UNITED STATES OF AMERICA 

DEPARTMENT OF TRANSPORTATION 

FEDERAL AVIATION ADMINISTRATION 

WASHINGTON, DC 

Regulatory Docket No. ___ _ 

IN THE MATTER OF THE PETITION FOR EXEMPTION OF: 

INNOVATIVE AERIAL PRODUCTIONS 

FOR AN EXEMPTION SEEKING REUEF FROM THE REQUIREMENTS OF 

TITLE 14 OF THE CODE OF FEDERAL REGULATIONS 

SECTIONS 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(1) & (a)(2), AND 91.417(a) & (b) CONCERNING COMMERCIAL OPERATION 

OF DJI Phantom 2 AND DJI Phantom 3 UNMANNED AIRCRAFT SYSTEMS 

PURSUANT TO SECTION 333 OF 

THE FAA MODERNIZATION AND REFORM ACT OF 2012 

CPUBUC LAW 112-95) 

Submitted on July 21, 2015 

INNVOATIVE AERIAL PRODUCTIONS 

John Quinn and Steve Lock 

961 Bradford Ct 

Marshfield, MO 65706 

417-300-5279 

johnmquinn@live.com 

UNITED STATES OF AMERICA 

DEPARTMENT OF TRANSPORTATION 

FEDERAL AVIATION ADMINISTRATION 

WASHINGTON, DC 

Regulatory Docket No. ____ _ 

IN THE MATTER OF THE PETITION FOR EXEMPTION OF: 

INNOVATIVE AERIAL PRODUCTIONS 

FOR AN EXEMPTION SEEKING REUEF FROM THE REQUIREMENTS OF 

TITLE 14 OF THE CODE OF FEDERAL REGULATIONS 

SECTIONS 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(1) & (a)(2), AND 91.417(a) & (b) CONCERNING COMMERCIAL OPERATION 

OF DJI Phantom 2 AND DJI Phantom 3 UNMANNED AIRCRAFT SYSTEMS 

PURSUANT TO SECTION 333 OF 

THE FAA MODERNIZATION AND REFORM ACT OF 2012 

CPUBUC LAW 112-95) 

Submitted on MAY 10, 2015 

INNVOATIVE AERIAL PRODUCTIONS 

John Quinn and Steve Lock 

961 Bradford Ct 

Marshfield, MO 65706 

417-300-5279 

johnmquinn@live.com 
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TABLE OF CONTENTS 

Page 

GLOSSARY OF ABBREVIATIONS ................................................................................... 3 

SUMMARY ........................................................................................................................... 4 

INTRODUCTION AND INTERESTS OF PETITIONERS ................................................... .4 

BACKGROUND .................................................................................................................... 4 

BASIS FOR PETITION ......................................................................................................... S 

NAME AND ADDRESS OF PETITIONERS ............................................................. 7 

THE SPECIFIC SECTIONS OF 14 C.F.R. FROM WHICH INNOVATIVE AERIAL 

PRODUCTIONS SEEKS EXEMPTION ................................................................. 8 

THE EXTENT OF RELIEF INNOVATIVE AERIAL PRODUCTIONS SEEKS AND THE 

REASON ERIC M ROBERTS, AlA SEEKS THE RELIEF ......................... ll 

THE REASONS WHY GRANTING INNOVATIVE AERIAL PRODUCTIONS REQUEST 

WOULD BE IN THE PUBLIC INTEREST ......................................................... 15 

THE REASONS WHY GRANTING THE EXEMPTION WOULD NOT ADVERSELY 

AFFECT SAFETY .......................................................................... 19 

SUMMARY THAT CAN BE PUBLISHED IN THE FEDERAL REGISTER ...... 34 
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ANY ADDITIONAL INFORMATION, VIEWS, OR ARGUMENTS AVAILABLE TO 

SUPPORT INNOVATIVE AERIAL PRODUCTIONS REQUEST ........ .34 

CONCLUSION .................................................................................................................... 35 

APPENDICES ........................................................................................ 37 

AGL 

AOI 

ATC 

ATO 

AV 

CFR 

COA 

FAA 

FAR 

GCS 

GPS 

LOL 

NAS 

NOT AM 

PIC 

Section 333 

333 

so 

GLOSSARY OF ABBREVIATIONS 

Above Ground Level 

Area of Interest 

Air Traffic Control 

Air Traffic Organization 

Aerial Vehicle 

Code of Federal Regulations 

Certificate of Authorization 

Federal Aviation Administration 

Federal Aviation Regulation 

Ground Control Station 

Global Positioning System 

Loss of Link 

National Airspace System 

Notice to Airman 

Pilot In Command 

FAA Modernization and Reform Act of 2012 (FMRA) Section 

Safety Observer 

SOP Standard Operating Procedures 

UA Unmanned Aircraft 

UAS Unmanned Aircraft System 

VFR Visual Flight Rules 

VLOS Visual Line of Site 

VMC Visual Meteorological Conditions 

VTOL Vertical Takeoff and Landing 

SUMMARY 

INNOVATIVE AERIAL PRODUCTIONS seeks exemption from the requirements of 14 C.F.R 

§§ 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), 

and 91.417(a) & (b), to operate an Unmanned Aircraft System pursuant to Section 333 of 

the FAA Modernization and Reform Act of 2012 (FMRA). This exemption will permit JOHN 

QUINN and STEVE LOCK to operate an Unmanned Aircraft System (UAS) for the 

commercial purpose of conducting aerial video and photography of golf courses, real 

estate, and landscape over certain areas of the United States. 

INTRODUCTION AND INTERESTS OF THE PETITIONER 

INNOVATIVE AERIAL PRODUCTIONS provides its clients with expertise and knowledge in 

advanced technologies and solutions to increase efficiency, productivity and effectiveness. 

INNOVATIVE AERIAL PRODUCTIONS has hundreds of hours flying experience. The 

objective of INNOVATIVE AERIAL PRODUCTIONS and its aerial operations is to provide 

high quality imaging for a variety of commercial, public, and residential uses, specifically 

targeting: 

• Golf Course fly over for each hole with focus on special features 

Appraisals 

• Real-estate marketing 

Motion Picture Filming 

Aerial acquisitions used for inspections of public and private 

structures. 

• Building Inspection operations 

BACKGROUND 

Unmanned Aircraft Systems: DJI Phantom 2, DJI Phantom 3 UASs 

INNOVATIVE AERIAL PRODUCTIONS seeks an exemption to operate DJI systems for 

compensation or hire within the NAS. The DJI Phantom 2 and DJI Phantom 3 are vertical 

takeoff and landing (VTOL) Unmanned Aircraft (UA) with a Ground Control Station (GCS) 

utilizing electronic tablet or smart phone systems. The DJI Phantom 2 has a maximum 

gross weight of approximately 2 pounds 11 ounces, while having a length of 16 inches 

width of 16 inches, height of 8 inches, and a maximum speed of approximately 29 knots. 

The DJI Phantom 3 has a maximum gross weight of 6 pounds 7.5 ounces, a length of 17.3 

inches, width of 17.7 inches, height of 11.8 inches, and a maximum speed of 

approximately 42 knots. The DJI Phantom 2 and DJI Phantom 3UAs are equipped with four 

main rotors; driven by Lithium Polymer battery powered electric motors. 

The DJI Phantom 2 and DJI Phantom 3 UAs that will be operated by INNOVATIVE AERIAL 

PRODUCTIONS by John Quinn and Steve Lock will be registered in accordance with 49 

U.S.C. 44103, Registration of Aircraft, as well as 14 C.F.R Part 47, Aircraft Registration, and 

marked in accordance with 14 C.F.R. Part 45, Identification and Registration Marking. 

BASIS FOR PETITION 

Petitioner, INNOVATIVE AERIAL PRODUCTIONS, pursuant to the provisions of the Federal 

Aviation Regulations (14 C.F.R. § 11.61) and the FAA Modernization and Reform Act of 

2012 (FMRA), Section 333, Special Rules for Certain Unmanned Aircraft Systems, hereby 

petitions the Administrator to commercially operate the DJI Phantom 2, DJI Phantom 3 

UASs in the National Airspace System (NAS), and for an exemption from the requirements 

of 14 C.F.R §§ 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(l) & (a)(2), and 91.417(a) & (b). 

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

unmanned aircraft and its operation, INNOVATIVE AERIAL PRODUCTIONS operation of DJI 
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Phantom 2 and DJI Phantom 3 UASs meets the conditions of FMRA Section 333 and 

therefore, will not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, 

Subpart H. 

Accordingly, INNOVATIVE AERIAL PRODUCTIONS requests relief from Sections 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), as these sections set forth 

requirements for maintenance that only apply to aircraft with an airworthiness certificate. 

INNOVATIVE AERIAL PRODUCTIONS submits that the requested relief is proper since an 

equivalent level of safety will be ensured. INNOVATIVE AERIAL PRODUCTIONS will use 

experienced personnel or technicians to perform maintenance, alterations, or preventive 

maintenance on the UASs using the methods, techniques, and practices prescribed in the 

operating documents (i.e., Monthly Maintenance Log, and DJI Phantom 2 and DJI 

Phantom 3 Instruction Manual). Furthermore, INNOVATIVE AERIAL PRODUCTIONS will 

document and maintain all maintenance records for the DJI Phantom 2 and DJI Phantom 3 

UASs. 

Relief from certain requirements of Section 61.113(a) and (b), entitled Private pilot 

privileges and limitations: Pilot in command, is requested by INNOVATIVE AERIAL 

PRODUCTIONS to the extent necessary to allow a Pilot in Command (PIC) holding a 

private pilot or higher level certificate, as well as an airman medical certificate, and who 

has demonstrated, by meeting minimum flight- hour and currency requirements, that the 

PIC is able to safely operate the DJI Phantom 2 and DJI Phantom 3 UASs in a manner 

consistent with this exemption, including evasive and emergency maneuvers and 

maintaining appropriate distances from people, vessels, vehicles and structures. 

INNOVATIVE AERIAL PRODUCTIONS seeks relief from Section 91.7(a), entitled Civil aircraft 

airworthiness, because the DJI Phantom 2 and DJI Phantom 3 UASs do not require an 

airworthiness certificate in accordance with 14 C.F.R. Part 21, Subpart H. As such, 

INNOVATIVE AERIAL PRODUCTIONS submits that we will ensure that the DJI Phantom 2 

and DJI Phantom 3UASs are in an airworthy condition, prior to every flight, by determining 

that the UASs are in compliance with the operating documents (i.e., Monthly Maintenance 

Log, and DJI Phantom 2 and DJI Phantom 3 Instruction Manual), and that the aircraft are in 

a condition for safe flight. 

INNOVATIVE AERIAL PRODUCTIONS also seeks an exemption from the requirements of 

Section 91.121, entitled Altimeter Settings, as the DJI Phantom 2 and DJI Phantom 3 UAs 

will not have a typical barometric altimeter onboard. However, altitude information of the 

DJI Phantom 2 and DJI Phantom 3UAs will be provided to the PIC via Global Positioning 

System (GPS) equipment and radio communications telemetry data link, which downlinks 
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from the UA to the GCS for active monitoring of the flight path. This altitude information, 

combined with INNOVATIVE AERIAL PRODUCTIONS operation of the DJI Phantom 2 and 

DJI Phantom 3 UASs within visual line of sight, at or below 500 feet AGL, will ensure a level 

of safety equivalent to Section 91.121. 

Additionally, INNOVATIVE AERIAL PRODUCTIONS seeks an exemption from the 

requirements of Section 91.151(b), entitled Fuel requirements for flight in VFR conditions. 

