### May 4, 2015

Exemption No. 11451

Regulatory Docket No. FAA

– 20 15

– 0234

Mr. Michael A. Mang

Vice President

Butler, Fairman and Seufert, Inc.

8450 Westfield Boulevard, Suite 300

Indianapolis, IN 46240

Dear Mr. Mang :

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 January 29, 2015 , you petitioned the Federal Aviation Administration (FAA)

on behalf of Butler, Fairman and Seufert, Inc. ( hereinafter petitioner or operator ) for an

exemption. The petitioner requested to operate an unmanned ai rcraft sys tem (UAS) to

conduct aerial inspection, environmental monitoring, construction monitoring, and

preliminary engineering report related imagery for civil engineering projects

.

See Appendix A for the petition submitted to the FAA describing the proposed oper ations 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 DJI Phantom 2.

### 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 P ublic 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 and any associated noise certification and testing r equirements 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.

Ther efore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701,

delegated to me by the Administrator, Butler, Fairman and Seufert, Inc. 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 limitations listed

below.

### 3

Conditions and Limitations

In this grant of exemption, Butler, Fairman and Seufert, Inc. is hereafter referred to as

the operator.

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 DJI Phantom 2

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

exe mption 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 manufact urer.

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 visua l 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 ;

e lectronic messaging or text ing 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 exempt ion and all documents 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 accessi ble 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,

### 4

the conditions and limitations herein take precedence 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 p resent updated and revised

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 de termines 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 FA A’s

UAS Integration Office (AFS− 80) may be contacted if questions aris e regarding

updates 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 fl ight 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 ai rcraft 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 limi t 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, recreatio nal, 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 Col u mbia, 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.

### 5

14. The operator may not permit any PIC to operate unless the PIC demonstrates the

ability to safely operate the UA S 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 mu st be logged in a manner consistent with

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

(traini ng, proficiency, and experience

- building) and determining the PIC’s ability to

safely operate the UAS in a manner consisten t 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

traini ng, 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 defin ed in 14 CFR § 1.1. All

operations must be conducted under visual meteorological conditions (VMC). Flights

under special visual flight rules (SVFR) 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 i s obtained or otherwise permitted by a COA issued to the exemption

holder. The letter of agreement with the airport management must be made available

to the Administrator or any law enforcement official upon request.

17. The UA may not be operated less than 5 00 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 pr ivate or co ntrolled

- 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 manufacturer if greater.

21. Air Traffic Organization (ATO) Certificate of Waiver or Authorization (COA). All

operations sha ll be cond ucted 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

.

### 6

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.

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 a vailable 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, vehicles, and structures unless:

a. Barriers or structures are present that sufficiently protect nonparticipating persons

from the UA and/or debris in the ev ent of an accident. The operator must ensure

that nonparticipating persons remain under such protection. If a situation arises

where nonparticipating persons leave such protection and are within 500 feet of

the UA, flight operations must cease immediatel y 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 cl oser 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 fligh t operation that transgresses the lateral or vertical

boundaries of the operational area as defined by the applicable COA must be reported

to the FA A's UAS Integration Office (AFS− 80) within 24 hours. Accidents must be

reported to the National Transportat ion Safety Board (NTSB) per instructions

contained on the NTSB Web site: www.ntsb.gov

.

### 7

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 television operations manual (MPTOM)

as documented in this grant of exemption.

30. At least 3 days before aerial filming, the operator of the UAS affected by t his

exemption must submit a written Plan of Activities to the local Flight Standards

District Office (FSDO) with jurisdiction over the a rea 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 th e person responsible for the on

- scene operation of

t he UAS;

d. Make, model, and serial or N− Number of UAS to be used;

e. Name and certificate number of UAS PICs involved 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 p roduction, as specified in the

exemption holder’s MPTOM.

Unless otherwise specified in this grant of exemption, 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, a nd 91.

### 8

This exemption terminates on May 31 , 2017 , unless sooner superseded or rescinded.

Sincerely,

/s/

John S. Duncan

Director, Flight Standards ServiceJanuary 29, 2015

U.S. Department of Transportation

Docket Operations

West Building Ground Floor, Room W12

‐ 140 1200 New Jersey Ave., SE

Washington, DC 20590

Electronically Submitted via www.regulations.gov

Regarding:

The Butler, Fairman and Seufert Inc. Petition for Exemption pursuant To Section 333 of the FAA

Modernization Reform Act of 2012 (FMRA) includes 14 C.F.R. 45.23(b); 14 C.F.R. Part 21; 14 C.F.R.

61.113(a)&(b); 91.7(a); 91.9(b) (2); 91.103(b); 91.109; 91.119; 91.121; 91.151(a); 91.203(a)&(b);

91.405(a); 91.407(a) (1); 91.409(a) (2); 91.417(a)&(b)

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the

“Reform Act”) and 14 C.F.R. as noted above, Butler, Fairman and Seufert Inc. (“BF&S” or

“Petitioner”) hereby submits this petition for exemption to authorize civil operations of small

Unmanned Aircraft Systems (“sUAS”) for the purposes of aerial inspection, environmental monitoring,

construction monitoring and preliminary engineering report related imagery for civil engineering related

projects. Including private properties and public properties owned by State or Local governments within

the Continental United States. As a full

‐ service civil engineering firm BF&S proposes to directly operate

sUAS for commercial operation by employees and contractors as a value added benefit for civil

engineering related projects.

This petition is, in most regards, similar to granted exemption No. 11138 both in operational approach

(closer than 500’) and equipment being utilized (DJI Phantom 2 ).

Applicant name and address is:

Butler, Fairman and Seufert Inc.

Attn: Michael A. Mang, Vice President

8450 Westfield Blvd, Suite 300

Indianapolis, Indiana 46240

Phone: (317)

‐ 713

‐ 4615

Fax: (317) 713

‐ 4616

Email: mmang@bfsengr.com

Public Interest

BF&S was incorporated in 1961 and is a multi

‐ faceted Civil Engineering firm with an emphasis on

transportation and related infrastructure. BF&S has multiple offices in Indiana and works with

communities throughout Indiana and surrounding states. Currently there are over 140 employees with

various disciplines and professional licenses providing services in core areas including airport design andinspection, asset management, bridges, construction inspection, environmental services, GIS, MS4,

greenways/streetscapes, historic architecture, landscape architecture, land use planning, parks, right

‐ of

‐

way services, roadways/highways, site development, survey, trails, water & wastewater.

The granting of this exemption request would provide State and Local officials (our clients), engineers

and environmental scientists with high

‐ resolution imagery of infrastructure and equipment, including

roadway, bridges, airports, elevated water tanks, water/wastewater treatment facilities and storm

water management. Such sUAS operation will provide safety enhancements in and around surrounding

areas and increase efficiency and reliability of inspections and investigations. The use of sUAS will

reduce the risk of inspections by reducing the need for human inspection by personnel on permanent

and temporary elevated structures currently being performed by bucket trucks, lifts, and ladders.

Reduce needs for boating or on water activities. It would also reduce personnel time in vehicle traffic

and reduce maintenance of traffic activities. sUAS operation will improve efficiency and reliability of

inspections by allowing for higher quality inspections which serve the public interest and provide a new

level of detail and transparency to public projects.

Additionally, BF&S uses for the sUAS have safety benefits that include reducing the danger and

emissions associated with full size aircraft. sUAS have no fuel to ignite or explode, and no crew adds a

greater degree of flexibility. The sUAS further minimizes ecological and ground safety issues to the

general public and property owners.

Proposed Location Areas

BF&S has years of experience in working with the FAA on airport construction and rehabilitation projects

and realizes that regulations are needed to protect the National Airspace System (NAS). We also do not

wish to create any new burdens on existing FAA processes and facilities. Our sUAS area of use will be

broad and that each project location has different requirements in terms of the NAS. The operation

location areas have been designated as follows:

1. Airport property (limited basis)

2. Airport property to five miles out

3. Populated areas and Public Right

‐ of

‐ Way

(Populated areas are determined by yellow areas on VFR Sectional Aeronautical Charts or as

determined by local public safety officials.)

4. Uncontrolled Airspace/Private Property

5. Municipally/locally owned utilities and structures

With respect to operations on or near airports the following is offered for consideration:

 Unlike proposals by individuals or persons with no aviation knowledge, our firm is uniquely

equipped to operate on/near airport property by virtue of our line of business. BF&S has

advanced licensed pilots on staff, with trained individuals that routinely escort contractors in the

AOA, as wells as SIDA badged staff, at numerous airports, including commercial airports with

Class C airspace. Collectively, this team knows airports intimately, and can make the call

whether a certain sUAS flying scenario makes sense or not and would be able to synthesize with

FAA on approaches to integrating sUAS into the NAS.

