. Fully charge before using the DJI VISION App.

This battery has been specially designed for the Phantom 2 series. It has a battery capacity of 5200mAh, voltage of 11.1 V and charge-discharge management functionality. It can only be charged with a DJI charger or Phantom 2 Car Charger.

Smart Flight Battery Figure 3 DJI Charger Figure 4 © 20:5 OJI All R1ghts Reserved. 7 :0 CD 3 0 < :;· CD G) 3' 0' !'C 0 

# '" 3 '0Assembly and Use

----**~~----------------------** ---- ---**--------~-------**

Discharging process

LED1 LED2 LED3 LED4 Current battery level



### 0 0 0 

### 0 87.5%-100% 

### 0 0 0 jj)) 75%-87.5% 

### 0 0 0 0 62.5%-75% 

### 0 0 

# a 0 50%-62.5% 

### 0 0 0 0 37.5%-50% 

### 0 

## 11

. 

### 0 0 25%-37.5% 

### 0 

### 0 0 0 12.5%-25% 

# n 0 

### 0 0 0%-12.5% 

### 0 0 

### 0 0 <0%
Battery life When the battery is powered off, press and hold the Circular Power Button for 5 seconds to check battery life. Battery Level Indicators will show light up and the Battery Power Indicators will blink for 10 seconds. All lights will then turn off. For details, please see below.**----~-~- ~---~-~--------~----------~-~~-·~,...,...,.~** 

Ballet;y life

- - -**~**

LED1 LED2 LED3 LED4 Current battery life



### 0 0 0 g 90%-100% 

### 0 0 0**~j** 80%-90% 

### 0 0 0 

### 0 70%-80% 

### 0 0 

# n 0 60%-70% 

### 0 0 

### 0 0 50%-60% 

### 0 

# n 0 0 40%-50% 

### 0 

### 0 0 0 30%-40% 

# n 0 0 0 20%-30% 

### 0 

### 0 0 0 Less than 20% 

## & When batter life reaches 0, it is no longer operational. 

### ffi More battery information is available in the battery tab of the Phantom 2 Vision+ Assistant.
2.3 Charging the Flight Battery (1) Connect charger to wall socket (100-240V, 50/60Hz, using the Plug Adaptors if necessary). (2) Connect battery to charger. If the current capacity of the battery is over 75%, you should turn it on before beginning

to charge. (3) Battery Level Indicators will display current capacity level as the battery charges. ( 4) Battery is fully charged when Battery Level indicator lights are off. Disconnect the charger and battery when charging

is complete.

Figure 6

© ?.015 DJ! All**f·1iqh~s** F10smvsd. 9Assembly and Use

The Phantom 2 Vision+ is a quad rotor with a built-in Flight Control System with integrated gimbal and camera. It features an FC Assistant Port, Camera Data Port and a specialized battery compartment for its flight battery. All these features make the Phantom 2 Vision+ easy to assemble and configure. 3.1 Introduction [1] [2] [3] [4] [5] [6] [7] [8]

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Figure 8

Figure 9

Figure 10 [1] [2] [3] [4] [5] [6] [7] [8] [9] [10] [11] [12] [13] [14] [15] [16] [17] [18] Propeller (P15) Motor Front Sticker Front LED (P12) FC Assistant Port (Mic;-c,USB slot) (P46) Vibration Absorber Camera LED Indicator (P15) Camera Function Button (P14) Anti-drop Kit (P13) 3-axial Stabilized Gimbal (P12) Camera Lens (P14) Rear LED Flight Indicator (P12) DJI Smart Flight Battery (P7) Receiver Antenna (P17) Landing Gear Camera Data Port (Micro-USB slot) (P14) Compass (P25) Micro-SO Slot (P13) 3.2 Built-in Flight Control System The Phantom 2 Vision+ is equipped with a DJI Naza-M V2 Flight Control System. This provides incredible ease of use and stability. Pilots can control the Phantom's movements in many directions, including pitch (!onwards and backwards), roll (left and right), elevator (up and down) and yaw (turn left or right). The flight control system also can provide IOC, Failsafe and battery level warnings.
Modules Flight Controller

IMU

GPS & Compass
LED Flight Indicators

FC Assistant Port Furictior:is Acts as the brains of the complete flight control system, responsible for connecting and controlling all the modules together. Has a built-in inertial sensor and a barometric altimeter that measures both attitude and altitude. The compass reads geomagnetic information and assists the GPS (Global Position System) to accurately calculate the position and height of the aircraft. Indicates the status of flight control system.