INNOVATIVE AERIAL PRODUCTIONS submits that safety will not be affected by operation 

of the DJI Phantom 2 and DJI Phantom 3 UAs during daylight hours in visual 

meteorological conditions (VMC) under visual flight rules (VFR), with enough battery 

power to fly for a total duration of approximately 14.5 minutes to the first point of 

intended landing and, assuming normal cruising speed, to fly after that for at least 4.5 

minutes. 

In accordance with 14 C.F.R. § 11.81, INNOVATIVE AERIAL PRODUCTIONS provides the 

following information in support of its petition for exemption: 

A. Name And Address Of The Petitioner. 

The name and address of the Petitioner and point of contact is: 

INNVOATIVE AERIAL PRODUCTIONS 

John Quinn and Steve Lock 

961 Bradford Ct 

Marshfield, MO 65706 

417-300-5279 

johnmquinn@live.com 

B. The Specific Sections Of 14 C.F.R. From Which INNVOATIVE AERIAL 

PRODUCTIONS Seeks Exemption. 

l.INNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Section 61.113(a) And (b). 

Section 61.113, entitled Private pilot privileges and limitations: Pilot in command, 

subsections (a) and (b) prescribe the following, in relevant part: 

(a) No person who holds a private pilot certificate may act as a pilot in 

command (PIC) of an aircraft that is carrying passengers or property for 
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compensation or hire; nor may that person, for compensation or hire, act as PIC 

of an aircraft. 

(b) A private pilot may, for compensation or hire, act as PIC of an aircraft in 

connection with any business or employment if-

(1) The flight is only incidental to that business or employment; and 

(2) The aircraft does not carry passengers or property for compensation or hire. 

2.1NNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Section 91.7(a). 

Section 91.7, entitled Civil aircraft airworthiness, subsection (a), states the 

following: 

(a) No person may operate a civil aircraft unless it is in an airworthy condition. 

3.1NNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Section 91.121. 

Section 91.121, entitled Altimeter settings, subsection (a), states the following, in 

part: 

(a) Each person operating an aircraft shall maintain the cruising altitude or 

flight level of that aircraft, as the case may be, by reference to an altimeter that 

is set, when operating--

(1) Below 18,000 feet MSL, to--

(i) The current reported altimeter setting of a station along the route 

and within 100 nautical miles of the aircraft; 

(ii) If there is no station within the area prescribed in paragraph (a)(1)(i) 

of this section, the current reported altimeter setting of an appropriate 

available station; or 

(iii) In the case of an aircraft not equipped with a radio, the elevation of 

the departure airport or an appropriate altimeter setting available 

before departure. 
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4.1NNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Section 91.15l{b). 

Section 91.151, entitled Fuel requirements for flight in VFR conditions, subsection 

(b), states the following: 

(b) No person may begin a flight in a rotorcraft 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, to fly 

after that for at least 20 minutes. 

S.INNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirement Of Section 91.405{a). 

Section 91.405, entitled Maintenance required, subsection (a), states the following: 

Each owner or operator of an aircraft-

(a) Shall have that aircraft inspected as prescribed in subpart E of this part and 

shall between required inspections, except as provided in paragraph (c) of this 

section, have discrepancies repaired as prescribed in part 43 of this chapter[.] 

6.1NNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Section 91.407{a){l) 

Section 91.407, entitled Operation after maintenance, preventive maintenance, 

rebuilding, or alteration, subsection (a)(1), states the following: 

(a) No person may operate any aircraft that has undergone maintenance, 

preventive maintenance, rebuilding, or alteration unless--

(1) It has been approved for return to service by a person authorized under 

§ 43.7 of this chapter[.] 

7.1NNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Sections 91.409{a){l) And 91.409{a){2). 

Section 91.409, entitled Inspections, subsection (a), states the following: 
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(a) Except as provided in paragraph (c) of this section, no person may operate 

an aircraft unless, within the preceding 12 calendar months, it has had --

(1) An annual inspection in accordance with part 43 of this chapter and has 

been approved for return to service by a person authorized by§ 43.7 of this 

chapter; or 

(2) An inspection for the issuance of an airworthiness certificate in 

accordance with part 21 of this chapter. 

S.INNVOATIVE AERIAL PRODUCTIONS Seeks Exemption From The 

Requirements Of Sections 91.417(a) And 91.417(b). 

Section 91.417, entitled Maintenance records, subsections (a) and (b), state the 

following: 

(a) Except for work performed in accordance with §§ 91.411 and 91.413, each 

registered owner or operator shall keep the following records for the periods 

specified in paragraph (b) of this section: 

(1) Records of the maintenance, preventive maintenance, and alteration and 

records of the 100-hour, annual, progressive, and other required or 

approved inspections, as appropriate, for each aircraft (including the 

airframe) and each engine, propeller, rotor, and appliance of an aircraft. The 

records must include--

(i) A description (or reference to data acceptable to the Administrator) of 

the work performed; and 

(ii) The date of completion of the work performed; and 

(iii) The signature, and certificate number of the person approving the 

aircraft for return to service. 

(2) Records containing the following information: 

(i) The total time in service of the airframe, each engine, each propeller, 

and each rotor. 

(ii) The current status of life-limited parts of each airframe, engine, 

propeller, rotor, and appliance. 

(iii) The time since last overhaul of all items installed on the aircraft 

which are required to be overhauled on a specified time basis. 

(iv) The current inspection status of the aircraft, including the time 

since the last inspection required by the inspection program under 

which the aircraft and its appliances are maintained. 

(v) The current status of applicable airworthiness directives (AD) and 

safety directives including, for each, the method of compliance, the AD 

or safety directive number and revision date. If the AD or safety 

directive involves recurring action, the time and date when the next 

action is required. 

(vi) Copies of the forms prescribed by§ 43.9(d) of this chapter for each 

major alteration to the airframe and currently installed engines, rotors, 

propellers, and appliances. 

(b) The owner or operator shall retain the following records for the periods 

prescribed: 

(1) The records specified in paragraph (a)(1) of this section shall be retained 

until the work is repeated or superseded by other work or for 1 year after 

the work is performed. 

(2) The records specified in paragraph (a)(2) of this section shall be retained 

and transferred with the aircraft at the time the aircraft is sold. 

(3) A list of defects furnished to a registered owner or operator under § 

43.11 of this chapter shall be retained until the defects are repaired and the 

aircraft is approved for return to service. 

C. The Extent Of Relief INNVOATIVE AERIAL PRODUCTIONS Seeks And The 

Reason INNVOATIVE AERIAL PRODUCTIONS Seeks The Relief. 

1. Extent Of Relief INNVOATIVE AERIAL PRODUCTIONS Seeks And The 

Reason INNVOATIVE AERIAL PRODUCTIONS Seeks Relief From Section 

61.113(a) And {b). 

Relief from Section 61.113(a) and (b) entitled Private pilot privileges and limitations: Pilot in 

command, is requested to the extent necessary to allow a PIC holding a private pilot or 

higher level certificate, as well as a current and valid airman medical certificate, and who 
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has met certain flight-hour and currency requirements, to conduct the proposed UAS 

flight operations for compensation or hire. 

This relief is requested since the limitations set forth in Section 61.113(a) and (b) state that 

a private pilot may, for compensation or hire, act as PIC of an aircraft in connection with 

any business or employment if: (1) The flight is only incidental to that business or 

employment; and (2) The aircraft does not carry passengers or property for compensation 

or hire. 

As set forth more fully below, INNVOATIVE AERIAL PRODUCTIONS submits that an 

equivalent level of safety will be maintained because no PIC will be allowed to operate the 

DJI Phantom 2 UAS or DJI Phantom 3 UAS unless that PIC has met certain flight-hour and 

currency requirements, demonstrating that the PIC is able to safely operate either the DJI 

Phantom 2 or DJI Phantom 3 UAS in a manner consistent with the operations 

specifications as described in this exemption, including evasive and emergency 

maneuvers, as well as maintaining appropriate distances from people, vessels, vehicles and 

structures. 

Further, INNVOATIVE AERIAL PRODUCTIONS submits that all flights of the DJI Phantom 2 

and DJI Phantom 3 UASs, conducted by the PIC pursuant to the grant of this Petition: (1) 

will be incidental to INNVOATIVE AERIAL PRODUCTIONS business; and (2) will not carry 

passengers or property for compensation or hire. 

2. Extent Of Relief INNVOATIVE AERIAL PRODUCTIONS Seeks And The 

Reason INNVOATIVE AERIAL PRODUCTIONS Seeks Relief From Section 

91.7{a). 

Relief from Section 91.7(a) entitled Civil aircraft airworthiness, is requested to the extent 

required to allow INNVOATIVE AERIAL PRODUCTIONS to determine that the DJI Phantom 

2 and DJI Phantom 3 UASs are in airworthy condition prior to every flight by ensuring that 

the UAS is in compliance with the operating documents (i.e., the INNVOATIVE AERIAL 

PRODUCTIONS Aerial Operations Manual, Monthly Maintenance Log, and DJI Phantom 2 

and DJI Phantom 3 Instruction Manual). 

INNVOATIVE AERIAL PRODUCTIONS seeks the requested relief because the DJI Phantom 2 

and DJI Phantom 3 UASs do not require an airworthiness certificate in accordance with 14 

C.F.R. Part 21, Subpart H. Therefore, INNVOATIVE AERIAL PRODUCTIONS will ensure that 

the DJI Phantom 2 and DJI Phantom 3 UASs are in airworthy condition based upon its 

compliance with the operating documents (i.e., Monthly Maintenance Log, and DJI 

Phantom 2 and DJI Phantom 3 Instruction Manual) prior to every flight, and further, 

determine that the aircraft are in condition for safe flight, as stated in the conditions and 

limitations below. 

3. Extent Of Relief INNVOATIVE AERIAL PRODUCTIONS Seeks And The 

Reason INNVOATIVE AERIAL PRODUCTIONS Seeks Relief From Section 

91.121. 

Relief from Section 91.121, entitled Altimeter settings, may be required to allow flight 

operations of the DJI Phantom 2 and DJI Phantom 3 UASs, which utilize a barometric 

pressure sensor, GPS equipment, and a radio communications telemetry data link to 

downlink altitude information from the UA to the PIC at the ground control station (GCS). 

Since the FAA requires that any altitude information concerning UAS operations be 

reported to air traffic control (ATC) in feet above ground level (AGL), INNVOATIVE AERIAL 

PRODUCTIONS seeks the requested relief because the DJI Phantom 2 and DJI Phantom 3 

UA's altimeter may be set on the ground to zero feet AGL, rather than the local barometric 

pressure or field altitude, before each flight. 

Considering the limited altitude of the proposed operations, relief from 14 CFR 91.121 is 

sought to the extent necessary to comply with the applicable conditions and limitations 

stated below. As more fully set forth herein, an equivalent level of safety will be 

maintained since the DJI Phantom 2 and DJI Phantom 3 UAs are equipped with a 

barometric pressure sensor and GPS equipment, which automatically ensures that a 

ground level pressure setting will be established prior to each flight, and provides the PIC 

with altitude information of the UA on the heads-up display of the GCS. 

4. Extent Of Relief INNVOATIVE AERIAL PRODUCTIONS Seeks And The 

Reason INNVOATIVE AERIAL PRODUCTIONS Seeks Relief From Section 

91.151(b). 

Relief from Section 91.151(b) entitled Fuel requirements for flight in VFR conditions, is 

requested to the extent required to allow flights of the battery powered DJI Phantom 2 

and DJI Phantom 3 UAs during daylight hours in visual meteorological conditions (VMC), 

under visual flight rules (VFR), for a total duration of 14.5 minutes to the first point of 

intended landing and, assuming normal cruising speed, to fly after that for at least 4.5 

minutes. INNVOATIVE AERIAL PRODUCTIONS seeks the requested relief because without 

an exemption from Section 91.151(b), the flight time duration of the battery powered DJI 
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Phantom 2 and DJI Phantom 3 UAs will severely constrain the practicality of any aerial 

video or still photo flight operations that INNVOATIVE AERIAL PRODUCTIONS proposes to 

conduct pursuant to this Petition. 