 In each case, a COA will be sought, and recommendations/restrictions will be followed. All possible coordination with airport management will take place prior to any operation on or

near airport property.

 All necessary NOTAM’s will be coordinated and issued per COA.

 Operations on airport property will not commence until such time that the PIC has established

proficiency by accumulating and logging in a manner consistent with 14 CFR 61.51(b) [as

applicable] at least 10 hours flight time as a sUAS pilot with a multi

‐ rotor sUAS consistent with

exemption No. 11062.

 sUAS operations will be limited to scenarios for which if attempted by normal aircraft, may

endanger the pilot, persons, or property and which may create the potential of operating in a

condition that may violate FAR’s.

 On airport operations will be sequenced utilizing the N# (submitted for issuance) on the CTAF or

with ATCT as appropriate, and shall always begin and terminate outside of any RSA.

Communications will be transmitted using a handheld radio capable of operating in the same

aviation frequency range and bandwidth as normally utilized by airport department staff during

airport inspection projects.

 BF&S will utilize the strictest right

‐ of

‐ way rules and yield to any other manned aircraft that may

potentially be in conflict.

 The pilot being utilized for this type of operation has 8 years airport management experience at

a towered airport, is a CFI with Multi

‐ Engine and Instrument ratings, and 6 years of experience

as listed named responsible party on 7711

‐ 1 Certificates of Waiver or Authorization for annual

airshow and R/C events at a FAR 139 airport, and has experience building and flying R/C aircraft.

His knowledge and experience will ensure that any COA on or near airport property is executed

with due diligence and within the confines of approval.

Proximity

With regard to operating in close proximity, generally operations will be conducted no closer than 500’.

In instances where, for the purposes of successful data acquisition, a flight closer than 500’ is required,

prior permission will be sought from any owner or oversight entity having jurisdiction. An example

would be gathering data and imagery to augment inspection of a bridge, water tower, or other tall

structure. Not only will the sUAS be able to capture images not possible in any other way, it removes

the risk of an individual attempting to climb, or reach areas in need of inspection. The risks to life

utilizing sUAS in this manner are far less than conventional methods.

All reasonable precautions will be considered and integrated into the flight plan to ensure the safety of

persons and property, and shall immediately cease should any barrier to safe operations be

encountered.

All reasonable precautions will be taken to ensure safety of non

‐ participating persons. In cases where

barriers or structures can be used, or operations conducted such that in a crash event, persons and

property will be shielded from any debris, the operation will be approached in that manner.

Any flight that is compromised by an unauthorized person shall be immediately terminated until the

breach is clear and precautions are taken to prevent further inadvertent entry.Small Unmanned Aircraft System

BF&S will utilize the DJI Phantom 2 Quadcopter for all locations, areas and operations specified herein.

The Phantom 2 sUASs have a maximum take

‐ off weight of less than 7 pounds, the flight speed will not

exceed 35 miles per hour, and it will not be flown at an altitude that exceeds 400 feet AGL. All flights will

be flown in such a way that they can be safely terminated with a reserve battery power of 25% of the

battery's maximum charge. The DJI Phantom 2 sUAS does not carry any flammable propellant or fuel.

The Phantom 2 sUAS also has an integrated GPS system that calculates the sUAS’s position and height

and relays that information via a secure connection back to ground control station. The on

‐ board flight

computer also can receive signals for flight controls from the ground control station. An on

‐ board

camera capable of capturing imagery in the form of full color, high definition still photos and video that

will also be transmitted back to the ground control station. Additionally, the Phantom 2 sUAS contains

gyro stabilized flight mode, GPS aided navigation, a compass, blinking LED’s on the bottom, a failsafe

mode if its connection to the remote control is lost, and the system permits the sUAS to return to a

predetermined location and land without injury or damage. For additional safety, the Phantom 2 will be

retrofitted with prop guards. The Phantom 2 will be identified by serial number, registered as a public

aircraft and have identification (N

‐ Number) markings with markings as large as practicable per guidance

of UAS Integration Office, AFS

‐ 80, at minimum 1 inch tall on all four sides of the main body.

A transportable Ground Control Station will be utilized in the sUAS. The Ground Control Station will be a

BF&S identifiable vehicle or trailer equipped with lighted beacons, strobes and horns capable of being

seen and heard from 500 feet away. The vehicle or trailer will be stationary during all flight operations.

The vehicle will carry temporary construction style signs for warning motorists of drone survey

operations, ground wind speed indicators, as well as all OSHA required safety equipment relating to

surveying and construction inspection related operations. All flight control equipment, documentation,

the Pilot in Command (PIC) and Visual Observer (VO) will be incorporated into the Ground Control

Station.

BF&S will carry out maintenance, inspections, and record keeping requirements, in accordance with the

operator’s manual. Maintenance, inspection, and alterations will be noted in the aircraft log, including

total flight hours, description of work accomplished, and the signature of the authorized sUAS technician

returning the sUAS to service.

Unmanned Aircraft Pilot in Command (PIC)

For uncontrolled airspace or private property the PIC will possess a private pilot certificate and a current

third

‐ class medical certificate. For all other airspaces the PIC will possess a commercial pilot certificate

and a current first or second class medical certificate. Additionally, all pilots will be assisted by a visual

safety observer, who will communicate verbally with the PIC at all times.

The sUAS will be operated within visual line of sight (VLOS) of the PIC at all times. The PIC shall use

human vision unaided by any device other than corrective lenses, as specified on the PIC’s FAA

‐ issued

medical certificate.

The PIC must have accumulated and logged, in a manner consistent with 14 CFR § 61.51 (b), a minimum

of five hours as sUAS pilot operating the make and model of sUAS to be utilized for operations under the

exemption and three take

‐ offs and three landings in the preceding 90 days. Training will be conductedper manufacturer’s recommendations to ensure proficiency and experience

‐ building, to include normal

and emergency maneuvers, and take

‐ off and landing.

Unmanned Aircraft Operation

Prior to each flight the PIC will inspect the sUAS to ensure it is in a condition for safe flight. If the

inspection reveals any issues that affect the safe operation of the sUAS, the aircraft will not be operated

until the necessary maintenance has been performed and the sUAS is found to be safe for flight. The

Ground Control Station, will be included in the preflight inspection. All maintenance and alterations will

be properly documented in aircraft records. These documents will be kept at the ground control station,

and project field office if available.

A Notice to Airman (NOTAM), coordination with local airport management, notices to private

landowners and local law enforcement officials will be submitted not more than 72 hours in advance,

but not less than 48 hours prior to all flights. A Plan of Activities will also be sent to the local FSDO with

jurisdiction over the flight area. These documents will be kept at the Ground Control Station, and project

field office if available.

Every effort to will be made to keep flight operations from directly over any person or as far away as

possible, and all flights will remain over the project or construction area. Construction style signs will be

temporarily set up to warn vehicles of drone flight in roadway areas. Construction crews in the project

area will be notified 30 minutes in advance of any flights. Drone flight awareness will also be

incorporated into project safety meetings.

The Ground Control Station will not move during flight operations. Light beacons and strobes will remain

on during all flight operations from takeoff to landing. Horns will be sounded during takeoff and landing.

Best safety practices shall be used to reduce public or non

‐ project related personnel exposure in flight

areas. Flights will be aborted in the event of unpredicted obstacles, emergencies within the flight area,

or as directed by local law enforcement agencies.

Right of Way will be yielded to all other flight manned operations and activities at all times. Including

but not limited to ultralight vehicles, hang gliders, or parachuting or parasailing activities.

Operations will only be conducted during daylight and under visual meteorological conditions. Ground

wind speeds at the Ground Control Station shall not exceed UA manufacturer’s recommendations.

Flights shall be operated at an altitude of no more than 400 feet above ground level (AGL).

The sUAS shall be operated within visual line of sight (VLOS) of the PIC.

Any accidents, or flight operation issues will be reported to the appropriate FAA office within 24 hours.Summary

The Butler, Fairman and Seufert Inc. Petition for Exemption pursuant to Section 333 of the FAA

Modernization Reform Act of 2012 (FMRA) includes 14 C.F.R. Part 21; 14 C.F.R. Part 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)&(b);

91.405(a); 91.407(a) (1); 91.409(a) (2); 91.417(a)&(b) as found below:

Respecting 14 CFR Part 21 Subpart H, entitled Airworthiness Certificates, sets forth requirements for

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

and restricted operational capabilities of the Phantom 2 permits exemption from Part 21 because it

meets (and exceeds) an equivalent level of safety pursuant to Section 333 of the Reform Act. The FAA is

authorized to exempt aircraft from the airworthiness certificate requirement under both the Act (49

U.S.C. § 44701 (f)) and Section 333 of the Reform Act. Both pieces of legislation permit the FAA to

exempt UAS's from the airworthiness certificate requirement in consideration of the weight, size, speed,

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

Respecting 14 CFR Part 45.23(b) Title 14 of the Code of Federal Regulations 45.22(d), Exhibition, antique,

and other aircraft: Special Rules, permits persons to apply to the Administrator for a different marking

procedure if it is impossible to mark an aircraft per §§45.21 and 45.23 through 45.33. BF&S is

requesting an alternate marking for the DJI Phantom 2 Quadcopter registration marks. The DJI Phantom

2 is a small Unmanned Aerial System (sUAS) Quadcopter that cannot comply with the aircraft marking

standards per §§45.21 and 45.23 through 45.33. The achievement of equivalent level of safety for the

Phantom 2 as that it will be identified by serial number, registered and have identification (N

‐ Number)

markings with markings as large as practicable per guidance of UAS Integration Office, AFS

‐ 80, minimum

1 inch tall on all four sides of the main body. The request was submitted on January 28, 2015.

