July 15, 2015 

U.S. Department of Transportation, Docket Operations 

West Building Ground Floor, Room w12-140 

1200 New Jersey Ave., SE 

Washington, DC 20590 

Re: Petition of Anderson Engineering Inc. for an Exemption Pursuant to Section 333 of 

the FAA Modernization and Reform Act of 2012 

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

Act”) and 14 C.P.R. Part 11, Anderson Engineering hereby applies for an exemption 

from the Federal Aviation Regulations identified below, to allow commercial operations 

of small unmanned aerial vehicles. 

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

accompanying DJI Phantom 2 Operators Manual (Appendix B) and the Anderson 

Engineering Operational Limitations (Appendix C). The DJI Phantom 2 UAS was 

selected because it has a proven capability for controlled flight as well as a gyro 

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

a failsafe mode for returning home, and prop guards. These devices are offered for 

general sale around the world and have often been used as Model Aircraft in the USA. 

The Requested exemption would authorize commercial operations using the DJI 

Phantom 2 for mapping and surveying applications. These operations will be subject to 

strict operating requirements defined in the user manual and conditions defined by the 

Safety Code of the Academy of Model Aeronautics (see Annex B), in order to ensure at 

least an equivalent level of safety to currently authorized operations using manned 

aircrafts. 

Specifically, the UAS is: 

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

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

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

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

receives signals for flight controls from a ground-based transmitter/controller; 

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

definition still photos and video; 
 An on-board telemetry system that delivers flight data from the on-board flight 

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

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

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

onboard camera plus all the flight data from the telemetry system described 

above; 

The Ground Station Includes: 

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

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

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

UAS while in flight; 

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

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

flight; 

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

visually track the UAS while in flight. 

Proposed Operations 

Anderson Engineering intends to use UAS in two general areas. First, Anderson 

Engineering seeks an exemption to perform video filming and photographing by air for 

public and private use. The purpose of this photography will be to aid in topographic 

mapping of ground based features on the earth. Second, it will employ UAS’s to inspect 

land, residential, commercial, industrial structures and property. 

Specifically, Anderson Engineering will use UAS’s that are equipped with cameras and 

sensors in order to engage in the following commercial activities: 

 Taking photographs to support professional operations in engineering, land 

surveying, architecture, real estate and other related professional activities.

 Inspections by air of agricultural areas.

 Inspections by air of infrastructure such as bridges, highways, electrical 

installations, dams, aqueducts, photovoltaic power stations, wind farms and 

pipes. These inspections will only be done under contract with the owners or 

with any local government authority.

 Inspections by air of land and residential, commercial and industrial structures, 

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

 Inspections by air to detect sources of pollution and gas emissions, under 

contract with the owners in the area or with any local government 

authority.Support provided to search and rescue operations and reconnaissance 

in cases of need, emergency or natural disasters and only when government 

authorities have requested it by contract or donation.
Relevant Statutory Authority 

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

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

FAA "to safely accelerate the integration of civil unmanned aircraft systems into the 

national airspace system." Pursuant to Section 333 of the Reform Act, the FAA 

Administrator is to permit unmanned aircraft systems to operate in the National Air 

Space ("NAS") where it is safe to do so based on the following considerations: 

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

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

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

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

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

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

authority of the Administrator); 49 U.S.C. § 44701(f) (permitting exemptions from§§ 

44701(a), (b) and§§ 44702-44716,et seq.). A party requesting an exemption must 

explain the reasons why the exemption: (1) would benefit the public as a whole, and (2) 

would not adversely affect safety (or how it would provide a level of safety at least equal 

to the existing rules). See 14 C.F.R. §11.81 (petitions for exemption). 

Anderson Engineering’s Proposed UAS Operations Meet the Requirements of 

Section 333 of the Reform Act 

Anderson Engineering’s proposed operations in this Petition for Exemption qualify for 

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

criteria and relevant factors are satisfied. 

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

Capability 

Anderson Engineering will employ the DJI Phantom 2 quadcopters for the operations 

specified in this Petition for exemption. The Phantom 2 UASs have a maximum take-off 

weight of less than 7 pounds, the flight speed will not exceed 35 miles per hour, and it 

will not be flown in controlled airspace (unless a letter of agreement with that airport’s 

management is obtained) or at an altitude that exceeds 400 feet AGL. All flights will be 

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

25% of the battery's maximum charge. The DJI Phantom 2 UAS do not carry any 

flammable propellant or fuel. The Phantom 2 UAS also has an integrated GPS system 

that calculates the UAS’s position and height and relays that information via a secure 

connection to the operator. Additionally, the Phantom 2 UAS contain a failsafe mode if 

its connection to the remote control is lost, and this system permits the UAS to return to 

a predetermined location and land without injury or damage. 
Approval is Warranted Based on the Operational Restrictions Set Forth in the 

Operations Manual. 

Anderson Engineering’s Operations Limitations and the DJI's operators manual contain 

all of the procedures and limitations necessary to successfully perform the operations 

specified in this Petition for Exemption. (Appendices B & C). 

Public Interest 

The public interest will be served by granting Anderson Engineering’s Petition for 

Exemption. Congress has established a national policy that favors early integration of 

UAS’s into the NAS in controlled, safe working environments such as those proposed in 

this Petition. In addition, the public also has an interest in reducing the hazards 

associated with alternate methods of conducting similar operations. Currently 

operations are conducted using teams that physically climb onto structures using 

ladders, using low flying helicopters or aircraft, or simply not available by traditional 

means. By using UAS, exposure to physical hazards will be reduced of conducting the 

operation while remaining safely on the ground. 