Significantly, as set forth below, the technical specifications of the DJI Phantom 2 and DJI 

Phantom 3 UASs, the DJI Phantom 2 and DJI Phantom 3 operating documents, and 

INNVOATIVE AERIAL PRODUCTIONS's proposed operating limitations, ensure that 

INNVOATIVE AERIAL PRODUCTIONS will safely operate the battery powered DJI Phantom 

2 and DJI Phantom 3 UAs during daylight hours in visual meteorological conditions (VMC), 

under visual flight rules (VFR), with enough battery power to fly for a total duration of 14.5 

minutes to the first point of intended landing and, assuming normal cruising speed, to fly 

after that for at least 4.5 minutes. 

5. Extent Of Relief INNVOATIVE AERIAL PRODUCTIONS Seeks And The 

Reason INNVOATIVE AERIAL PRODUCTIONS Seeks Relief From Sections 

91.405(a), 91.407(a)(l), 91.409(a)(l) & (a)(2), And 91.417(a) & (b). 

Since Sections 91.405(a), 91.407(a)(l), 91.409(a)(l) & (a)(2), and 91.417(a) & (b) only apply 

to aircraft with an airworthiness certificate, INNVOATIVE AERIAL PRODUCTIONS requests 

relief from these Sections because the DJI Phantom 2 and DJI Phantom 3 UASs do not 

require airworthiness certificates. As set forth more fully below, the DJI Phantom 2 and DJI 

Phantom 3 UASs meet the conditions of FMRA Section 333 for operation without an 

airworthiness certificate. Accordingly, INNVOATIVE AERIAL PRODUCTIONS will use trained 

technicians to perform maintenance, alterations, or preventive maintenance on the UASs 

using the methods, techniques, and practices prescribed in the UAS operating documents 

(i.e., the INNVOATIVE AERIAL PRODUCTIONS, Aerial Operations Manual, Monthly 

Maintenance Log, and DJI Phantom 2 and DJI Phantom 3 Instruction Manual). 

Furthermore, INNVOATIVE AERIAL PRODUCTIONS will document and maintain all 

maintenance records for the DJI Phantom 2 and DJI Phantom 3 UASs. 

D. The Reasons Why Granting INNVOATIVE AERIAL PRODUCTIONS Request 

Would Be In The Public Interest; That Is, How It Would Benefit The Public As A 

Whole. 

Granting the present Petition will further the public interest by allowing INNVOATIVE 

AERIAL PRODUCTIONS to safely, efficiently, and economically perform aerial video and 
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photography of golf courses, real estate, and landscape over certain areas of the United 

States. 

Additionally, use of the DJI Phantom 2 and DJI Phantom 3 UASs will decrease congestion 

of the NAS, reduce pollution, and provide significant benefits to the economy. Notably, 

the benefits of INNVOATIVE AERIAL PRODUCTIONS proposed operation of the DJI 

Phantom 2 and DJI Phantom 3 UASs will be realized without implicating any privacy issues. 

1. The Public Will Benefit From Decreased Congestion Of The NAS. 

The DJI Phantom 2 and DJI Phantom 3 UAs are battery powered and serve as a safe, 

efficient, and economical alternative to the manned aircraft traditionally utilized to obtain 

aerial imagery. By reducing the amount of manned aircraft needed to perform aerial 

acquisitions, an exemption allowing the use of a DJI Phantom 2 or DJI Phantom 3 UAS 

would reduce the amount of manned aircraft in the NAS, reduce noise and air pollution, as 

well as increase the safety of life and property in the air and on the ground. 

Furthermore, by reducing the number of manned aircraft operating in the NAS, 

congestion around airports caused by arriving and departing aircraft will be reduced. The 

DJI Phantom 2 and DJI Phantom 3 UAs do not require an airport to takeoff or land. 

Likewise, a reduction of manned aircraft conducting aerial video and photography 

missions would result in fewer aircraft that must be handled by air traffic control during 

the ground, takeoff, departure, arrival, and landing phases of flight operations. 

2. The Public Will Benefit From The Safety And Efficiency Of The DJI 

Phantom 2 and DJI Phantom 3 UASs. 

Conducting aerial acquisitions with the DJI Phantom 2 and DJI Phantom 3 UASs, instead of 

manned aircraft, will greatly benefit the public by drastically reducing the levels of air and 

noise pollution generated during traditional aerial video and still photography flight 

operations. By using battery power and electric motors, the DJI Phantom 2 and DJI 

Phantom 3 UASs produce no air pollution, and is the most viable environmentally 

conscious alternative to the cabin class, six cylinder internal combustion engine aircraft 

that are typically utilized for aerial video and photography, while burning approximately 

20-30 gallons per hour of leaded aviation fuel. The DJI Phantom 2 and DJI Phantom 3 UAs, 

while reducing the carbon footprint of aerial acquisitions, also eliminates noise pollution, 

as the UAs are propelled by battery powered electric motors, rather than an internal 

combustion engine. 
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By using the DJI Phantom 2 and DJI Phantom 3 UASs to perform aerial acquisitions, the 

substantial risk to life and property in the air and on the ground, which is usually 

associated with traditional manned aircraft flight operations, will be substantially reduced 

or completely eliminated. Aside from the lack of flight crew members located on board the 

aircraft, the DJI Phantom 2 and DJI Phantom 3 UAs (weighing approximately 2 pounds 11 

ounces and 6 pounds 7.5 ounces respectively, at their maximum gross weights with 

lengths of 16 inches and 17.3 inches respectively, widths of 16 inches and 17.7 inches 

respectively, and with no fuel on board), has less physical potential for collateral damage 

to life and property on the ground, and in the air, compared to the manned aircraft that 

typically conduct similar operations (weighing approximately 6,000 pounds with a 

wingspan of approximately 42 feet, a length of 34 feet, and a fuel capacity of 180 gallons). 

3. Performing Aerial Video and Photography Operations With The DJI 

Phantom 2 and DJI Phantom 3 UASs Will Benefit The Economy. 

In addition to being safe and efficient, the DJI Phantom 2 and DJI Phantom 3 UASs are 

also an economical alternative to using manned aircraft to conduct similar aerial 

operations. As such, operation of the DJI Phantom 2 and DJI Phantom 3 UASs will allow 

United States based companies, like INNVOATNE AERIAL PRODUCTIONS, to remain 

competitive and contribute to growth of the U.S. economy. Specifically, with the rising cost 

of aviation fuel and the Environmental Protection Agency ("EPA") regulatory actions 

phasing out leaded aviation fuels, U.S. owned and operated companies must adopt new 

and alternative technology in order to remain competitive. Operating the battery powered 

DJI Phantom 2 and DJI Phantom 3 UASs is one such technology that not only allows 

companies greater operational flexibility compared to manned aircraft, but provides such 

flexibility without the high operational cost of a traditional manned aircraft. 

By operating the DJI Phantom 2 and DJI Phantom 3 UASs, companies such as INNVOATIVE 

AERIAL PRODUCTIONS can remain competitive and profitable, and therefore, provide 

greater job stability to employees and contractors, which will ultimately contribute to 

growth of the U.S. economy. Improved financial performance of U.S. companies, through 

commercial use of the DJI Phantom 2 and DJI Phantom 3 UASs, provides a stable 

workforce that increases consumer spending; improves local, state, and federal tax 

revenues; and allows companies to invest in research and development in order to remain 

competitive both in the United States and abroad. 

4. There Are No Privacy Issues. 
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Similar to the manned aerial acquisition flight operations that have been conducted for 

decades, INNVOATIVE AERIAL PRODUCTIONS's proposed operation of the DJI Phantom 2 

and DJI Phantom 3 UASs will not implicate any privacy issues. Specifically, the DJI Phantom 

2 and DJI Phantom 3 UASs will be operated only in compliance with operating documents 

(i.e., the INNVOATIVE AERIAL PRODUCTIONS Aerial Operations Manual, Monthly 

Maintenance Log, and DJI Phantom 2 and DJI Phantom 3 Instruction Manual) which 

requires property owner involvement as well as local law enforcement notification, and in 

accordance with the Federal Aviation Regulations, including the minimum altitude 

requirements of 14 C.F.R. § 91.119. 

E. The Reasons Why Granting The Exemption Would Not Adversely Affect Safety, 

Or How The Exemption Would Provide A Level Of Safety At Least Equal To That 

Provided By The Rule From Which INNVOATIVE AERIAL PRODUCTIONS Seeks 

Exemption. 

1. Reasons Why The DJI Phantom 2 and DJI Phantom 3 UAs Meet The 

Conditions Of The FAA Modernization and Reform Act of 2012 (FMRA) 

Section 333. 

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

unmanned aircraft and its operation, INNVOATIVE AERIAL PRODUCTIONS's operation of 

the DJI Phantom 2 and DJI Phantom 3 UASs meet the conditions of FMRA Section 333, 

and will not require an airworthiness certificate in accordance with 14 C.F.R. Part 21, 

Subpart H. 

Section 333 provides authority for a UAS to operate without airworthiness certification and 

sets forth requirements for considering whether a UAS will create a hazard to users of the 

NAS or the public, or otherwise pose a threat to national security. Specifically, FMRA 

Section 333 states the following, in part: 

(a) In General. --Notwithstanding any other requirement of this subtitle, and not 

Later than 180 days after the date of enactment of this Act, the Secretary of 

Transportation shall determine if certain unmanned aircraft systems may operate 

safely in the national airspace system before completion of the plan and 

rule making required by section 332 of this Act or the guidance required by 

section 334 of this Act. 
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(b) Assessment of Unmanned Aircraft Systems.--/n making the determination 

under subsection (a), the Secretary shall determine, at a minimum--

(1) which types of unmanned aircraft systems, if any, as a result of their 

size, weight, speed, operational capability, proximity to airports and 

populated areas, and operation within visual Line of sight do not create a 

hazard to users of the national airspace system or the public or pose a 

threat to national security; and 

(2) whether a certificate of waiver, certificate of authorization, or 

airworthiness certification under section 44704 of title 49, United States 

Code, is required for the operation of unmanned aircraft systems 

identified under paragraph (1). 

(c) Requirements for Safe Operation. --If the Secretary determines under this 

section that certain unmanned aircraft systems may operate safely in the 

national airspace system, the Secretary shall establish requirements for the safe 

operation of such aircraft systems in the national airspace system. 

In seeking this exemption, INNVOATIVE AERIAL PRODUCTIONS submits that the DJI 

Phantom 2 and DJI Phantom 3 UASs can operate safely in the NAS pursuant to FMRA 

Section 333, as demonstrated by: (a) the characteristics of the DJI Phantom 2 and DJI 

Phantom 3 UASs; (b) the pilot certification requirement; and (c) the specific operating 

limitations. 

a. The Specifications Of The DJI Phantom 2 and DJI Phantom 3 UASs 

Demonstrate Its Safe Characteristics. 

The DJI Phantom 2 and DJI Phantom 3 UASs do not create a hazard to users of the NAS or 

the public, or otherwise pose a threat to national security considering its size, weight, 

speed, and operational capability. 

i. Technical Specifications Of The DJI Phantom 2 and DJI Phantom 3 

UASs. 

The technical specifications of the DJI Phantom 2 and DJI Phantom 3 UASs are set forth by 

the DJI Phantom 2 and DJI Phantom 3 User Manuals, attached hereto as Appendix A and 

B. 

ii. The DJI Phantom 2 and DJI Phantom 3 UASs Autonomous Flight 

And Navigation Modes Enable The UASs To Remain Within A 

Defined Operational Area. 