Respecting 14 CFR Part 61.113(a)&(b) relief is requested since limitations state that a private pilot may,

for compensation or hire, act as PIC of an aircraft in connection with any business or employment if (1)

The flight is only incidental to that business or employment; and (2) The aircraft does not carry

passengers or property for compensation or hire. BF&S proposes an equivalent level of safety in that a

PIC with a private license will operate the sUAS for hire in the locations where a private license is

sufficient (i.e. private property not in the vicinity of an airport) which may be the majority of the time,

not just incidentally. The proficiency of the sUAS pilot with a private license versus a commercial license

does not correlate with operating a sUAS in the NAS. BF&S contends an equivalent level of safety will be

maintained because no PIC will be allowed to operate the Phantom 2 unless the PIC has demonstrated,

through ongoing training and currency requirements that the PIC is able to safely operate in a manner

consistent with applicable rules and operating criteria for that specific sUAS.

Respecting 14 CFR Part 91.7(a) prohibits the operation of an aircraft without an airworthiness

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

Regulation does not apply.

Respecting 14 CFR Part 91.9(b) (2) requires an aircraft flight manual in the aircraft. As there are no pilots

on board, or passengers, and no cockpit, and given the size of the sUAS, this Regulation is not

applicable.Respecting 14 CFR Part 91.103(b) prescribes that a pilot shall for any flight, become familiar with runway

lengths at airports of intended use, and takeoff and landing distance information. Reference Exemption

No. 11138 for reason why exemption is not necessary.

Respecting 14 CFR Part 91.109 Flight instruction; Simulated instrument flight and certain flight tests.

Reference Exemption No. 11138 for reason why exemption is not necessary.

Respecting 14 CFR Part 91.119 Minimum safe altitudes. With regard to operating in close proximity,

generally operations will be conducted no closer than 500’. In instances where, for the purposes of

successful data acquisition, a flight closer than 500’ is required, prior permission will be sought from any

owner or oversight entity having jurisdiction. An example would be gathering data and imagery to

augment inspection of a bridge, water tower, or other tall structure. Not only will the sUAS be able to

capture images not possible in any other way, it removes the risk of an individual or crew attempting to

climb, or reach areas in need of inspection. The risks to life utilizing sUAS in this manner are far less

than conventional methods. All reasonable precautions will be considered and integrated into the flight

plan to ensure the safety of persons and property, and shall immediately cease should any barrier to

safe operations be encountered. All reasonable precautions will be taken to ensure safety of non

‐

participating persons. In cases where barriers or structures can be used, or operations conducted such

that in a crash event, persons and property will be shielded from any debris, the operation will be

approached in that manner.

Respecting 14 CFR Part 91.121 Altimeter Settings. BF&S will set the altimeter to zero feet AGL rather

than local barometric pressure or field altitude before flight.

Respecting 14 CFR Part 91.151(a) Fuel requirements for flight in VFR conditions. Prior UAS

‐ specific relief

has been granted in Exemption Nos. 8811, 10808, and 10673 for daytime, VFR conditions. To achieve an

equivalent level of safety, BF&S proposes flying the Phantom 2 per the operating manual leaving ample

power to safely conclude the flight with power remaining, even auto land when a low battery is

detected.

Respecting 14 CFR Part 91.203(a)&(b) Civil aircraft: Certifications required. BF&S requests relief from the

requirement of Section 91.203(a) (i.e., that an appropriate and current airworthiness certificate and an

effective U.S. registration certificate be carried within the aircraft), and further, BF&S requests relief

from the requirement of Section 91.203(b) (i.e., that the airworthiness certificate be displayed at the

cabin or cockpit entrance so that it is legible to passengers or crew). As the DJI Phantom 2 sUAS is

unmanned, it has no cabin, cockpit, pilot station, or entrances thereto. Therefore, the aircrew member

is located at a ground control station and no passengers are carried at any time. As such, BF&S proposes

the following conditions and limitations to its request for exemption from Sections 91.203(a) and (b):

The documents required by Sections 91.203(a) and (b) must be kept at the ground control station,

where it is immediately available to the aircrew member (pilot in command) of the DJI Phantom 2 sUAS

any time the unmanned aircraft is operating. The documents required by 91.203(a) and (b) will be made

available within 10 days to any FAA, U.S. Department of Defense, or law enforcement official upon

request.

Respecting 14 CFR Part 91.405(a) Maintenance required, and Respecting 14 CFR Part 91.407(a) (1)

Operation after maintenance, preventive maintenance, rebuilding, or alteration, and Respecting 14 CFR

Part 91.409(a) (1) and (2) Inspections, and Respecting 14 CFR Part 91.417(a)&(b) Maintenance records.

As noted previously, BF&S will carry out maintenance, inspections, and record keeping requirements, inDJI PHANTOM 2

‐ Maintenance and Flight Log

GENERAL

PIC:__________________________________

VO:__________________________________

Date:____________________ Location:

_____________________________________________

AIRCRAFT

N______________

Pre

‐ flight Inspection: Yes No Aircraft Maintenance Status:______________________

Return to Service by:_____________________________________________

Comments:

_________________________________________________

WEATHER

Ceiling:__________

Visibility:_____________

Winds:_______________

FLIGHT DETAILS

Nearest major intersection:

____________________________________________________ Proximity to local road:

__________________________________________________ Proximity to Structure:

________________________________________________

Approx. Takeoff Time :___________________

Approx. Landing Time:______________________

Estimated Elevation:_______________________

Safety Concerns:

Additional Comments:

Inititals of Preparer:__________ Proximity to airport:

_________________ (reference attached map indicating approximate location

of flight) Airport notified: Yes No Date:_______________

Time:

______________ Phone Number:

_______________________ Contact Name:

__________________________ COA Requested:___________

Make available to administrator/local law enforcement upon request.©2013

- 2014 DJI. All Rights Reserved. 1 | 

# PHANTOM 2 User Manual V1. 2

For PHANTOM 2 Flight Controller Firmware version V 3 .0 8

& PHANTOM 2 Assistant version V 3. 4

& PHANTOM RC Assistant version V1.1

2014. 10

Congratulations on purchasing your new DJI product. Please thoroughly read the entire contents of this manual to

fully use and understand the product.

It is advised that you regularly check the PHANTOM 2 ’s product page at www.dji.com which is updated on a

regular basis. This will provide services such as product information, technical updates and manual corrections. Due

to any unforeseen changes or product upgrades, the information contained within this manual is subject to change

wit hout notice.

DJI and PHANTOM 2 are registered trademarks of DJI. Names of product, brand, etc., appearing in this manual are

trademarks or registered trademarks of their respective owner companies. This product and manual are copy

righted by DJI with all r ights reserved.

