April 8, 2015

 Exemption No. 11302

 Regulatory Docket No. FAA−2014−1032

Mr. Mark Pickens 

M&G Enterprises

645 Wildwood Trace

Winchester, TN 37398

Dear Mr. Pickens:

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 December 9, 2014, you petitioned the Federal Aviation Administration (FAA) 

on behalf of M&G Enterprises (hereinafter petitioner or operator) for an exemption. The 

exemption would allow the petitioner to operate an unmanned aircraft system (UAS) to 

conduct video filming and photography; inspection of land, residential, commercial, and 

industrial structures and property; and training.

See Appendix A for the petition submitted to the FAA describing the proposed operations and 

the regulations that the petitioner seeks an exemption.

The FAA has determined that good cause exists for not publishing a summary of the petition 

in the Federal Register because the requested exemption would not set a precedent, and any 

delay in acting on this petition would be detrimental to the petitioner.

Airworthiness Certification

The UAS proposed by the petitioner is a DJI Phantom 2.
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The petitioner requested relief from 14 CFR part 21, Certification procedures for products 

and parts, Subpart H—Airworthiness Certificates. In accordance with the statutory criteria 

provided in Section 333 of Public Law 112−95 in reference to 49 U.S.C. § 44704, and in 

consideration of the size, weight, speed, and limited operating area associated with the 

aircraft and its operation, the Secretary of Transportation has determined that this aircraft 

meets the conditions of Section 333. Therefore, the FAA finds that the requested relief from 

14 CFR part 21, and any associated noise certification and testing requirements of part 36, is 

not necessary.

The Basis for Our Decision

You have requested to use a UAS for aerial data collection. The FAA has issued grants of 

exemption in circumstances similar in all material respects to those presented in your petition. 

In Grants of Exemption Nos. 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 Labs, 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 the 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 find that a grant of exemption is in the public interest. 

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

delegated to me by the Administrator, M&G Enterprises is granted an exemption from 

14 CFR §§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 91.7(a), 91.119(c), 

91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 91.417(a) and (b), to 

the extent necessary to allow the petitioner to operate a UAS to perform aerial data collection. 

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

Conditions and Limitations

In this grant of exemption, M&G Enterprises is hereafter referred to as the operator.
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Failure to comply with any of the conditions and limitations of this grant of exemption will be 

grounds for the immediate suspension or rescission of this exemption.

1. Operations authorized by this grant of exemption are limited to the DJI Phantom 2

when weighing less than 55 pounds including payload. Proposed operations of any 

other aircraft will require a new petition or a petition to amend this exemption.

2. Operations for the purpose of closed-set motion picture and television filming are 

not permitted. 

3. The UA may not be operated at a speed exceeding 87 knots (100 miles per hour). The 

exemption holder may use either groundspeed or calibrated airspeed to determine 

compliance with the 87 knot speed restriction. In no case will the UA be operated at 

airspeeds greater than the maximum UA operating airspeed recommended by the 

aircraft manufacturer.

4. The UA must be operated at an altitude of no more than 400 feet above ground level 

(AGL). Altitude must be reported in feet AGL.

5. The UA must be operated within visual line of sight (VLOS) of the PIC at all times. 

This requires the PIC to be able to use human vision unaided by any device other than 

corrective lenses, as specified on the PIC’s FAA-issued airman medical certificate or 

U.S. driver’s license.

6. All operations must utilize a visual observer (VO). The UA must be operated within 

the visual line of sight (VLOS) of the PIC and VO at all times. The VO may be used 

to satisfy the VLOS requirement as long as the PIC always maintains VLOS 

capability. The VO and PIC must be able to communicate verbally at all times; 

electronic messaging or texting is not permitted during flight operations. The PIC must 

be designated before the flight and cannot transfer his or her designation for the 

duration of the flight. The PIC must ensure that the VO can perform the duties 

required of the VO.

7. This exemption and all documents needed to operate the UAS and conduct its 

operations in accordance with the conditions and limitations stated in this grant of 

exemption, are hereinafter referred to as the operating documents. The operating 

documents must be accessible during UAS operations and made available to the 

Administrator upon request. If a discrepancy exists between the conditions and 

limitations in this exemption and the procedures outlined in the operating documents, 

the conditions and limitations herein take precedence and must be followed. 

Otherwise, the operator must follow the procedures as outlined in its operating 

documents. The operator may update or revise its operating documents. It is the 

operator’s responsibility to track such revisions and present updated and revised 

documents to the Administrator or any law enforcement official upon request. The 
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operator must also present updated and revised documents if it petitions for extension 

or amendment to this grant of exemption. If the operator determines that any update or 

revision would affect the basis upon which the FAA granted this exemption, then the 

operator must petition for an amendment to its grant of exemption. The FAA’s UAS 

Integration Office (AFS-80) may be contacted if questions arise regarding 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 other people. The functional test flight must be conducted in such 

a manner so as to not pose an undue hazard to persons and property.

9. The operator is responsible for maintaining and inspecting the UAS to ensure that it is 

in a condition for safe operation.

10. Prior to each flight, the PIC must conduct a pre-flight inspection and determine the 

UAS is in a condition for safe flight. The pre-flight inspection must account for all 

potential discrepancies, e.g. inoperable components, items, or equipment. If the 

inspection reveals a condition that affects the safe operation of the UAS, the aircraft is 

prohibited from operating until the necessary maintenance has been performed and the 

UAS is found to be in a condition for safe flight.

11. The operator must follow the UAS manufacturer’s maintenance, overhaul, 

replacement, inspection, and life limit requirements for the aircraft and aircraft 

components.

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

bulletins.

13. Under this grant of exemption, a PIC must hold either an airline transport, 

commercial, private, recreational, or sport pilot certificate. The PIC must also hold a 

current FAA airman medical certificate or a valid U.S. driver’s license issued by a 

state, the District of Columbia, Puerto Rico, a territory, a possession, or the Federal 

government. The PIC must also meet the flight review requirements specified in 

14 CFR § 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

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

ability to safely operate the UAS in a manner consistent with how the UAS will be 

operated under this exemption, including evasive and emergency maneuvers and 

maintaining appropriate distances from persons, vessels, vehicles and structures. PIC 

qualification flight hours and currency must be logged in a manner consistent with 

14 CFR § 61.51(b). Flights for the purposes of training the operator’s PICs and VOs 
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(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 UA may not operate within 5 nautical miles of an airport reference point (ARP) as 

denoted in the current FAA Airport/Facility Directory (AFD) or for airports not 

denoted with an ARP, the center of the airport symbol as denoted on the current FAApublished aeronautical chart, unless a letter of agreement with that airport’s 

management is obtained or otherwise permitted by a COA issued to the exemption 

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

to the Administrator or any law enforcement official upon request.

17. The UA may not be operated less than 500 feet below or less than 2,000 feet 

horizontally from a cloud or when visibility is less than 3 statute miles from the PIC.

18. If the UAS loses communications or loses its GPS signal, the UA must return to a predetermined location within the private or controlled-access property.

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

20. The PIC is prohibited from beginning a flight unless (considering wind and forecast 

weather conditions) there is enough available power for the UA to conduct the 

intended operation and to operate after that for at least five minutes or with the reserve 

power recommended by the manufacturer if greater.

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

operations shall be conducted in accordance with an ATO-issued COA. The 

exemption holder may apply for a new or amended COA if it intends to conduct 

operations that cannot be conducted under the terms of the attached COA.

22. All aircraft operated in accordance with this exemption must be identified by serial 

number, registered in accordance with 14 CFR part 47, and have identification (NNumber) markings in accordance with 14 CFR part 45, Subpart C. Markings must be 

as large as practicable.
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23. Documents used by the operator to ensure the safe operation and flight of the UAS and 

any documents required under 14 CFR §§ 91.9 and 91.203 must be available to the 

PIC at the Ground Control Station of the UAS any time the aircraft is operating. These 

documents must be made available to the Administrator or any law enforcement 

official upon request.

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

activities at all times. 

25. The UAS may not be operated by the PIC from any moving device or vehicle. 

26. All Flight operations must be conducted at least 500 feet from all nonparticipating 

persons, vessels, 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 protection and are within 500 feet of 

the UA, flight operations must cease immediately in a manner ensuring the safety 

of nonparticipating persons; and

b. The owner/controller of any vessels, vehicles or structures has granted permission 

for operating closer to those objects and the PIC has made a safety assessment of 

the risk of operating closer to those objects and determined that it does not 

present an undue hazard.

The PIC, VO, operator trainees or essential persons are not considered 

nonparticipating persons under this exemption.