The DJI Phantom 2 and DJI Phantom 3 UASs may be operated in both manual and fully 

autonomous flight modes. A complete description of the flight and navigational modes of 

the DJI Phantom 2 and DJI Phantom 3 UASs is provided at pages 25-35 of the DJI 

Phantom 2 and pages 12-16 and 45-50 of the DJI Phantom 3 User Manuals, attached 

hereto as Appendix A and B. 

iii. The DJI Phantom 2 and DJI Phantom 3 UASs Are Designed For 

Automatic Return To Home Point Or Hover In The Event Of Loss Of 

The Control Link Or Navigation. 

When the Control Link is lost, the DJI Phantom 2 and DJI Phantom 3 UAs will remain 

stationary, in flight, for 3 seconds or more. If, after 3 seconds, the DJI Phantom 2 and DJI 

Phantom 3 UAs do not reacquire control link data from the GCS, the UAs will assume that 

the Control Link is lost and the UAs will return to the home position (i.e., failsafe mode) via 

GPS, and will descend to the takeoff position and shutdown. 

A complete description of the Failsafe Functions of the DJI Phantom 2 UAS are set forth at 

pages 27 through 29 and for the DJI Phantom 3 at pages 13 through 15 of the DJI 

Phantom 2 and DJI Phantom 3 User Manuals, attached hereto as Appendix A and B. 

iv. The DJI Phantom 2 and DJI Phantom 3 GCS And Its Operation. 

A complete description of the operation and specifications of the DJI Phantom 2 and DJI 

Phantom 3 GCS and flight control software is provided at pages 32 through 43 of the DJI 

Phantom 2 User Manual and pages 40 through 47 of the DJI Phantom 3 User Manual. DJI 

Phantom 2 and DJI Phantom 3 User Manuals are attached hereto as Appendix A and B. 
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b. Flight Operations Of DJI Phantom 2 and DJI Phantom 3 UASs Are 

Limited To The Line Of Sight Of A Certificated Pilot in Command With A 

Safety Observer. 

INNVOATIVE AERIAL PRODUCTIONS partners John Quinn and Steve Lock will be the only 

persons to act as a pilot in command (PIC) of the DJI Phantom 2 and DJI Phantom 3 UASs. 

Additionally, a safety observer will assist them during flight time. 

c. Flights Of DJI Phantom 2 and DJI Phantom 3 UASs Will Be Conducted 

Pursuant To Specific Operating Limitations. 

In seeking this exemption, INNVOATIVE AEB.IAL PRODUCTIONS proposes to commercially 

operate DJI Phantom 2 and DJI Phantom 3 UASs for the special purpose of conducting 

aerial video and photography over certain areas of United States, pursuant to the 

following specific operating limitations: 

1. Operations authorized by this grant of exemption will be limited to the 

following aircraft described in the operating documents, rotorcraft UASs 

weighing less than 55 pounds maximum gross weight: DJI Phantom 2 and DJI 

Phantom 3 Unmanned Aircraft Systems. Proposed operations of any other 

aircraft will require a new petition or a petition to amend this grant. 

2. UAS operations under this exemption will be limited to conducting operations 

for the purpose of aerial video and photography. 

3. The UAs may not be flown at an indicated airspeed exceeding 20 knots. 

4. The UA must be operated at an altitude of no more than 500 feet above 

ground level (AGL), as indicated by the procedures specified in the operating 

documents unless a special request is made and approved by ATC. All altitudes 

reported to ATC must be in feet AGL. 
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5. The UAs 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. 

6. The use of first person view (FPV) by the PIC or safety observer (SO) is not 

permitted. 

7. All operations must utilize a safety observer (SO). The SO may be used to 

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

capability. The SO 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 SO can 

perform the functions prescribed in the operating documents. 

8. The SO must not perform any other duties beyond assisting the PIC with 

seeing and avoiding other air traffic and other ground based 

obstacles/obstructions and is not permitted to operate the camera or other 

instruments. 

9. The operating documents and the grant of exemption must be accessible 

during UAS operations and made available to the Administrator upon request. If 

a discrepancy exists between the conditions and limitations contained in the 

grant of exemption and the procedures outlined in the operating documents, 

the conditions and limitations contained in the grant of exemption 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 

upon request. The operator must also present updated and revised documents 

if it petitions for extension or amendment to the grant of exemption. If the 

operator determines that any update or revision would affect the basis upon 
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which the FAA granted the exemption, then the operator must petition for 

amendment to its grant of exemption. The FAA's UAS Integration Office (AFS80) may be contacted if questions arise regarding updates or revisions to the 

operating documents. 

10. Prior to each flight the PIC must inspect the UAS to ensure that 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 must be included in the 

preflight inspection. All maintenance and alterations must be properly 

documented in the aircraft records. 

11. 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. The PIC who conducts the 

functional test flight must make an entry in the aircraft records. 

12. The pre-flight inspection must account for all potential discrepancies, e.g. 

inoperable components, items, or equipment, not already covered in the 

relevant sections of the operating documents. 

13. The operator must follow the UAS manufacturer's aircraft/component, 

maintenance, overhaul, replacement, inspection, and life limit requirements. 

14. The operator must carry out its maintenance, inspections, and record 

keeping requirements, in accordance with the operating documents. 

Maintenance, inspection, alterations, and status of replacement/overhaul 

component parts must be noted in the aircraft records, including total time in 

service, description of work accomplished, and the signature of the authorized 

person returning the UAS to service. 
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15. Each UASs operated under this exemption must comply with all 

manufacturer Safety Bulletins. 

16. The authorized person must make an entry in the aircraft record of the 

corrective action taken against discrepancies discovered between inspections. 

17. The PIC must possess at least a private pilot certificate and at least a current 

third- class medical certificate. 

18. The operator may not permit any PIC to operate unless the PIC meets the 

operator's qualification criteria and demonstrates the ability to safely operate 

the UAS in a manner consistent with how the UAS will be operated under the 

exemption, including evasive and emergency maneuvers and maintaining 

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

qualification flight hours must be logged in a manner consistent with 14 C.F.R. 

§ 61.51(b). Flights for the purposes of training the operator's PICs are permitted 

under the terms of the 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 C.F.R. § 91.119. 

19. UAS operations may not be conducted during night, as defined in 14 C.F.R. 

§ 1.1. All operations must be conducted under visual meteorological conditions 

(VMC). If flight at night is required, a special request will be made at the FAA 

office closest to proposed area of operations. Flights under special visual flight 

rules (SVFR) are not authorized. 

20. The UA may not operate within 5 nautical miles of an airport reference 

point 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 NOT AM as required by the operator's COA. 
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The letter of agreement with the airport management must be made available 

to the Administrator upon request. 

21. 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. 

22. If the UA loses communications or loses its GPS signal, it must return to a 

pre- determined location within the planned operating area and land or be 

recovered in accordance with the operating documents. 

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

emergencies in accordance with the operating documents. 

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

forecast weather conditions) there is enough power to fly at normal cruising 

speed to the intended landing point and land the UA with 25% battery power 

remaining. 

25. The operator must obtain an Air Traffic Organization (ATO) issued 

Certificate of Waiver or Authorization (COA) prior to conducting any operations 

under the grant of exemption. This COA will also require the operator to 

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

not less than 48 hours prior to the operation. All operations shall be conducted 

in accordance with airspace requirements in the ATO issued COA including 

class of airspace, altitude level and potential transponder requirements. 

26. All aircraft operated in accordance with the exemption must be identified 

by serial number, registered in accordance with 14 C.F.R. part 47, and have 

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

Subpart C. Markings must be as large as practicable. 
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27. Before conducting operations, the radio frequency spectrum used for 

operation and control of the UA must comply with the Federal 

Communications Commission (FCC) or other appropriate government 

oversight agency requirements. 

28. The documents required fewer than 14 C.F.R. 91.9 and 91.203 must be 

available to the PIC at the Ground Control Station of the UAS any time the UAS 

is operating. These documents must be made available to the Administrator or 

any law enforcement official upon request. 

29. The UA must remain clear and yield the right of way to all manned aviation 

operations and activities at all times. 

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

31. Flight operations must be conducted at least 500 feet from all 

nonparticipating persons (persons other than the PIC, SO, operator trainees or 

essential 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 and/or; 

b. The aircraft is operated near vessels, vehicles or structures where the 

owner/controller of such vessels, vehicles or structures has granted 

permission 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, and; 

c. Operations nearer to the PIC, SO, operator trainees or essential 

persons do not present an undue hazard to those persons per § 

91.119(a). 

32. All operations shall be conducted over private or controlled-access 

property with permission from the land owner/controller or authorized 

representative. Permission from land owner/controller or authorized 

representative will be obtained for each flight to be conducted. 

33. 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. 

2. Reasons Why An Exemption From The Requirements Of Section 

61.113(a) And (b) Would Not Adversely Affect Safety. 

INNVOATIVE AERIAL PRODUCTIONS submits that the equivalent level of safety 

established by Section 61.113(a) and (b) will be maintained because no PIC will be allowed 

to operate the DJI Phantom 2 and DJI Phantom 3 UASs unless that PIC has demonstrated, 

by meeting minimum flight-hour and currency requirements, that the PIC is able to safely 

operate the DJI Phantom 2 or DJI Phantom 3 UAS in a manner consistent with the 

exemption, including evasive and emergency maneuvers and maintaining appropriate 

distances from people, vessels, vehicles and structures. 

Considering INNVOATIVE AERIAL PRODUCTIONS's proposed area of operations, and the 

operating limitations set forth-above; the parallel nature of private pilot aeronautical 

knowledge requirements to those of commercial pilot requirements (See Exemption No. 

11062); and the airmanship skills necessary to safely operate the DJI Phantom 2 or DJI 
'. 
Phantom 3 UAS, INNVOATIVE AERIAL PRODUCTIONS submits that the additional manned 

airmanship experience of a commercially certificated pilot would not correlate to the 

airmanship skills necessary for INNVOATIVE AERIAL PRODUCTIONS's specific proposed 

flight operations. 

The FAA has previously granted relief from Section 61.113(a) and (b) specific to UAS, in 

circumstances similar, in all material respects, to those presented herein (e.g. Exemption 

Nos. 11062,11063,11064,11065,11066,11067,11080,11109,11110,11112,11136, 

11138, 11150, 11153, 11156, 11158, 11159, 11160, 11161). 

INNVOATIVE AERIAL PRODUCTIONS will not allow any PIC to operate the DJI Phantom 2 

or DJI Phantom 3 UAS unless that PIC has demonstrated, by meeting minimum flight-hour 

requirements or the DJI Phantom 2 or DJI Phantom 3 UAS training and currency 

requirements, that the PIC is able to safely operate the DJI Phantom 2 or DJI Phantom 3 

UAS in a manner consistent with this exemption, including evasive and emergency 

maneuvers and maintaining appropriate distances from people, vessels, vehicles and 

structures. 

Specifically, the PIC must have accumulated and logged, in a manner consistent with 14 

C.F.R. § 61.51(b), 25 hours of total time as a UAS rotorcraft pilot (with a minimum of 5 

hours of those hours as a UAS pilot operating the same make and model of UAS to be 

used for operations under the exemption). In addition to the hour requirements, the PIC 

must accomplish 3 takeoffs and landings in the preceding 90 days (for currency purposes). 