If you have any questions or concerns regard ing your product, please contact your dealer or DJI Customer Service

.©2013

- 2014 DJI. All Rights Reserved. 2 | C ontent

CONTENT

................................ ................................ ................................ ........................ 2

IN THE BOX

................................ ................................ ................................ ..................... 4

LEGEND

................................ ................................ ................................ .......................... 4

1. PHANTOM 2 AIRCRAF T

................................ ................................ ............................... 5

1.1 B UILT

- IN F LIGHT C ONTROL S YSTEM I NSTRUCTIONS

................................ ................................ .. 5

1.2 C ONNECTIONS WITH O THER DJI P RODUCTS

................................ ................................ ........... 5

Important Notes of Using with Other DJI Products

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

Connections with Other DJI Products

................................ ................................ ............. 7

1.3 LED F LIGHT I NDICATORS D ESCRIPTION

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

1.4 N OTES FOR PHANTOM 2 USING WITH OTHER DJI PRODUCTS

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

2 PROPELLERS

................................ ................................ ................................ ............... 13

2.1 A SSEMBLY

................................ ................................ ................................ ..................... 13

2.2 D ISASSEMBLY

................................ ................................ ................................ ................ 13

2.3 N OTES

................................ ................................ ................................ ......................... 13

3 REMOTE CONTROL

................................ ................................ ................................ .... 14

3.1 P OWER ON THE R EMOTE C ONTROL

................................ ................................ .................... 14

3.2 R EMOTE C ONTROL LED I NDICATOR S TATUS

................................ ................................ ......... 15

3.2.1 Remote Control Power LED Indicator Status

................................ ....................... 15

3.2.2 Remote Control Battery Level Indicator Status

................................ .................... 15

3.3 A NTENNA O RIENTATION

................................ ................................ ................................ .. 16

3.4 R EMOTE C ONTROL O PERATION

................................ ................................ ......................... 16

3.5 L INKING THE R EMOTE C ONTROL & B UILT

- IN R ECEIVER

................................ ........................... 18

4 INTELLIGENT BATTER Y

................................ ................................ ............................... 19

4.1 C H ARGING P ROCEDURES

................................ ................................ ................................ .. 19

4.2 I NSTALL THE B ATTERY

................................ ................................ ................................ ...... 20

4.3 B ATTERY U SAGE

................................ ................................ ................................ ............. 20

4.4 D ESCRIPTION OF THE B ATTERY L EVEL I NDICATOR

................................ ................................ ... 21

4.5 C ORRECT B ATTERY U SAGE N OTES

................................ ................................ ...................... 22

5 CALIBRATING THE CO MPASS

................................ ................................ ...................... 23©2013

- 2014 DJI . All Rights Reserved. 3 | 5.1 C ALIBRATION W

ARNINGS

................................ ................................ ................................ . 23

5.2 C ALIBRATION P ROCEDURES

................................ ................................ .............................. 23

5. 3 W HEN R ECALIBRATION IS REQU IRED

................................ ................................ ................... 23

6 FLIGHT

................................ ................................ ................................ ....................... 24

6.1 F LYING E NVIRONMENT R EQUIREMENTS

................................ ................................ .............. 24

6.2 S TARTING THE M OTORS

................................ ................................ ................................ ... 24

6.3 T AKEOFF /L ANDING P ROCEDURES

................................ ................................ ....................... 24

6.4 F AILSAFE F UNCTION

................................ ................................ ................................ ........ 25

6.5 L OW B ATTERY C APACITY W ARNING F UNCTION

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

6.6 F LIGHT L IMITS F UNCTION

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

Max Height & Radius Limits

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

6.7 F LIGHT L IMITS OF S PECIAL A REAS

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

6.8 C ONDITIONS OF F LIGHT L IMITS

................................ ................................ ......................... 30

Disclaimer

................................ ................................ ................................ ..................... 30

7 ASSISTANT INSTALLA

TION AND CONFIGURATI ON

................................ ...................... 31

7.1 I NSTALLING D RIVER AND PHANTOM 2 A SSISTANT

................................ ............................... 31

7.2 U SING THE PHANTOM 2 A SSISTANT ON A PC

................................ ................................ .... 32

7.3 F IRMWARE UPGRADE OF PHANTOM 2

................................ ................................ ............. 33

7.4 PHANTOM RC A SSISTANT D ESCRIPTION

................................ ................................ ........... 33

8 APPENDIX

................................ ................................ ................................ .................. 35

8.1 S PECIFICATIONS

................................ ................................ ................................ .............. 35

8.2 LED F LIGHT I NDICATORS D ESCRIPTION

................................ ................................ ............... 35©2013

- 2014 DJI . All Rights Reserved. 4 | I n the Box

PHANTOM 2 Remote C ontrol

- 2.4 GHz Propeller Pair

Intelligent Battery Charger Plug Set

Screwdriver Assistant Wrench Cables

Micro

- USB Cable Screws Accessories Box

Legend

Forbidden(Important) Caution Tip Reference©2013

- 2014 DJI . All Rights Reserved. 5 | 1. PHANTOM 2 Aircraft

Figure 1

- 1 Figure 1

- 2

[1] Propeller [2] Motor [3] Front Side [4] Front LEDs [5] Micro

- USB Port [6] Landing Gear [7] Receiver

Antenna [8] CAN

- Bus Connector [9] LED Flight Indicators [10 ] DJI Intelligent Battery [11] Compass

1.1 Built

- in Flight Control System Instructions

The built

- in flight control system is u s ed 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 (turn left or right). The flight controller

contains the MC (Ma in Con troller), IMU, GPS, compass, receiver.

The IMU (Inertial Measurement Unit) has a built

- in inertial sensor and a barometric altimeter that measures both

attitude and altitude. The compass reads geomagnetic information which assists the GPS (Global Position System)

to accurately calculate the aircrafts position and height in order to lock the aircraft in a stable hover. The receiver is

used to communicate with the remote control and the MC acts as the brains of the complete flight control system

connecting a nd controlling all the modules together.

The PHANTOM 2 can be configured in the Assistant , by choosing Naza

- M mode or P hantom 2 mode.

This manual is for P hantom 2 mode. Please refer to the Naza

- M V2 Quick Start Manual for more

information.

1.2 Connections with Other DJI Products

PHANTOM 2 is compatible with other DJI products, inclu ding ZENMUSE H3

- 2D and H3

- 3D gimbal

, iOSD mini

,

iOSD Mark II. Below are connections for these products and wireless video transmission module.

Figure 1

- 3©2013

- 2014 DJI . All Rights Reserved. 6 | Important Notes of Using with Other DJI Products

( 1 ) The video cable can provide power for the wireless video transmission module with a battery voltage

(11.1V~12.6V) and a maximum current 2A.

( 2 ) Make sure the working current of the wireless video transmission module you connect can work with an

operational voltage between 11.1V~12.6V and the total working current of the iOSD and wireless video

transmission module is under 2A, as an overcurrent will damage the central board’s components. If the

total current exceeds 2A, please be sure to provide power supplied from a separat e power source for the

wireless video transmission module.

( 3 ) PHANTOM 2 uses a 2.4GHz RC system. To avoid communication interference, it’s not recommended to

use other 2.4GHz devices (including 2.4G Wi

- Fi or 2.4G wireless video transmission module) except the

2.4G Bluetooth and 2.4G Datalink.

( 4 ) Be sure to keep the wireless video transmission module and other communicating devices away from the

compass during installation and connection to avoid interference.

( 5 ) To improve the compatibility with ZENMUSE gimbals, the latest factory deliveries of PHANTOM 2 has

updat ed to the Version 2 shown below. H3

- 2D / H3

- 3D gimbal can be directly installed for the Version 2

while for Version 1 , a H3

- 3D adapter kit ( coming soon) is required to install the H3

- 3D gimbal

.

Figure 1

- 4

( 6 ) When using the H3

- 3D gimbal, please connect the 8

- Pin cable of PHANTOM 2 to the G8 port of H3

- 3D

shown below.

Figure 1

- 5©2013

- 2014 DJI . All Rights Reserved. 7 | Connection s with Other DJI Products

( 1 ) C onnecting the H3

- 2D and H3

- 3D gimbal and wireless video transmission module , the figure below use s

H3

- 2D as a n example.

F ig ure 1

- 6

( 2 ) C onnecting the H3

- 2D and H3

- 3D gimbal, iOSD mini and wireless video transmission module , the figure

below uses H3

- 2D as an example.

F igure 1

- 7©2013

- 2014 DJI . All Rights Reserved. 8 |

( 3 ) Connecting the H3

- 2D and H3

- 3D gimbal, iOSD mini and DJI specified wireless video transmission module

AVL58 , the figure below uses H3

- 2D as an example.

F igure 1

- 8

W e recommend connect ing the V Bat+ port of the video cable to the two BATT+ ports of the AVL58

simultaneously

. T he same is true of the GND port of the video cable and two BATT

- ports.

( 4 ) C onnecting the H3

- 2D and H3

- 3D gimbal, iOSD Mark II and wireless video transmission module , the figure

below uses H3

- 2D as an example.©2013

- 2014 DJI . All Rights Reserved. 9 | F igure 1

- 9

The diagram below illustrates the conneciton between the iOSD Mark II and the wireless video transmission module

.

Use the 8

- Pin cable in the iOSD Mar k II package when connecting to the DJI specified wireless video

transmission module AVL58.

( 5 ) U sing the i Pad Ground Station©2013

- 2014 DJI . All Rights Reserved. 10 | Figure 1

- 10

Connect the Air End of 2.4G Bluetooth Datalink to a spared CAN

- Bus port of iOSD if an iOSD is used.

( 6 ) U sing the PC Ground Station

Figure 1

- 11©2013

- 2014 DJI . All Rights Reserved. 11 | 1.3 LED Flight Indicators Description

1. LED flight indicators are used to show the aircraft ’ s current status. O nce power ed on, the indicators will light

up.

