# April 8
, 2015

Exemption No. 11289 Regulatory Docket No. FAA

− 20 14

− 0944

Mr. David P. Geisler Manager Bird’s Eye Solutions, LLC 8300 Airport Road, Suite 3 Middleton, WI 53562

Dear Mr. Geisler : 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.

The Basis for Our Decision
By letter dated November 7, 2014 , you petitioned the Federal Aviation Administration (FAA) on behalf of Bird’s Eye Solutions, LLC ( hereinafter petitioner or operator ) for an exemption

. The exemption would all ow the petitioner to operate an unmanned ai rcra ft system (UAS) to conduct aerial photograph y , closed

- set filming of motion pictures , and scientific data collection.
See Appendix A for the petition submitted to the FAA des cribing the proposed operations and the regulations that the petitioner seeks an exemption

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

.

# 2

Airworthiness Certification

The UAS proposed by the petitioner is a DJI Phantom 2

. 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 relief from 14 CFR part 21, C erti fication procedures for products and parts, Subpart H

— Airworthiness Certificates
, and any associated noise certification and testing requirements of part 36, is not necessary.

The Basis for Our Decision
You have requested to use a UAS for aerial data collection and closed set motion picture and filming . 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

− 2014

− 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 petitioner 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 th e UAS operation enabled by this exemption is in the public interest.
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 fin d that a grant of exemption is in the public interest. Therefore, pursuant to the authority contained in 49 U.S.C. 106(f), 40113, and 44701, delegated to me by the Administrator, Bird’s Eye Solutions, LLC 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 col lection and closed set motion picture and filming

. This exemption is subject to the conditions and limitations listed below.

# 3

Conditions and Limitations

In this grant of exemption, Bird’s Eye Solutions, LLC 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 we ighing 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 permitted.

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The exemption holder may use either groundspeed or calibrated airspeed to determine compliance with the 87 knot speed restriction. In no case will the UA be operated at airspeeds greater than the maximum UA operating airspeed recommended by the aircraft manufacturer.

4. The UA must be operated at an altitude of no more than 400 feet above ground level (AGL). Altitude must be reported in feet AGL.

5. The UA must be operated within visua l line of sight (VLOS) of the PIC at all times. This requires the PIC to be able to use human vision unaided by any device other than corrective lenses, as specified on the PIC’s FAA

- issued airman medical certificate or U.S. driver’s license.

6. All operations must utilize a visual observer (VO). The UA must be operated within the visual line of sight (VLOS) of the PIC and VO at all times. The VO may be used to satisfy the VLOS requirement as long as the PIC always maintains VLOS capability. The VO and PIC must be able to communicate verbally at all times ;
e lectronic messaging or texting is not permitted during flight operations. The PIC must be designated before the flight and cannot transfer his or her designation for the duration of the flight. T he PIC must ensure that the VO can perform the duties required of the VO.

7. This exemption 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 herein after referred to as the operating documents. The operating documents must be accessible during UAS operations and made available to the Administrator upon request. If a discrepancy exists between the conditions and limitations in this exemption and the p rocedures outlined in the operating documents, the conditions and limitations herein take precedence and must be followed.

# 4 Otherwise, the operator must follow the procedures as outlined in its operating documents. The operator may update or revise its op erating documents. It is the operator’s responsibility to track such revisions and present 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 determines that any update or revision would affect the basis upon which the FAA granted this exemption, then the operator must petition for an amendment to its grant of exem ption. The FAA’s UAS Integration Office (AFS

- 80) may be contacted if questions arise 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 flight prior to conducting further operations under this exemption. Functional test flights may only be conducted by a PIC with a VO and must remain at least 500 feet from ot her people. The functional test flight must be conducted in such a manner so as to not pose an undue hazard to persons and property.

9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is in a condition for safe operation

.
10. Prior to each flight, the PIC must conduct a pre

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

- flight inspection must account for all potential discrepancies, e.g. inoperable components, items, or equipment. If the inspection reveals a condition that affects the safe operation of the UAS, the aircraft is prohibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight.

11. The operator must follow the UAS manufacturer’s maintenance, overhaul, replacement, inspection, and life limit requirements for the aircraft and aircraft components.

12. Each UAS operated under this exemption must comply with all manufacturer safety bulletins.

13. Under this grant of exemp tion, a PIC must hold either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC must also hold a current FAA airman medical certificate or a valid U.S. driver’s license issued by a state, the District of 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.

14. The operator may not permit a ny PIC to operate unless the PIC demonstrates the ability to safely operate the UAS in a manner consistent with how the UAS will be

# 5 operated under this exemption, including evasive and emergency maneuvers and maintaining appropriate distances from persons, vessels, vehicles and structures. PIC qualification flight hours and currency must be logged in a manner consistent with 14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs (training, proficiency, and experience

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

- building flights, all persons not essential for flight operations are considered nonparticipants, and the PIC must operate the UA with appropriate distance from nonparticipants in accordance with 14 CFR § 91.119.

15. UAS operations may not be conducted during night, as defined in 14 CFR § 1.1. All operations must be conducted under visual meteorological conditions (VMC). Flights under special visual flight rules (SVFR) are not authorized.

16. The U A 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 symbol as denoted on the current FAA

published a eronautical chart, unless a letter of agreement with that airport’s management is obtained or otherwise permitted by a COA issued to the exemption holder. The letter of agreement with the airport management must be made available to the Administrator or an y law enforcement official upon request.

17. The UA may not be operated less than 500 feet below or less than 2,000 feet horizontally from a cloud or when visibility is less than 3 statute miles from the PIC.

18. If the UAS loses communications or loses its GPS signal, the UA must return to a pre

determined location within the private or controlled

- access property.

19. The PIC must abort the flight in the event of unpredicted obstacles or emergencies.

20. The PIC is prohibited from beginning a flight unless (considerin g 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 Orga nization (ATO) Certificate of Waiver or Authorization (COA). All operations shall be conducted in accordance with an ATO

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

.
22. All aircraft operated in accordance with this exemption must be identified by serial number, registered in accordance with 14 CFR part 47, and have identification (N

-

# 6 Number) markings in accordance with 14 CFR part 45, Subp art 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 available to the Administrator or any law enforcement official upon request.