Additionally, Anderson Engineering’s intended uses for the UAS’s have identifiable 

safety benefits that include reducing the danger and emissions associated with full size 

helicopters. UAS have no fuel to ignite or explode, no crew, adds a greater degree of 

flexibility which supplements the current capabilities offered by manned aircraft, and 

public interest for a ground impact of a small lightweight UAS is further minimized from 

an ecological and safety standpoint. 

Federal Register Summary 

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

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

Anderson Engineering seeks an exemption from the following rules: 

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

91.119(c), 91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)(1) and (2), and 

91.417(a) and (b) 

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

owners from the substantial hazards associated with performing equivalent work with 

conventional aircraft, rotorcraft, or other methods. 

Conclusion 

Anderson Engineering’s Petition for Exemption satisfies the criteria articulated in 

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

national security. Additionally, the Petition provides more than adequate justification for 

the grant of the requested exemptions to permit Anderson Engineering to operate the 

selected UAS for the operations specified herein. 

Granting the exemption will benefit the public interest as a whole in several ways, 

including (1) significantly improving safety and reducing risk by alleviating human 

exposure to danger, and (2) improving the quality of services and decreasing operating 

costs compared with conventional flight operations. 

With the advent and availability of this technology surveying and mapping functions are 

changing from a traditional ground based operations to the aerial platform. Anderson 

Engineering will have the ability to collect a tremendous amount of data in a small 

fraction of the time that would be needed for ground based efforts. As project sizes 

increase, the savings to both Anderson Engineering and our Clients will increase 

greatly. The cost of purchasing our DJI Phantom 2 is next to nothing in comparison to 

that of a traditional manned aircraft. A major advantage of the low operational expenses 

is that Anderson Engineering can provide these aerial acquisition services at a much 

lower cost to the consumer while remaining competitive and profitable. This will in turn 

lead to economic growth and stability at a local, state and federal level. 

Anderson realizes that other survey and engineering firms have already been granted 

an exemption to use their UAS for commercial purposes, as shown in FAA exemption 

No. 11266, Docket No. FAA-2014-0733 & FAA exemption No. 11285, Docket No. FAA2014-1015 & FAA exemption No. 11299, Docket No. FAA-2014-1008 & FAA exemption 

No. 11302, Docket No. FAA-2014-1032. 

With the DJI Phantom 2’s small and lightweight design it can be assembled and 

deployed in a manner of only a few minutes once the survey crews arrive on site. It will 

perform its mission effectively and efficiently and land directly at our feet. The data we 

collect will be able to be processed immediately. All of these factors prove to be a huge 

benefit to the consumer, and help to advance the land surveying profession.

Sincerely, 

ANDERSON ENGINEERING, INC. 

 by 

_____________________________ 

Neil S. Brady, P.E. 

CEO/President 

Enclosures 
1 

Appendix A

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

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

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

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

91.119; 91.121; 91.151(a); 91.203(a) and (b); 91.405(a); 91.407(a)(1); 91.409(a)(2); and 

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

Exemptions Requested 

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

This statutory authority, by its terms, includes exempting civil aircraft, as the term is 

defined under§ 40101 of the Act, including UASs, from its safety regulations and 

minimum standards when the Administrator decides a requested exemption is in the 

public interest. 

Anderson Engineering seeks an exemption from several interrelated provisions of 14 

C.F.R. Parts 21, 27, 45, 61 and 91 for purposes of conducting the requested operations 

using a UAS. Listed below are the specific sections of 14 C.F.R. for which exemption is 

sought: 

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

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

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

compared to aircraft normally used for the same application. (Regulatory Docket No. 

FAA-2014-0352). These criteria are met, and therefore no exemption is needed. 

Equivalent Level of Safety 

The UAS selected by Anderson Engineering is safe when taking into account their size, weight, 

speed, and operational capability. The UAS weigh less than 7 pounds and will be flown at less 

than 35 miles per hour and completely outside controlled airspace (unless a letter of 

agreement with that airport’s management is obtained). Additionally, the UAS carry 

neither pilots nor passengers, carry no explosive materials and or flammable liquid fuels, and 

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

Limitations. 

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

operator and will be conducted in compliance with local public safety requirements, to 

provide security for the area of operation. Anderson Engineering will also provide the 

FAA with advance notice of all operations via NOTAMS and coordination with the local 

FSDO. In all cases, the UAS operated under the proposed conditions, will be at least as 
2 

safe as, or safer than conventional rotorcraft operating with an airworthiness certificate 

without the restrictions and conditions of the proposed UAS operations. 

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

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

of normal category rotorcraft. To the extent the Anderson Engineering UAS would 

otherwise require certification under Part 27, we seek an exemption from Part 27's 

airworthiness standards for the same reasons identified in the request for exemption 

from 14 C.F.R. Part 21, Subpart H. 

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

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

registration number in letters at least 2 inches high. Additionally, the aircraft must 

display the word "EXPERIMENTAL" in letters at least 2 inches high near the entrance to 

the cabin, cockpit, or pilot station. The UAS does not have an entrance in which the 

word "EXPERIMENTAL" can be placed, and may not have a registration number 

assigned to it by the FAA. 

