December 31, 2015 

John S. Duncan 

Manager, Flight Standards Service 

Unmanned Aircraft Systems Integration 

Office Federal Aviation Administration 

800 Independence Avenue, SW 

Washington, DC 20591 

Jeff Kincart 

Vice President 

American Compliance Technologies, Inc. 

1875 West Main Street 

Bartow, FL 33830 

(863) 533-2000 x246 

jkincart@A-C-T.com 

www.A-C-T.com 

U.S. Department of Transportation, Docket Operations 

West Building Ground Floor, Room W12-140 

1200 New Jersey Avenue, SE 

Washington, DC 20590 

Re: Request for exemption from multiple regulatory provisions to allow the use of small 

unmanned aerial systems on land controlled by clients of American Compliance 

Technologies, Inc. (A-C-T) to assist in the safe evaluation of emergency response 

operations, environmental and infrastructure assessments, and compliance audits for 

our clients. 

Dear Mr. Duncan: 

American Compliance Technologies, Inc. (A.K.A. A-C-T Environmental & lnstructure or A-C-T) 

respectfully requests an exemption from several provisions of Title 14 of the Code of Federal 

Regulations (C.F.R.) to permit the use of small unmanned aerial systems (sUAS) to assist in the 

evaluation of emergency response operations, environmental and infrastructure assessments, 

and compliance audits for our clients. This request is motivated primarily by the desire to 

maximize safety in areas of hazardous materials emergency response evaluation and 

assessment, environmental contamination assessments and compliance audits. While an 

exemption would not eliminate the current need for in-person visual inspection required by 

various federal regulatory departments, it would allow A-C-T to broadly evaluate our clients 

emergency scenes and environmental and infrastructure assessments with sUAS, resulting in a 

safer and more comprehensive assessment of site conditions. Accordingly, the grant of an 

exemption is consistent with Congress' intent, reflected in Section 333 of the FAA Modernization 

and Reform Act of 2012 (Modernization Act)\ that safe systems be permitted in the national 

airspace prior to the issuance of final regulations governing general use of these systems2. A 

summary of this request suitable for publication in the Federal Register is provided as Appendix 

A. 

Appendix B provides the manufacturers information regarding the design, aircraft 

performance, and fail-safe features. We have provided manufacturer information related to 

operating limitations, normal and emergency procedures, and maintenance and inspection 

procedures. As we add aircraft designs, we will update this appendix appropriately. 

1 P.L. 112-95, 126 Stat 11, February 14,2012. 

2 Section 333(b) (2) specifically contemplates that the FAA may issue a certificate of waiver upon a finding that a 

type of UAS, as a result of Its size, weight, speed, operational capacity, proximity to airports and populated 

areas, and operations within visual line of sight do not create a hazard to users of the NAS or the public or 

pose a threat to national security. 
Appendix C provides the A·C-T Operations Manual for flights covered under this Exemption 

Request. 

Background Information 

A-C-T is in the business of Hazardous Materials Emergency Response, Civil and Environmental 

Consulting on environmental and infrastructure projects and compliance audits for our clients. 

A-C-T clients look to us for providing professionals to assess sites as safely and efficiently as 

possible as time is usually of the essence. We have developed specific A-C-T Safe UAV 

Operational Procedures. 

Emergency. Environmental, Infrastructure, and Compliance Assessment Operations 

• Emergency Response Site Assessments 

• Environmental Contamination Assessments 

• Civil Site Surveys 

• Construction Site Surveys 

• Petro/ChemicaVManufacturing Inspections 

• Compliance Audits 

• Safety Inspections 

As part of this, A-C-T is requesting FAA Exemption for sUAS operations for safety, inspection and 

video capture usage. 

Regulatory Basis for Exemption Request 

In addition to the waiver authority provided in §333 of the Modernization Act, the FAA may grant 

an exemption under 49 U.S.C. §44701(f) if it has determined that such an exemption is in the 

public interest. The FAA has imposed a separate requirement in its procedural regulations, 

providing that the petitioner shall explain why granting the exemption would not adversely affect 

safety or how the exemption would provide at least an equivalent level of safety as compliance 

with the underlying regulation. In this case, approval of this exemption would advance the public 

interest by significantly enhancing the safety and efficiency of emergency and infrastructure 

operations and by providing the FAA with valuable user experience on sUAS in a context with 

appreciable economic and societal benefits. As described more fully below, the requested 

exemption would permit the operation of sUAS under tightly controlled conditions, thus ensuring 

that operations will not have an adverse impact on safety. To the contrary, as explained below, 

A-C-T anticipates that use of sUAS will enhance safety in emergency and infrastructure 

operations. Granting an Exemption is in the Public Interest. The safety and efficiency of 

emergency and infrastructure operations is heavily dependent upon constant analysis of site 

conditions on emergency response scenes, right-of-way, infrastructure and other facilities I Sites. 

There are a wide variety of factors that can affect conditions and cause problems for the public. 