As in Exemption Nos. 11062, 11138, and 11153, prior documented flight experience that 

was obtained in compliance with applicable regulations will ensure an equivalent level of 

safety during INNVOATIVE AERIAL PRODUCTIONS's proposed operations. The 

Administrator has held that prior documented flight experience that was obtained in 

compliance with applicable regulations would ensure safe operations, stating as follows: 

In Exemption No. 11062, the FAA required that prior to conducting operations for 

the purpose of motion picture filming (or similar operations), the PIC must have 

accumulated and logged, in a manner consistent with 14 CFR 61.51(b), 25 hours of 

total time as a UAS rotorcraft pilot including at least 10 hours logged as a UAS 

pilot with a multi-rotor UAS. Prior to operations under Exemption No. 11062, the 

PIC must also have accumulated and logged a minimum of 5 hours as a UAS pilot 

operating the same make and model of UAS to be used for operations under the 

exemption. For clarification, the FAA considers these minimum hour requirements 

to be inclusive rather than additive; i.e. 5 hours make and model time may be 

included in the 10 hours of multi-rotor time and the 10 hours may be included in 
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the total 25 hours of UAS rotorcraft time. In addition to the hour requirements, the 

PIC must accomplish 3 takeoffs and landings in the preceding 90 days (for currency 

purposes). The FAA finds that at a minimum, the flight-hour requirements in 

Exemption No. 11062 are appropriate to practice and build proficiency in the skills 

necessary to safely conduct the petitioner's proposed operations. The FAA also 

finds that prior documented flight experience that was obtained in compliance 

with applicable regulations would satisfy this requirement. Training, proficiency, 

and experience-building flights can also be conducted under the grant of 

exemption to accomplish the required flight time. During training, proficiency, and 

experience-building flights the PIC is required to operate the UA with appropriate 

distances in accordance with 14 C.F.R 91.119. 

Exemption No. 11138 at page 15. 

Accordingly, INNVOATIVE AERIAL PRODUCTIONS will ensure safe operations by not 

allowing any PIC to operate the DJI Phantom 2 or DJI Phantom 3 UAS unless that PIC has 

demonstrated, by meeting minimum flight-hour and currency requirements, that the PIC is 

able to safely operate the DJI Phantom 2 or DJI Phantom 3 UAS in a manner consistent 

with the exemption, including evasive and emergency maneuvers and maintaining 

appropriate distances from people, vessels, vehicles and structures. 

3. Reasons Why An Exemption From The Requirements Of Section 91.7(a) 

Would Not Adversely Affect Safety. 

The equivalent level of safety established by Section 91.7(a) will be maintained because 

prior to every flight, INNVOATIVE AERIAL PRODUCTIONS will ensure that the DJI Phantom 

2 or DJI Phantom 3 UAS is in an airworthy condition based upon the UAS's compliance 

with its operating documents and as stated in the conditions and limitations herein. 

Additionally, the FAA has previously granted relief from Section 91.7(a) specific to UAS, in 

circumstances similar, in all material respects, to those presented herein (e.g. Exemption 

Nos. 11062,11063,11064,11065,11066,11067,11080,11109,11110,11112,11136, 

11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 

4. Reasons Why An Exemption From The Requirements Of Section 91.121 

Would Not Adversely Affect Safety. 

The equivalent level of safety established by Section 91:121 will be maintained because 

the altitude information of the DJI Phantom 2 and DJI Phantom 3 UAs will be provided to 

the PIC via GPS equipment and a radio communications telemetry data link, which 

downlinks from the UA to the GCS for active monitoring of the flight path and altitude. 

This altitude information, combined with INNVOATIVE AERIAL PRODUCTIONS's operation 

of the DJI Phantom 2 and DJI Phantom 3 UAs within visual line of sight, at or below 500 

feet AGL, will ensure a level of safety equivalent to Section 91.121. The altitude 

information will be generated by GPS equipment installed onboard the aircraft. Prior to 

each flight, a zero altitude initiation point is automatically established by the UASs at 

ground level. 

The FAA has previously granted relief from Section 91.121 specific to UAS, in 

circumstances similar, in all material respects, to those presented herein (e.g. Exemption 

Nos. 11062,11063,11064,11065,11066,11067,11080,11109,11112,11136,11138, 

11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 

5. Reasons Why An Exemption From The Requirements Of Section 

91.151(b) Would Not Adversely Affect Safety. 

A grant of this exemption would ensure an equivalent level of safety established by 14 

C.F.R. Section 91.151(b) as a result of (1) the technical specifications of the DJI Phantom 2 

and DJI Phantom 3 UASs; (2) the limitations on the proposed flight operations; and (3) the 

location of the proposed flight operations. Accordingly, INNVOATIVE AERIAL 

PRODUCTIONS will ensure that it will safely operate the battery powered DJI Phantom 2 

and DJI Phantom 3 UAs during daylight hours in VFR conditions, with enough battery 

power to fly for a total duration of 13.5 minutes to the first point of intended landing and, 

assuming normal cruising speed, to fly after that for at least 4.5 minutes. 

Here, as in Exemption No. 11109, the technical specifications of the DJI Phantom 2 and DJI 

Phantom 3 UASs; the limitations on the proposed flight operations; and the location of the 

proposed operations, will ensure an equivalent level of safety established by 14 C.F.R. 

Section 91.151(b). Furthermore, safety will be ensured as the DJI Phantom 2 and DJI 

Phantom 3 UASs provide audible and visual warnings to the PIC at the GCS when the UAs 

experiences low battery voltage, the first warning occurring at approximately 33% 

remaining battery power, and again at approximately 10% remaining battery power. At the 

critically low battery level, the DJI Phantom Vision+ and DJI Phantom 3 UASs will descend 

and land automatically. 
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Significantly, previous exemptions granted by the FAA concerning Section 91.151 establish 

that safety is not adversely affected when the technical characteristics and operating 

limitations of the UAS are considered. Relief has been granted for manned aircraft to 

operate at less than the minimums prescribed in Section 91.151, including Exemption Nos. 

2689, 5745, and 10650. Moreover, the FAA has previously granted relief from Section 

91.151 specific to UAS, in circumstances similar, in all material respects, to those presented 

herein (e.g. Exemption Nos. 8811, 10808, 10673, 11042, 11062, 11063, 11064, 11065, 

11066, 11067, 11080, 11109, 11110, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 

11159, 11160, 11161). 

6. Reasons Why An Exemption From The Requirements Of Sections 

91.405(a). 91.407(a)(l). 91.409(a)(l) & (a)(2). And 91.417(a) & (b) Would 

Not Adversely Affect Safety. 

In seeking this exemption, INNVOATIVE AERIAL PRODUCTIONS submits that the 

equivalent level of safety with regard to the regulatory maintenance and alteration 

requirements established by Sections 91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 

91.417(a) & (b) will be met because INNVOATIVE AERIAL PRODUCTIONS will use trained 

technicians to perform maintenance, alterations, or preventive maintenance on the UASs 

using the methods, techniques, and practices prescribed in the operating documents (i.e., 

the INNVOATIVE AERIAL PRODUCTIONS Aerial Operations Manual, Monthly Maintenance 

Log, and DJI Phantom 2 and DJI Phantom 3 Instruction Manual). Furthermore, 

INNVOATIVE AERIAL PRODUCTIONS will document and maintain all maintenance records 

for the DJI Phantom 2 and DJI Phantom 3 UASs. 

Since the DJI Phantom 2 and DJI Phantom 3 UASs will be inspected as prescribed by the 

operating documents, INNVOATIVE AERIAL PRODUCTIONS will maintain the equivalent 

level of safety established by Sections 91.405(a), 91.409(a)(1), and 91.409(a)(2). A copy of 

the DJI Phantom 2 and DJI Phantom 3 User Manuals are attached hereto as Appendix A 

and B; a copy of the DJI Phantom 2 and DJI Phantom 3 UAS Maintenance LOG is attached 

hereto as Appendix C. 

Likewise, the exemption sought will not adversely affect safety because INNVOATIVE 

AERIAL PRODUCTIONS will use trained technicians to perform maintenance, alterations or 

preventive maintenance on the UAS using the methods, techniques, and practices 

prescribed by the operating documents. 

Furthermore, the exemption sought would maintain an equivalent level of safety 

established by Sections 91.407, 91.417(a) and 91.417(b), because all maintenance of the 
'· •'• .· 

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DJI Phantom 2 and DJI Phantom 3UASs will be performed by trained technicians. 

Maintenance will be documented and maintained utilizing the monthly maintenance log. 

Significantly, previous exemptions granted by the FAA concerning Sections 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b) establish that safety is not adversely 

affected when the technical characteristics and operating limitations of the UAS are 

considered. 

In consideration of INNVOATIVE AERIAL PRODUCTIONS's proposed operating limitations, 

the operating documents, and the technical aspects of the DJI Phantom 2 and DJI 

Phantom 3 UASs, INNVOATIVE AERIAL PRODUCTIONS submits that safety will not be 

adversely affected by granting exemption from 14 C.F.R. Sections 91.405(a), 91.407(a)(1) 

and (a)(2), 91.409(a)(2), and 91.417(a) and (b). The FAA has previously granted relief 

specific to UAS in circumstances similar, in all material respects, to those presented herein 

(e.g. Exemption Nos. 11062, 11063, 11064, 11065, 11066, 11067, 11080, 11109, 11110, 

11112, 11136, 11138, 11150, 11153, 11156, 11157, 11158, 11159, 11160, 11161). 

7. The FAA May Prescribe Any Other Conditions For Safe Operation. 

In accordance with Section 333 of the FAA Modernization and Reform Act of 2012 (FMRA) 

and 14 C.F.R. § 21.16 entitled Special Conditions, INNVOATIVE AERIAL PRODUCTIONS 

requests that the FAA prescribe special conditions for the intended operation of the DJI 

Phantom 2 and DJI Phantom 3 UASs, which contain such safety standards that the 

Administrator finds necessary to establish a level of safety equivalent to that established 

by 14 C.F.R. Part 21, Subpart H, and 14 C.F.R §§ 61.113(a) & (b), 91.7 (a), 91.121, 91.151(b), 

91.405(a), 91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). Such special conditions 

will permit safe operation of the UAs for the limited purpose of conducting aerial video 

and photography over certain areas of the United States for compensation or hire. FMRA 

Section 333 sets forth the requirements for considering whether a UAS will create a hazard 

to users of the NAS or the public, or otherwise pose a threat to national security; and 

further, provides the authority for such UAS to operate without airworthiness certification 

in accordance with any requirements that must be established for the safe operation of 

the UAS in the NAS. 

Likewise, the Administrator may prescribe special conditions pursuant to 14 C.F.R. 

§ 21.16, for operation of the DJI Phantom 2 and DJI Phantom 3 UASs, since the 

airworthiness regulations of 14 C.F.R. Part 21 do not contain adequate or appropriate 

safety standards, due to the novel or unusual design features of the aircraft. Section 21.16, 

entitled Special Conditions, states the following: 

If the FAA finds that the airWorthiness regulations of this subchapter do not 

contain adequate or appropriate safety standards for an aircraft, aircraft engine, or 

propeller because of a novel or unusual design feature of the aircraft, aircraft 

engine or propeller, he prescribes special conditions and amendments thereto for 

the product. The special conditions are issued in accordance with Part 11 of this 

chapter and contain such safety standards for the aircraft, aircraft engine or 

propeller as the FAA finds necessary to establish a level of safety equivalent to that 

established in the regulations. 

See 14 C.F.R. § 21.16. 

Therefore, in accordance with FMRA Section 333 and 14 C.F.R. § 21.16, the FAA may 

prescribe special conditions for Leading Edge's intended operation of the DJI Phantom 2 

and DJI Phantom 3 UASs, which contain such safety standards that the Administrator finds 

necessary to establish a level of safety equivalent to that established by 14 C.F.R. Part 21, 

Subpart H, and 14 C.F.R Sections 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b). 