Anderson Engineering proposes to achieve an equivalent level of safety by including the 

word "EXPERIMENTAL" as large as practicable on the top of the aircraft, where the 

PIC, VO and others in the vicinity of the aircraft while it is preparing for launch will be 

able to see the designation. Finally, the ground station will display a high contrast flag or 

banner that contains the words "Unmanned Aircraft Ground Station" in letters 3 inches 

high or greater. Since the aircraft will operate within 3/4 NM of the ground station, the 

banner should be visible to anyone that observes the aircraft and chooses to investigate 

its point of origin. 

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

determined that exemption from these requirements was warranted provided that the 

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

Subpart C if the markings are as large as practicable." 

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

Medical Certificate 

In addition, Anderson Engineering seeks exemption from 14 C.F.R § 61.113, which 

restricts private pilot certificate holders from flying aircraft for compensation or hire, and 

which would also require a second class medical certificate. The purpose of this section 

is to ensure the skill and competency of any PIC where the aircraft is carrying 

passengers or cargo for hire. In this case, while the UAS will be operated as part of a 

commercial operation, it carries neither passengers nor cargo. In the Grant of 

Exemption in FAA Docket No. FAA-2014-0352, the FAA determined that the unique 

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

additional cost and restrictions attendant with requiring the PIC to have a commercial 
3 

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

or third class medical, we suggest that the PIC exercise the privileges similar to that of a 

sport pilot, requiring only a valid US driver’s license. 

Safety Mitigation 

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

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

unique aspects of UAS flight. An employee of Anderson Engineering will have a private 

pilot’s license. The experience obtained beyond a private pilot certificate in pursuit of a 

commercial pilot certificate in manned flight does not necessarily aid a pilot in the 

operational environment proposed. To that end, Anderson Engineering will require a 

PIC to have a minimum of a private pilot’s license and adhere to the flight limitations 

listed in Appendix C. 

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

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

qualifications, given that operations will be conducted within the limitations outlined in 

this petition. 

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

Anderson Engineering seeks an exemption from 14 C.F.R. § 91.7(a), which requires 

that a civil aircraft be in airworthy condition to be operated. The FAA has stated 

(Regulatory Docket No. FAA-2014-0352) that no exemption is required to the extent that 

the requirements of Part 21 are waived or found inapplicable. 

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

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

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

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

Safety Mitigation 

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

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

Phantom 2 will have immediate access to it. Accordingly, we request an exemption from 

§ 91.9(b) (2)'s flight manual requirements, on the condition that the Phantom 2 flight 

manual be available at the control point during each operation. 

14 C.F.R. § 91.103: Preflight Action 

Anderson Engineering seeks an exemption from 14 C.P.R.§ 91.103, which requires a 

PIC to become familiar with specific information before each flight, including information 
4 

contained in the FAA-approved Flight Manual on board the aircraft. While the PIC will 

be familiar with all information necessary to safely conduct the flight, an exemption is 

requested to the extent that an FAA-approved Flight manual is required. 

Safety Mitigation 

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

and flight manual provided by the manufacturer. The PIC will take all required preflight 

actions- including performing all required checklists and reviewing weather, flight 

requirements, battery charge, landing and takeoff distance, aircraft performance data, 

and contingency landing areas- before initiation of flight. The Operators Manual and 

Operational Limitations will be kept at the ground station with the operator at all times. 

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

Anderson Engineering seeks an exemption from 14 C.F.R. § 91.109(a), which provides 

that "no person may operate a civil aircraft (except a manned free balloon) that is being 

used for flight instruction unless that aircraft has fully functioning dual controls." UAS 

and remotely piloted aircraft, by their design, do not have functional dual controls. 

Instead, flight control is accomplished through the use of a device that communicates 

with the aircraft via radio communications. 

Safety Mitigation 

Given the size and speed of the UAS employed by Anderson Engineering, an 

equivalent level of safe training can still be performed without dual controls because no 

pilot or passengers are aboard the UAS, and all persons will be a safe distance away in 

the event that the UAS encounters any difficulties during flight instruction. In addition, 

we will conduct flight training at our Research and Development test sites, which are 

located on its own property. These training flights will be conducted in a sterile area and 

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

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

is required. 

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

Anderson Engineering requests an exemption from the minimum safe altitude 

requirements of 14 C.F.R. § 91.119. Section 91.119 prescribes the minimum safe 

altitudes under which aircraft may not operate, including 500 feet above the surface and 

away from any person, vessel, vehicle, or structure in non-congested areas. See 14 

C.F.R. § 91.119(c). Section 91.119(d) allows for a helicopter to operate at less than 

those minimum altitudes when it can be operated "without hazard to persons or property 

on the surface," provided that "each person operating the helicopter complies with any 

routes or altitudes specifically prescribed for helicopters by the FAA." 
5 

Safety Mitigation 

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

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

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

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

as well as the location where it is operated. In order to avoid any risk to aircraft, flight 

operations will be restricted to 400' AGL or below. 

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

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

operating an aircraft to maintain cruising altitude or flight level by reference to an 

altimeter that is set to the elevation of the departure airport or barometric pressure. An 

exemption is required to the extent that the UAS do not have a barometric altimeter, but 

rather a GPS altitude read out. 