A ircraft in Normal status D escriptions

Power On Self

- Test

Warming Up & Aircraft cannot take off during warming up

Ready to Fly

Ready to Fly (non

- GPS)

Aircraft in abnormal status W arnings and errors

Remote C ontrol Signal Lost

1 st Level Low Battery Capacity Warning

2 nd Level Low Battery Capacity Warning

Not Stationary or Sensor Bias is too big

Error s & Aircraft c annot fly.

Compass data abnormal because of ferro

- magnetic interference or

the compass needs calibration.

( 1 ) The LED indicators diagram above are for P hantom 2 mode. In Naza

- M mode, LED indicators

will work according to the Naza

- M flight control system

.

( 2 ) Conn ect to the PHANTOM 2 Assistant for detailed information about warnings and errors.

2. The front LEDs are f or indicating where the nose of the aircraft is. They light up solid red only after the motors

have s pooled up

.©2013

- 2014 DJI . All Rights Reserved. 12 | 1.4 Notes for PHANTOM 2 using with other DJI products

Before using PHANTOM 2 with other DJI products, users should connecting the products correctly and upgrade

the firmware as requirements below .

Items to upgrade Firmware versions required Assistant for upgrading Assistant version

P330CB (built

- in

central board) V1.0.1.19 or above PHANTOM 2 V1.0 8 or above

Zenmuse H3

- 2D CMU V1.0

, IMU V1.6 or above PHANTOM 2 V1.0 8 or above

iOSD Mark II V3. 0 1 or above iOSD V 4.0 or above

iOSD mini V1.0 6 or above iOSD V 4.0 or above

* T he iOSD Assistant is applied to both iOSD Mark II and iOSD mini.©2013

- 2014 DJI . All Rights Reserved. 13 | 2 Propellers

PHANTOM 2 use s the original 9

- inch propellers which are classified by the color of each central nut. Damaged

p ropellers should be replaced by purchas ing new ones if necessary.

Propellers Grey Nut (94 50 ) Black Nut (94 50 R)

Diagram

Assembly Location Atta ch to the motor thread that does

not have a black dot

. Atta ch to the motor thread that has a

black dot

.

Fastening/Un

- fastening

Instructions Lock: T ighten 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 propeller s with the correctly marked black dot motors. T ighten the propellers according to the

fastening instructions

.

Figure 2

- 1 Figure 2

- 2 Figure 2

- 3

2

. 2 D isassembly

( Figure 2

- 3 ) Keep the motor deadlock ed in place with the assistant wrench (or one hand) and remove the

propeller according to the un

- fastening instructions

.

2

. 3 Notes

1. P ropellers are self tightening during flight. DO NOT use any t hread locker on the threads.

2. Make sure to match the propeller nut colors with the corre sponding motors.

3. I t is advised to wear protective gloves during propeller assembly and remov al

.

4. Check that the propellers and motors are installed correctly and firmly before every flight.

5. Check that all p ropell e rs are in good condition before flight. DO NOT use any ageing , chipped, or broken

p ropellers

.

6. To avoid injury, STAND CLEAR of and DO NOT touch the propellers or motors when th ey are spinning.

7. ONLY use original DJI propellers for a better and safer flight experience

.©2013

- 2014 DJI . All Rights Reserved. 14 | 3 Remote C ontrol

T he PHANTOM 2 remote control can be configured in the PHANTOM RC Assistant

. T he sticks mode is Mode 2 on

delivery.

For upgraded remote control (models: NDJ6 or NRC900), select “Upgrade Version” in Phantom Assistant.

For basic remote control (models: DJ6 or RC900), select “Basic Version” in Phantom Assistant.

F igure 3

- 1 Figure 3

- 2

[1] Antenna [2] Carrying Handle [3] Left Dial [4] 3

- Position Switch S1 [ 5 ] 3

- Position Switch S2 [ 6 ] Joystick1 ( J1;J2 )

[ 7 ] Joystick2 ( J3;J4 ) [ 8 ] Neck Strap Attachment [ 9 ] Power Switch [ 10 ] Power Indicator

[ 1 1 ] Battery Level Indicator s LED1/LED2/LED3/LED4 (from left to right) [ 12 ]Trainer Port

[13 ] Battery Charge & RC Assistant Port (m icro

- USB p ort ) [ 1 4 ] Potentiometer

3.1 Power on the Remote C ontrol

1. Set the S1 and S2 switches to the upper most position and ensure both joy sticks are at

the mid

- point position. Then toggle on the power switch.

2. P ush the power switch to the right to power on the remote control

. I f the power LED

indicator is solid on, the remote control is functioning normally. The batt ery level

i ndicators display the current battery level

.

1. P lease make sure the battery level of remote control is enough . If the low voltage warning alert

sounds ( refer to < Remote C ontrol Po wer LED Indicator Status >), please re charge the battery as soon as

possible.

2. Charge the remote control’s battery by using the included micro

- USB cable. Using the incorrect

type of charging cable may cause damage.

3

. Turn off the remote control before charging. The po wer LED indicator will display solid red when

charging is in progress. The LED indicators will display solid green when the battery is fully charged.©2013

- 2014 DJI . All Rights Reserved. 15 | 3.2 Remote C ontrol LED Indicator Status

3.2.1 Remote C ontrol Power LED Indicator Status

Power LED Indicator Sound Remote C ontrol Status

None Functioning n ormal ly

.

None Charging( remote control is powered off)

None Remote control joysticks calibration error , need to be re

- calibrate.

BB

--- BB

--- BB Low voltage (from 3. 5 V

- 3.53 V) , rec harge the remote control.

B

- B

- B

...... Critical l ow voltage ( from 3. 4 5 V

- 3.5 V)

. Recharge the remote control

immediately

.

B

-- B

-- B

...... Al ert will sound after 15 minutes of in activity. It will stop once you

start using the remote control

.

T he remote control will power off automatically when battery voltage drops below 3.45 V

. Land and

re charge the battery as soon as possible when the low voltage alert occurs to avoid loss of control

during flight.

3.2.2 Remote Control Battery Level Indicator Status

The battery level indicators will show the current battery level during both the discharging process

. T he following is

a description of the indicators.

: The LED is solid on : The LED will blink regularly

: The LED is light off

D ischarging process

LED1 LED2 LED3 LED4 C urrent battery level

75 %~100%

50 %~75%

2 5%~50%

12.5%~25%

0%~12.5%

<0%©2013

- 2014 DJI . All Rights Reserved. 16 | 3.3 Antenna Orientation

The remote control ’ s antenna should point skyward s without obstructions for maximum communication range

during flight.

F igure 3

- 3

3.4 Remote C ontrol Operation

The operations of remote control are based on mode 2 stick configuration

.

Definitions

The ‘ stick neutral’ position s and ‘ stick released’ mean the control stick s of the remote control are p laced at

the central position.

To ‘move the stick ’ means that the stick of remote control is pushed away from the central position.

Slide Lever is used for the pitch control of the H3

- 2D and H3

- 3D gimbal.

Remote

C ontrol

(Mode 2) Aircraft

( nose direction ) Operation details

T he t hrottle stick controls aircraft altitude/ elevation.

Push the stick up and the aircraft will rise.

Pull the stick down and the aircraft will descend

.

The aircraft will automatically hover and hold its

altitude if the stick s are centered.

P ush the throttle stick above the centered (mid

- point )

position to make the aircraft tak e off. When flying, we

suggest that you push the throttle stick slowly to

prevent the aircraft from sudden and unexpected

elevation changes.©2013

- 2014 DJI . All Rights Reserved. 17 | The y aw stick controls the aircraft rudder.

Push the stick left and the aircraft will rotate counter

clock

- wise

.

Push the stick right and the aircraft will rotate

clock

- wise

. If the stick is centered, the aircraft will

remain facing the same direction.

The yaw stick controls the rotating angular velocity of

the aircraft. Pushing the stick further away from center

results in a faster aircraft rotation velocity.

The pitch stick controls the aircraft’ s front & back tilt

.

Push the stick up and the aircraft will tilt and fl y

forward

.

Pull the stick down and the aircraft will tilt and fl y

back ward

. The aircraft will keep level and straight if the

stick is centered.

Pushing or pulling the stick further away from center

will result in a larger tilt angle (maximum of is 35 ̊) and

faster flight velocity.

The roll stick controls the aircraft ’s left & right tilt.

Push the stick left and the aircraft will tilt and fl y left.

Pu sh the stick right and the aircraft will tilt and fl y right.

The aircraft will keep level and straight if the stick is

centered.

Pushing the stick further away from center will result in

a larger tilt angle (maximum of 35 ̊) and faster flight

velocity.

Position

- 1 Position

- 2 Position

- 3 S1 is for compass calibration. T oggle the S1 switch from

position

- 1 to po sition

- 3 and back to position

- 1 at least 5

times, which will force the aircraft to enter into

compass calibration mode.