24. The UA must remain clear and give way to all manned aviation operations and activities at all times.

25. The U AS 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 event of an accident. The operator must ensure that nonparticipating persons remain under such protection. If a situation arises where nonparticipating persons leave such protec tion and are within 500 feet of the UA, flight operations must cease immediately in a manner ensuring the safety of nonparticipating persons ; and b. The owner/controller of any vessels, vehicles or structures has granted permission for operating closer to tho se objects and the PIC has made a safety assessment of the risk of operating closer to those objects and determined that it does not present an undue hazard.
The PIC, VO, operator trainees or essential persons are not considered nonparticipating persons u nder this exemption.

27. All operations shall be conducted over private or controlled

- access property with permission from the property owner/controller or authorized representative. Permission from property owner/controller or authorized representative will be obtained for each flight to be conducted.

28. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of the operational area as defined by the applicable COA must be reported to the FAA's UAS Integration Office (AF S

- 80) within 24 hours. Accidents must be reported to the National Transportation Safety Board (NTSB) per instructions contained on the NTSB Web site: www.ntsb.gov

. If this exemption permits operations for the purpose of closed

- set motion picture and television filming and production, the following additional conditions and limitations apply.

# 7

29. The operator must have a motion picture and television operations manual (MPTOM) as documented in this grant of exemption.

30. At lea st 3 days before aerial filming, the operator of the UAS affected by this exemption must submit a written Plan of Activities to the local Flight Standards District Office (FSDO) with jurisdiction over the area of proposed filming. The 3

- day notification m ay 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 p hone number of the person responsible for the on

- scene operation of the UAS; d. Make, model, and serial or N

- Number of UAS to be used;

e. Name and certificate number of UAS PICs 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 o f 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 part icipating persons consenting to be involved and necessary for the filming production, as specified in the exemption holder’s MPTOM.
Unless otherwise specified in this grant of exemption, the UAS, the UAS PIC, and the UAS operations must comply with all ap plicable parts of 14 CFR including, but not limited to, parts 45, 47, 61, and 91.
This exemption terminates on April 30, 2017 , unless sooner superseded or rescinded.
Sincerely,

/s/ John Barbagallo Acting Deputy Director, Flight Standards Service

## 1 November 7 , 2014
U.S. Department of Transportation
Docket Management System

1200 New Jersey Ave., SE
Washington, DC 20590

Bird’s Eye Solutions, LLC Petition for Exemption to Operate
Unmanned Aircraft Systems fo r Aerial Photography, Filming and Scientific Data collection.

FAA Regulatory Docket

NAME AND ADDRESS OF PETITIONER
Bird’s Eye Solutions, LLC Attn: David Geisler 8300 Airport Road, STE 3 Middleton, WI 53562

Phone: 608

- 469

- 3531

E

- mail: birdseyesolutionsllc@gmail.com U.S. Department of Transportation Docket Management System 1200 New Jersey Ave., SE Washington, DC 20590

## 2

I. PETITION SUMMARY
Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012,

Pub. L. No. 112

- 95 (2012), 126 Stat. 11 (“Section 333”) and the Federal Aviation Administration’s (“FAA”)
general exemption authority under 49 U.S.C. § 44701(f), Bird’s Eye Solutions L.L.C. (“Petitioner”) hereby
petitions for exemptions from 14 C.F.R. §§ 61. 113(a) and (b), 61.133(a), 91.7(a),
91.9(b)(2), 91.103(b)(1), 91.119(c), 91.121, 91.151, 91.203(a) and (b), 91.405(a), 91.407(a)(1)
91.409(a)(2), 91.417(a)

- (b). The proposed exemptions, if granted, would allow Petitioner to operate

small, camera

- mounted unmanned aircraft systems (“UAS”) weighing 55 pounds or less
for the purpose of closed

- set filming of motion pictures, music videos, web videos,
corporate videos, television programs and commercials, and still photography. Additionally the

collection of agriculture and conservation supporting scientific data in FAA approved COE’s.
Based on the small size of Petitioner’s UAS, the qualifications and experience of
Petitioner’s UAS operators, and the restricted, sterile environment within which

Petitioner will operate, the requested exemptions fall squarely within the zone of safety
envisioned by Congress and set forth in Section 333. Additionally, the enhanced safety
achieved by replacing significantly larger manned aircraft carrying crew and flammable
fuel with small UAS carrying no passengers or crew and operated under the specific
guidelines and procedures proposed by Petitioner gives the FAA good cause to find that
the UAS operations enabled by the instant Petition are in the public interest. Thus, the
requested exemptions should be granted.

## 3

II. BACKGROUND
For more than two decades, Petitioner’s Operational experience, Unmanned Systems Piloting and
Instructing for the U.S. Army, United States Navy , United States Marines offers a track record of safety
and broad exposure to safe FAA Coordination. In addition to the petitioners UAS Experience the
petitioner has worked extensively with the FAA SmarTopo Obstacle Verification operations

. Combining

th e latest technology with a long track record of safe and successful projects,
Petitioner seeks regulatory exemptions that will allow Petitioner to employ camera mounted UAS
technology in the filming, production , and scientific data collection for conserv ation and agriculture

process.