Facilities that produce environmentally hazardous chemicals could contaminate public drinking 

water or crop land. Emergency scenes that have hazardous materials spilled currently require 

in-person assessments in potentially dangerous situations. These are just a few reasons why 

utilizing a sUAS would protect the health, well-being and safety of not just A·C-T's employees but 

also the public. 

As a result, pursuant to federal regulations and company policy, our clients are required to do 

facility inspections, environmental cleanup of spilled or released chemicals, storm water 

inspections for infrastructure projects, etc. and as a result they currently do these type of 

compliance inspections in-person, in personal protective equipment, motor vehicles and 

specialized equipment. 

2 
This is often a labor-intensive and dangerous job. While our clients do all they can to make these 

inspections as safe as possible, there is an irreducible element of risk involved whenever 

employees are required to go into these environments. Employees may need to climb over or 

onto structures, which can be slippery, rough, and/or exposed to the elements to see that certain 

infrastructure is sound. Some structures, such as fuel tanks, are high above the ground. 

Equipment moving through inspection zones can increase risk as well, especially in high-traffic 

areas. While the use of sUAS for supplemental infrastructure and site assessment evaluation 

would not eliminate these risks entirely (as it is an additive safety measure), it would reduce the 

risks to employees by allowing for remote aerial review. 

Additionally, the potential for contaminates to travel through conveyances to bodies of water or 

public lands means that visual inspection in all instances by company personnel can be inefficient 

and not comprehensive. Aerial analysis by traditional fixed wing aircraft is impractical because the 

required altitudes for safe flight reduce visibility below meaningful levels- it is simply not possible 

to see all these issues from such heights. Helicopters present better vantage points; however 

manned helicopters are much costlier, subject to human safety and carry highly explosive jet fuel 

making them impractical for deployment on certain sites. By using sUAS for site assessment 

evaluations, A-C-T will be able to substantially upgrade its ability to detect and address issues 

that could potentially affect the health, safety and wellness of the public before they become a 

problem. Thus, the use of sUAS has the potential to improve efficiency, an overall greater picture 

of the "whole situation", potential safety hazards during the evaluation of emergency scenes, 

environmentally sensitive lands, contamination assessments and public safety. 

Granting an Exemption Will Not Adversely Affect Safety 

A-C-T notes that there is no applicable standard for an equivalency determination. Some have 

argued that the appropriate standard is that for model aircraft, noting that their operations, if 

conducted for recreational purposes, would fall completely within the allowable operations for 

model aircraft. We believe it is difficult to argue that there is sufficient correlation between model 

operations controlled by the Academy of Model Aeronautics and the ones contemplated by 

A-C-T. At the same time, it is clear that equivalency cannot be established for traditional, manned 

civil aircraft because the design and use profiles between traditional aircraft and sUAS are simply 

too different. As such, we believe it makes more sense to focus on why the contemplated 

operations would not adversely affect safety, which is all that §11.81 (e) requires.

3 

3 NotesRegardinq: 14C.F.R.Part21 . SubpartH 

In accordance with the statutory criteria provided in Section 333 of PL 112---95 in reference to 49 USC 44704 

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

operation, we request that this aircraft exemption meets the conditions of Section 333. Therefore, if granted 

Section 333 relief of 14 CFR part 21, and any associated noise certification and testing requirements of part 36, 

is not necessary. 

Notes Regarding: 14 C.F.R. § 45.23 {b) Marking of the Aircraft 

Given the size of the sUAS, two-inch lettering will be impossible. UA will be identified by serial number, registered 

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

part 45, Subpart C. Markings will be as large as practicable. 

Notes Regarding: 14 CFR § 91.7{a) Civil Aircraft Airworthiness 

A-C-T's request is based on the fact that no airworthiness certifiCate will be issued for the UAS. A-C-T's UAS will not 

require an airworthiness certificate in accordance with 14 CFR part 21, Subpart H. Based on the fact that an 

airworthiness certificate will not be issued, exemption from§ 91 .7{a) is not necessary. 

Notes Regarding: 14 CFR § 91 .9(b)(2) Civil Aircraft Flight Manual. Marking and Placard 

Certifications required, the original intent of these regulations was to display an aircraft's airworthiness, certification, and 

registration documents so they would be easily available to inspectors and passengers. Based on the FAA 

Memorandum subject "Interpretation regarding whether certain required documents may be kept at an unmanned 

3 
Granting an exemption will not adversely affect safety. A-C-T contemplates conducting sUAS 

operations over client owned or controlled land, solely during daylight hours, at altitudes well 

below that which would pose a risk to other aircraft. In general, sUAS operations are intended to 

be conducted in areas that will have spotters and be cleared (as much as possible) of anyone or 

anything that could be hurt or damaged by the sUAS. The nature of operations anticipated by 

A-C-T requires that the sUAS be flown at relatively low altitudes and relatively low speeds. A-C-T 

expects that in most instances, the sUAS will be flown less than 200 feet along the path of the of 

the assessment area. Accordingly, the risk of interference with another aircraft is minimal. A-C-T 

also plans to conduct sUAS operations at least three miles from any public airports (including 

heliports). In the event an operation needs to be conducted closer to an airport, A-C-T will inform 

the airport operator and airport air traffic control tower of the contemplated operation and will 

comply with any directions issued by air traffic control at that airport. 