U sers can configure position 3 (bottom position) of the

S1 switch to trigger the Failsafe in the Assistant

.

OFF Course Lock Home

point Lock S2 is the IOC mode switch. IOC (Intelligent

Orientation Control) function can be enabled in the

Assistant when in Naza

- M mode . Only use the IOC

function after you are familiar with flying

.©2013

- 2014 DJI . All Rights Reserved. 18 | The l eft d ial control s the pitch of the H3

- 2D and H3

- 3D

gimbal. T he position of left dial determines the pitch

angle relative to the horizontal level.

Turn the left dial to the right to make th e gimbal pitch

up

.

Turn the left dial to the left to make the gimbal pitch

down.

The gimbal will keep its current position if t he dial is

static.

( 1 ) For ‘ R eady to F ly’ the aircraft will hover when all stick s are released.

( 2 ) For ‘ Ready to Fly (non

- GPS) ’ the aircraft will only keep the altitude when all stick s are released.

3.5 Linking the R emote C ontrol & B uilt

- in R eceiver

PHANTOM 2 has a built

- in receiver, the link button and indicator located on the bottom of the aircraft as illustrated

in the Figure 3

- 4

.

The link between the remote control and a ircraft is already established for you so you can initially skip this

procedure . If you ever replace the remote control

, re

- establishing the link is required.

F igure 3

- 4

Linking procedures

1. Power on the PHANTOM 2.

2. Turn on the remote control and place it 0.5m~1m away from the aircraft.

3. P ush the link button with a thin object and hold it until the Link indicator blinks red , then r elease it

.

4. When the Link indicator turn s solid green

, the link between the remote control and the built

- in receiver has

been successfully established.

Link Indicator S tatus

T he remote control is turned off and there is no 2.4GHz signal around , please turn on

the remote control

.

T he receiver is ready for linking

.

There is 2.4GHz signal around but the remote control is not linked with the receiver

,©2013

- 2014 DJI . All Rights Reserved. 19 | please carry out the linking procedures.

T he remote control is linked with the receiver successfully.

4 Intelligent Battery

The i ntelligent battery is specially designed for the PHANTOM 2 , with a battery capacity of 5200mA h, voltage of

11.1 V and charge

- discharge management functionality. The battery should only be charged with the DJI charger.

I ntelligent Battery Charger

DJI Intelligent Battery Functions

( 1 ) B alance Charg ing Automatically balance the voltage of each battery cell during charging.

( 2 ) C apacity Display D isplay the current battery level

.

( 3 ) Communicating T he main controller communicate s with the battery via communicat ion ports

for battery voltage, capacity, current and other information.

( 4 ) O vercharging Protection C harging stop s automatically when the battery voltage reaches 12.8V to

prevent overcharging damage

.

( 5 ) Over D ischarging

Protection D ischarging stop s automatically when the battery voltage reaches 8.4V to

prevent over discharging damage

.

( 6 ) S hort C ircuit Protection A utomatically cut s off the power supply when a short circuit is detected.

( 7 ) Sleep Protection The battery will enter sleep mode after 10 minutes of inactivity to save

power

. The static current is 10nA in sleep mode when the battery is

powered on without connecting to other devices

.

( 8 ) C harging T emperature

D etection T he battery will charge only when its temperature is within 0 °C

~ 55 °C

. I f the

battery temperature is out of this ran ge, the battery will stop charging

.

( 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 ) T he battery should only be charged with the charger provided by DJI. DJI does not take any

responsibility for operation of any charger from a third party.

4

. 1 Charging Procedures

1. Connect the charger to a wall socket (Use the plug set if necessary )

.

2. Connect the batte ry to the charger. If the current capaci ty of the battery is over 75%, you should power on

the battery to begin charging

.

3. T he Battery Level indicators display current capacity level as the battery charges. P lease refer to battery©2013

- 2014 DJI . All Rights Reserved. 20 |

level indicator descriptio n for details.

4. T he battery is full y charged when the Battery Level indicator light s are off

. P lease disconnect the charger

and battery when the charging is completed

.

4

. 2 Install the Battery

Push the battery into the battery compartment correctly as the following diagram show s . Make sure to push the

battery into the compartment until you hear a ‘click’ sound.

F igure 4

- 1

An incorrectly inserted battery may cause one of the following to occur : (1) Bad contact. (2) Unavailable

battery information. (3) Unsafe for flight. (4) Unable to take off.

4

. 3 Battery Usage

F igure 4

- 2

(1) Checking the battery level: When t he battery is powered off; press ing the battery power button once will

indicate the current battery level. Refer to < Battery Level Indicator Description> for details.

(2) Powering on: When t he battery is powered off; press the battery power b utton once and then press and hold for

2 seconds to turn on the intelligent battery.

(3) Powering off: When the battery is powered o n ; press the battery power button once and then press and hold for

2 seconds to turn off the intelligent battery. LED3

LED4

Battery Power Button

(Built

- in Battery Power Indicator) LED2

LED1

Battery Level Indicator©2013

- 2014 DJI . All Rights Reserved. 21 | (4) Check ing the battery life: When t he battery is powered off; press and hold the battery power button for 5

seconds to check the battery life. T he battery level indicators will show the life and the battery power indicator

will blink for 10 seconds, then all LEDs will light out and the intelligent battery will turn off

. Refer to < Battery

Level Indicator Description> for details.

More battery information is available in the battery tab of the PHANTOM 2 Assistant

.

4.4 Description of the Battery Level Indicator

The battery level indicators will show the current battery level during both the charging and discharging process as

well as battery life. T he following is a description of the indicators.

: The LED is solid on : The LED will blink regularly

: The LED is light off

C harging process

LED1 LED2 LED3 LED4 C urrent battery level

0%~25%

25%~50%

50%~75%

75%~100%

F ull charged

D ischarging process

LED1 LED2 LED3 LED4 C urrent battery level

87.5%~100%

75%~87.5%

62.5%~75%

50%~62.5%

37.5%~50%

25%~37.5%

12.5%~25%

0%~12.5%

<0%

B attery life

LED1 LED2 LED3 LED4 C urrent battery life

90 %~100%©2013

- 2014 DJI . All Rights Reserved. 22 | 80 %~ 90 %

70 %~ 80 %

60 %~ 70 %

50 %~ 60 %

40 %~ 50 %

30 %~ 40 %

20 %~ 30 %

L ess than 20 %

4

. 5 Correct B attery Usage Notes

1. N ever plug or unplug the battery into the aircraft when it is power ed on.

2. The battery should be charg ed in an environment that is between 0 °C to 40 °C , and be discharg ed in an

environment that is between

- 20 °C to 50 °C

. B oth charging and discharging should be in an environment

where the relative humidity is lower than 80%.

3. It’s recommended to charge and discharge the battery thoroughly once every 20 charge/discharge cycles.

Users should discharge the battery until there is less than 8% power left or until the battery can no longer

be turned on. U sers shou ld then fully recharge the battery to maximum capacity. This power cycling

procedure will ensure the battery is working at its optimal level.

4. F or long term storage please p lace the battery with only a 40~50% capacity in a strong battery box

securely. W e recommend discharging and charging the battery completely once every 3 months to keep it

in good condition. The capacity should be varie d in such a cycle ( 40%~50% )

— 0%

— 100%

— ( 40%~50% )

.

5. It’s suggested you purchase a new battery after you have discharg ed you r current battery over 300 times.

Please completely discharge a batter y prior to disposal

.

6. It’s suggested that you purchase a new battery if the current battery is swollen or damaged in any way.

7. Never try to recharge or fly with a battery that is swollen or damaged in any way.

8. Never charge the battery unattended. Always charge the battery on a non

- flammable surface such as

concrete and never near any flammable materials.

9. S afety is extremely important and users can get more information in the DISCLAIMER.©2013

- 2014 DJI . All Rights Reserved. 23 | 5 Calibrating the Compass

IMPORTANT: Make sure to perform the Compass Calibration procedure s prior to the first flight.

The compass is very sensitive to electromagnetic interference which cause s abnormal compass data and lead s to

poor flight performance or even flight failure . Regular calibration of the compass enables the compass to perform at

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.

( 2 ) DO NOT carry ferromagnetic materials with you during calibration such as keys or cell ular

phones.

( 3 ) Compass Calibration is very important; otherwise the flight control system will work abnormal ly

.

5 .2 Calibration Procedures

Please carry out the calibrating procedures in the flight field before flight. Please watch the quick start video of the

PHANTOM 2 for more compass calibration details.

5 .3 When Recalibration is required

( 1 ) When Compass D ata is abnormal

, the LED flight indicator will blink alternating between red and yellow.

( 2 ) Last compass calibration was performed at a completely different flying field/location.