III. STATUTORY AUTHORITY

A. Section 333
Section 333, titled “Special Rules for Certain Unmanned Aircraft Systems,”
provides a mechanism for seeking expedited FAA authorization of safe civil UAS

operations in the National Airspace System (“NAS”). Section 333(a) states that the FAA
“shall determine if certain unmanned aircraft systems may operate safely in the national
airspace system before completion of the [comprehensive] plan and rulemaking required

b y section 332(b)(1) of this Act or the guidance required by section 334 of this Act.” In Section 332(b)(1),
Congress made it clear that Section 333 provides a mechanism for “expedited operational
authorization.” The FAA has committed to complying with t his mandate by granting several petitions
almost identical to the one at hand. See, e.g., Exemption No. 11062, Regulatory Docket No. FAA

- 2014

- 0352 (granting regulatory exemptions to Astraeus Aerial for operation of unmanned aircraft systems for

the purpose of filming for the motion picture and television industry).
Section 333(b) identifies several factors that the FAA should consider in determining whether
commercial UAS operations should be approved. These include UAS that, “as a result of their size,

## 4

weight, speed, operational capability, proximity to airports and populated areas, and operation within
visual line of sight do not create a
hazard to users of the [NAS] or the public or pose a threat to national security.” See
Section 333(b).

B. Section 44701(f)
In addition to the specific authority conferred by Section 333, the FAA Administrator has general
authority to grant exemptions from the FAA’s safety regulations and minimum standards when the
Administrator decides a requested exemption is in the public interest. See U.S.C. § 44701(f).

IV. REQUESTED EXEMPTIONS
Petitioner requests relief from the following regulations:

.
Section 61.113 prescribes that “no person who holds a private pilot certificate

may act as a pilot in command of an aircraft that is carrying passengers or property for compensation or
hire; nor may that person, for compensation or hire, act as pilot in command of an aircraft,” (see Section
61.113(a)), and that “a private pilot may, for compensation or hire, act as pi lot in command 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,” (see Section 61.113(b )).
Section 61.133(a) sets forth privileges for persons holding commercial pilot certificates,
including a provision impliedly limiting to persons holding a commercial pilot certificate the
ability to act as pilot in command of an aircraft “[f]or compensation or hire.”
Section 91.103(b)(1) prescribes, in pertinent part, that each pilot in command shall, before
beginning a flight, become familiar with all available information concerning that fligh t, to
include, “For any flight, runway lengths at airports of intended October 1, 2014 use, and the following
takeoff and landing distance information:... For civil aircraft for which an approved Airplane or

## 5

Rotorcraft Flight Manual containing takeoff and landing distance data is required, the takeoff and
landing distance data contained therein.”
Section 91.119(c) prescribes that, except when necessary for takeoff or landing, no person may
operate an aircraft below the following altitudes: “Over other th an congested areas. An altitude
of 500 feet above the surface, except over open water or sparsely populated areas. In those
cases, the aircraft may not be operated closer than 500 feet to any person, vessel, vehicle, or structure.”

Section 91.121 requires, in pertinent part, each person operating an aircraft to maintain cruising
altitude by reference to an altimeter that is set “to the elevation of the departure airport or an
appropriate altimeter setting available before departure.”

Section 91. 151(a) prescribes that no person may begin a flight in an airplane under
VFR conditions unless (considering wind and forecast weather conditions) there is
enough fuel to fly to the first point of intended landing and, assuming normal cruising
speed, (1) during the day, to fly after that for at least 30 minutes; or (2) at night, to fly

after that for at least 45 minutes.

Section 91.203 prohibits, in subpart (a), any person from operating a civil aircraft
unless it has within it (1) an appropriate and cu rrent airworthiness certificate; and (2) an
effective U.S. registration certificate issued to its owner or, for operation within the United States, the
second copy of the Aircraft Registration Application as provided for in October 1,
§ 47.31(c). Sectio n 91.203 prescribes, in subpart (b), that no person may operate a civil
aircraft unless the airworthiness certificate or a special flight authorization issued under §

91.715 is displayed at the cabin or cockpit entrance so that it is legible to passengers or crew.
Section 91.405(a) requires, in pertinent part, that an aircraft operator or owner
shall have the aircraft inspected as prescribed in subpart E of the same part and sh all,
between required inspections, except as provided in paragraph (c) of the same section,
have discrepancies repaired as prescribed in Part 43 of the chapter.

## 6

Section 91.407(a)(1) prohibits, in pertinent part, any person from operating an

aircraft tha t has undergone maintenance, preventative maintenance, rebuilding, or
alteration unless it has been approved for return to service by a person authorized under
§ 43.7 of the same chapter.
Section 91.409(a)(2) prescribes, in pertinent part, that no person may operate an
aircraft unless, within the preceding 12 calendar months, it has had an inspection for the
issuance of an airworthiness certificate in accordance with part 21 of this chapter.
Section 91.417(a) and (b) prescribes, in pertinent part, that

- (a) Each registered owner or operator shall keep the following records

for the periods specified in paragraph (b) of this section:
(1) Records of the maintenance, preventative maintenance, and

alteration and records of the 100

- hour, annual, progressive,

and ot her required or approved inspections, as appropriate,
for each aircraft (including the airframe) and each engine,
propeller, rotor, and appliance of an aircraft. The records

must include

- (i) A description (or reference to data acceptable to the
Administrator) of the work performed; and
(ii) The date of completion of the work performed; and
(iii) The signature, and certificate number of the person approving the aircraft for

return to service.
(2) Records containing the following informati on:
(i) The total time in service of the airframe, each engine, each propeller, and each

rotor.

## 7 (ii) The current status of life

- limited parts of each airframe, engine, propeller, rotor,
and appliance.
(iii) The time since last overhaul of all i tems installed on the aircraft which are
required to be overhauled on a specified time basis.
(iv) The current inspection status of the aircraft, including t he time since the last
inspection required by the inspection program under which the aircraft a nd its
appliances are maintained.
(v) The current status of applicable airworthiness directives (AD) and safety
directives including, for each, the method of compliance, the AD or safety

directive number and revisions date. If the AD or safety directive involves
recurring action, the time and date when the next action is required.
(vi) Copies of the forms prescribed by § 43.9(d) of this chapter for each major

alteration to the airframe and cur rently installed engines, rotors, propellers, and
appliances.
(b) The owner or operator shall retain the following records for the periods prescribed:

(1) The records specified in paragraph (a)(1) of this section shall
be retained until the work is rep eated or superseded by other
work or for 1 year after the work is performed.
(2) The records specified in paragraph (a)(2) of this section shall

be retained and transferred with the aircraft at the time the

aircraft is sold.
(3) A list of defects furn ished to a registered owner or operator
under § 43.11 of this chapter shall be retained until the
defects are repaired and the aircraft is approved for return to

service.