Safety Mitigation 

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

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

altitude information relayed in real time to the operator. See Grant of Exemption to 

Astraeus Aerial, Docket No. FAA-2014-0352. As the attached Operations Manual 

indicates, the chosen UAS meets these requirements, and a zero altitude initiation point 

will be obtained prior to flight 

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

Anderson Engineering requests an exemption from 14 C.F.R. § 91.15l(a)'s fuel 

requirements for flight in VFR conditions. Section 91.151 states: 

(a) No person may begin a flight in an airplane under VFR conditions unless 

(considering wind and forecast weather conditions) there is enough fuel to fly to the first 

point of intended landing and, assuming normal cruising speed - 

(1) During the day, to fly after that for at least 30 minutes; or 

(2) At night, to fly after that for at least 45 minutes. 

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

flight operations can be conducted while still maintaining a 30 minute reserve. Anderson 

Engineering proposes that all flights comply with this requirement by mandating that the 

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

Safety Mitigation 

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

terminated with at least 25% reserve battery power still available. See Grant of 
6 

Exemption to Astraeus Aerial, Docket No. PAA-2014-0352. The Operations Manual 

conforms to this limit, providing an equivalent level of safety. 

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

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

assigned to the aircraft and a registration certificate must be aboard the aircraft. 

Additionally, subparagraph (b) provides that the airworthiness certificate be "displayed 

at the cabin or cockpit entrance so that it is legible to passengers or crew." 

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

documentation, does not have an entrance, and is not capable of carrying passengers 

or crew. To obtain an equivalent level of safety and meet the intent of 91.203, we 

propose that documents deemed appropriate for this aircraft by the FAA will be colocated with the crew at the ground control station and available for inspection upon 

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

exemption is required. 

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

Required 

Anderson Engineering seeks an exemption from the maintenance inspection 

requirements contained in 14 C.P.R.§ 91.405(a), 91.407(a)(1), 91.409(a)(2); 91.417(a) 

and (b). These regulations specify maintenance and inspection standards in reference 

to 14 C.P.R. Part 43. See, e.g., 14 C.P.R. § 91.405(a) (stating that each owner or 

operator of an aircraft "[s]hall have the aircraft inspected as prescribed in subpart E of 

this part and shall between required inspections ...have discrepancies repaired as 

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

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

certificate, which the UASs will not have. 

Safety Mitigation 

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

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

Manual, flights will not be conducted unless a flight operations checklist is performed 

that includes all of the aircraft's components. 
©2013-2015 DJI. All Rights Reserved.1 | 

PHANTOM 2 User Manual V1.4 

For PHANTOM 2 Flight Controller Firmware version V3.10 

& PHANTOM 2 Assistant version V3.8 

& PHANTOM RC Assistant version V1.1 

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.

 

Appendix B
©2013-2015 DJI. All Rights Reserved. 2 |

Content 

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

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

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

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

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

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

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

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

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

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

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

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

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

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

3 REMOTE 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

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

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

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

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

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

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

5 CALIBRATING THE COMPASS......................................................................................23
©2013-2015 DJI. All Rights Reserved.3 | 

5.1 CALIBRATION WARNINGS .................................................................................................23

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

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

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

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

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

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

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

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

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

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

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

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

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

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

7.1 INSTALLING DRIVER AND 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.4 | 

In the Box 

PHANTOM 2 Remote Controller-2.4GHz Propeller Pair

Intelligent Battery Charger Plug Set

Screwdriver Assistant Wrench Cables

Micro-USB Cable Screws Accessories Box

 

Legend

Forbidden(Important) Caution Tip Reference
©2013-2015 DJI. All Rights Reserved.5 | 

1 PHANTOM 2 Aircraft

[1]

[2]

[3]

[4]

[5]

[6]

[7]

[8]

[10]

[11]

[9]

Figure 1-1 Figure 1-2

[1]Propeller [2]Motor [3]Front Side [4]Front LEDs [5]Micro-USB Port [6]Landing Gear [7]Receiver 

Antenna [8]CAN-Bus Connector [9]LED Flight Indicators [10]DJI Intelligent Battery [11]Compass

1.1 Built-in Flight Control System Instructions

The built-in flight control system is used to control the entire aircraft’s functions in flight such as Pitch (forwards 

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

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

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

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

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

used to communicate with the remote 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.

Compass Gimbal Mounting Position Mount the H3-2D/H3-3D gimbal using 4 screws.

CAN-Bus Connector

Video Cable To the iOSD module or wireless video transmission module. 8-Pin Cable To the G8 port on the H3-2D/H3-3D gimbal.

5-Pin Cable To the compass.

Figure 1-3
©2013-2015 DJI. All Rights Reserved.6 | 

Important Notes of Using with Other DJI Products 

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

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

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

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

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

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

wireless video transmission module.

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

use other 2.4GHz devices (including 2.4G Wi-Fi or 2.4G wireless video transmission module) except the

2.4G Bluetooth and 2.4G Datalink.

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

compass during installation and connection to avoid interference.

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

updated to the Version 2 shown below. H3-2D/H3-3D gimbal can be directly installed for the Version 2 

while for Version 1, a H3-3D adapter kit (coming soon) is required to install the H3-3D gimbal.

Version 1 Gimbal Mounting Position

Version 2 Gimbal Mounting Position

Figure 1-4

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

shown below.

Figure 1-5
©2013-2015 DJI. All Rights Reserved.7 | 

Connections with Other DJI Products 

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

H3-2D as an example.

ZENMUSE H3-2D

Compass

VIDEO VIDEO GND

Batt+ Wireless Batt- video transmission module Transmitter

Description of the Video Cable (sequence by color) VIDEO GND VBat+

VIDEO

GND

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.