( 3 ) The mechanical structure of the ai rcraft has changed, i.e. changed mounting position of the compass

.

( 4 ) E vident drifting occurs in flight , i.e. the aircraft doesn ’ t fly in straight lines.©2013

- 2014 DJI . All Rights Reserved. 24 | 6 Flight

6 .1 Flying Environment Requirements

( 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 ) D O NOT fly in bad weather, such as rain or wind (more than moderate breeze) or fog.

( 3 ) The flying field should be open and void of tall buildi ngs or other obstacles; the steel structure

within buildings may interfere with the compass.

( 4 ) Keep the aircraft away from obstacles, crowds, power lines, trees, lakes and rivers etc.

( 5 ) Try to avoid interference between the remote control and other wireless eq uipment (No base

stations or cell towers around ).

( 6 ) The flight control system will not work properly at the South Pole or North Pole.

( 7 ) N ever use the aircraft in a manner that infringes upon or contravenes international or domestic

lays and regulations.

6 .2 Starting the Motors

A Combination Stick Command (CSC) is used to start the motors

. Push the sticks according to one of the options

below to start motors. Once the motors have started , release both stick s simultaneously. The same CSC is used to

st op the motors

.

F igure 6

- 1

6 .3 Takeoff/Landing Procedures

1. Start by placing the PHANTOM 2 on the ground with the battery level indicator s facing you

.

2. T urn on the remote control

.

3. Power on the aircraft by turning 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 CSC command.

5. Push the throttle stick up slowly to lift the aircraft off the ground

. R efer to < Remote C ontr ol Operation > for

more details.

6. Be sure you are hovering over a level surface. Pull down the throttle stick to descend. The stick will lock into©2013

- 2014 DJI . All Rights Reserved. 25 |

place and the aircraft will descend steadily.

7. After landing, leave the throttle stick down for 3 to 5 seconds t o stop the motors. Return throttle stick to

middle position after the motors have stopped.

You SHOULD NOT execute the CSC during normal flight ! This will stop the motors and cause the

aircraft to descend rapidly and drop without any type of control.

( 1 ) When the LED flight indicator blinks yellow rapidly during flight , the aircraft has entered in to

Failsafe mode , refer to <Failsafe Function> for details.

( 2 ) A low battery capacity warning is indicated by the LED flight indicator blink ing red slowly or

rapidly during flight . R efer to the <Low Battery Capacity Warning Function> for details.

( 3 ) Watch the quick start video about flight for more flight information.

( 4 ) Aircraft and battery performance is subject to environmental factors such as air density and

temp erature. Be very careful when flying 3000 meters (9800 feet) or more above sea level, as

battery and aircraft performance may be reduced.

( 5 ) When used wit h a H3

- 3D gimbal, a GoPro camera, and the iOSD mini, your Phantom 2 will be very

close to its maximum takeoff weight. It is not recommended that you attach the Phantom 2

propeller guards at this weight. Otherwise, the aircraft will be unable to fly normall y.

6 .4 Failsafe Function

The aircraft will enter Failsafe mode when the connecti on from the remote control is lost . T he flight control system

will automatically control the aircraft to return to home and land to reduce injuries or damage. T he following

situations w ould make the aircraft fail to receiv e a signal from the remote control and enter Failsafe mode:

( 1 ) The remote control is power ed off.

( 2 ) The remote control is power ed on but the S1 is toggled in the position triggering the Failsafe (this must have

been configured in t he PHANTOM 2 Assistant )

.

( 3 ) The aircraft has flown out of the effective communication range of the remote control

.

( 4 ) There is an obstacle obstructing the signal between the remote control and the aircraft, essentially reducing

the distance the signal can travel.

( 5 ) There is interference causing a signal proble m with the remote control

.

Failsafe works different ly depending on the mode the aircraft is in when Failsafe mode is initiated whether it i s in

the Ready to Fly or Ready to Fly (non

- GPS) mode.

Ready to Fly (non

- GPS)

---- Automatic l anding

The flight 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.

Ready to Fly

---- Automatic g o h ome and land

The flight control system will automatic ally control the aircraft to fly back to the home point and land.©2013

- 2014 DJI . All Rights Reserved. 26 | Home Point

When the aircraft is initializing the Ready to Fly status, the aircraft will record the current GPS coordinates as

the home point. I t is recommended to lift off only after Ready to Fly status is confirmed for the safety of being

able to fly back to home point successfully in case the Failsafe mode is initiated.

Go Home Procedures

Figure 6

- 2

( 1 ) I n a Failsafe 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. Q ui ckly flipping the S2 switch of the remote

control from upper most to lower most positions 5 times or more will reset the current aircraft position as

a new home point of PHANTOM 2. When successfully reset, you will see a series of rapid green blinks on

the LED Flight Indicator. T he 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 if using iOSD module.

Regaining Control during Failsafe Procedure

Position of

Switch S1 Position

- 1 Position

- 2 Position

- 3

(No triggering the Failsafe)

How to regain

control When the S1 switch is switched to Position

- 1,

toggle the S1 switch to any other position once to

regain control . I f remote control ’s signal is

recovered, control is returned back to the pilot. R egain control as soon as signal is

recover ed.©2013

- 2014 DJI . All Rights Reserved. 27 | 6 .5 Low Battery Capacity Warning Function

The low battery capacity warning alerts users when the battery is close to depletion during flight. When it appears,

users should promptly fly back and land to avoid accidental damage. The PHANTOM 2 has two levels of low battery

capacity warning. The first appears when the batter y has less than 30% power and the second appears when it has

less than 15 % power

.

( 1 ) When battery power drops below 30% and LED indicator will blink red slowly

.

( 2 ) At lower than 15 % the LED indicator will blink red rapidl y, the PHANTOM 2 will also begin to desce nd and

land automatically. After it has landed, keep the throttle stick at its lowest point or execute CSC

.

( 3 ) There is a hidden third low battery threshold in addition to the 1st and 2nd level warnings. This uses 10.65V

as its threshold. Both this voltage th reshold and the 2nd Level Low Battery Warning will trigger auto

- landing.

Altitude can be maintained if necessary by pu sh ing up on the throttle stick

.

( 1 ) Remember to fly your P HANTOM 2 back as soon as you see a low battery capacity warning.

( 2 ) Keeping the battery contact needles and pads clean is very important. Any dirt and dust may

cause a communication failure.

6

. 6 Flight Limits Function

All UAV (unmanned aerial vehicle) operators should abide by all regulations from such organizations at ICAO

(International Civil Aviation Organization) and per country airspace regulations. For safety reasons, the flight limits

function is enabled by default to help users use this product safely and legally. The flight limits function includes

height, distance l imits

.

In Ready to Fly status, height, distance limits works together to restrict the flight. In Ready to Fly (non

- GPS) status,

only height limit works and the flying height restricted to be not over 120m.

(1) The default parameters in the Assistant is compl iant 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 comp ly with these rules too , before using the

PHANTOM 2

.

(2) Users in Mainland China can refer to 民用航空空域使用办法

.

Max Height & Radius Limits

The Max Height & Radius restricts the flying height and distance. Configuration can be done in the PHANTOM 2

Assistant . Once complete, your aircraft will fly in a restricted cylinder.©2013

- 2014 DJI . All Rights Reserved. 28 | Figure 6

- 3 Figure 6

- 4

Ready to Fly

Limits Ground Station Rear LED flight indicator

Max Height The flight height is restricted to fly

under the max height. Warning: Height limit

reached. None.

Max Radius The flight distance is restricted to fly

within the max radius. Warning: Distance limit

reached. Rapid red flashings

when close to the Max radius limit.

Ready to Fly(non

- GPS)

Flight Limits Ground Station Rear LED flight indicator

Max Height The flight height is restricted to fly

under the minor height between the

Max height and 120m. Warning: Height limit reached.

None.

Max Radius Not limited, no warnings or LED indicators.

(1) If the aircraft flies out of the limits, you can still control your aircraft except to fly it further 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 if 6 or more GPS satellites have been found.

6. 7 Flight Limits of Special Areas

Special areas include airports worldwide. All special areas are listed on the DJI official website. Please refer to

http://www.dji.com/fly

- safe/category

- mc for details. These areas have been divided into category A and category B.©2013

- 2014 DJI . All Rights Reserved. 29 | Category A Category B

Ready to Fly

Airspace Limits Rear LED

Flight Indicator

A

Orange Motors will not start.

If the Phantom flies into a special area in Ready to Fly

(non

- GPS) mode and Ready to Fly mode activates, it will

automatically descend and land then stop its motors.

B

Yellow If the Phantom flies into a special area in Ready to Fly

(non

- GPS) mode and Ready to Fly mode activates, it will

descend to airspace C and hover 5 meters below edge d

.

C

Green No restrictions of flight, but the Phantom will not enter

Category A, the aircraft can fly free, but it will not enter

Airspace B through Boundary b & d.