## 8

V. PETITIONER’S PROPOSED OPERATIONS SATISFY SECTION 333.

A. Unmanned Aircraft System
The UAS to be operated under this request are less than 55 lbs. fully loaded, will
be operated at a speed of no more than 50 knots, carry neither a pilot nor passenger, carry
no explosive materials or flammable liquids, and operate exclusively with in a secured
area. Petitioner’s UAS use a radio frequency spectrum for operation and control that
complies with Federal Communications Commission (“FCC”) requirements, and
Petitioner has integrated safety features into the UAS, as described in Petitioner’s Flight
Operations and Procedures Manual (“FOPM”) (collectively, “operations manuals”).
Petitioner’s UAS are equipped with redundant safety mechanisms allowing them

to op erate safely after experiencing certain in

- flight failures. If a lost

- link event occurs,
including the loss of ground communications and/or the loss of a GPS signal, Petitioner’s
UAS have the ability to perform a pre

- coordinated, predictable, automated fl ight
maneuver and return to a predetermined location within a designated security perimeter
for landing. The UAS further have the ability to abort a flight in the event of unpredicted
obstacles or emergencies. All flights will be terminated after a maxi mum of 30 minutes
or with 25% remaining battery power, whichever occurs first. Thus, good cause exists
for granting Petitioner’s requested relief from 14 C.F.R. § 91.151(a) (setting forth fuel
requirements for flight in VFR conditions).

Petitioner’s UAS will be identified by serial number, registered in accordance with
14 C.F.R. Part 47, and have identification (N

- Number) markings in accordance with 14
C.F.R. Part 45, Subpart C. Markings will be as large as practicable.
Regarding Petitioner’s requested relief from 14 C.F.R. § 91.121 (Altimeter
Settings), Petitioner seeks such relief because Petitioner will not have a typical
barometric altimeter onboard the UAS. Instead, altitude information will be provided to

## 9

the UAS PIC via a digitally encoded tel emetric data feed, which downlinks from the
aircraft to a ground

- based on

- screen display. The altitude information will be generated
by equipment installed onboard the UAS, using GPS triangulation, digitally encoded

barometric altimeter, radio altimeter , or any combination thereof. Prior to each flight, a
zero altitude initiation point will be established and confirmed for accuracy by the UAS
PIC. Thus, good cause exists for granting the requested relief from 14 C.F.R. § 91.121.
Given the size, weight, speed, and limited operating area associated with the
aircraft to be utilized by the applicant, an exemption from 14 C.F.R. Par t 21, Subpart H
(Airworthiness Certificates), subject to certain conditions and limitations, is warranted (if

necessary ) and meets the requirements for an equivalent level of safety under 14 C.F.R.
Part 11 and Section 333. The UAS operated without an airworthiness certificate in the
restricted environment and under the conditions and limitations proposed by Petitioner

w ill be at least as safe, or safer, than a conventional aircraft (fixed wing or rotorcraft)
operating with an airworthiness certificate issued under 14 C.F.R. Part 21, Subpart H, and
not subject to the proposed limitations and conditions.

Petitioner will strictly comply with safety and maintenance procedures included in
all applicable UAS manufacturer’s instructions and operating manuals. To the extent
such information is not included in the guidelines developed by the manufacturers,

Petitioners will de velop and document maintenance, overhaul, replacement, and
inspection requirements, procedures to document and maintain maintenance records with
regard to Petitioner’s UAS, and UAS technician qualification criteria. Petitioner’s
operations manuals will include maintenance requirements for Petitioner’s UAS,
including “on

- condition” maintenance and modifications. In light of these mitigating
factors, exemptions from 14 C.F.R. §§ 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and
91.417(a) and (b) are wa rranted.

## 10

B. UAS Pilot in Command
Petitioner’s UAS pilot in command (PIC) shall have passed the FAA ground

school examination and shall hold at least a third

- class medical certificate an be
required to hold a current pilot’s license. Since there are no st andards for either private
or commercial UAS pilot certificates, knowledge of airspace regulations acquired from
FAA ground school and dexterity in the control and operation of the UAS acquired from
actual operation of the aircraft will be the most impo rtant factors in establishing an
equivalent level of safety. According to the FAA, “the FAA considers the overriding
safety factor for the limited operations proposed by the petitioner to be the airmanship
skills acquired through UAS

- specific flight cyc les, flight time, and specific make and
model experience, culminating in verification through testing.” See Exemption No.
11062, Regulatory Docket No. FAA

- 2014

- 0352, at p. 18. With those factors in mind,
Petitioner’s UAS PIC shall be required to meet several conditions and limitations as

outlined in the FOPM , including the following:

• The UAS PIC will have accumulated and logged a minimum of 200 flight
cycles and 25 hours of total time as a UAS pilot a nd at least 10
hours logged as a UAS pilot with a similar UAS type (single blade or
multirotor).

• The UAS PIC will have accumulated and logged a minimum of five hours
of flight time with the specific make and model of the UAS to be utilized
for opera tions under the exemption and three take

- offs and landings in the
preceding 90 days.

• The UAS PIC will have successfully completed the qualification process as
specified in the operations manuals, to include a knowledge and skill test.