ZENMUSE H3-2D

Compass CAN-Bus Connector

VIDEO GND VBat+ GND VIDEO GND VIDEO

Batt+ Batt- VIDEO

DJI

Description of the Video Cable (sequence by color) Wireless video transmission module Transmitter

Figure 1-7
©2013-2015 DJI. All Rights Reserved.8 | 

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

AVL58, the figure below uses H3-2D as an example.

ZENMUSE H3-2D

Compass

DJI

DJI specified wireless video transmission module AVL58 Transmitter

CAN-Bus connector

VIDEO GND VBat+ GND

VIDEO Description of the Video Cable (sequence by color)

 

Figure 1-8

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

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

 

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

below uses H3-2D as an example.
©2013-2015 DJI. All Rights Reserved.9 | 

ZENMUSE H3-2D

VBat+ GND

VIDEO

DJI

VIDEO GND Wireless video transmission module Transmitter specified by DJI(AVL58) OR Other wireless video transmission module Transmitter

CAN-Bus Connector Compass

Description of the Video Cable (sequence by color)

Figure 1-9

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

iOSD Mark II Other wireless video transmission module Transmitter VIDEO GND VIDEO

BATT- Batt- BATT- BATT+ BATT+ UART UART AV-OUT AV-GND

Batt- Batt+ Batt+

Wireless video transmission module AVL58 Transmitter specified by DJI iOSD Mark II

AV-OUT AV-GND

BATT- BATT- BATT+ BATT+ UART UART

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.10 | 

iPad Ground Station iPad Ground Station

+ -

3S-6S Battery 3S-6S Battery

Air End Ground End

Figure 1-10

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

(6) Using the PC Ground Station 

Air End Ground End

PC Ground Station

Figure 1-11
©2013-2015 DJI. All Rights Reserved.11 | 

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. 

LED flight indicators

Aircraft in Normal status Descriptions 

Power On Self-Test

Warming Up & Aircraft cannot take off during warming up

Ready to Fly

Ready to Fly (non-GPS)

Aircraft in abnormal status Warnings and errors

Remote Controller Signal Lost

1

st Level Low Battery Capacity Warning

2

nd Level Low Battery Capacity Warning

Not Stationary or Sensor Bias is too big

Errors & Aircraft cannot fly.

Compass data abnormal because of ferro-magnetic interference or 

the compass needs calibration. 

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

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

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

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

have spooled up.

The front LEDs
©2013-2015 DJI. All Rights Reserved.12 | 

1.4 Notes for PHANTOM 2 using with other DJI products

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

the firmware as requirements below .

Items to upgrade Firmware versions required Assistant for upgrading Assistant version 

P330CB (built-in 

central board)

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

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

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

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

*The iOSD Assistant is applied to both iOSD Mark II and iOSD mini.
©2013-2015 DJI. All Rights Reserved.13 | 

2 Propellers 

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

propellers should be replaced by purchasing new ones if necessary.

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

Diagram

Assembly Location

Attach to the motor thread that does 

not have a black dot.

Attach to the motor thread that has a

black dot.

Fastening/Un-fastening 

Instructions

Lock: Tighten the propeller in this direction.

Unlock: Remove the propeller in this direction.

2.1 Assembly 

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

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

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

fastening instructions.

 

Figure 2-1 Figure 2-2 Figure2-3

2.2 Disassembly 

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

propeller according to the un-fastening instructions.

2.3 Notes

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

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

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

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

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

propellers.

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

7. ONLY use original DJI propellers for a better and safer flight experience.
©2013-2015 DJI. All Rights Reserved.14 | 

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.

[1]

[2]

[5] [4]

[9]

[10]

J2

J1

J3

J4 [7]

[8]

[6]

[3]

[11]

[12]

[13]

[14]

Figure 3-1 Figure 3-2 

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

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

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

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

3.1 Power on the Remote Controller

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

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

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

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

indicators display the current battery 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.

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.15 | 

3.2 Remote Controller LED Indicator Status 

3.2.1 Remote Controller Power LED Indicator Status 

Power LED Indicator Sound Remote Controller Status 

 None Functioning normally. 

 None Charging( remote controller is powered off)

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

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

 B-B-B...... 

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

controller immediately.

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

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

start using the 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

Discharging process 

LED1 LED2 LED3 LED4 Current battery level 

75%~100%

50%~75%

25%~50%

12.5%~25%

0%~12.5%

<0%
©2013-2015 DJI. All Rights Reserved.16 | 

3.3 Antenna Orientation

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

during flight.

Figure 3-3

3.4 Remote Controller Operation

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.

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

Remote 

Controller 

(Mode 2)

Aircraft 

( nose direction)

Operation details 

The throttle stick controls aircraft altitude/elevation. 

Push the stick up and the aircraft will rise.

Pull the stick down and the aircraft will descend.

The aircraft will automatically hover and hold its 

altitude if the sticks are centered. 

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

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

suggest that you push the throttle stick slowly to 

prevent the aircraft from sudden and unexpected 

elevation changes.
©2013-2015 DJI. All Rights Reserved.17 | 

The yaw stick controls the aircraft rudder.

Push the stick left and the aircraft will rotate counter 

clock-wise. 

Push the stick right and the aircraft will rotate 

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

remain facing the same direction.

The yaw stick controls the rotating angular velocity of 

the aircraft. Pushing the stick further away from center 

results in a faster aircraft rotation velocity. 