The flight control system communicates with the PC Assistant through a Micro-USB cable between the Phantom FC Assistant Port and the PC. Users can use Assistant to configure the aircraft and upgrade the Phantom firmware. Please refer to Using the Phantom 2 Vision+ Assistant (Page 46) for details. © 2015 DJI. All Fiigl'to::**f~eserved,** 11 -u (0 u**~** :;· co :;. 

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Gimbal specifications Control accuracy ±0.03° Controllable range Pitch : -90°-0° Maximum angular velocity Pitch : 90°/s EEj • Non-FPV Mode: the gimbal will stabilize across 3-axial for smooth aerial creativity. • FPV Mode (First Person View Mode): Gimbal will lock to the movements of the Phantom for a FPV experience.
Anti-drop Kit The Anti-drop Kit helps keep the gimbal and camera connected to the aircraft. Two have been mounted on delivery. If new ones are required. take the gimbal and press part [ 1] through the center hole of the Vibration Absorber the center hole of part [2]. Lock them together as shown in [3]. Mounting the Anti-drop Kit diagonally is recommended. [1]

[2]

Figure 14 

### ffi Once part [1] and part [2] are connected, the Anti-drop Kit cannot be disconnected and reused.

Micro-SO Slot With flight battery powered off, make sure the Micro-SO card is inserted correctly into the Micro-SO Slot before taking any photos or recording any video.
The Phantom 2 Vision+ comes with a 4GB Micro-SO card and can support cards up to 32GB. The DJI VISION App may not be able to read some Micro-SO cards. Using the DJI VISION App to reformat new Micro-SO cards is recommended. Refer to Format Micro-SO Card (Page 37) for details. 

### 0 Do not insert or remove Micro-SO card when flight battery**i~** powered on.
Gimbal Error Warnings Figure 15

Before the aircraft takes off, if a gimbal motor error is detected or the gimbal clamp is not removed, there will be a warning prompt on the camera page of the DJI VISION App. This will disappear after the problem is resolved.



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__ _J 0 Distance:O.Oft**Alt~ude:O.Oft** Spe_ed:O.Omph Figure 16 Figure 17 © 2015 DJI. All Fiigbts neserved. 13Assembly and Use

Camera LED Indicator Camera LED Indicator lights up after the flight battery is powered on. It provides information on the working status of the camera. Camera LED lndicater 

### :If$> Green Solid ·:/f$:i: Slow Green Blink (0.2s on, 1.8s off) Wi;Fi**st~tus** OFF ON**·:i~?:-** Green Blink(0.1s on, 0.3s off, 0.1s on, 1.8s off) ON 

### :if$;:· Fast Green Blink (0.1 s on, 0.3s off) ON 

### -it;?t Orange Solid 

### :I[J;:- Orange Blink Once (0.2s on, 0.3s off)**:~f-Orange** Blink3 Times(0.1s on, 0.1s off) ·:ifJ!: Orange Fast Blink (0.1 s on, 0.3s off) OFF ON/OFF ON/OFF ON/OFF**·:r'~\-''g'** Green, Orange (0.2s green, 1.8s orange) ON**:(~** Red Solid**·i~\** Slow Red Blink (0.2s on, 1.8s off)**·:~"** Red Blink Once (0.2s on, 0.3s off) :C(li:- Red Blink 3 Times(0.1s on, 0.1s off)**:(~:;** Fast Red Blinks (0.1 s on, 0.3s off)**'(~1:-I~>@-** Fast Green, Orange and Red Blink (0.1s on, 0.3s off) ON/OFF ON/OFF ON/OFF ON/OFF ON/OFF
ON/OFF Camera. status Power On; Idle Idle Micro-SO card connected to PC Synchronizing Recording Taking a single picture. Taking 3 or 5 photos per shot Firmware Upgrading Recording Critical error CMOS sensor error Operation failed Micro-SO card error Upgrade error Overheated Camera