## 11

Regarding P etitioner’s requested relief from 14 C.F.R. § 91.7(a), it is Petitioner’s
understanding that Petitioner’s UAS will not require an airworthiness certificate in accordance with
14 C.F.R. Part 21, Subpart H, and that exemption from 14 C.F.R. § 91.7(a) is th erefore unnecessary. To
the extent such an exemption is deemed necessary, Petitioner asserts that it should be granted in light
of the safety procedures proposed herein. In accordance with the pertinent part of 14 C.F.R. § 91.7(b),
the operator in comma nd of Petitioner’s UAS shall be responsible for determining whether the aircraft is
in a safe condition for flight. Petitioner’s manuals for maintenance and operations shall
include safety checklists to be used by the operator in command prior to each fl ight.
Regarding Petitioner’s requested relief from 14 C.F.R. § 91.9(b)(2) (Civil aircraft
flight manual, marking, and placard requirements and § 91.203(a) and (b), (Civil aircraft:

certifications required), it is Petitioner’s understanding that relief from these regulations
is no longer necessary in light of the FAA Memorandum “Interpretation regarding
whether certain required documents may be kept at an unmanned aircraft’s control
station,” dat ed August 8, 2014. To the extent the FAA deems an exemption from this
section necessary for Petitioner’s proposed operations, such exemption should be granted
in light of the mitigating fact that Petitioner will maintain the documents required under

14 C.F.R. §§ 91.9 and 91.203 at the UAS ground control station during flights.
Additionally, 100% of Petitioner’s operations will utilize a visual observer
(“VO”). The VO may be used to satisfy the VLOS requirement as long as the PIC
always maintains VLOS c apability. The VO and the PIC will be able to communicate
verbally at all times during operational flights.
Regarding Petitioner’s requested relief from 14 C.F.R. § 91.103(b)(1), Petitioner
will comply with the other applicable procedures and requirement s stated in § 91.103(a)
and (b). Specifically, the PIC will take all actions including reviewing weather, flight
battery requirements, aircraft performance data, and landing and takeoff distances before

## 12

initiation of a flight. The PIC will also account for all relevant site

- specific conditions in
their preflight procedures. Risks presented by sun glare will be mitigated by the PIC’s
and VO’s ability to see other air traffic and initiate a return

- to

- home sequence if needed.

C. O p erating Parameters of Pe titioner’s UAS
Petitioner’s UAS operations will be conducted within a sterile environment of

closed

- set filming. In this controlled environment, Petitioner’s operations will remain
within VLOS of the PIC and VO, below 400 feet AGL, and at speeds below 50 knots.
Only participating persons will be permitted within the operating area.
Consistent with the relief typically provided to manned operations under FAA
Order 8900.1, Volume 3, Chapter 8, Section 1, Petitioner requests relief from 14 C.F.R.

§ 91.119 (c) with respect to those participating persons, vehicles, and structures directly
involved in the performance of the actual filming. Regarding distance from participating
persons, the operations manuals set forth safety factors for authorized and consen ting
production personnel. Because those procedures are specific to participating persons, no
further FSDO or aviation safety inspector approval is necessary for reductions to the
distances specified in Petitioner’s manuals.
Regarding the distance from nonparticipating persons, Petitioner will ensure that
no persons are allowed within 500 feet of the operating area except those consenting to
be involved and necessary for the filming production, with the possibility of reduci ng this
distance to no less than 200 feet if it would not adversely affect safety and the
Administrator has approved it. This is consistent with FAA Order 8900.1, V3, C8, S1.
Petitioner will not conduct UAS operations within 5 nautical miles of the

geog raphic center of a non

- towered airport unless a letter of agreement with that airport’s
management is obtained and the operation is conducted in accordance with a Notice to
Airmen (“NOTAM”). Additionally, Petitioner will not operate in Class B, C, or D

## 13

airspace without written approval from the FAA. Nor will Petitioner operate the UAS
less than 500 feet below or less than 2,000 feet horizontally from a cloud or when
visibility is less than 3 statute miles from the PIC.

Petitioner’s UAS will remain clea r and yield the right of way to all manned
operations and activities at all times (including, but not limited to, ultralight vehicles,
parachute activities, parasailing activities, and hangliders).
Although Petitioner seeks to comply with the waiver proc ess as described in FAA
Order 8900.1, Volume 3, Chapter 8, Section 1 (Issue a Certificate of Waiver for Motion
Picture and Television Filming), the current section of Order 8900.1 has specific
processes that preclude a jurisdictional FAA FSDO from issui ng the required Certificate
of Waiver, because the section did not originally provide for UAS operations. Thus,
Petitioner seeks exemption from the applicable regulations normally waived during that
process. Petitioner proposes that the FAA include the required notifications and
coordination with jurisdictional FSDOs through the conditions and limitations
accompanying the requested exemption, and that the exemption sought herein will take

the place of the Certificate of Waiver normally issued by a jurisdictional FSDO under
8900.1. Under this rubric, Petitioner will notify every FSDO with jurisdiction over the
area that Petitioner plans to operate, just as with manned filming operations, and those
FSDOs will have the ability to coordinate further conditions and limitations with the
UAS Integration Office to address any local concerns.
Petitioner will obtain an Air Traffic Organization (“ATO”) issued Certificate of
Waiver or Authorization (“ COA”) prior to conducting any operations under this grant of
exemption. In fulfilling its requirements under the COA, Petitioner will be required to
request a NOTAM not more than 72 hours in advance, but not less than 48 hours prior to
the operation.

## 14

D. The Requested Exemption Promotes the Public Interest
The enhanced safety achieved by replacing significantly larger manned aircraft
carrying crew and flammable fuel with small UAS carrying no passengers or crew and
operated under the specific guideline s and procedures proposed by Petitioner gives the
FAA good cause to find that the UAS operations enabled by the instant Petition are in the
public interest. Moreover, as the FAA has already recognized, “UAS provide an
additional tool for the filmmaking industry, Agriculture and Conservation adding a greater degree of
flexibility, which supplements the current capabilities offered by manned aircraft.” See Exemption No.
11062, Regulatory Docket No. FAA

- 2014

- 0352, at p. 22.

VI. CONCLUSION
For the foregoi ng reasons, the regulatory exemptions requested herein should be
granted and Petitioner should be permitted to conduct small UAS operations for the
purpose of closed

- set filming.