Around Category B sites, the phantom can fly freely, but it will

not enter into Airspace A through Bou ndary a.

D

Blue No restrictions. None.©2013

- 2014 DJI . All Rights Reserved. 30 |

Semi

- automatic descent : All stick commands are available except the throttle stick command during

the descent and landing process. Motors will stop automatically after landing. Users must toggle the S1

switch to regain control. This is the same as regaining control during Failsafe. Please refer to Regaining

Control During Failsafe Procedure (Page 23 )

.

(1) When flying in the airspace (A/B/C) of restricted special area, LED flight indicators will blink red

quickly and continue for 3 seconds, then switch to indicate current flying

status and continue for 5 seconds at which point it will switch back to red blinking.

(2) For safety reasons, please do not fly close to airports, highways, railway stations, railway l ines,

city centers and other special areas. Try to ensure the aircraft is visible.

6. 8 Conditions of Flight Limits

In different working modes and flight modes, flight limits will differ according to number of GPS satellites found.

The following table demonstrates all the cases( √ : available; × :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

special area limits built in to Ground Station. Refer to the Ground Station manual for details.

Phantom mode

Flight Status Limits of Special Area Max Height Max Radius

Ready to Fly √ √ √

Ready to Fly (non

- GPS) × √ ×

Naza

- M mode

Control Mode number of GPS found Limits of Special Area Max Height Max Radius

GPS ≥ 6 √ √ √

< 6 × √ ×

ATTI. ≥ 6 √ √ ×

< 6 × √ ×

Manual ≥ 6 × × ×

< 6 × × ×

Disclaimer

Please ensure that you are kept up to date with International and Domestic airspace rules and regulations before

using this product. By using this product, you hereby agree to this disclaimer and signify that you have read this fully.

You agree that you are responsible for your own conduct and content while using this pr oduct, and for any direct or

indirect consequences caused by not following this manual, violate or disregard any other applicable local laws,

administrative rules and social habits thereof.©2013

- 2014 DJI . All Rights Reserved. 31 | 7 Assistant Installation and Configuration

7. 1 Install ing Driver and PHANTOM 2 Assistant

Install ing and run ning on Windows

1. Download driver installer and Assistant installer in EXE format from the download page of PHANTOM 2

on the DJI website.

2. Connect the PHANTOM 2 to a PC via a Micro

- USB cable.

3. Run the driver installer and follow the prompts to finish installation.

4. N ext, r un the Assistant installer and follow the prompts to finish installation.

5. Double click the PHANTOM 2 icon on your Windows desktop to launch the software.

T he i nstaller in EXE format only supports Windows operating systems (Win XP, Win7, Win8 (32 or 64

bit)).

Install ing and run ning on Mac OS X

1. Download the Assistant installer in DMG format from the download page of PHANTOM 2 on the DJI

website.

2. Run the installer and follow the prompts to finish installation.

3. When launching for the first time if use Launchpad to run the PHANTOM 2 Assistant

, Launchpad won ’ t

allow access because the software has not been reviewed by Mac App Store.

4. L ocate the PHANTOM 2 icon in the Finder, p ress the Control key and then click the PHANTOM 2 icon

(or right

- click the PHANTOM 2 icon using a mouse). Choose Open from the shortcut menu, click open in

the prompt dialog box and the n software will launch

.

5. After the first successful launch, directly lau nching of the software can be achieved by double

- clicking

the PHANTOM 2 icon in the Finder or using Launchpad.©2013

- 2014 DJI . All Rights Reserved. 32 |

Installer in DMG format supports only Mac OS X 10.6 or above.

Usage of PHANTOM 2 Assistant on Mac OS X and Windows are e xactly the same. The Assistant pages

appear in other places of this manual are on the Windows for example.

7 .2 Using the PHANTOM 2 Assistant on a PC

1. Start up the PC, power on the PHANTOM 2 , then c onnect the PHANTOM 2 to the PC with a Micro

- USB

cable. DO NOT disconnect until configuration is finished.

2. Run the PHANTOM 2 Assistant and wait for the PHANTOM 2 to connect to the Assistant

. Observe the

indicators on the bottom of the screen. When connected successfully, the connection indicator is

and communication indicator is blinking

.

3. Choose [Basic] or [Advanced] configuration page s

.

4. View and check the current configuration in the [View] page.©2013

- 2014 DJI . All Rights Reserved. 33 |

( 1 ) Users should not enable the Naza

- M function before finishing Advanc ed Flight Maneuvers

procedure in the " PHANTOM Pilot Training Guide”. If the 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 loca ted on the rear frame arms will display

Naza

- M flight status indications instead of the PHANTOM 2's indicator s . Do not enable the

Naza

- M mode unless you are an experienced user or guided by a professional.

( 2 ) You can change to the P hantom 2 mode by clicking the same button used to turn on the Naza

- M

mode

. This operation will disable the N aza

- M mode and enable P hantom 2 mode

. All parameters

will be returned to factory settings

.

7

. 3 F irmware upgrade of PHANTOM 2

Please re fer to the PHANTOM 2 Assistant to install d river and PHANTOM RC Assistant

, and then follow the

procedure s below to upgrade the software and firmware; otherwise the PHANTOM 2 might not work properly

.

1. An internet connection is required to upgrade PHANTOM 2’s firmware.

2. Click the [ U pgrade] icon to check the current firmware version and whether the installed firmware is the

latest version

. I f not, click the relative links to upgrade.

3. Be su re to wait until the Assistant shows “finished”. Click OK and power cycle the PHANTOM 2 after 5

seconds. Once completed, t he firmware is up to date.

( 1 ) DO NOT power off until the upgrade is finished.

( 2 ) If the firmware upgrade failed, the main controller will enter a waiting for firmware upgrade

status automatically. If this happens, repeat the above procedures.

F irmware upgradable items: ( 1 ) Main Controller ( 2 ) P330CB (Main Board) ( 3 ) Receiver ( 4 ) Gimbal

C MU ( 5 ) Gimbal IMU ( 6 ) Battery

7 .4 PHANTOM RC Assistant Description

Please follow the procedures to finish the configuration of the remote control

.©2013

- 2014 DJI . All Rights Reserved. 34 |

1. Turn off the remote control and find the Micro

- USB port on the bottom of it.

2. Start up the PC, power on the remote control , and then connect the remote control to the PC with a

Micro

- USB cable. DO NOT disconnect until th e configuration is finished.

3. Run the PHANTOM RC Assistant and wait for the remote control to connect to the Assistant

. Observe the

indicators on the bottom left of the screen. When connected successfully, the connection indicator is

and communication indicator is blinking

.

4. Finish c onfiguration in the [ Main ] page.

5. Finish upgrade in the [ Info ] page if necessary

.

M ain P age of the 2.4G Hz R emote C ontrol©2013

- 2014 DJI . All Rights Reserved. 35 | 8 Appendix

8. 1 Specification s

A ircraft

O perating environment temperature

- 10 °C to 50 °C

P ower consumption 5.6W

S upported Battery DJI Intelligent battery

W eight (including the battery) 1000g

Take

- off W eight ≤ 1300g

Hovering Accuracy ( Ready to Fly ) Vertical: 0.8m ; Horizontal: 2.5m

Max Yaw Angular Velocity 200°/s

Max Tilt Angle 35°

Max Ascent / Descent Speed Ascent: 6m/s; Descent: 2 m/s

Max Flight Speed 15 m/s (Not Recommended)

W heelbase 350mm

2.4GHz Remote Control

Operating Frequency 2.4GHz ISM

Communication Distance ( open area ) 1000m

Receiver Sensitivity ( 1%PER )

- 9 7 dBm

W orking Current/Voltage 1 2 0 mA@ 3.7 V

Built

- in LiPo Battery Working Current/Capacity 3.7V, 2000mAh

DJ I Intelligent Battery

T ype 3S LiPo Battery

C apacity 5200mAh

, 11.1V

Charging Environment R ange 0 °C to 40 °C

Discharging Environment R ange

- 20 °C to 50 °C

8

. 2 LED Flight Indicators Description

A ircraft in Normal status D escriptions

Power On Self

- Test

Warming Up & Aircraft cannot take off during warming up

Ready to Fly

Ready to Fly (non

- GPS)

Aircraft in abnormal status W arnings and errors

Remote C ontrol Signal Lost

1 st Level Low Battery Capacity Warning©2013

- 2014 DJI . All Rights Reserved. 36 | 2 nd Level Low Battery Capacity Warning

Not Stationary or Sensor Bias is too big

Errors & Aircraft c annot fly.*

Compass data abnormal because of ferro

- magnetic interference or

the compass needs calibration.

* U sers can connect to the PHANTOM 2 Assistant to get detailed information about warnings and errors.