• A Summary That Can Be Published In The Federal Register, 

stating: The Rules From Which INNVOATIVE AERIAL PRODUCTIONS Seeks 

Exemption: 

INNVOATIVE AERIAL PRODUCTIONS seeks exemption from the requirements of 14 

C.F.R Sections 61.113(a)&(b), 91.7(a), 91.121, 91.151(b), 91.405(a), 91.407(a)(1), 

91.409(a)(l) & (a)(2), and 91.417(a) & (b). 

A Brief Description Of The Nature Of The Exemption INNVOATIVE AERIAL 

PRODUCTIONS Seeks: 

This exemption will permit INNVOA T/VE AERIAL PRODUCTIONS to commercially 

operate an Unmanned Aircraft System (UAS) for the purpose of conducting aerial 

video and photography over certain areas of the United States. 
'. 

'' 

• f l 
• Any Additional Information. Views. Or Arguments Available To 

Support INNVOATIVE AERIAL PRODUCTIONS's Request. 

This Petition is made pursuant to the FAA Modernization and Reform Act of 2012 

(FMRA) Section 333, which directs the Secretary of Transportation to determine if certain 

UAS may operate safely in the NAS. As such, INNVOATIVE AERIAL PRODUCTIONS's 

request for exemption may be granted pursuant to the authority of FMRA Section 333 and 

14 C.F.R. Part 11, as set forth above. 

FMRA Section 333 sets forth the requirements for considering whether a UAS will create a 

hazard to users of the NAS or the public, or otherwise pose a threat to national security; 

and further, provides the authority for such UAS to operate without airworthiness 

certification. 

As discussed in detail above, INNVOATIVE AERIAL PRODUCTIONS will operate the DJI 

Phantom 2 and DJI Phantom 3 UASs safely in the NAS, without creating a hazard to users 

of the NAS, or the public, or otherwise pose a threat to national security. 

CONCLUSION 

As set forth herein, INNVOATIVE AERIAL PRODUCTIONS seeks an exemption pursuant to 

14 C.F.R. § 11.61 and Section 333 of the FAA Modernization and Reform Act of 2012 

(FMRA), which will permit safe operation of the DJI Phantom 2 and DJI Phantom 3 UASs 

commercially, without an airworthiness certificate, for the limited purpose of conducting 

aerial video and photography over certain areas of the United States. By granting this 

Petition, the FAA Administrator will be fulfilling the Congressional mandate of the FAA 

Modernization and Reform Act of 2012, while also advancing the interests of the public, by 

allowing INNVOATIVE AERIAL PRODUCTIONS to safely, efficiently, and economically 

operate the DJI Phantom 2 and DJI Phantom 3 UASs commercially within the NAS. 

WHEREFORE, in accordance with the Federal Aviation Regulations and the FAA 

Modernization and Reform Act of 2012, Section 333, INNVOATIVE AERIAL PRODUCTIONS 

respectfully requests that the Administrator grant this Petition for an exemption from the 

requirements of 14 C.F.R Sections 61.113(a) & (b), 91.7(a), 91.121, 91.151(b), 91.405(a), 

91.407(a)(1), 91.409(a)(1) & (a)(2), and 91.417(a) & (b), and permit INNVOATIVE AERIAL 

PRODUCTIONS to operate the DJI Phantom 2 and DJI Phantom 3 UASs commercially for 

the purpose of conducting aerial video and photography over certain areas of the United 

States. 

Dated: April 20, 201 5 

Respectfully submitted, 

INNVOATIVE AERIAL PRODUCTIONS 

Steve lock &C'kuc 

Innovative Aerial Productions 

961 Bradford Ct 

Marshfield, MO 65706 

4173005279 

Appendices: 

A- DJI Phantom 2 Manual: 

B - DJI Phantom 3 Specifications Data Sheet 

C - Monthly Maintenance Log 

D- DJI Phantom Users Guide 

APPENDIX-A 

DJI PHANTOM 2 VISION+ TECHNICAL SPECIFICATIONS 

INNVOATIVE AERIAL PRODUCTIONS onlv utilizes safe and reliable UASs. DJI is an industry 

leader in small UAS oroduction. DJI UASs are loaded with around breakina software 

enablina the user to set oarameters which will not allow fliaht into controlled airsoace. 

Parameters can also be set to limit fliaht to no hiaher than a oredetermined and set 

altitude as well as limit fliaht to a oredetermined and set distance. In addition. DJI software 

orovides real-time altitude and location information to the PIC via the linked monitor 

(smart phone/tablet devices) 

1.1 DJI Phantom 2 Vision+ 

1.1.1 Aircraft 

1.1.1.1 Supported Battery- DJI 5200mAH LiPo Battery 

1.1.1.2 Weight (Battery & Propellers Included) - 21bs 11.810oz (1242g) 

1.1.1.3 Hover Accuracy (Ready to Fly) -Vertical: .8m; Horizontal: 2.5m 

1.1.1.4 Max Yaw Angular Velocity - 200° /s 

1.1.1.5 Max Tilt Angel - 35° 

1.1.1.6 Max Ascent Speed - 6m/s 

1.1.1.7 Max Descent Speed - 2m/s 

1.1.1.8 Max Flight Speed- 15m/s (NOT RECOMMENDED) 

1.1.2 Gimbal 

1.1.2.1 Working Current- Static: 750mA; Dynamic: 900mA 

1.1.2.2 Control Accuracy - ±0.03° 

1.1.2.3 Controllable Range - Pitch: -90° - 0° 

1.1.2.4 Maximum Angular Speed - Pitch: 90° /s 

1.1.3 Camera 

1.1.3.1 Operating Temperature Range - 32°F - 104°F (0°C - 40°C) 

1.1.3.2 Sensor Size - l/2.3" 

1.1.3.3 Effective Pixels- 14M 

1.1.3.4 Resolution - 4384x3288 

4.1.3.5 HD Video Recording- 1080p30 & 720p 

4.1.3.6 Recording Field of View - 110°/85° 

1.1.4 Transmitter 

1.1.4.1 Operating Frequency- 5.728GHz- 5.85GHz 

1.1.4.2 Communication Distance (unobstructed) - FCC Compliance: BOOm 

1.1.4.3 Receiver Sensitivity (1 %PER) - -93dBm 

1.1.4.4 Transmitter Power- FCC Compliance: lOOmW 

1.1.4.5 Working Voltage- 120mA@3.7V 

1.1.5 Range Extender 

1.1.5.1 Operating Frequency- 2412-2462MHz 

1.1.5.2 Communication Distance (unobstructed) - 500-700m 

1.1.5.3 Transmitter Power- 20dBm 

1.1.5.4 Power Consumption - 2W 
,·, 

~ :. -- · .. 

. , 

.• 
APPENDIX- B 

DJI Phantom 3 TECHNICAL SPECIFICATIONS 

INNVOATIVE AERIAL PRODUCTIONS onlv utilizes safe and reliable UASs. DJI is an industry 

leader in small UAS oroduction. DJI UASs are loaded with around breakina software 

enablina the user to set oarameters which will not allow fliaht into controlled airsoace. 

Parameters can also be set to limit fliaht to no hiaher than a oredetermined and set 

altitude as well as limit fliahtto a oredetermined and set distance. In addition. DJI software 

orovides real-time altitude and location information to the PIC via the linked monitor 

(smart phone/tablet devices) 

2.2 DJI Inspire 1 

2.2.1 Aircraft 

1m 

2.2.1.1 Model - Phantom 3 

2.2.1.2 Weight (Battery Included) - 1280 grams 

2.2.1.3 Hovering Accuracy (GPS Mode)- Vertical:+/- 10cm; Horizontal:+/-

2.2.1.4 Max Angular Velocity -Yaw: 200° /s 

2.2.1.5 Max Tilt Angle- 35° 

2.2.1.6 Max Ascent Speed - 5m/s 

2.2.1.7 Max Descent Speed - 3m/s 

2.2.1.8 Max Speed -16m/s (Am mode, no wind- NOT RECOMMENDED) 

2.2.1.9 Max Flight Altitude- 6000m 

2.2.1.10 Max Flight Time- Approximately 23 minutes 

2.2.1.12 Motor Model - DJI 3510 

2.2.1.13 Propeller Model - DJI 1345 

2.2.1.14 Operating Temperature Range -14°F to 104°F (-10°C to 40°(} 

2.2.1.15 Dimensions -17 1!4" x 17 %" x 12" 

2.2.2 Gimbal 

2.2.2.1 Model- ZENMUSE X3 

2.2.2.2 Output Power (with camera)- Static: 9W; In Motion: llW 
',' 
2.2.2.3 Operating Current- Static: 750mA; In Motion: 900mA 

2.2.2.4 Angular Vibration Range - ±0.03° 

2.2.2.5 Mounting - Detachable 

2.2.2.6 Controllable Range- Pitch: -90° to +30°; Pan: ±320° 

2.2.2.7 Mechanical Range- Pitch: -125° to 45°; Pan: ±330° 

2.2.2.8 Max Controllable Speed - Pitch: 120° /s; Pan: 180° /s 

2.2.3 Camera 

2.2.3.1 Name- Sony EXMOR 

2.2.3.2 Model - 12.4M Pixel 

2.2.3.3 Total Pixels -12.4M 

2.2.3.4 Effective Pixels- 12.76M 

2.2.3.5 Image Max Size - 4000x3000 

2.2.3.6 ISO Range -100-3200 

2.2.3.7 Field of View- 94° 

2.2.3.8 CMOS- Sony EXMOR 1/2.3" 

2.2.3.9 HD Video Recordina- UHD(4K): 4096x2160o24/25. 

3840x2160o24/25/30: FHD: 1920x1080p24/25/30/48/50/60; HD: 

1280x720p24/25/30/48/50/60 

2.2.3.10 Operating Temperature Range- 32°F- 104°F (0°C- 40°() 

2.2.4 Transmitter 

2.2.4.1 Name - C1 

2.2.4.2 Operating Frequency- 5.728-5.850GHz; 2.400-2.483GHz 

2.2.4.3 Communicating Distance (unobstructed) - 2000m 

2.2.4.4 Output Power - 9W 

2.2.4.5 Operating Temperature Range- 14°F to 104°F (-10°C to 40°() 

2.2.4.6 Battery- 600mAh LiPo 2S 

Inspection Date AircFaft RepaiFS needed Repaired? (YIN} -~---

PHANTOM 2 User Manual Vl.4 

For PHANTOM 2 Flight Controller Firmware version V3.10 

& PHANTOM 2 Assistant version V3.8 

& PHANTOM RC Assistant version Vl.l 

2015.01 

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. 