27. All operations shall be conducted over private or 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 (AFS-80) within 24 hours. Accidents must be 

reported to the National Transportation Safety Board (NTSB) per instructions 

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

If this exemption permits operations for the purpose of closed-set motion picture and 

television filming and production, the following additional conditions and limitations apply.

29. The operator must have a motion picture and television operations manual (MPTOM) 

as documented in this grant of exemption.
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30. At least 3 days before aerial filming, the operator of the UAS affected by this 

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

District Office (FSDO) with jurisdiction over the area of proposed filming. The 3-day 

notification may be waived with the concurrence of the FSDO. The plan of activities 

must include at least the following:

a. Dates and times for all flights;

b. Name and phone number of the operator for the UAS aerial filming conducted 

under this grant of exemption;

c. Name and phone number of the person responsible for the on-scene operation of 

the UAS;

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

e. Name and certificate number of UAS PICs involved in the aerial filming;

f. A statement that the operator has obtained permission from property owners 

and/or local officials to conduct the filming production event; the list of those 

who gave permission must be made available to the inspector upon request;

g. Signature of exemption holder or representative; and

h. A description of the flight activity, including maps or diagrams of any area, city, 

town, county, and/or state over which filming will be conducted and the altitudes 

essential to accomplish the operation.

31. Flight operations may be conducted closer than 500 feet from participating persons 

consenting to be involved and necessary for the filming 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 applicable 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
December 09, 2014

U.S. Department of Transportation, Docket Operations

West Building Ground Floor, Room w12-140

1200 New Jersey Ave., SE Washington, DC 20590

Re: Petition of M&G Enterprises for an Exemption Pursuant to Section 333 of the FAA 

Modernization and Reform Act of 2012

Dear Gentlemen:

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

("Reform Act") and 14 C.P.R. Part 11, M&G Enterprises hereby applies for an 

exemption from the Federal Aviation Regulations ("FARs") identified below, to

allow commercial operations of small unmanned aerial vehicles.

This exemption is made based on information outlined in this petition, as well as the 

accompanying DJI Phantom 2 Operators Manual (Appendix B) and the M&G Enterprises 

Operational Limitations (Appendix C). The DJI Phantom 2 UAS was selected because it 

has a proven capability for controlled flight as well as a gyro stabilized flight mode, GPS

aided navigation, a compass, blinking LED’s on the bottom, a failsafe mode for returning 

home, and prop guards. These devices are offered for general sale around the world and 

have often been used as Model Aircraft in the USA.

Specifically, the UAS is:

A lightweight (< 7.0 lb gross weight with all on-board equipment), battery operated 4-

motor rotorcraft in the form of a quadcopter that takes off and lands vertically, 

manufactured by DJI, Model Phantom 2 , with the following equipment:

 An on-board flight computer with GPS navigation and location ability that

receives signals for flight controls from a ground-based 

transmitter/controller;

 An on-board camera capable of capturing imagery in the form of full color, high 

definition still photos and video;

 An on-board telemetry system that delivers flight data from the on-board flight 

computer to the on-board radio transmitter including altitude AGL, horizontal 

and vertical speed, compass direction of flight and direction back to its launch 

site;

 A 600mW, 5.8GHz on-board radio transmitter that transmits live video from the 

on-board camera plus all the flight data from the telemetry system described 

above;
The Ground Station Includes:

 A Pilot in Command (PIC) in operational control of a flight operation from 

beginning to end and who controls the UAS while in the air;

 A 100mW, 2.4GHz radio transmitter/controller operated by the PIC to control 

the UAS while in flight;

 A radio receiver receiving live video and flight data from the on-board 

camera and computer projects it all together onto a screen for the PIC to 

view during flight;

 A Visual Observer (VO) is a person who provides a second pair of eyes to

visually track the UAS while in flight.

 Proposed Operations

M&G Enterprises intends to use UAS in three general areas. First, M&G Enterprises seeks an 

exemption to perform video filming and photographing by air for public and private use. 

Second, it will employ UAS’s to inspect land, residential commercial and industrial structures 

and property. Third, M&G Enterprises seeks permission to use UAS to offer training to 

persons, from both private and public entities, which are interested in the safe operation of 

UAS.

Specifically, M&G Enterprises will use UASs which are equipped with cameras and sensors, 

in order to engage in the following commercial activities:

(a) Video filming by air and photographing for public and private purposes, including: 

television, cinematography, advertising, promotions, public or news mass events.

(b) Video filming by air and photographing to support professional operations in 

engineering, land surveying, architecture, real estate and other related professional 

activities.

(c) Inspections by air of agricultural areas.

(d) Inspections by air of infrastructure such as bridges, highways, electrical installations, 

dams, aqueducts, photovoltaic power stations, wind farms and pipes. These inspections 

will only be done under contract with the owners or with any local government authority.

(e) Inspection by air of land and residential, commercial and industrial structures, only 

under contract with the owners or with any local government authority.

(f) Inspections by air to detect sources of pollution and gas emissions, under contract

with the owners in the area or with any local government authority.

(g) Support provided to search and rescue operations and reconnaissance in cases of need, 

emergency or natural disasters and only when government authorities have requested it 

by contract or donation.
(h) M&G Enterprises is passionate about offering training to persons, private and public 

entities, which are interested in the safe use of UASs, for purposes of enhancing the skills 

and safety controls which make the NAS safer and for the protection of persons and 

property.

Relevant Statutory Authority

This Petition for Exemption is submitted pursuant to Section 333(a) through (c) of the FAA 

Modernization and Reform Act of 2012 ("Reform Act"). Congress has directed the FAA "to 

safely accelerate the integration of civil unmanned aircraft systems into the national airspace 

system." Pursuant to Section 333 of the Reform Act, the FAA Administrator is to permit 

unmanned aircraft systems to operate in the National Air Space ("NAS") where it is safe to do 

so based on the following considerations:

• The UAS’s size, weight, speed and operational capability;

• Operation of the UAS in close proximity to airports and populated areas; and

• Operation of the UAS within the visual line of sight of the operator.

Additionally, the FAA Administrator has general authority to grant exemptions from the 

agency's safety regulations and minimum standards when the Administrator decides a 

requested exemption is in the public interest. See 49 U.S.C. § 106(f) (defining the authority of 

the Administrator); 49 U.S.C. § 44701(f) (permitting exemptions from§§ 44701(a), (b) and§§ 

44702-44716,et seq.). A party requesting an exemption must explain the reasons why the 

exemption: (1) would benefit the public as a whole, and (2) would not adversely affect safety 

(or how it would provide a level of safety at least equal to the existing rules). See 14 C.F.R. § 

11.81 (petitions for exemption).

 M&G Enterprises Proposed UAS Operations Meet the Requirements of Section 333 of the 

Reform Act

M&G Enterprises proposed operations in this Petition for Exemption qualify for expedited 

approval pursuant to Section 333 of the Reform Act as each of the statutory criteria and 

relevant factors are satisfied.

Approval is Warranted Based on the UAS Size, Weight, Speed, and Operational Capability

M&G Enterprises will employ the DJI Phantom 2 quadcopters for the operations specified in 

this Petition for exemption. The Phantom 2 UASs have a maximum take-off weight of less than 

7 pounds, the flight speed will not exceed 35 miles per hour, and it will not be flown in 

controlled airspace or at an altitude that exceeds 400 feet AGL. All flights will be flown in such 

a way that they can be safely terminated with a reserve battery power of 25% of the battery's 

maximum charge. The DJI Phantom 2 UAS do not carry any flammable propellant or fuel. The 

Phantom 2 UAS also has an integrated GPS system that calculates the UAS’s position and 

height and relays that information via a secure connection to the operator. Additionally, the 

Phantom 2 UAS contain a failsafe mode if its connection to the remote control is lost, and 
this system permits the UAS to return to a predetermined location and land without injury 

or damage. For additional safety, the Phantom 2 will be retrofitted with prop guards.

Approval is Warranted Based on the Operational Restrictions Set Forth in the Operations 

Manual.

The M&G Enterprises Operations Limitations and the DJI's operators manual contain all of the 

procedures and limitations necessary to successfully perform the operations specified in this 

Petition for Exemption. (Appendices B &C). 

Public Interest

The public interest will be served by granting M&G Enterprises Petition for Exemption. 

Congress has established a national policy that favors early integration of UASs into the NAS 

in controlled, safe working environments such as those proposed in this Petition. In addition, 

the public also has an interest in reducing the hazards associated with alternate methods of 

conducting similar operations. Currently operations are conducted using teams that physically 

climb onto structures using ladders, using low flying helicopters or aircraft, or simply not 

available by traditional means. By using UAS, exposure to physical hazards will be reduced 

of conducting the operation while remaining safely on the ground.