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

Push the stick up and the aircraft will tilt and fly 

forward. 

Pull the stick down and the aircraft will tilt and fly 

backward. The aircraft will keep level and straight if the 

stick is centered. 

Pushing or pulling the stick further away from center 

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

faster flight velocity. 

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

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

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

The aircraft will keep level and straight if the stick is 

centered. 

Pushing the stick further away from center will result in 

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

velocity. 

 

Position-1 Position-2 Position-3

S1 is for compass calibration. Toggle the S1 switch from 

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

times, which will force the aircraft to enter into

compass calibration mode.

Users can configure position 3(bottom position) of the 

S1 switch to trigger the Failsafe in the Assistant.

 

OFF Course Lock Home 

point Lock

S2 is the IOC mode switch. IOC (Intelligent 

Orientation Control) function can be enabled in the 

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

function after you are familiar with flying. 
©2013-2015 DJI. All Rights Reserved.18 | 

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.

Link button & Link indicator

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.

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

has been successfully established.

Link Indicator Status 

 

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 DJI. All Rights Reserved.19 | 

please carry out the linking procedures. 

 The remote controller is linked with the receiver successfully.

4 Intelligent Battery

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

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

 

Intelligent Battery Charger 

DJI Intelligent Battery Functions 

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

(2) Capacity Display Display the current battery level.

(3) Communicating 

The main controller communicates with the battery via communication ports 

for battery voltage, capacity, current and other information.

(4) Overcharging Protection 

Charging stops automatically when the battery voltage reaches 12.8V to 

prevent overcharging damage.

(5) Over Discharging

Protection 

Discharging stops automatically when the battery voltage reaches 8.4V to 

prevent over discharging damage.

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

(7) Sleep Protection

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

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

powered on without connecting to other devices.

(8) Charging Temperature 

Detection

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

battery temperature is out of this range, the battery will stop charging.

(1) Before use, please read and follow the user manual, disclaimer, and the warnings on the battery. 

Users take full responsibility for all operations and usage.

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

responsibility for operation of any charger from a third party.

4.1 Charging Procedures

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

2. Connect the battery to the charger. If the current capacity of the battery is over 75%, you should power on 

the battery to begin charging.

3. The Battery Level indicators display current capacity level as the battery charges. Please refer to battery 
©2013-2015 DJI. All Rights Reserved.20 | 

level indicator description for details.

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

and battery when the charging is completed.

Wall Socket

4.2 Install the Battery

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

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

Figure 4-1

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

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

4.3 Battery Usage

Figure 4-2

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

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

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

2 seconds to turn on the intelligent battery.

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

2 seconds to turn off the intelligent battery.

LED3

LED4

Battery Power Button

(Built-in Battery Power Indicator)

LED2

LED1

Battery Level Indicator
©2013-2015 DJI. All Rights Reserved.21 | 

(4) Checking the battery life: When the battery is powered off; press and hold the battery power button for 5 

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

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

Level Indicator Description> for details.

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

4.4 Description of the Battery Level Indicator 

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

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

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

: The LED is light off

Charging process 

LED1 LED2 LED3 LED4 Current battery level 

0%~25%

25%~50%

50%~75%

75%~100%

Full charged

Discharging process 

LED1 LED2 LED3 LED4 Current battery level 

87.5%~100%

75%~87.5%

62.5%~75%

50%~62.5%

37.5%~50%

25%~37.5%

12.5%~25%

0%~12.5%

<0%

Battery life 

LED1 LED2 LED3 LED4 Current battery life 

90%~100%
©2013-2015 DJI. All Rights Reserved.22 | 

80%~90%

70%~80%

60%~70%

50%~60%

40%~50%

30%~40%

20%~30%

Less than 20%

4.5 Correct Battery Usage Notes

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

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

environment that is between -20°C to 50°C. Both charging and discharging should be in an environment

where the relative humidity is lower than 80%.

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

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

be turned on. Users should then fully recharge the battery to maximum capacity. This power cycling 

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

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

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

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

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

Please completely discharge a battery prior to disposal. 

6. It’s suggested that you purchase a new battery 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.23 | 

5 Calibrating the Compass

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

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

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

its optimal level.

5.1 Calibration Warnings

 

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

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

underground.

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

phones.

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

5.2 Calibration Procedures

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

PHANTOM 2 for more compass calibration details.

Normal LED

Quickly flip the switch S1 360o Rotate the aircraft horizontally 360o

Rotate the aircraft vertically (Nose downward) Position-1

Start horizontal calibration Start vertical calibration Succeed Fail

Position-1->Position-3->Position-1 Flip no less than 5 times Start cali

LED Flight Indicator

Position-1->Position-3->Position-1 Flip once

Position-3

LED Flight Indicator LED Flight Indicator

Re-calibrate Position-1 Position-3 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.24 | 

6 Flight 

6.1 Flying Environment Requirements

 

(1) Before your first flight, please allow yourself some flight training (Using a flight simulator to 

practice flying, getting instruction from an experienced person, etc.).

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

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

within buildings may interfere with the compass.

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

(5) Try to avoid interference between the remote 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

6.3 Takeoff/Landing Procedures

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

2. Turn on the remote controller.

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

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

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

5. Push the throttle stick up slowly to lift the aircraft off the ground. Refer to <Remote Controller Operation> 

for more details.