Respectfully submitted,

David P. Geisler

Manager
Bird’Eye Solutions, LLC

## AP PENDIX A

– FLIGHT MANUAL

FLIGHT RESTRICTIONS (a) No flight will be made with a UA Gross weight exceeding 55 pounds; (b) All operations must occur in FAA approved airspace at no more than 400' AGL, at an airspeed of no more than 25 knots and no further than 3/4 NM from the PIC; (c) All operations must utilize a visual observer (VO). The VO and PIC must be able to

c ommunicate verbally at all times during a flight operation; (d) Operations will be restricted to flights over private property with the pe rmission of the property owner; (e) The PIC must have accumulated and logged, in a manner consistent with 14 CFR § 61.51 (b), a minimum of 100 flight cycles and 25 hours of total time as a UA rotorcraft pilot and at least ten hours logged as a UA pilot wi th a similar UA type;

(f) All required permits will be obtained from state and local government prior to operation; (g) The UA will not be operated over densely populated areas; (h) The UA will not be operated at air shows; (i) The UA will not be opera ted over any open

- air assembly of people; (j) The UA will not be operated over heavily trafficked roads; (k) The UA will not be operated within 5 NM of an airport or heliport without written permission Airport Manager. (l) Operations will be restricted t o day only and weather conditions equivalent to VFR; (m) The PIC will brief the VO and property owner about the operation and risk before the first flight at each new location; (n) No flight may be made without a successful Pre

- Flight Inspection by the P IC before each operation to ascertain that the UA is in a condition safe for flight.

PIC SHOULD VERIFY THE FOLLOWING ITEMS BEFORE STARTING THE PRE

- FLIGHT PROCESS (1) Verify COA Approved (2) Verify NOTAM Filed (if applicable) (3) Verify FSDO coordination completed (4) Ve rify closest Unicom/Tower Frequency for Monitoring.

PRE

- FLIGHT CHECKLIST (1) Check UA battery health (press self check button) verify 4 green bars illuminate (2) Check all wiring connections are tight; (3) Check all propellers are undamaged and no cr acks exist in any structural members of the UA;

(5) Turn on radio controller, move all control switches to forward or UP position and throttle control stick neutral position; (6) Turn On UA power (7) Await Aft Lights to flash green (8) Turn on tr ansmitter and camera.



## PRE

- TAKEOFF CHECKLIST (1) Confirm Green Lights on aircraft (2) Confirm Observer is ready (3) Confirm area cleared of all non

- essential pe rsonnel

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 1 | 

# PHANTOM 2 User Manual V1. 1

For PHANTOM 2 Main Controller Firmware version V 3 .0 2
& PHANTOM 2 Assistant version V 3.0
& PHANTOM RC Assistant version V1.1 

## April 30 , 2014 Revision

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 rights reserved.

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

.

### ©2013 DJI Innovations. All Rights Reserved. 2 | 

## C ontent

CONTENT

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

IN THE BOX

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

REQUIRED ITEMS

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

SYMBOL LEGEND

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

1. PHANTOM 2 AIRCRAF T

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

1.1 B UIL T



## - 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



## ................................ ................................ ............... 10
1.4 N OTES FOR 

## PHANTOM 2 USING WITH OTHER 

## DJI PRODUCTS



## ................................ ................ 11

2 PROPELLERS

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

2.1 A SSEMBLY



## ................................ ................................ ................................ ..................... 12
2.2 D ISASSEMBLY



## ................................ ................................ ................................ ................ 12
2.3 N OTES



## ................................ ................................ ................................ ......................... 12

3 REMOTE CONTROLLER

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

3.1 P OWE R ON THE 

## R EMOTE 

## C ONTROLLER



## ................................ ................................ ............... 13
3.2 R EMOTE CONTROLLER 

## P OWER 

## LED I NDICATOR 

## S TATUS



## ................................ .......................... 13
3.3 A NTENNA 

## O RIENTATION



## ................................ ................................ ................................ .. 14
3.4 R EMOTE 

## C ONTROLLER 

## O PERATION



## ................................ ................................ .................... 14
3.5 L INKING THE REMOTE CO NTROLLER 

## & BUILT



## - IN RECEIVER



## ................................ ........................ 16

4 INTELLIGENT BATTER Y

................................ ................................ ............................... 17

4.1 C HARGING 

## P ROCEDURES



## ................................ ................................ ................................ .. 17
4.2 I NSTALL THE 

## B ATTERY



## ................................ ................................ ................................ ...... 18
4.3 B ATTERY 

## U SAGE



## ................................ ................................ ................................ ............. 18
4.4 D ESCRIPTION OF THE 

## B ATTERY 

## L EVEL 

## I NDICATOR



## ................................ ................................ ... 19
4.5 C ORRECT 

## B ATTERY 

## U SAGE 

## N OTES



## ................................ ................................ ...................... 20

5 CALIBRATING THE CO MPASS

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

5.1 C ALIBRATION 

## W

ARNINGS



## ................................ ................................ ................................ . 21

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

## 5.2 C ALIBRATION 

## P ROCEDURES



## ................................ ................................ .............................. 21
5.3 W HEN 

## R ECALIBRATION IS 

## R EQUIRED



## ................................ ................................ .................. 21

6 FLIGHT

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

6.1 F LYING 

## E NVIRONME NT 

## R EQUIREMENTS



## ................................ ................................ .............. 22
6.2 S TARTING THE 

## M OTORS



## ................................ ................................ ................................ ... 22
6.3 T AKEOFF 

## /L ANDING 

## P ROCEDURES



## ................................ ................................ ....................... 22
6.4 F AILSAFE 

## F UNCTION



## ................................ ................................ ................................ ........ 23
6.5 L O W 

## B ATTERY 

## C APACITY 

## W ARNING 

## F UNCTION



## ................................ ................................ ..... 24
6.6 F LIGHT 

## L IMITS 

## F UNCTION



## ................................ ................................ ................................ . 25 Max Height & Radius Limits