Additionally, M&G Enterprise intended uses for the UAS’s have identifiable safety benefits that 

include reducing the danger and emissions associated with full size helicopters, UAS have no 

fuel to ignite or explode, no crew, adds a greater degree of flexibility, which supplements the

current capabilities offered by manned aircraft, and public interest for a ground impact for of a 

small lightweight UAS is further minimized from an ecological and safety standpoint. 

Federal Register Summary

Pursuant to 14 C.F.R. Part 11, the following summary is provided for publication in the

Federal Register, should it be determined that publication is needed:

M&G Enterprises seeks an exemption from the following rules:

Parts 21; §§ 45.23(b); 27; 61.113(a) and (b); 61.3; 91.7(a); 91.9(b)(2); 91.103; 91.109; 91.119; 

91.121; 91.151(a); 91.203(a) and (b); 91.405(a); 91.407(a)(1); 91.409(a)(2); and 91.417(a) and

(b) of Title 14, Code of Federal Regulations (14 CFR). 

The exemption will enhance safety by reducing risk to the general public and property 

owners from the substantial hazards associated with performing equivalent work with 

conventional aircraft, rotorcraft, or other methods.

Conclusion 

M&G Enterprises Petition for Exemption satisfies the criteria articulated in Section

333 of the Reform Act of 2012 including weight, speed, operating capabilities, proximity to 
airports and populated areas, operation within visual line of sight and national security. 

Additionally, the Petition provides more than adequate justification for the grant of the requested 

exemptions to permit M&G Enterprises to operate the selected UAS for the operations specified 

herein.

Granting the exemption will benefit the public interest as a whole in several ways, including (1) 

significantly improving safety and reducing risk by alleviating human exposure to danger, and 

(2) improving the quality of services and decreasing operating costs compared with 

conventional flight operations.

Very Respectfully,

Mark Pickens

645 Wildwood Trace

Winchester, TN 37398

Pickens196018@gmail.com

Appendix A

The regulations from which the exemption is requested are listed below. Beside each 

regulation number is the page of the attached Appendix A upon which each may be

found together with our proposed equivalent level of safety for each regulation:

Parts 21,§§ 45.23(b); 27, 61.113(a) and (b) 61.3; 91.7(a); 91.9(b)(2); 91.103; 91.109; 91.119; 

91.121; 91.151(a); 91.203(a) and (b); 91.405(a); 91.407(a)(1); 91.409(a)(2); and 91.417(a) and

(b) of Title 14, Code of Federal Regulations (14 CFR).

Exemptions Requested 

The Federal Aviation Act expressly grants the FAA the authority to issue exemptions. This 

statutory authority, by its terms, includes exempting civil aircraft, as the term is defined under§ 

40101 of the Act, including UASs, from its safety regulations and minimum standards when 

the Administrator decides a requested exemption is in the public interest.

M&G Enterprises seeks an exemption from several interrelated provisions of 14 C.F.R. Parts 21,

27, 45, 61 and 91 for purposes of conducting the requested operations using a UAS. Listed below 

are the specific sections of 14 C.F.R. for which exemption is sought:

14 C.F.R. Part 21, Subpart H - Airworthiness Certificates

The FAA has stated that no exemption is needed from this section if a finding is made 

under the Reform Act that the UAS selected provides an equivalent level of safety when 

compared to aircraft normally used for the same application. (Regulatory Docket No. FAA2014-0352). These criteria are met, and therefore no exemption is needed. 
EquivalentLevel of Safety

The UAS selected by M&G Enterprises is safe when taking into account their size, weight, speed, 

and operational capability. T he UAS weigh less than 7 pounds and will be flown at less than 35

miles per hour and completely outside controlled airspace. Additionally, the UAS carry neither

pilots nor passengers, carry no explosive materials and or flammable liquid fuels, and operate

exclusively within the parameters stated in the Operator’s Manual and Operations Limitations.

Operations under this exemption will be closely controlled and monitored by the operator and will

be conducted in compliance with local public safety requirements, to provide security for the area

of operation. M&G Enterprises will also provide the FAA with advance notice of all operations

via NOTAMS and coordination with the local FSDO. In all cases, the UAS operated under the

proposed conditions, will be at least as safe as, or safer than conventional rotorcraft operating with

an airworthiness certificate without the restrictions and conditions of the proposed UAS

operations.

14 C.F.R. Part 27 Airworthiness Standards: Normal Category Rotorcraft

14 C.P.R. Part 27 sets forth the procedural requirements for airworthiness certification of normal

category rotorcraft. To the extent the M&G Enterprises UAS would otherwise require certification

under Part 27, we seek an exemption from Part 27's airworthiness standards for the same reasons

identified in the request for exemption from 14 C.F.R. Part 21, Subpart H.

14 C.F.R. §§45.23(b), Display of marks; general

These regulations provide that each aircraft must display "N" and the aircraft's registration number

in letters at least 2 inches high. Additionally, the aircraft must display the word 

"EXPERIMENTAL" in letters at least 2 inches high near the entrance to the cabin, cockpit, or 

pilot station. The UAS does not have an entrance in which the word "EXPERIMENTAL" can be 

placed, and may not have a registration number assigned to it by the FAA.

M&G Enterprises proposes to achieve an equivalent level of safety by including the word

"EXPERIMENTAL" as large as practicable on the top of the aircraft, where the PIC, VO and 

others in the vicinity of the aircraft while it is preparing for launch will be able to see the

designation. Finally, the ground station will display a high contrast flag or banner that contains

the words "Unmanned Aircraft Ground Station" in letters 3 inches high or greater. Since the

aircraft will operate within 3/4 NM of the ground station, the banner should be visible to anyone

that observes the aircraft and chooses to investigate its point of origin.

In a previous Grant of Exemption, Regulatory Docket No. FAA-2014-0352, the FAA determined 

that exemption from these requirements was warranted provided that the aircraft "have 

identification (N-Number) markings in accordance with 14 C.F.R part 45, Subpart C if the 

markings are as large as practicable."

14 CFR § 61.113 (a) and (b); 61.3 (c,2-v): Private Pilot Privileges and Limitations, Medical 

Certificate
In addition, M&G Enterprises seeks exemption from 14 C.F.R § 61.113, which restricts private 

pilot certificate holders from flying aircraft for compensation or hire, and which would also 

require a second class medical certificate. The purpose of this section is to ensure the skill and 

competency of any PIC where the aircraft is carrying passengers or cargo for hire. In this case, 

while the UAS will be operated as part of a commercial operation, it carries neither passengers 

nor cargo. In the Grant of Exemption in FAA Docket No. FAA-2014-0352, the FAA determined 

that the unique characteristics of UAS operation outside of controlled airspace did not warrant 

the additional cost and restrictions attendant with requiring the PIC to have a commercial pilot 

certificate and class II medical certificate. Additionally, instead of having a second or third class 

medical, we suggest that the PIC exercise the privileges similar to that of a sport pilot, requiring 

only a valid US driver’s license. 

Safety Mitigation

Petitioner seeks to ensure safe operation by ensuring that any PIC is thoroughly versed in 

airspace and communication issues pertaining to all aircraft operators but also in the unique 

aspects of UAS flight. The owners of M&G Enterprises have commercial pilot’s license,

however, the experience obtained beyond a private pilot certificate in pursuit of a commercial 

pilot certificate in manned flight does not necessarily aid a pilot in the operational environment 

proposed. To that end, M&G Enterprises will require a PIC to have a minimum of a private 

pilot’s license and adhere to the flight limitations listed in Appendix C.

We find that the combination of aeronautical knowledge, UAS airmanship skills, and 

verification through remaining current is a sufficient method to evaluate a pilot’s qualifications, 

given that operations will be conducted within the limitations outlined in this petition. 

14 C.F.R. § 91.7(a): Civil Aircraft Airworthiness

M&G Enterprises seeks an exemption from 14 C.F.R. § 91.7(a), which requires that a civil 

aircraft be in airworthy condition to be operated. The FAA has stated (Regulatory Docket No. 

FAA-2014-0352) that no exemption is required to the extent that the requirements of Part 21 are 

waived or found inapplicable.

14 C.F.R. § 91.9(b)(2): Civil Aircraft Flight Manual in the Aircraft

Given its size, configuration, and load capacity, the Phantom 2 has no ability to carry such a 

manual on the aircraft, not only because there is no pilot on board, but because there is simply 

no room or capacity to carry such an item on the aircraft.

Safety Mitigation

The safety related purpose of this manual requirement can be equally satisfied by maintaining 

the Phantom 2 Manual at the ground control point where the pilot flying the Phantom 2 will 

have immediate access to it. Accordingly, we request an exemption from § 91.9(b) (2)'s flight 

manual requirements, on the condition that the Phantom 2 flight manual be available at the 

control point during each operation. 
14 C.F.R. § 91.103: Preflight Action

M&G Enterprises seeks an exemption from 14 C.P.R.§ 91.103, which requires a PIC to become 

familiar with specific information before each flight, including information contained in the FAAapproved Flight Manual on board the aircraft. While the PIC will be familiar with all information 

necessary to safely conduct the flight, an exemption is requested to the extent that an FAAapproved Flight manual is required.