6. Be sure you are hovering over a level surface. Pull down the throttle stick to descend. The stick will lock into 
©2013-2015 DJI. All Rights Reserved.25 | 

place and the aircraft will descend steadily.

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

middle position after the motors have stopped.

 

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

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

 

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

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

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

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

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

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

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

battery and aircraft performance may be reduced.

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

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

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

6.4 Failsafe Function

The aircraft will enter Failsafe mode when the connection from the remote 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 S1 is toggled in the position triggering the Failsafe (this must 

have been configured in the PHANTOM 2 Assistant).

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

The flight control system will try to keep the aircraft level during descent and landing. Note that the aircraft may 

be drifting during the descent and landing process.

 

Ready to Fly ---- Automatic go home and land 

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

 
©2013-2015 DJI. All Rights Reserved.26 | 

Home Point 

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

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

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

Go Home Procedures 

1 Record Home Point. 2 Flying. 3 Remote controller signal lost.

4 Signal lost lasts 3s, begin to go home. 5 Fly back to home point. 6 Landing after hovering 15s.

LED Flight Indicator  LED Flight Indicator LED Flight Indicator

LED Flight Indicator LED Flight Indicator LED Flight Indicator

Height over home point<=2 0m

Height over home point>2 0m

20m

Elevate to 2 0m

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 S2 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 

D

if using iOSD module.

Regaining Control during Failsafe Procedure 

Position of 

Switch S1 

 

Position-1 Position-2 

Position-3 

(No triggering the Failsafe) 

How to regain 

control

When the S1 switch is switched to Position-1, 

toggle the S1 switch to any other position once to 

regain control. If remote controller’s signal is

recovered, control is returned back to the pilot.

Regain control as soon as signal is 

recovered.
©2013-2015 DJI. All Rights Reserved.27 | 

6.5 Low Battery Capacity Warning Function

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

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

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

less than 15% power.

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

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

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

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

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

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

 

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

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

cause a communication failure.

6.6 Flight Limits Function

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

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

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

height, distance limits.

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

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

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

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

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

PHANTOM 2.

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

Max Height & Radius Limits 

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

Assistant. Once complete, your aircraft will fly in a restricted cylinder. 
©2013-2015 DJI. All Rights Reserved.28 | 

Max Height Max Radius

Home Point The height of aircraft when it is powered on Figure 6-3 Figure 6-4

Ready to Fly 

 Limits Ground Station Rear LED flight indicator 

Max Height 

The flight height is restricted to fly 

under the max height. 

Warning: Height limit 

reached. 

None.

Max Radius 

The flight distance is restricted to fly 

within the max radius. 

Warning: Distance limit 

reached.

Rapid red flashings 

when close to the Max radius limit. 

Ready to Fly(non-GPS) 

 Flight Limits Ground Station Rear LED flight indicator 

Max Height 

The flight height is restricted to fly 

under the minor height between the 

Max height and 120m. 

Warning: Height limit reached. 

None.

Max Radius Not limited, no warnings or LED indicators. 

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

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

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

6.7 Flight Limits of Special Areas 

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

http://www.dji.com/fly-safe/category-mc for details. These areas have been divided into category A and category B. 
©2013-2015 DJI. All Rights Reserved.29 | 

 Category A Category B

Ready to Fly 

Airspace Limits 

Rear LED 

Flight Indicator 

A 

Orange 

Motors will not start.

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

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

automatically descend and land then stop its motors. 

B 

Yellow 

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

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

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

C 

Green 

No restrictions of flight, but the Phantom will not enter 

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

Airspace B through Boundary b & d.

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

not enter into Airspace A through Boundary a.

D 

Blue 

No restrictions. None. 

10.5m

2400m

Center of Special Area 8000m

120m A B C

8100m

D

b

d

c b a a c

d

a

b

c

Airspace: A,B,C,D Boundary: a, b, c, d

1000m

A C D c a a c

a 2000m c Center of Special Area

Airspace: A,C,D Boundary: a, c,
©2013-2015 DJI. All Rights Reserved.30 | 

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

the descent and landing process. Motors will stop automatically after landing. Users will regain control 

once the motors have stopped. There is no need to toggle the S1 switch.

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

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

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

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

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

6.8 Conditions of Flight Limits 

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

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

All flights are restricted by height, distance and special areas simultaneously.

Phantom mode 

Flight Status Limits of Special Area Max Height Max Radius 

Ready to Fly √ √ √

Ready to Fly (non-GPS) × √ ×

Naza-M mode 

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

GPS 

≥6 √ √ √

<6 × √ ×

ATTI.

≥6 √ √ ×

<6 × √ ×

Manual

≥6 × × ×

<6 × × ×

Disclaimer 

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

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

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

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

administrative rules and social habits thereof.
©2013-2015 DJI. All Rights Reserved.31 | 

7 Assistant Installation and Configuration

7.1 Installing Driver and PHANTOM 2 Assistant

Installing and running on Windows 

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

on the DJI website.

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

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

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

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

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

bit)).

Installing and running on Mac OS X

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

website.

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

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

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

4. Locate the PHANTOM 2 icon in the Finder, press the Control key and then click the PHANTOM 2 icon 

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

the prompt dialog box and then software will launch.

5. After the first successful launch, directly launching of the software can be achieved by double-clicking 

the PHANTOM 2 icon in the Finder or using Launchpad.
©2013-2015 DJI. All Rights Reserved.32 | 

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

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

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

7.2 Using the PHANTOM 2 Assistant on a PC

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

cable. DO NOT disconnect until configuration is finished.