................................ ................................ ......................... 25
6.7 F LIGHT 

## L IMITS OF 

## S PECIAL 

## A REAS



## ................................ ................................ ...................... 26
6.8 C ONDITIONS OF 

## F LIGHT 

## L IMITS



## ................................ ................................ ......................... 27 Disclaimer

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

7 ASSISTANT SOFTWARE INSTALLATION AND CON FIGURATION

................................ .... 29

7.1 I NSTALLING 

## D RIVER AND 

## PHANTOM 2 A SSISTANT 

## S OFTWARE



## ................................ ............... 29
7.2 U SING THE 

## PHANTOM 2 A SSISTANT 

## S OFTWARE ON A 

## PC

................................ ..................... 30
7.3 F IRMWARE UPGRADE OF 

## PHANTOM 2

................................ ................................ ............. 31
7.4 PHANTOM RC A SSISTANT 

## S OFTWARE 

## D ESCRIPTION



## ................................ ............................ 32

8 APPENDIX

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

8.1 S PECIFICATIONS



## ................................ ................................ ................................ .............. 33
8.2 LED F LIGHT 

## I NDICATORS 

## D ESCRIPTION



## ................................ ................................ ............... 33

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

## I n the Box

PHANTOM 2 2.4 GHz Remote Controller Propeller Pair

Intelligent Battery Charger Plug Set

Screwdriver Assistant Wrench Cables

Micro

- USB Cable Screws Accessories Box



## Required Items

AA Batte ry X 4



## Symbol Legend

Forbidden(Important) Caution Tip Reference

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

## 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 Controller), 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 in formation 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 controller and the MC acts as the brains of the complete flight control
system connecting and controlling all the modules together.

The PHANTOM 2 can be configured in the Assistant S oftware, 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 Innovations. All Rights Reserved. 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~1 2.6V 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 separate 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 wifi or 2.4G wireless video transmission module) except the

2.4G Bl uetooth 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 Innovations. All Rights Reserved. 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 Innovations. All Rights Reserved.

( 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 Innovations. All Rights Reserved. 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 Markk II package when connecting to the DJI specified wireless video

transmission module AVL58.

( 5 ) U sing the i Pad Ground Station

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.

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

( 6 ) U sing the PC Ground Station

Figure 1

- 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 Controller Signal Lost

1 st Level Low Battery Capacity Warning

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 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 S oftware 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

.



### 1.4 Notes for PHANTOM 2 using with other DJI products Before using PHANTOM 2 with other DJI products, users should connecting th e products correctly and upgrade
the firmware as requirements below .

Items to upgrade Firmware versions required Assistant S oftware for upgrading Assistant S oftware
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 S oftware is applied to both iOSD Mark II and iOSD mini.

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

## 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 (9443) Black Nut (9443 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 bef ore 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 Innovations. All Rights Reserved. 

## 3 Remote Controller

T he PHANTOM 2 remote controller can be configured in the PHANTOM RC Assistant S oftware. T he sticks mode is Mode 2 on delivery.

F igure 3

- 1 Figure 3

- 2
[1] Antenna [2] Carrying Handle [3] 3

- Position Switch S1 [4] 3

- Position Switch S2 [5] Joystick1 ( J1;J2 )
[6] Joystick2 ( J3;J4 ) [7] Neck Strap Attachment [8] Power Switch [ 9] Power Indicator [ 10] Battery C ompartment [11]Micro

- USB Port [ 12 ]Slide Lever [13] P otentiometer


### 3.1 Power on the Remote Controller
1. Install the four AA Batteries (not included) in to the battery compartment on the back of

the remote controller according to the negative and positive poles.

2. Set the S1 and S2 switches to the upper most positi on and all sticks are at mid

- point

before switching on the power switch.

3. P ush the power switch to the right to power on the remote controller. I f the power LED

indicator is solid on, the remote controller is functioning normally.

( 1 ) P lease make sure the batteries have enough capacity before use. If the low voltage warning

alert sounds ( refer to the < Remote Controller Power Indicator Status Information>), please
replace batteries as soon as possible. ( 2 ) Using the correct type of battery wi ll pre v ent risk of damage or malfunction

. ( 3 ) For long term storage, be sure to remove the batteries from the remote controller.



### 3.2 R emote controller Power LED Indicator Status
Power LED Indicator Sound R emote Controller Status
None N ormal
B

- B

- B

...... Low voltage (at 4V

- 4.3V)

. R eplace the batteries immediately

B

-- B

-- B

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

using the remote controller

.

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

T he remote controller will power off automatically when battery voltage drops below 4V

. Land and
change batteries as soon as possible when the low voltage alert occurs to avoid loss of control during
flight.



### 3.3 Antenna Orientation
The remote controller ’ s antenna should point skyward s without obstructions for maximum communication range
during flight.

F igure 3

- 3


### 3.4 Remote Controller Operation The operations of remote controller are based on mode 2 stick configuration

. 

### Definitions

The ‘ stick neutral’ position s and ‘ stick released’ mean the control stick s of the r emote c ontroller are p laced at the central position.
To ‘move the stick ’ means that the stick of r emote c ontroller 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 ontroller (Mode 2) Aircraft ( nose direction ) Operation details

T he t hrottle stick controls the aircraft 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 ing the throttle stick above the centered (neutral) position will result in the aircraft tak ing off. We suggest that you push t he throttle stick slowly to prevent the aircraft from sudden and unexpected ascent

.

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 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 always fly in the same direction. The command stick controls the rotating angular velocity of the aircraft. Increasing movement of
the command stick results in 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. Increasing movement of the command stick will result in a larger tilt angle (maximum is 35 ̊) and faster flight velocity.
The roll stick controls the aircraft 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. Increasing movement of the command stick will result in a larger tilt angle (maximum is 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, 5 times or more to enter into compass calibration mode. U sers can configure position 3 (bottom po sition) of the S1 switch to trigger the Failsafe in the A ssistant S oftware.

OFF Course Lock Home point Lock S2 is the IOC mode switch. IOC (Intelligent Orientation Control) function can be enabled in the Assistant S oftware when in Naza

- M mode

. Only use the IOC function after you are familiar
with flying

.