Safety Mitigation

An equivalent level of safety will be provided by following the Aircraft Operations Manual and 

flight manual provided by the manufacturer. The PIC will take all required preflight actionsincluding performing all required checklists and reviewing weather, flight requirements, battery 

charge, landing and takeoff distance, aircraft performance data, and contingency landing areasbefore initiation of flight. The Operators Manual and Operational Limitations will be kept at the 

ground station with the operator at all times.

14 C.F.R. § 91.109(a): Flight Instruction

M&G Enterprises seeks an exemption from 14 C.F.R. § 91.109(a), which provides that "no 

person may operate a civil aircraft (except a manned free balloon) that is being used for flight 

instruction unless that aircraft has fully functioning dual controls." UAS and remotely piloted 

aircraft, by their design, do not have functional dual controls. Instead, flight control is 

accomplished through the use of a device that communicates with the aircraft via radio 

communications.

 

Safety Mitigation

Given the size and speed of the UAS employed by M&G Enterprises, an equivalent level of safe 

training can still be performed without dual controls because no pilot or passengers are aboard the 

UAS, and all persons will be a safe distance away in the event that the UAS encounters any difficulties 

during flight instruction. In addition, we will conduct flight training at our Research and Development 

test sites, which are located on its own property. These training flights will be conducted in a sterile 

area and will otherwise comply with the provisions in the Operator’s Manual for flights at the R&D 

facility. The FAA has stated (Regulatory Docket No. FAA-2014-0352) that no exemption is required. 

14 C.F.R. § 91.119: Minimum Safe Altitudes

M&G Enterprises requests an exemption from the minimum safe altitude requirements of 14

C.F.R. § 91.119. Section 91.119 prescribes the minimum safe altitudes under which aircraft may 

not operate, including 500 feet above the surface and away from any person, vessel, vehicle, or 

structure in non-congested areas. See 14 C.F.R. § 91.119(c). Section 91.119(d) allows for a 

helicopter to operate at less than those minimum altitudes when it can be operated "without 

hazard to persons or property on the surface," provided that "each person operating the helicopter 

complies with any routes or altitudes specifically prescribed for helicopters by the FAA."
Safety Mitigation

Compared to flight operations with rotorcraft weighing far more than the maximum weights 

proposed herein, and given the lack of flammable fuel, any risk associated with these 

operations is far less than those that presently exist with conventional aircraft. An equivalent 

level of safety will be achieved given the size, weight, and speed of the UAS, as well as the 

location where it is operated. In order to avoid any risk to aircraft, flight operations will be 

restricted to 400' AGL or below. 

14 C.F.R. § 91.121: Altimeter Settings

This petition seeks an exemption from 14 C.F.R. § 91.121, which requires a person operating an 

aircraft to maintain cruising altitude or flight level by reference to an altimeter that is set to the 

elevation of the departure airport or barometric pressure. An exemption is required to the extent 

that the UAS do not have a barometric altimeter, but rather a GPS altitude read out.

Safety Mitigation

The FAA has stated that an equivalent level of safety can be achieved if the UAS will be operated at 

400' AGL or below and within visual line-of-sight in addition to GPS based altitude information 

relayed in real time to the operator. See Grant of Exemption to Astraeus Aerial, Docket No. FAA2014-0352. As the attached Operations Manual indicates, the chosen UAS meets these requirements, 

and a zero altitude initiation point will be obtained prior to flight

14 C.F.R. § 91.151(a): Fuel Requirements for Flight in VFR Conditions

M&G Enterprises requests an exemption from 14 C.F.R. § 91.15l(a)'s fuel requirements for 

flight in VFR conditions. Section 91.151 states:

(a) 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.

Here, the technological limitations on UAS battery power means that no meaningful flight 

operations can be conducted while still maintaining a 30 minute reserve. M&G Enterprises 

proposes that all flights comply with this requirement by mandating that the aircraft be safely 

landed with no less than 25% of battery life remaining.

Safety Mitigation

The FAA has stated that an equivalent level of safety is provided if the UAS flight is 

terminated with at least 25% reserve battery power still available. See Grant of Exemption to 
Astraeus Aerial, Docket No. PAA-2014-0352. The Operations Manual conforms to this limit, 

providing an equivalent level of safety.

14 CFR 91.203(a) & (b) Civil aircraft: Certifications required.

The regulation provides that an airworthiness certificate, with the registration number assigned to

the aircraft and a registration certificate must be aboard the aircraft. Additionally, subparagraph 

(b) provides that the airworthiness certificate be "displayed at the cabin or cockpit entrance so 

that it is legible to passengers or crew."

At a maximum gross weight of less than 7 pounds, the UAS is too small to carry documentation, does 

not have an entrance, and is not capable of carrying passengers or crew. To obtain an equivalent level 

of safety and meet the intent of 91.203, we propose that documents deemed appropriate for this aircraft 

by the FAA will be co-located with the crew at the ground control station and available for inspection 

upon request. The FAA has stated (Regulatory Docket No. FAA-2014-0352) that no exemption is 

required. 

14 C.F.R. 91.405(a); 91.407(a)(1); 91.409(a)(2); and 91.417(a) and (b) Maintenance 

Required

M&G Enterprises seeks an exemption from the maintenance inspection requirements contained in 

14 C.P.R.§ 91.405(a), 91.407(a)(1), 91.409(a)(2); 91.417(a) and (b). These regulations specify 

maintenance and inspection standards in reference to 14 C.P.R. Part 43. See, e.g., 14 C.P.R. § 

91.405(a) (stating that each owner or operator of an aircraft "[s]hall have the aircraft inspected as 

prescribed in subpart E of this part and shall between required inspections ...have discrepancies 

repaired as prescribed in part 43 of this chapter"). An exemption from these regulations is needed 

because Part 43 and these sections only apply to aircraft with an airworthiness certificate, which 

the UASs will not have.

Safety Mitigation

An equivalent level of safety will be achieved because maintenance and inspections will be 

performed in accordance with the Operators Manual. As provided in the Operators Manual, 

flights will not be conducted unless a flight operations checklist is performed that includes all of 

the aircraft's components. 
Appendix B:

PHANTOM 2 User Manual V1.2

For PHANTOM 2 Flight Controller Firmware version V3.08

& PHANTOM 2 Assistant version V3.4

& PHANTOM RC Assistant version V1.1

2014.10

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

product.

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

services such as product information, technical updates and manual corrections. Due

to any unforeseen changes or product upgrades, the information contained within this manual is subject to change without 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 regarding your product, please contact your dealer or DJI Customer Service.
Content

CONTENT........................................................................................................................2

IN THE BOX.....................................................................................................................4

LEGEND ..........................................................................................................................4

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

1.1 BUILT-IN FLIGHT CONTROL SYSTEM INSTRUCTIONS..................................................................5

1.2 CONNECTIONS WITH OTHER DJI PRODUCTS...........................................................................5

Important Notes of Using with Other DJI Products........................................................6

Connections with Other DJI Products.............................................................................7

1.3 LED FLIGHT INDICATORS DESCRIPTION ...............................................................................11

1.4 NOTES FOR PHANTOM 2 USING WITH OTHER DJI PRODUCTS ................................................12

2 PROPELLERS...............................................................................................................13

2.1 ASSEMBLY.....................................................................................................................13

2.2 DISASSEMBLY ................................................................................................................13

2.3 NOTES .........................................................................................................................13

3 REMOTE CONTROL ....................................................................................................14

3.1 POWER ON THE REMOTE CONTROL....................................................................................14

3.2 REMOTE CONTROL LED INDICATOR STATUS .........................................................................15

3.2.1 Remote Control Power LED Indicator Status.......................................................15

3.2.2 Remote Control Battery Level Indicator Status....................................................15

3.3 ANTENNA ORIENTATION ..................................................................................................16

3.4 REMOTE CONTROL OPERATION.........................................................................................16

3.5 LINKING THE REMOTE CONTROL& BUILT-IN RECEIVER...........................................................18

4 INTELLIGENT BATTERY ...............................................................................................19

4.1 CHARGING PROCEDURES..................................................................................................19

4.2 INSTALL THE BATTERY ......................................................................................................20

4.3 BATTERY USAGE.............................................................................................................20

4.4 DESCRIPTION OF THE BATTERY LEVEL INDICATOR...................................................................21

4.5 CORRECT BATTERY USAGE NOTES ......................................................................................22

5 CALIBRATING THE COMPASS......................................................................................23
5.1 CALIBRATION WARNINGS .................................................................................................23