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

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

and communication indicator is blinking .

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

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

Language swap View configurations

Connection indicator Communication indicator

RC, Gain Gimbal, Battery IMU calibration Firmware upgrade Account, software version

*This image is for reference only. Please refer to the actual user interface.

Function switch of Phantom 2 and Naza-M mode
©2013-2015 DJI. All Rights Reserved.33 | 

(1) Users should not enable the Naza-M function before finishing Advanced Flight Maneuvers 

procedure in the " PHANTOM Pilot Training Guide”. If the Naza-M mode is enabled, users can 

switch the control mode between ATTI. Mode, GPS Mode or Manual Mode, and access the 

advanced settings (e.g. IOC). In addition, the LED located on the rear frame arms will display

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

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

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

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

will be returned to factory settings.

7.3 Firmware upgrade of PHANTOM 2

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

procedures below to upgrade the software and firmware; otherwise the PHANTOM 2 might not work properly.

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

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

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

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

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

Firmware upgradable items

Current firmware version

Upgrade link

*This image is for reference only. Please refer to the actual user interface.

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

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

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

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

CMU(5)Gimbal IMU(6)Battery 

7.4 PHANTOM RC Assistant Description

Please follow the procedures to finish the configuration of the remote controller.
©2013-2015 DJI. All Rights Reserved.34 | 

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

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

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

3. Run the PHANTOM RC Assistant 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 and communication indicator is blinking .

4. Finish configuration in the [Main] page.

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

DT7调参软件

Main Page of the 2.4GHz Remote Controller 

Language swap Main page

Connection indicator Communication indicator

Firmware upgrade Account, software version

*This image is for reference only. Please refer to the actual user interface. 
©2013-2015 DJI. All Rights Reserved.35 | 

8 Appendix

8.1 Specifications

Aircraft

Operating environment temperature -10°C to 50°C

Power consumption 5.6W

Supported Battery DJI Intelligent battery

Weight (including the battery) 1000g

Take-off Weight ≤1300g 

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

Max Yaw Angular Velocity 200°/s

Max Tilt Angle 35°

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

Max Flight Speed 15m/s (Not Recommended)

Wheelbase 350mm

2.4GHz Remote Controller 

Operating Frequency 2.4GHz ISM

Communication Distance (open area) 1000m

Receiver Sensitivity (1%PER) -97dBm

Working Current/Voltage 120 mA@3.7V

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

DJI Intelligent Battery

Type 3S LiPo Battery

Capacity 5200mAh, 11.1V

Charging Environment Range 0°C to 40°C

Discharging Environment Range -20°C to 50°C

8.2 LED Flight Indicators Description

Aircraft in Normal status Descriptions 

Power On Self-Test

Warming Up & Aircraft cannot take off during warming up

Ready to Fly

Ready to Fly (non-GPS)

Aircraft in abnormal status Warnings and errors

Remote Controller Signal Lost

1

st Level Low Battery Capacity Warning
©2013-2015 DJI. All Rights Reserved.36 | 

2

nd Level Low Battery Capacity Warning

Not Stationary or Sensor Bias is too big

Errors & Aircraft cannot fly.*

Compass data abnormal because of ferro-magnetic interference or 

the compass needs calibration. 

* Users can connect to the PHANTOM 2 Assistant to get detailed information about warnings and errors.
Appendix C

Operational Limitations

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

energy source(s) and equipment. 

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

3. Flights will be operated at an altitude of no more than 400 feet above ground level 

(AGL), as indicated by the procedures specified in the operator’s manual. All 

altitudes reported to ATC must be in feet AGL. 

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

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

than corrective lenses. 

5. All operations will utilize a visual observer (VO). The VO may be used to satisfy the 

VLOS requirement as long as the PIC always maintains VLOS capability. The VO 

and PIC must be able to communicate verbally at all times. 

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

flight. If the inspection reveals a condition that affects the safe operation of the 

UAS, the aircraft is prohibited from operating until the necessary maintenance has 

been performed and the UAS is found to be in a condition for safe flight. The 

Ground Control Station, if utilized, will be included in the preflight inspection. All 

maintenance and alterations will be properly documented in the aircraft records. 

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

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

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

conducts the functional test flight will make an entry in the UAS aircraft records of 

the flight. The requirements and procedures for a functional test flight and aircraft 

record entry will be added to the operator’s manual. 

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

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

aircraft maintenance/component/overhaul, replacement, and 

inspection/maintenance requirements will be established and identified in the 

operator’s manual. At a minimum, requirements for the following will be included in 

the operator’s manual: 

a. Actuators / Servos; 

b. Transmission (single rotor); 

c. Powerplant (motors); 

d. Propellers; 

e. Electronic speed controller; 

f. Batteries; 

g. Mechanical dynamic components (single rotor); 

h. Remote command and control; 

i. Ground control station (if used); and 

j. Any other components as determined by the operator; 

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

least a valid driver’s license. 
10. The UAS may not be operated directly over any person, except authorized and 

consenting personnel, below an altitude that is hazardous to persons or property on 

the surface in the event of a UAS failure or emergency. 

11. The operator will ensure that no persons are allowed within 500 feet of the area 

except those consenting. This provision may be reduced to no less than 200 feet if 

it would not adversely affect safety. The UAS will abort the flight in the event of 

unpredicted obstacles or emergencies in