©2013-2015 DJI. All Rights Reserved.l I 
. ' 
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 OJ/ Products ........................................................ 6 

Connections with Other OJ/ 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 CONTROLLER ............................................................................................... 14 

3.1 POWER ON THE REMOTE CONTROLLER ............................................................................... 14 

3.2 REMOTE CONTROLLER LED INDICATOR STATUS .................................................................... 15 

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

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

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

3.4 REMOTE CONTROLLER OPERATION .................................................................................... 16 

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

41NTELLIGENT BATIERY ............................................................................................... 19 

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

4.21NSTALL THE BATIERY ...................................................................................................... 20 

4.3 BATIERY USAGE ............................................................................................................. 20 

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

4.5 CORRECT BATIERY USAGE NOTES ...................................................................................... 22 

5 CALIBRATING THE COMPASS ...................................................................................... 23 

©2013-2015 DJI. All Rights Reserved. 2 I 
.. ,'t-

;, 
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 

7.11NSTALLING DRIVER AND PHANTOM 2 ASSISTANT ..................•............................................ 31 

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

7.3 FIRMWARE UPGRADE OF PHANTOM 2 ..................•...•..............•.•....................•................ 33 

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

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

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

8.2 LED FLIGHT INDICATORS DESCRIPTION ................................................•.............................. 35 

©2013-2015 DJI. All Rights Reserved.3 I 

/ 

Legend 

0 Forbidden(lmportant) A Caution ·'t' •. r· .. op e. Reference 

©2013-2015 DJI. All Rights Reserved.41 

1 PHANTOM 2 Aircraft 

[1] 

~~~~~~~~~~~ 

~~j~ .. ~ t4 ·~--­ [5]~-~ 

[6]· 

[7]~~ 

[8] 

Figure 1-1 

[9]· 

[10]~ 

Figure 1-2 

[l]Propeller [2]Motor [3]Front Side [4]Front LEDs [S]Micro-USB Port [6]Landing Gear [?]Receiver 

Antenna [B]CAN-Bus Connector [9]LED Flight Indicators [lO]DJIIntelligent Battery [ll]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 controller and the MC acts as the brains of the complete flight control 

system connecting and controlling all the modules together. 

The PHANTOM 2 can be configured in the Assistant, 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. 

I Vld;;-o cable- - - - - - 1 

I To the iOSD module or wirelessf----;>-'7, 

I video transmission module. I 

-----------

~ cAN-:-s;;; ~_;;edo71 

I 

I 

I I 

I I 

L-------

I· 

(Gimbal Mounting Position! 

I Mount the H3-2D/H3-3D !-_.:::"""-',;----' 

fgimbal using 4 screws. I 

L ________ l 

Figure 1-3 

©2013-2015 DJI. All Rights Reserved.5 I 

----, 

I Compass 

'+-7'-:::::_-----1: ~ : 

L.: u, ___ _. 
i. 
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) PHANTOtvl 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 Datal ink. 

( 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 ZENtviUSE gimbals, the latest factory deliveries of PHANTOtvl 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. 

Figure 1-4 

( 6 ) When using the H3-3D gimbal, please connect the 8-Pin cable of PHANTOtvl 2 to the G8 port of H3-3D 

shown below. 

Figure 1-5 

©2013-2015 DJL All Rights Reserved.6 I 

Connections with Other OJI Products 

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

H3-2D as an example. 

1 video Batt• 

l

transmiuion 

module VIDEO GND 

lrransmitter VIDEO~' L-------.J I 

r------------- 1 Description of the Video Cable I 

I (sequence by color) 1 

VIDEO I 

I - VIDEO GND I 

1-----'l -- v .... 

L -=--G~-- - - - - - - _! 

I 

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. 

1-D;;crl';ti;"n -;f the Vid;,; C";bj; - - .., 

1 (sequence by color) 

~ --VIDEO - VIDEOGND I • 1 -- v.p I 

I '--:-_Gl!_D_ - - - - - - - -

I 

Figure 1-7 

©2013-2015 DJI. All Rights Reserved.? I 

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

A VL58, the figure below uses H3-2D as an example. 

I ~s:ip~o~f~h~i~o~a~e-- -~ 

I {sequence by color) I 

VIDEO I 

video 

tra;:~~~~on 1 r;:====~~ 

: - VIDEO GND I - -- v.... I 

AVL58 ~~Y~---------

1 

Figure 1-8 

""7 ZENMUSE, H3-2D I 

I 

I 

I 

I 

I 

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. 

©2013-2015 DJI. All Rights Reserved.8 I 
. J "·' ,: .. , 
r----------, 

Wireless video transmission I 

I module Transmitter specified by 

I DJI(AVL58) I 

I OR lr------7"~ 

ii 

Figure 1-9 

I Oe7crlpti;;;; ;t th"; Vide-; c7bl;- - - 1 

1 (sequence by color} I VIDEO 

, ~ - VIDEO GND 

r------< - v.... I 

I L -=--G,!:P_--------

I 

~ 

-~-- Co;;a-;;1 

:n· I • • : I 

I • • I L..:------~ 

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

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

transmission module AVL58. 

( 5 ) Using the iPad Ground Station 

©2013-2015 DJI. All Rights Reserved.9 I 

Ground End 

I 

J 

Figure 1-10 

iPad Ground 

Station 

·'f· Connect the Air End of 2.4G Bluetooth Datal ink to a spared CAN-Bus port of iOSD if an iOSD is used. 

( 6 ) Using the PC Ground Station 

Ground End 

- Figure 1-11 

©2013-2015 DJI. All Rights Reserved.10 I 

1.3 LED Flight Indicators Description 

1. LED flight indicators are used to show the aircraft's current status. Once powered on, the indicators will light 

up. 

Aircraft in Normal status Descriptions 

••••• ij Self-Test 

••••• Warming Up & Aircraft cannot take off during warming up 

••••• Ready to Fly 

·!P 'fp Ready to Fly (non-GPS) 

Aircraft in abnormal status Warnings and errors ·--1---------------

~ ~~t Remote Controller Signal Lost 

---·---·----!-------·············-·---···-·-·---------------------·-

••••• l'' Level Low Battery Capacity Warning 

•••••• 2nd 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. 

( l ) 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 fronL.::::.-._~_ -"""'"""'" 

LEDs 

©2013-2015 DJI. All Rights Reserved.11 I 

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. 

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

©2013·2015 DJI. All Rights Reserved.121 

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. 

F'it:lpell~rs .. : :"tsl!:( <:;re¥ Nut (9450)/. ·: 

... . .:. ~~ , "'!f;f!Z';" ~., ...... <:,> " (9450 ,,J' ., .,, ,,,, --: c I 

Diagram = ~ I 

Attach to the motor thread that does 

Assembly Location ""'h ro <ho moro' '"'''d """ "'' • ~ not have a black dot. black dot. 

Fastening/Un-fastening El'l Lock, Tighten the propeller in this direction. 

Instructions 'b'l Unlock, Remove the propeller in this dtrection. I 

~.1 Assembly_ 

1. ( Figure 2-1 ) Remove the four warning cards fro·m 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 

~~_[)iiS;I_SSe_1!11:)1y 

( 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. 

!_-~~V. u~~-origi~a_I_~J_I_p~op~~s!or ~-b~tter __ an_d_~!:~_fl~ght_:x_perience. 

©2013-2015 DJI. All Rights Reserved.13 I 

3 Remote Controller 

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

on delivery. 

• For upgraded remote controller (models: NDJ6 or NRC900), select "Upgrade Version" in Phantom Assistant. 

For basic remote controller (models: DJ6 or RC900), select "Basic Version" in Phantom Assistant. 

J3 

J4 ••• • [7] 

• [8] 

[9] 

[10] --'.;:==-....... -

Figure 3-1 

[4] J2 

[6J••• • Jl 

• - [14] 

Figure 3-2 

[l)Antenna [2)Carrying Handle [3)Left Dial [4)3-Position Switch Sl [5)3-Position Switch 52 [6)Joystickl(Jl;J2) 

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

[ll]Battery Level Indicators LED1/LED2/LED3/LED4 (from left to right) [12)T rainer Port 

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

3.1 Power on the Remote Controller 

~--- 1: .Setthe Sl ;ma s?:~~f£17~e~ tRt~e up~~,i~~~~~J~o~:~~~Jre b~t~)d~~-ii~Ks are at 

1 th~ ~ntd:~oint posrttcm.J.f!~~~t~~~~ op~the ~flvt:~ :sw1~e:h. 

I 2. Push the power switch toth~ rtgll~i~;~\>l~~-~~~~~ re~q~~E~"it<>ller: If t~~ power LED 

i 

I 

i 

indkator is solid on, ttl~ remote -c:6ntrolli!r r;·i~n<:~ionirig oo~fnally; The_ battery level L indicators display the ~urrent b:ttery level. 

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

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

as possible. 

A 2. Charge the remote controller's battery by using the included micro-USB cable. Using the incorrect 

type of charging cable may cause damage. 

3. Turn off the remote controller 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. 

©2013-2015 DJI. All Rights Reserved.141 

3.2 Remote Controller LED Indicator Status 

3.2.1 Remote Controller Power LED Indicator Status 

•••••• B-B-B ...... 

•••• 8-B--B •.•... remote controller. 

The remote controller 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 Controller 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 

©2013-2015 DJI. All Rights Reserved.151 

3.3 Antenna Orientation 

The remote controller's antenna should point skywards without obstructions for maximum communication range 

during flight. 

Figure 3-3 

~~~ .. !!!'!'~~-f~.n_!!~~.r_Qp~.r~~i.~!'----~ __ 

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

Definitions 

The 'stick neutral' positions and 'stick released' mean the control sticks of the remote controller are placed at 

the central position. 

To 'move the stick' means that the stick of remote controller is pushed away from the central position. 

©2013-2015 DJI. All Rights Reserved.161 

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 :gJ~c:raft rotation.':'_E!Iocity: _____ ~--

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. 

:(j': ,-, 

,'~ ' ' ,_, ' I .... -,...; 

Position-1 Position-2 

'(Jf:~~- 1 • 

\ I 

-- :ri:.';:. 

,l.!fT:t 

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

OFF Course Lock 

point Lock 

©2013-2015 DJI. All Rights Reserved.17 I 

'® ' I 

' ........... 

Position-3 

I 

~~---, I 

' --~ 

Home 

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 

S1 ;, foe oompm "llbc.,loo. Togglo <h==l 

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

times, which will force the aircraft to enter into 

compass calibration mode. 

Users can configure position 3(bottom position) of the 

Sl switch to trigger the Failsafe in the Assistant. 

52 is the IOC mode switch. IOC (Intelligent 

Orientation Control) function can be enabled in the 

Assistant when in Naza-1'-1 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 Controller & 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 controller and aircraft is already established for you so you can initially skip this 

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

Figure 3-4 

Linking procedures 

1. Power on the PHANTOM 2. 

2. Turn on the remote controller and place it 0.5m-1m away from the aircraft. 

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

When the Link indicator turns solid green, the link between the remote controller and the built-in receiver 

•••••• 

•••••• 

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

on the remote controller . 

The receiver is ready for linking . 

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

©2013-2015 OJ I. All Rights Reserved.18 I 
·.J r."• 
please carry out the linking procedures. 

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. 

IDD~ I 

Intelligent Battery Charger 

( 1 ) Balance Charging 

( 2 ) Capacity Displi>)' 

( 3 ) Communicating 

( 5 ) Over Discharging 

Protection 

( 6 ) Short Circuit Prowetion 

( 7 ) Sleep Protection 

( 8) Charging Temperature 

Detection 

Automatically balance the voltage of each battery cell during charging. 

--- ----- ------

Display the c~rrent b~tfety}&\i~i~ 

The main controller communicates with the battery via communication ports 

for battery voltage, capacity, current and other information. 

reaches 12.8V to 

Discharging stops automatically when the battery voltage reaches 8.4V to · 

prevent over discharging damage. 

Automaticaily'c~ts ofitfie power :Supply wtien a·sliprt circuit is detected. 

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

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

powered on without connecting to other devices. 

The.b~tt!lry.wlllcharg~ .. ogly v;ol!en it.tt~mperature is withinO·C-55"C.If the ' ' ' ' '"' e ~ Y ; ' 

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 f»l'ocec!_ures _ ___ __ ~ 

1.· G'oone~t-tne c'ha~ge( · %~:j~tJf:ri~~~s~~>-

z; ¢onnee;the baJery to the ch~,l'~eitJf•th~ cu~rent C;!pacl~ ~~the b~tt~ri is ciVE!r 75%, you should power on 

1 ·· ~e b•¥r:Y·t?•~~~.m-~n~rsi!\9; . I .-~, 1}1~Bat~J~ij~ve.~~~~~tor~~~s~lf~ ~~rr~p.7.~~fr:?~ityle~el~s tl!e-6~tte'! .cha~ges. Please refer to-battery 

©2013-2015 DJI. All Rights Reserved.191 

4. ·The~at.j:ecyis.fUIIy i:har§edwh Level indicato(;l~~~~t a~eoff~':'i:ite~se Clisconnect the char~er - ., ~ ' -:c : - -- ;,, - - _,- -, - ~-

and battecy when theY~If~f{Jfrig;~~cPn1:ar(!f~c( 

4.2 Install the Battery 

Push the battecy 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 -ll....;:,..."f=~~liij~"'"""'~~LED3 

LEDl LED4 

Battery Power Button 

(Built-in Battery Power Indicator) 

Figure4-2 

0) Checking the battecy 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. 