5.2 CALIBRATION PROCEDURES ..............................................................................................23

5.3 WHEN RECALIBRATION IS REQUIRED...................................................................................23

6 FLIGHT .......................................................................................................................24

6.1 FLYING ENVIRONMENT REQUIREMENTS ..............................................................................24

6.2 STARTING THE MOTORS ...................................................................................................24

6.3 TAKEOFF/LANDING PROCEDURES.......................................................................................24

6.4 FAILSAFE FUNCTION........................................................................................................25

6.5 LOW BATTERY CAPACITY WARNING FUNCTION.....................................................................27

6.6 FLIGHT LIMITS FUNCTION.................................................................................................27

Max Height & Radius Limits.........................................................................................27

6.7 FLIGHT LIMITS OF SPECIAL AREAS ......................................................................................28

6.8 CONDITIONS OF FLIGHT LIMITS .........................................................................................30

Disclaimer.....................................................................................................................30

7 ASSISTANT INSTALLATION AND CONFIGURATION ......................................................31

7.1 INSTALLING DRIVER AND PHANTOM2 ASSISTANT...............................................................31

7.2 USING THE PHANTOM 2 ASSISTANT ON A PC....................................................................32

7.3 FIRMWARE UPGRADE OF PHANTOM2 .............................................................................33

7.4 PHANTOM RC ASSISTANT DESCRIPTION ...........................................................................33

8 APPENDIX..................................................................................................................35

8.1 SPECIFICATIONS..............................................................................................................35

8.2 LED FLIGHT INDICATORS DESCRIPTION ...............................................................................35
In the Box

PHANTOM 2 Remote Control-2.4GHz Propeller Pair

Intelligent Battery Charger Plug Set

Screwdriver Assistant Wrench Cables

Micro-USB Cable Screws Accessories Box

Legend

Forbidden(Important) Caution Tip Reference
1. PHANTOM 2 Aircraft

[1]

[2]

[3]

[4]

[5]

[6]

[7] 

[8]

[9] 

[10]

[11]

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 used to control the entire aircraft’s functions in flight such as Pitch (forwards 

and backwards), Roll (left and right), Elevator (up and down) and Yaw (turn left or right). The flight controller 

contains the MC (Main Controller), IMU, GPS, compass, receiver.

The IMU (Inertial Measurement Unit) has a built-in inertial sensor and a barometric altimeter that measures both 

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

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

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

connecting and controlling all the modules together.

The PHANTOM 2 can be configured in the Assistant, by choosing Naza-M mode or Phantom 2 mode. 

 This manual is for Phantom 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, including ZENMUSE H3-2D and H3-3D gimbal,iOSD mini,

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

Video Cable

To the iOSD module or wireless 

video transmission module.

CAN-Bus Connector

8-Pin Cable

To the G8 port on 

the H3-2D/H3-3D 

gimbal.

5-Pin Cable

To the compass.

Gimbal Mounting Position 

Mount the H3-2D/H3-3D 

gimbal using 4 screws.

Compass

Figure 1-3
Important Notes of Using with Other DJI Products

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

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

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

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

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

total current exceeds 2A, please be sure to provide power supplied from a 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 Wi-Fi or 2.4G wireless video transmission module) except the

2.4G Bluetooth and 2.4G Datalink.

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

compass during installation and connection to avoid interference.

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

updated 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.

Version 1

Gimbal Mounting

Position

Version 2

Gimbal Mounting

Position

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
DJI

Connections with Other DJI Products

(1) Connecting the H3-2D and H3-3D gimbal and wireless video transmission module, the figure below uses

H3-2D as an example.

Wireless 

video 

transmission

BattBatt+

Description of the Video Cable

(sequence by color)

VIDEO

module

Transmitter

VIDEO GND

VIDEO

VIDEO GND

VBat+

GND

ZENMUSE 

H3-2D

Compass

Figure 1-6

(2) Connecting the H3-2D and H3-3D gimbal, iOSD mini and wireless video transmission module, the figure 

below uses H3-2D as an example.

Description of the Video Cable

(sequence by color) 

Batt- VIDEO

Batt+ Wireless VIDEO GND

VIDEO GND video VBat+

VIDEO

transmission

module

Transmitter

GND

ZENMUSE 

H3-2D

CAN-Bus

Connector

Compass

Figure 1-7
DJI

(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.

DJI specified 

wireless 

video 

transmission 

module 

AVL58

Transmitter

Description of the Video Cable

(sequence by color)

VIDEO 

VIDEO GND 

VBat+

GND

ZENMUSE 

H3-2D

CAN-Bus 

connector Compass

Figure 1-8

We recommend connecting the VBat+ port of the video cable to the two BATT+ ports of the AVL58 

simultaneously. The same is true of the GND port of the video cable and two BATT- ports.

(4) Connecting the H3-2D and H3-3D gimbal, iOSD Mark II and wireless video transmission module, the figure

below uses H3-2D as an example.
DJI

Wireless video transmission 

module Transmitter specified by 

DJI(AVL58)

OR

Other wireless video transmission 

module Transmitter

Description of the Video Cable

(sequence by color)

 VIDEO 

VIDEO GND 

VBat+

GND

ZENMUSE 

H3-2D

CAN-Bus

Connector Compass

Figure 1-9

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

BATTBATTBATT+ 

BATT+

iOSD Mark II UART

UART 

AV-GND

AV-OUT

BattBattBatt+ Other wireless video

Batt+ transmission module

Transmitter

VIDEO GND 

VIDEO

iOSD Mark II

BATTBATTBATT+ 

BATT+ 

UART 

UART

AV-GND

AV-OUT

Wireless video 

transmission 

module

AVL58 Transmitter 

specified by DJI

Use the 8-Pin cable in the iOSD Mark II package when connecting to the DJI specified wireless video

transmission module AVL58.

(5) Using the iPad Ground Station
Air End

Ground End

3S-6S

+ -

Figure 1-10

Connect the Air End of 2.4G Bluetooth Datalink to a spared CAN-Bus port of iOSD if an iOSD is used.

(6) Using the PC Ground Station

Air End

Ground End

PC Ground

Station

Figure 1-11
1.3 LED Flight Indicators Description

1. LEDflight indicators are used to show the aircraft’s current status. Once powered on, the indicators will light

up.

LED flight

indicators

Aircraft in Normal status Descriptions

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 Warnings and errors

Remote Control Signal Lost

1

st Level LowBattery Capacity Warning

2

nd Level Low Battery Capacity Warning

Not Stationary or Sensor Bias is too big

Errors & Aircraft cannot fly.

Compass data abnormal because of ferro-magnetic interference or

the compass needs calibration.

(1) The LED indicators diagram above are for Phantom 2 mode. In Naza-M mode, LED indicators

will work according to the Naza-M flight control system.

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

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

have spooled up.

The front

LEDs
1.4 Notes for PHANTOM 2 using with other DJI products

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

the firmware as requirements below .

Items to upgrade Firmware versions required Assistant for upgrading Assistant version

P330CB (built-in

central board)

V1.0.1.19 or above PHANTOM 2 V1.08 or above

Zenmuse H3-2D CMU V1.0,IMU V1.6 or above PHANTOM 2 V1.08 or above

iOSD Mark II V3.01 or above iOSD V4.0 or above

iOSD mini V1.06 or above iOSD V4.0 or above

*The iOSD Assistant is applied to both iOSD Mark II and iOSD mini.
2 Propellers

PHANTOM 2 uses the original 9-inch propellers which are classified by the color of each central nut. Damaged

propellers should be replaced by purchasing new ones if necessary.

Propellers Grey Nut (9450) Black Nut (9450 R)

Diagram

Assembly Location

Attach to the motor thread that does

not have a black dot.

Attach to the motor thread that has a

black dot.

Fastening/Un-fastening

Instructions

Lock: Tighten the propeller in this direction.

Unlock: Remove the propeller in this direction.

2.1 Assembly

1. (Figure 2-1)Remove the four warning cards from the motors after you’ve read them.

2. (Figure 2-2)Prepare the two grey nut propellers and two black nut propellers. Make sure to match the

black nut propellers with the correctly marked black dot motors. Tighten the propellers according to the

fastening instructions.

Figure 2-1 Figure 2-2 Figure2-3

2.2 Disassembly

(Figure 2-3)Keep the motor deadlocked in place with the assistant wrench (or one hand) and remove the

propeller according to the un-fastening instructions.

2.3 Notes

1. Propellers are self tightening during flight. DO NOT use any thread locker on the threads.

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

3. It is advised to wear protective gloves during propeller assembly and removal.

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

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

propellers.