Always use original 9-inch propellers, classified by the color of each central nut. 4.1 Introduction Propellers Diagram Grey Nut (9450)
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__ Assembly Location Attach to motor without black dot. Fastening/ Un-fastening Instructions

4.2 Assembly El") Lock: Tighten propeller in this direction. "b

") Unlock: Loosen propeller in this direction. Black Nut (9450 R}

Attach to motor with black dot.

(1) (Figure 20) Remove warning cards from motors after you have read them. (2) (Figure 21) Spin grey marked propellers clockwise onto unmarked motors and black marked propellers anticlockwise for black marked motors.

Figure 20 Figure 21
@ 2015 DJI. A!l Flights Fiest:1rved. 155.1 The Remote Controller

[2] J3 [4] [3] J2 J4+i• [6] [5] 

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[7] [8] [9] [11] Figure 24 5.2 Power on the Remote Controller [1] Antenna [2] Left Dial [3] Switch S1 [4] Switch S2 (Reserved) Assembly and Use

[5] Right Stick: J1, Roll [left & right], J2, Pitch [front & back] [6] Left Stick: J3, Throttle [up & down], J4, Yaw [rotation] [7] Neck Strap Attachment [8] Power Switch [9] Power Indicator [10] Battery Charge & RC Assistant Port (micro-USB port) [ 11] Battery Level Indicator [12] Training Port (on back)
(1) Set S1 and S2 switches to the upper most position and place all sticks in the mid-point. (2) Toggle power switch to the right to switch on. (3) There will be a power on indicator beep. If the remote controller is set to be CE compliant. then there will be one beep, while the FCC compliant version will emit two beeps. The battery level indicator displays the current battery level. The indicator will blink green quickly, indicating the remote controller and receiver are linking. Once fully linked, the power indicator will change to a solid green. 

### & • If the low voltage warning alert sounds (refer to Remote Controller Power LED Status Information (Page 17) for details), please recharge the battery as soon as possible. • Using the incorrect type of charging cable may cause damage. • Following long term storage, recharge the battery before use. 5.3 Remote Controller Power LED Status Information Power LED Indicator Sound**:~:~'·-Solid** Green None**:~i--Solid** Red None '(\:i:-Solid Yellow None :®:·-Solid Red BB-BB-BB**'\~:'-** ...... Quick Red flashing B-B-B

......**:~::······Slow** Green flashing B-B-B

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5.4 Battery Level Indicator Remote Controllet$tatus Functioning normally. Charging( remote controller is powered off) Remote controller joysticks calibration error, need to be re-calibrate. Low voltage (from 3.5V-3.53V), recharge the remote controller. Critical low voltage (from 3.45V-3.5V). Recharge the remote controller immediately. Alert will sound after 15 minutes of inactivity. It will stop once you start using the remote controller.

Built-in LiPo Battery: The remote controller includes a rechargeable LiPo battery with a capacity of 2000mAh. You can monitor the current battery level using the LED indicators on the front panel of the remote controller as the figure shown: Battery Level Indicator 

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25% 50% 75% 100% 

### & The remote controller will show a blinking LED and sound an alert when the voltage drops below 3.45V, then automatically power off after 3 seconds. This process will repeat even if you power cycle the remote controller. If this low voltage warning occurs during flight. the remote controller will automatically power off, causing the aircraft to enter Failsafe mode, which cannot be interrupted (refer to Failsafe Function (Page27) for details). It is strongly recommended that you recharge the battery immediately when the 3.45V-3.5V low voltage warning occurs. 5.5 Antenna Orientation Keep the antennas pointing skyward, perpendicular to the ground for maximum remote controller range during flight. © 2015 DJI. All F1ight8 Fi8served. 17 g. CD :0 CD 3 0 (j) 0 0 

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