©2013-2015 DJI. All Rights Reserved.20 I 

(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. 

E\ 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 

©2013-2015 OJ I. All Rights Reserved.21 I 

• • • • 80%·90% --·---· _____ ,, ___ 

• • • • 70%·80% 

• • • • 60%·70% --

• • • • 50%-60% 

-- • • • • 40%·50% ··------~---

• • • • 30%·40% 

• • • • 20%·30% ---------- • • • • Less than 20% -·-----·-·--.. ·--"" 

;4.5 c_o~r~c.!_I:Jiil!!e.!'Y ~~agtt_t-IC)~!S __ _ 

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 o•c to 4o•c. and be discharged in an 

environment that is between -20°( to 5o•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 riew battery if the current battery is swollen or damaged in any way. 

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

8. Never charge the battery unattended. Always charge the battery on a non-flammable surface such as 

concrete and never near any flammable materials. 

9. Safety is extremely important and users can get more information in the DISCLAIMER. 

©2013-2015 DJI. All Rights Reserved.22 I 

5 Calibrating the Compass 

IIVIPORTANT: tvlake 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. 0 ( 2) DO NOT carry ferromagnetic materials with you during calibration such as keys or cellular 

phones. 

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

5.2 Calibration Procedures 

Please carry 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. 

Position-]~) 

·rii:l·', Position-3 \~ '·· 

- -;~----, 

Position-1 ~~) ! 

•tii:. -,, Position-3~~ 

'-· Position-l-~Position-3-·Position-1 

I ___ _£Hp .on~e 

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. 

®2013-2015 DJI. All Rights Reserved.231 

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. 

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

( 5 ) Try to avoid interference between the remote controller and other wireless equipment (No base 

stations or cell towers around). 

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

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

lays and regulations. 

6.2 Starting the Motors 

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 

!~!!lkeo_!f/Landi~S Procedu.r~s. ·. _ _ _ _ .. -. . .... _ ~ __ _ 

I T. Start by placlng th~~~NTe;AA~·b,.. the;gr()l,lrJ(:{v;;ttnthe battery. lev~! in(iicatorsfa.cing you. 

2. 

s. Poweronc~he ..:ir~ra 

4; kP;. gl'een/Yellow; the i1!!'1ANTOM 2 is entering Ready to Fly/Ready to Fly -- "· ~'- _"' ~--:" _' -----~- :· ' ,' '\:-,_::-:· .. ·::-,: \:.·;:·~<~.,-> __ : __ '.·/·; __ ;:----;<,-~:~~:~::<-. •, .( .~:::J, '\' -

(non-GPS) mode; Start the ni:otoruvi~h tfiJ~sc ccimni"n~If• i. ·. · ·· · 

Push the th~otflestick·u~ slowlyto liftth~f~ir~r~fti:,ff ih~gro~~d. RefeFto <Remote Controller Operation• ~ _. "'"~>-~--- •. , ' --~-- '·::·:···/-;···,';:"','l'\'·"<"·,;-;/<'-:'~.. __ ,_,· -. 

©2013·2015 DJI. All Rights Reserved.24 I 

[~ pla~e ~nd''~ne ~lfcraf;;;;~:sc:~~ ~teadily. ~ .. · .... ·' , . ·... . . . . . . . . 

' 7. After landmg, leave the th.£ottle st1c;k dowrrfor 3 to 5 seconds to stop the.m·otors. Return throttle sbck to I . . . . . 

middle position after the motors. ~ave sto~ped. 

.. ---

0 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. 

A ( 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 controller 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 controller and enter Failsafe mode: 

( 1 ) The remote controller is powered off. 

( 2 ) The remote controller is powered on but the 51 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 controller. 

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

reducing the distance the signal can travel. 

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

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

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

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

rr~:~~~;t cont(ol system~"'!ill t~.t~ ke~pt-h-~-~~·-u:c-,r-!t!ft-,, .. -~~~:~-.~-:un-.-.· "'>·"'· "'-~-,~-~e"'ht,~~-wd-J-~~~i~-g.-Note that the aircraft: may l ..~e drifting . ·~ ·' . "····· .• .,.,..... . ·"''~' 

Ready to Fly --- Automatic go home and land 

I The flight c~n;ttllrfst~m·;~t;~;t9~;tl<;~ti~cpb~t~lth~~~~craftt~ flybac:lt:t~ ~~~ hol!1epointandl·a~;;- . ! L-···-~ .. ~-- . . . . .. , . .... . .. . ' . . . . ... . . -~~~-____J 

©2013-2015 DJI. All Rights Reserved.25 I 
:,, 
Home Point 

When the' '!irc:raft is inftializiq~~be Rea~}' f()'Fiy status, the aircraft win record ,the current GPS coordinates as 

tllebo-me point. It .is'recommeJfded to,fift off, only, after Ready to Fly status is confirmed for the safety of being 

able.tctfly back to home pointsuccessfuiJyWH,case;the Fails~fe 91Pt'!eJs initiated .. 

Go Home Procedures 

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. 

( 2 ) When the aircraft is landing automatically, users can control the aircraft's position and altitude if 

the remote controller signal is recovered. 

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 52 switch of the remote 

controller 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 .14 if using iOSD module. 

Regaining Control during Failsafe Procedure 

When the Sl switch is switched to Position· I, 

How to regain toggle the Sl switch to any other position once to 

control regain control. If remote controller's signal is 

control is returned back to the 

©2013-2015 DJI. All Rights Reserved.26 I 

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 lo,;., 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. 

(2) Users in Mainland China can refer to ~fflNi;~~~1YYf.llt.J.)il;;. 

Max Height & Radius Limits 

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

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

©2013-2015 DJI. All Rights Reserved.27 I 

Max Height 

Max Radius 

Max Height 

Max Radius 

(l) 

(2) 

is powered on 

Figure 6-3 Figure 6-4 

The flight height is restricted to fly 

under the max height. 

Warning: Height limit 

reached. 

None. 

The flight distance is restricted to fly Warning: Distance limit Rapid red flashings --

within the max radius. reached. when close to the Max radius limit. 

The flight height is restricted to fly Warning: Height limit reached. 

under the minor height between the 

Max height and 120m. 

Not limited, no warnings or LED indicators. 

None. 

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

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 

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

©2013-2015 DJI. All Rights Reserved.28 I 

10.5m 

of 

Special 

Area 

Airspace' A,C,D 

Boundary: iJ., £, 

Category A Category B 

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. 

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 sf.. 

No restrictions of flight, but the Phantom will not enter 

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

c 

Airspace B through Boundary b & d 

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

not enter into Airspace A through Boundary~ 

·Rear LED 

Flight Indicator 

...... 

!-------+--··--"""""""" _________ ,_ -------··-----·--·1----"""""--""-"""""--i 

D 

No restrictions. None. 

Blue 

©2013-2015 OJ I. All Rights Reserved.29 I 

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 will regain control 

once the motors have stopped. There is no need to toggle the 51 switch. 

(l) 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(V: available; x :unavailable). 

All flights are restricted by height, distance and special areas simultaneously. 

~6 X X X 

Manual 

<6 X X X 

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. 

©2013-2015 DJI. All Rights Reserved.30 I 

7 Assistant Installation and Configuration 

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. 

A The installer in EXE format only supports Windows operating systems (Win XP, Win?, WinS (32 or 64 

bit)). 

Installing a"'4'~il~ning·~ri'M--!;;~;*:c· - '' ' ' -- ,- .l' ,~- -,,;, -

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' 

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. 

©2013-2015 DJI. All Rights Reserved.31 I 

2. 

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........................ c~: .-. ..................... · .• "!!-; 

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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. 

St~rt-uptlie Pe;~o~~~.oi:{Jt~!! P ePHANT0,~-2to the PC with a Micro-USB '\ u'<','>' 

c;able. DO NOT disconneCt until <:?t:tfiguratiol) is fini~Hed. 

.---------- Function switch of Phantom 2 

PHANTON 2 ~- =m¥? 

and Naza·M mode 

Language swap 

View configurations - c!' i)' ;:;;; "~' L ----- - --- Account, software 

, version 

RC, Gain 

, 

_ ..... ..... ..................... -. _ ......... i""'""='= 

Firmware upgrade 

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1nd1cator ~t...'lll~ only. Please refer to the 

Connection indicator lil1iiiiiiiiiiil"'ll'"l-~~iiiiiiiiiiiiiii actual user interface. 

©2013-2015 DJI. All Rights Reserved.32 I 
") ·"' ··' 
( 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 A TTl. 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 

PHANIOM2 "~''J • - X 

II~ .r o~ a ; "" ' j \ 

_ ...F'irmware upgradable items 1.04 

Hlt1il Upgrade iink 

Current firmware version 

(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 controller. 

©2013-2015 DJI. All Rights Reserved.33J 
.-,• 
Start up the PC, power on the remote controller, and then connect the remote controller to the PC with a 

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

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

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

indicator is e and communic;~tion indicator is blinking •. 

4. Finish configuration in the [Main] page. 

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

Main Page of the 24GHz Remote Controller 

PHANT0!-4 RC ~ -

Main page- i 

l- ~- -~- ~---~ ---~~~---~--- ~-~~ 

-

n OJIPMJ~tom--.COfMlllet ~i 

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Connection indicator .............................. . 

©2013-2015 DJI. All Rights Reserved.341 

Language swap 

Firmware upgrade 

Account. software 

"This image is for 

reference only. Please 

refer to the actual 

user interface. 
. . ; . 

. i 
8 Appendix 

Operating environment temperature 

Power consumption 

Supported Battery 

Weight (including the battery) 

Take-off Weight 

Hovering Accuracy (Ready to Fly) 

Max Yaw Angular Velocity 

Max Tilt Angle 

Max Ascent / Descent Speed 

Max Flight Speed 

Wheelbase 

Operating Frequency 

Communication Distance (open anaa) 

Receiver Sensitivity (1%PER) 

Working Current/Voltage 

-10°( to 50°( 

5.6W 

DJIIntelligent battery 

lOOOg 

51300g 

Vertical: 0.8m; Horizontal: 2.5m 

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

lSm/s (Not Recommended) 

350mm 

2.4GHz ISM 

1000m 

-97dBm 

Built-in LiPo Battery Working Current/Capacity 

120mA@3.7V 

3.7V, 2000mAh 

Type 

Capacity 

Charging Environment Range 

Discharging Environment Range 

••••• 

©2013-2015 DJI. All Rights Reserved.35 I 

3S LiPo Battery 

5200mAh. ll.lV 

0°( to 40°( 

-2o•c to so•c 

1'' Level Low Battery Capacity Warning 

•••••• 

,,. 

2nd Level Low Battery Capacity Warning 

Errors & Aircraft cannot fly.• 

Compass di!t;t;obnormalq~b~q~, oHerr~-rl!agnetic interferens.a or 

.t~: :<>T!"Jl.3J; a~eqs ~alibratior1: 

• Users can connect to the PHANTOM 2 Assistant to get detailed information about warnings and errors. 

©2013-2015 DJL All Rights Reserved.36 I