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

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

The PHANTOM 2 remote control can be configured in the PHANTOM RC Assistant. The sticks mode is Mode 2 on 

delivery.

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

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

[1]

[2]

[3]

J3 [5] [4] J2

J4 [7]

[8]

[9] 

[10]

[6] J1

[11]

[12]

[13]

[14]

Figure 3-1 Figure 3-2

[1]Antenna [2]Carrying Handle [3]Left Dial [4]3-Position Switch S1 [5]3-Position Switch S2 [6]Joystick1(J1;J2) 

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

[11]Battery Level Indicators LED1/LED2/LED3/LED4 (from left to right) [12]Trainer Port

[13]Battery Charge & RC Assistant Port (micro-USB port) [14] Potentiometer

3.1 Power on the Remote Control

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

the mid-point position. Then toggle on the power switch.

2. Push the power switch to the right to power on the remote control. If the power LED

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

indicators display the current battery level.

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

sounds (refer to <Remote Control Power LED Indicator Status>), please recharge the battery as soon as 

possible.

 2. Charge the remote control’s battery by using the included micro-USB cable. Using the incorrect

type of charging cable may cause damage.

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

charging is in progress. The LED indicators will display solid green when the battery is fully charged.
3.2 Remote Control LED Indicator Status

3.2.1 Remote Control Power LED Indicator Status

Power LED Indicator Sound Remote Control Status

None Functioning normally.

None Charging( remote control is powered off)

None Remote control joysticks calibration error, need to be re-calibrate.

BB---BB---BB Low voltage (from 3.5V-3.53V), recharge the remote control.

B-B-B......

Critical low voltage (from 3.45V-3.5V). Recharge the remote control

immediately.

B--B--B......

Alert will sound after 15 minutes of inactivity. It will stop once you 

start using the remote control.

The remote control will power off automatically when battery voltage drops below 3.45V. Land and

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

during flight.

3.2.2 Remote Control Battery Level Indicator Status

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

a description of the indicators.

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

: The LED is light off

Discharging process

LED1 LED2 LED3 LED4 Current battery level

75%~100%

50%~75%

25%~50%

12.5%~25%

0%~12.5%

<0%
3.3 Antenna Orientation

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

during flight.

Figure 3-3

3.4 Remote Control Operation

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

Definitions

The ‘stick neutral’ positions and ‘stick released’ mean the control sticks of the remote control are placed at 

the central position.

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

Slide Lever is used for the pitch control of the H3-2D and H3-3D gimbal.

Remote

Control

(Mode 2)

Aircraft

( nose direction)

Operation details

The throttle stick controls aircraft altitude/elevation. 

Push the stick up and the aircraft will rise.

Pull the stick down and the aircraft will descend.

The aircraft will automatically hover and hold its 

altitude if the sticks are centered.

Push the throttle stick above the centered (mid-point) 

position to make the aircraft take off. When flying, we 

suggest that you push the throttle stick slowly to 

prevent the aircraft from sudden and unexpected

elevation changes.
The yaw stick controls the aircraft rudder.

Push the stick left and the aircraft will rotate counter 

clock-wise.

Push the stick right and the aircraft will rotate 

clock-wise. If the stick is centered, the aircraft will 

remain facing the same direction.

The yaw stick controls the rotating angular velocity of 

the aircraft. Pushing the stick further away from center 

results in a faster aircraft rotation velocity.

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

Push the stick up and the aircraft will tilt and fly

 forward.

Pull the stick down and the aircraft will tilt and fly 

backward. The aircraft will keep level and straight if the 

stick is centered.

Pushing or pulling the stick further away from center

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

faster flight velocity.

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

Push the stick left and the aircraft will tilt and fly left. 

Push the stick right and the aircraft will tilt and fly right. 

The aircraft will keep level and straight if the stick is 

centered.

Pushing the stick further away from center will result in 

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

velocity.

Position-1 Position-2 Position-3

S1 is for compass calibration. Toggle the S1 switch from 

position-1 to position-3 and back to position-1 at least 5 

times, which will force the aircraft to enter into 

compass calibration mode.

Users can configure position 3(bottom position) of the

S1 switch to trigger the Failsafe in the Assistant.

OFF Course Lock Home 

point Lock

S2 is the IOC mode switch. IOC (Intelligent 

Orientation Control) function can be enabled in the 

Assistant when in Naza-M mode. Only use the IOC 

function after you are familiar with flying.
The left dial controls the pitch of the H3-2D and H3-3D

gimbal. The position of left dial determines the pitch

angle relative to the horizontal level.

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

up.

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

down.

The gimbal will keep its current position if the dial is

static.

(1) For ‘Ready to Fly’ the aircraft will hover when all sticks are released.

(2) For ‘Ready to Fly (non-GPS)’ the aircraft will only keep the altitude when all sticks are released.

3.5 Linking the Remote Control & Built-in Receiver

PHANTOM 2 has a built-in receiver, the link button and indicator located on the bottom of the aircraft as illustrated 

in the Figure 3-4.

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

procedure. If you ever replace the remote control, re-establishing the link is required.

Link button & 

Link indicator

Figure 3-4

Linking procedures

1. Power on the PHANTOM 2.

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

3. Push the link button with a thin object and hold it until the Link indicator blinks red, then release it.

4. When the Link indicator turns solid green, the link between the remote control and the built-in receiver has 

been successfully established.

Link Indicator Status

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

the remote control.

The receiver is ready for linking.

There is 2.4GHz signal around but the remote control is not linked with the receiver,
please carry out the linking procedures.

The remote control is linked with the receiver successfully.

4 Intelligent Battery

The intelligent battery is specially designed for the PHANTOM 2, with a battery capacity of 5200mAh, voltage of

11.1V and charge-discharge management functionality. The battery should only be charged with the DJI charger.

Intelligent Battery Charger

DJI Intelligent Battery Functions

(1) Balance Charging Automatically balance the voltage of each battery cell during charging.

(2) Capacity Display Display the current battery level.

The main controller communicates with the battery via communication ports

(3) Communicating

for battery voltage, capacity, current and other information.

(4) Overcharging Protection

(5) Over Discharging

Protection

Charging stops automatically when the battery voltage reaches 12.8V to 

prevent overcharging damage.

Discharging stops automatically when the battery voltage reaches 8.4V to

prevent over discharging damage.

(6) Short Circuit Protection Automatically cuts off the power supply when a short circuit is detected.

The battery will enter sleep mode after 10 minutes of inactivity to save

(7) Sleep Protection

(8) Charging Temperature

Detection

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

powered on without connecting to other devices.

The battery will charge only when its temperature is within 0°C~55°C. If the

battery temperature is out of this range, 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) The 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 capacity of the battery is over 75%, you should power on

the battery to begin charging.

3. The Battery Level indicators display current capacity level as the battery charges. Please refer to battery
level indicator description for details.

4. The battery is fully charged when the Battery Level indicator lights are off. Please disconnect the charger

and battery when the charging is completed.

Wall Socket

4.2 Install the Battery

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

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

Figure 4-1

An incorrectly inserted battery may cause one 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

LED2

LED1

Battery Level Indicator

LED3

LED4

Battery PowerButton

(Built-in Battery PowerIndicator)

Figure 4-2

(1) Checking the battery level: When the battery is powered off; pressing the battery power button once will 

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

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

2 seconds to turn on the intelligent battery.

(3) Powering off: When the battery is powered on; 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 the battery is powered off; press and hold the battery power button for 5 

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

will blink for 10 seconds, then all LEDs will light out and the intelligent battery will turn off. Refer to < Battery 

Level Indicator Description> for details.

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

4.4 Description of the Battery Level Indicator

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

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

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

: The LED is light off

Charging process

LED1 LED2 LED3 LED4 Current battery level

0%~25%

25%~50%

50%~75%

75%~100%

Full charged

Discharging process

LED1 LED2 LED3 LED4 Current 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%

Battery life

LED1 LED2 LED3 LED4 Current battery life

90%~100%
80%~90%

70%~80%

60%~70%

50%~60%

40%~50%

30%~40%

20%~30%

Less than 20%

4.5 Correct Battery Usage Notes

1. Never plug or unplug the battery into the aircraft when it is powered on.

2. The battery should be charged in an environment that is between 0°C to 40°C, and be discharged in an

environment that is between -20°C to 50°C. Both 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. Users should then fully recharge the battery to maximum capacity. This power cycling

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

4. For long term storage please place the battery with only a 40~50% capacity in a strong battery box

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

in good condition. The capacity should be varied in such a cycle (40%~50%)—0%—100%—(40%~50%).

5. It’s suggested you purchase a new battery after you have discharged your current battery over 300 times.

Please completely discharge a battery prior to disposal.