### ©2013

- 2014 DJI Innovations. All Rights Reserved. Slide Lever control s the pitch of the H3

- 2D and H3

- 3D gimbal. T he position of slide lever determines the pitch angle relative to the
horizontal level. S lide the lever left to make th e gimbal pitch
down up to a
- 90 ° position. S lide the lever right to pitch up to + 0 ° position resulting in gimbal being at a horizonta lly level
orientation.
( 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 remote controller& built

- in receiver
PHANTOM 2 has a built

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

in the Figure 3

- 4

. The link between the remote controller and a ircraft is already established for you so you can initially skip this
procedure . If you ever replace the remote controller, re
- establishing the link is required.

F igure 3

- 4 Linking procedures

1. Power on the PHANTOM 2.

2. Turn on the remote controller 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 controller and the built

- in receiver
has been successfully established.

Link Indicator S tatus

T he remote controller is linked with the receiver successfully

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

. T he receiver is ready for linking

. There is 2.4GHz signal around but the remote controller is not linked with the receiver
,

### ©2013

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

## 4 Intelligent Battery

The i ntelligent battery is specially designed for the PHANTOM 2 , with a bat tery 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 a utomatically when the battery voltage reaches 12.8V to prevent overcharging damage

. ( 5 ) Over D ischarging
Protection D ischarging s top s a utomatically 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

. T he 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 battery 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

level indicator description for details.

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

4. T he battery is full y charged when t he 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 button once an d 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. (4) Checking 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 LED3

LED4
Battery Power Button
(Built

- in Battery Power Indicator) LED2

LED1 Battery Level Indicator

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

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 S oftware.


### 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%

80 %~ 90 %

70 %~ 80 %

60 %~ 70 %

50 %~ 60 %

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 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 should 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 completel y 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 your 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 informati on in the DIS CLAIMER.

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

## 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

magnet ic 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 ) T he mechanical structure of the aircraft 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 Innovations. All Rights Reserved. 

## 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 sho uld be open and void of tall buildings 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 r emote control ler and other wireless equipment. (No base

stations or cell towers around) ( 6 ) The flight control system will not work properly at the South Pole or North Pole. ( 7 ) 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 needed to start the motors

. Push the sticks according to one of the options

below to start motors. Once the motors have sp u n up, release both stick s simultaneously. The same com mand 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 controller.

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 Controller Operation >

for more details.

6. Be sure you are hovering over a level surface. Pull down on the throttle stick gently to de scend and land.

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

7. After landing the aircraft on the ground, keep the throttle stick at its lowest position for about 3 to 5

seconds which will automatically stop the motors.

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.


### 6 .4 Failsafe Function
T he aircraft will enter Failsafe mode when the connection from the remote controller 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 controller and enter Failsafe mode: ( 1 ) The remote controller is power ed off. ( 2 ) The remote controller 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 S oftware )

. ( 3 ) The aircraft has flown out of the effective communication range of the remote controller. ( 4 ) There is an obstacle obstructing the signal between the remote controller and the aircraft, ess entially reducing the distance the signal can travel. ( 5 ) There is interference causing a signal problem with the remote controller.

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 automatically control the aircraft to fly back to the home point and land.

Home Point

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

the home point. 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 Fail safe mode is initiated.

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 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 uickly flipping the S2 switch of the remote controller from upper most to lower most positions 5 times or more w ill 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 controller’s signal is recovered, control is returned back to the pilot. R egain control as soon as signal is

recover ed.



### 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

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 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 Software is compliant within the definitions of class G ruled by ICAO. (Refer to Airspace Classification to get more details). As each country has its

own rules, make sure to configure t he 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.

Figure 6

- 3 Figure 6

- 4

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

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.

Category A Category B

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

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.

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 Fails afe 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.

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

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 Innovations. All Rights Reserved. 

## 7 Assistant Software Installation and Configuration
7. 1 Install i ng Driver and PHANTOM 2 Assistant Software
Install ing and run ning on Windows

1. Download driver installer and A ssistant S oftware 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 A ssistant S oftware 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 A ssistant S oftware 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 S oftware, 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 launching of the software can be achieved by double

- clicking

the PHANTOM 2 icon in the Finder or using Launchpad.

### ©2013

- 2014 DJI Innovations. All Rights Reserved.

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

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

Assistant S oftware pages appear in other places of this manual are on the Windows for example.



### 7 .2 Using the PHANTOM 2 Assistant Software on a PC
1. Start up the PC, power on the PHANTOM 2 , then 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 A ssistant Software and wait for the PHANTOM 2 to connect to the A ssistant

Software

. 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 Innovations. All Rights Reserved.

( 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 located 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 S oftware to install d river and PHANTOM RC Assistant S oftware, 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 S oftware 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 u pgradable items: ( 1 ) Main Controller ( 2 ) P330CB (Main Board) ( 3 ) Receiver ( 4 ) Gimbal

C MU ( 5 ) Gimbal IMU ( 6 ) Battery

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

### 7 .4 PHANTOM RC Assistant S oftware Description Please follow the procedures to finish the configuration of the remote controller.

1. Turn off the remote controller and find the Micro

- USB port on the bottom of it.

2. Start up the PC, power on the remote controller, and then Connect the remote controller to the PC with a

Micro

- USB cable. DO NOT disconnect until the configuration is finished.

3. Run the PHANTOM RC Assistant Software and wait for the remote controller to con nect to the Assistant

Software

. 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 page of the 2.4G Hz remote controller

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 

## 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 Recommend payload ≤ 1300g Maximum payload 1350g Hovering Accuracy ( Ready to Fly ) Vertical: 0.8m ; Horizontal: 2.5m Max Yaw Angular Velocity 200°/s Max Tiltable 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 Controller Operating Frequency 2.4GHz ISM Communication Distance ( open area ) 1000m Receiver Sensitivity ( 1%PER )

- 9 7 dBm

W orking Current/Voltage 100 mA@ 6 V Battery 4 AA Batteries 

## 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 Controller Signal Lost

### ©2013

- 2014 DJI Innovations. All Rights Reserved. 1 st Level Low Battery Capacity Warning

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 A ssistant S oftware to get detailed information about warnings and errors.