6. It’s suggested that you purchase a new battery ifthe 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. Safety is extremely important and users can get more information in the DISCLAIMER.
5 Calibrating the Compass

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

The compass is very sensitive to electromagnetic interference which causes abnormal compass data and leads to 

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

its optimal level.

5.1 Calibration Warnings

(1) DO NOT calibrate your compass where there is a possibility for the existence of strong 

magnetic interference such as magnetite, parking structures, and steel reinforcement 

underground.

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

phones.

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

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.

360o Rotate the aircraft

Quickly flip the switch S1

horizontally

360oRotate the aircraft 

vertically (Nose downward)

Position-1

Start 

cali

Position-3

Position-1->Position-3->Position-1

Flip no less than 5 times

LED Flight

Indicator

LED Flight Indicator LED Flight Indicator

Normal LED

Start horizontal calibration Start vertical calibration Succeed Fail

Position-1

Position-3

Position-1->Position-3->Position-1

Flip once

 Re-calibrate

5.3 When Recalibration is required

(1) When Compass Data is abnormal, the LED flight indicator will blink alternating between red and yellow.

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

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

(4) Evident drifting occurs in flight, i.e. the aircraft doesn’t fly in straight lines.
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) DO NOT fly in bad weather, such as rain or wind (more than moderate breeze) or fog.

(3) The flying field should be open and void of tall 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 remote control and other wireless equipment (No base 

stations or cell towers around).

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

(7) Never use the aircraft in a manner that infringes upon or contravenes international or domestic 

lays and regulations.

6.2 Starting the Motors

A Combination Stick Command (CSC) is used to start the motors. Push the sticks according to one of the options 

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

stop the motors.

A B C D

Figure 6-1

6.3 Takeoff/Landing Procedures

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

2. Turn on the remote control.

3. Power on the aircraft by turning on the intelligent battery.

4. When LED flight indicator blinks green/yellow, the PHANTOM 2 is entering Ready to Fly/Ready to Fly

(non-GPS) mode. Start the motors with the CSC command.

5. Push the throttle stick up slowly to lift the aircraft off the ground. Referto <Remote Control Operation> for

more details.

6. Be sure you are hovering over a level surface. Pull down the throttle stick to descend. The stick will lock into
place and the aircraft will descend steadily.

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

middle position after the motors have stopped.

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

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

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

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

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

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

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

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

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

battery and aircraft performance may be reduced.

(5) When used with a H3-3D gimbal, a GoPro camera, and the iOSD mini, your Phantom 2 will be very 

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

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

6.4 Failsafe Function

The aircraft will enter Failsafe mode when the connection from the remote control is lost. The flight control system 

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

situations would make the aircraft fail to receive a signal from the remote control and enter Failsafe mode:

(1) The remote control is powered off.

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

been configured in the PHANTOM 2 Assistant).

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

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

the distance the signal can travel.

(5) There is interference causing a signal problem with the remote control.

Failsafe works differently depending on the mode the aircraft is in when Failsafe mode is initiated whether it is in 

the Ready to Fly or Ready to Fly (non-GPS) mode.

Ready to Fly (non-GPS) ---- Automatic landing

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 go home and land

The flight control system will automatically control the aircraft to fly back to the home point and land.
2 Flying.

LED Flight Indicator

5 Fly back to home point.

Height over home point>20m

Elevate to 20m

20m

Height over home point<=20m

LED Flight Indicator

3 Remote controller signal lost.

LED Flight Indicator

6 Landing after hovering 15s.

LED Flight Indicator

Home Point

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

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

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

Go Home Procedures

1 Record Home Point.

LED Flight Indicator 

4 Signal lost lasts 3s, begin to go home.

LED Flight Indicator

Figure 6-2

 (1) In 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. Quickly flipping the S2 switch of the remote 

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

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

the LED Flight Indicator. The definition of “home point” is:

(1) The home point is the place PHANTOM 2 returns to when the control signal is lost, which is

recorded last time.

(2) The home point is used to calculate the horizontal distance between you and the aircraft, the

distance will be displayed as 

D if using iOSD module.

Regaining Control during Failsafe Procedure

Position of

Switch S1 Position-1 Position-2

Position-3

(No triggering the Failsafe)

Howto regain 

control

When the S1 switch is switched to Position-1, 

toggle the S1 switch to any other position once to 

regain control. If remote control’s signal is

recovered, control is returned back to the pilot.

Regain control as soon as signal is 

recovered.
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 battery has less than 30% power and the second appears when it has 

less than 15% power.

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

(2) At lower than 15% the LED indicator will blink red rapidly, the PHANTOM 2 will also begin to descend and 

land automatically. After it has landed, keep the throttle stick at its lowest point or execute 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 threshold and the 2nd Level Low Battery Warning will trigger auto-landing. 

Altitude can be maintained if necessary by pushing up on the throttle stick.

(1) Remember to fly your PHANTOM 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 limits.

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

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

(1) The default parameters in the Assistant is compliant within the definitions of class G ruled by

ICAO. (Refer to Airspace Classification to get more details). As each country has its own rules, 

 make sure to configure the parameters to comply with these rules too, before using the

PHANTOM 2.

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.
Max

Height

Max

Radius

Home Point

The height of 

aircraft when it 

is powered on

Figure 6-3 Figure 6-4

Ready to Fly

Limits Ground Station Rear LED flight indicator

Max Height

The flight height is restricted to fly

under the max height.

Warning: Height limit

reached.

None.

Max Radius

The flight distance is restricted to fly

within the max radius.

Warning: Distance limit

reached.

Rapid red flashings

when close to the Max radius limit.

Ready to Fly(non-GPS)

Flight Limits Ground Station Rear LED flight indicator

Max Height

The flight height is restricted to fly 

under the minor height between the

Max height and 120m.

Warning: Height limit reached.

None.

Max Radius Not limited, no warnings or LED indicators.

 (1) If the aircraft flies out of the limits, you can still control your aircraft except to fly it further away. 

(2) If the aircraft is flying out of the max radius in Ready to Fly (non-GPS) status, it will fly back

within the limits range automatically if 6 or more GPS satellites have been found.

6.7 Flight Limits of Special Areas

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

http://www.dji.com/fly-safe/category-mc for details. These areas have been divided into category A and category B.
8100m

c

8000m b

a

Center of 

Special 

Area

2000m c

a

Center of 

Special 

Area

2400m

c b

Airspace: A,B,C,D 

Boundary: a, b, c, d

a a b c

1000m

c

Airspace: A,C,D 

Boundary: a, c,

a a c

120m

d

10.5m

A B C D

d

A C D

Category A Category B

Ready to Fly

Airspace Limits

Rear LED

Flight Indicator

A 

Orange

Motors will not start.

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

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

automatically descend and land then stop its motors.

B 

Yellow

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

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

descend to airspace C and hover 5 meters below edge d.

C 

Green

No restrictions of flight, but the Phantom will not enter 

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

Airspace B throughBoundary b & d.

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

not enter into Airspace A through Boundary 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 Failsafe Procedure (Page23).

(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 lines,

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

6.8 Conditions of Flight Limits

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

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

All flights are restricted by height, distance and special areas simultaneously. The Failsafe and Ground Station 

operations are not restricted to flight limits, but if Ground Station function is used, the flight will be restricted the

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

Phantom mode

Flight Status Limits of Special Area Max Height Max Radius

Ready to Fly √ √ √

Ready to Fly (non-GPS) × √ ×

Naza-M mode

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

GPS

≥6 √ √ √

<6 × √ ×

ATTI.

≥6 √ √ ×

<6 × √ ×

Manual

≥6 × × ×

<6 × × ×

Disclaimer

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

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

You agree that you are responsible for your own conduct and content while using this product, 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.
7 Assistant Installation and Configuration

7.1 Installing Driver and PHANTOM 2 Assistant

Installing and running on Windows

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

on the DJI website.

2. Connect the PHANTOM 2 to a PC via a Micro-USB cable.

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

4. Next, run the Assistant installer and follow the prompts to finish installation.

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

The installer in EXE format only supports Windows operating systems (Win XP, Win7, Win8 (32 or 64

bit)).

Installing and running on Mac OS X

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

website.

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

3. When launching for the first time if use Launchpad to run the PHANTOM 2 Assistant, Launchpad won’t 

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

4. Locate the PHANTOM 2 icon in the Finder, press 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 then 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.
Installer in DMG format supports only Mac OS X 10.6 or above.

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

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

7.2 Using the PHANTOM 2 Assistant on a PC

1. Start up the PC, power on the PHANTOM 2, then connect the PHANTOM 2 to the PC with a Micro-USB

cable. DO NOT disconnect until configuration is finished.

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

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

and communication indicator is blinking .

3. Choose [Basic] or [Advanced] configuration pages.

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

View configurations

RC, Gain

Function switch of Phantom 2 

and Naza-M mode

Language swap

Account, software 

version

Firmware upgrade

Gimbal, Battery IMU calibration

Communication 

indicator

Connection indicator

*This image is for reference 

only. Please refer to the 

actual user interface.
(1) Users should not enable the Naza-M function before finishing Advanced 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 indicators. Do not enable the

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

(2) You can change to the Phantom 2 mode by clicking the same button used to turn on the Naza-M

mode. This operation will disable the Naza-M mode and enable Phantom 2 mode. All parameters 

will be returned to factory settings.

7.3 Firmware upgrade of PHANTOM 2

Please refer to the PHANTOM 2 Assistant to install driver and PHANTOM RC Assistant, and then follow the

procedures 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 [Upgrade] icon to check the current firmware version and whether the installed firmware is the

latest version. If not, click the relative links to upgrade.

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

seconds. Once completed, the firmware is up to date.

Firmware upgradable items

Upgrade link

Current firmware version

*This image is for reference 

only. Please refer to the 

actual user interface.

(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.

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

CMU(5)Gimbal IMU(6)Battery

7.4 PHANTOM RC Assistant Description

Please follow the procedures to finish the configuration of the remote control.
DT7调参软件

1. Turn off the remote control and find the Micro-USB port on the bottom of it.

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

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

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

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

and communication indicator is blinking .

4. Finish configuration in the [Main] page.

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

Main Page of the 2.4GHz Remote Control

Language swap

Main page

Communication indicator

Connection indicator

Firmware upgrade 

Account, software 

version

*This image is for 

reference only. Please 

refer to the actual

user interface.
8 Appendix

8.1 Specifications

Aircraft

Operating environment temperature -10°C to 50°C

Power consumption 5.6W

Supported Battery DJI Intelligent battery

Weight (including the battery) 1000g

Take-off Weight ≤1300g

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

Max Yaw Angular Velocity 200°/s

Max Tilt Angle 35°

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

Max Flight Speed 15m/s (Not Recommended)

Wheelbase 350mm

2.4GHz Remote Control

Operating Frequency 2.4GHz ISM

Communication Distance (open area) 1000m

Receiver Sensitivity (1%PER) -97dBm

Working Current/Voltage 120 mA@3.7V

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

DJI Intelligent Battery

Type 3S LiPo Battery

Capacity 5200mAh, 11.1V

Charging Environment Range 0°C to 40°C

Discharging Environment Range -20°C to 50°C
Appendix C

Operational Limitations

1. The unmanned aircraft system (UAS) will weigh less than 7 pounds, including energy source(s)

and equipment.

2. The UAS will not be flown at a ground speed exceeding 35 MPH.

3. Flights will be operated at an altitude of no more than 400 feet above ground level (AGL), as 

indicated by the procedures specified in the operator’s manual. All altitudes reported to ATC

must be in feet AGL.

4. The UAS will be operated within visual line of sight (VLOS) of the PIC at all times. This 

requires the PIC to be able to use human vision unaided by any device other than corrective

lenses.

5. All 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 capability. The VO and PIC must be

able to communicate verbally at all times.

6. Prior to each flight the PIC will inspect the UAS to ensure it is in a condition for safe flight. 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. The Ground Control Station, if utilized, will be

included in the preflight inspection. All maintenance and alterations will be properly

documented in the aircraft records.

7. If the UAS has undergone maintenance or alterations that affect the UAS operation or flight 

characteristics, e.g. replacement of a flight critical component, will undergo a functional test 

flight in accordance with the operator’s manual. The PIC who conducts the functional test flight 

will make an entry in the UAS aircraft records of the flight. The requirements and procedures 

for a functional test flight and aircraft record entry will be added to the operator’s manual.

8. The operator will follow the manufacturer’s UAS aircraft/component, maintenance, overhaul, 

replacement, inspection, and life limit requirements. When unavailable, aircraft 

maintenance/component/overhaul, replacement, and inspection/maintenance requirements will

be established and identified in the operator’s manual. At a minimum, requirements for the

following will be included in the operator’s manual:

a. Actuators / Servos;

b. Transmission (single rotor);
c. Powerplant (motors);

d. Propellers;

e. Electronic speed controller;

f. Batteries;

g. Mechanical dynamic components (single rotor);

h. Remote command and control;

i. Ground control station (if used); and

j. Any other components as determined by the operator;

9. The Pilot In Command (PIC) will possess at least a private pilot certificate and at least a valid 

driver’s license. The PIC will also meet the flight review requirements specified in 14 CFR § 

61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.

10. Prior to operations the PIC will have accumulated and logged, in a manner consistent with 

14 CFR § 61.51(b), a minimum of 200 flight cycles and 25 hours of total time as a UAS 

rotorcraft pilot and at least ten hours logged as a UAS pilot with a similar UAS type 

(single blade or multirotor). Prior documented flight experience that was obtained in 

compliance with applicable regulations may satisfy this requirement. Training, 

proficiency, and experience-building flights can also be conducted to accomplish the

required flight cycles and flight time. 

11. Prior to operations the PIC will have accumulated and logged, in a manner consistent with 

14 CFR § 61.51(b), a minimum of five hours as UAS pilot operating the make and model 

of UAS to be utilized for operations and three take-offs and three landings in the

preceding 90 days. Training, proficiency, experience-building, and take-off and landing

currency flights can be conducted to accomplish the required flight cycles and flight time. 

12. The UAS may not be operated directly over any person, except authorized and consenting 

personnel, below an altitude that is hazardous to persons or property on the surface in the

event of a UAS failure or emergency.

13 The operator will ensure that no persons are allowed within 500 feet of the area except those

consenting. This provision may be reduced to no less than 200 feet if it would not adversely

affect safety.

14. The UAS will abort the flight in the event of unpredicted obstacles or emergencies in 
accordance with the operator’s manual.

15. Each UAS operation will be completed within 30 minutes flight time or with 25% battery power

remaining, whichever occurs first.

16. The operator will obtain an Air Traffic Organization (ATO) issued Certificate of Waiver or

Authorization (COA) prior to conducting any operations. This COA will also require the

operator to request a Notice to Airman (NOTAM) not more than 72 hours in advance, but not 

less than 48 hours prior to the operation.

17. All aircraft operated in accordance will be identified by serial number, registered in 

accordance with 14 CFR part 47, and have identification (N- Number) markings in 

accordance with 14 CFR part 45, Subpart C. Markings must be as large as practicable.

18. Each UAS operated will comply with all manufacturer Safety Bulletins.

19. The radio frequency spectrum used for operation and control of the UA will comply with the

Federal Communications Commission (FCC) or other appropriate government oversight agency

requirements.

20. At least three days before scheduled flight, the operator will submit a written Plan of

Activities to the local FSDO with jurisdiction over the area of proposed flight area. The 3-

day notification may be waived with the concurrence of the FSDO. The plan of activities 

must include at least the following:

a. Dates and times for all flights;

 b. Name and phone number of the operator

c. Make, model, and serial or N-number of UAS to be used;

d. Name and certificate number of UAS PIC involved 

 e. A statement that the operator has obtained permission from property owners and/or 

local officials to conduct the flight operations; the list of those who gave permission 

must be made available to the inspector upon request;

f. Signature of exemption-holder or representative; and

 g. A description of the flight activity, including maps or diagrams of any area, city, town, 

county, and/or state over which flights will be conducted and the altitudes essential to 

accomplish the operation.

22. The documents required under 14 CFR §§ 91.9 and 91.203 will be available to the PIC at the

Ground Control Station of the UAS any time the aircraft is operating. 
23. The UA will remain clear and yield the right of way to all other manned operations and activities 

at all times (including, but not limited to, ultralight vehicles, parachute activities, parasailing

activities, hang gliders, etc.).

24. UAS operations will not be conducted during night, as defined in 14 CFR § 1.1. All 

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

special visual flight rules (SVFR) are not authorized.

25. The UAS will not be operated by the PIC from any moving device or vehicle.

 26. The UAS will 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.

27. The UAS will not operate in Class B, C, or D airspace without written approval from the FAA. 

The UAS may not operate within 5 nautical miles of the geographic center of a non- towered 

airport as denoted on a current FAA-published aeronautical chart unless a letter of agreement 

with that airport’s management is obtained, and the operation is conducted in accordance with a

NOTAM as required by the operator’s COA. The letter of agreement with the airport 

management must be made available to the Administrator upon request.

28. Any incident, accident, or flight operation that transgresses the lateral or vertical boundaries of

the operational area as defined by the applicable COA will be reported to the FAA’s UAS

Integration Office (AFS-80) within 24 hours.