Approval of exemptions allowing commercial operations of sUASs in the hazardous materials 

emergency response and environmental assessment and compliance industry will enhance 

safety by reducing risk. Conventional operations, using jet or piston power aircraft, operate at 

extremely low altitudes just feet from' the subject being inspected and in extreme proximity to 

people and structures; and present the risks associated with vehicles that weigh in the 

neighborhood of 4,0001bs., carrying large amounts of jet A or other fuel (140 gallons for jet 

helicopters). Such aircraft must fly to and from the inspection site. In contrast, a sUAS weighing 

fewer than 55 lbs. and powered by batteries eliminates virtually all of that risk given the reduced 

mass and lack of combustible fuel carried on board. The sUAS is carried to the inspection site. 

The sUAS will carry no passengers or crew and, therefore, will not expose them to the risks 

associated with manned aircraft flights. 

The operation of small UASs, weighing less than 55 lbs., conducted in the strict conditions 

outlined above, will provide an equivalent level of safety supporting the grant of the exemptions 

requested herein, including 333 Aircraft Exemption Status exempting the applicant from 

conventional aircraft requirements and allowing commercial operations. These .lightweight aircraft 

operate at slow speeds, close to the ground, and in a controlled environment and, as a result, are 

far safer than conventional operations conducted with turbine helicopters operating in close 

proximity to the ground and people. . 

The safety of those on the ground is protected by the fact that no one will be allowed into the area 

aircraft's control station,• dated August 8, 2014, the requested relief from 14 CFR §§ 91.9(bX2) and 91.203(a) and (b) 

is not necessary. 

Notes Reaarding: §91.109 Flight Instruction: Simulated Instrument and Certain Flight Tests 

Small UASs, by their design, do not have fully functional dual controls. Flight control is accomplished through the use of 

a control box that communicates with the aircraft via radio communications. Aircraft being considered for use by A-C-T 

allow the UAS Instructor to place the aircraft into 'loiter' mode (fixed altitude stationary hold). In the event of the student 

losing control, the UAS Instructor can quickly and via alternate equipment {equipment not in the hands of the student) 

place the aircraft into a mode that then allows the instructor to bring the aircraft back into control and back to the predetermined and/or safe landing location. 

A-C-T does not describe training scenarios in which a dual set of controls would be utilized or required , i.e. dual flight 

instruction, provided by a flight instructor or other company-designated individual that would require that individual to 

have fully functioning dual controls. Rather, A-C-T evaluates the qualification of its PICs based on their experience with 

the UAS to be operated and verifies through testing, in lieu of formalized training. As such, A-C-T does seek relief from 

14 CFR § 91.109 due to the fact that a certified flight Instructor may not be available and would be a hardship. 

Notes Reaarding § 14 CFR 91.119(b) 

Relief from § 14 CFR 91 .119(b }, operation over congested areas, is applicable, because the A-C-Ts operations could be 

conducted over or near congested areas during emergency operations or assessment activities. 

4 
without the permission of the company. Security will be established for the flight area as part of 

the pre-flight control. Each individual within the secure area will be briefed prior to flight and will 

consent to being in the area. All others will be excluded from the area. 

A-C-T initially intends to use a dedicated staff for sUAS operations. All operations will be within 

visual line-of-sight (i.e., no more than approximately 0.5 miles from the manipulator of the 

controls, or pilot in command (PIC)). Each PIC will conduct at least three take-offs and landings 

with the sUAS on which he or she is trained every 90 days. PIC's will establish their qualifications 

thru a combination of aeronautical knowledge, UAS airmanship skills, and verification through 

testing of flight ability before operations have commenced. Depending on the type of 

operation, additional ground-based visual observers may be employed as well. These observers 

will be within constant visual line of sight and in constant contact with the PIC. The visual 

observers will assist the PIC in avoiding objects near the sUAS. 

There are no standards for either Private or Commercial sUAS pilot certificates. The safe 

operation and control of the UAS as described in this application does not depend on the type of 

FAA license held by the PIC. Given the restricted and controlled airspace within which operations 

will take place, the key factors needed by the PIC are knowledge of the airspace within which the 

operation will take place and how that airspace fits into the National Airspace System (NAS). That 

knowledge can be and is gained primarily through ground school and not through flight training in 

fixed wing or rotor aircraft, nor is it dependent on the acquisition of a commercial or private pilot's 

·certificate. Those certificates demonstrate knowledge of the factors and skills needed for the safe 

operation of those types of aircraft (fixed wing or rotorcraft). It cannot be assumed that a 

commercial pilot, approved to operate a helicopter or fixed wing aircraft, has the skill or ability to 

safely operate a small unmanned aerial vehicle, operating at 400 AGL or lower, within strictly 

controlled pre-approved airspace. Besides knowledge of airspace regulations, dexterity in the 

control and operation of the sUAS acquired from actual operation of the aircraft is the most 

important factor in establishing an equivalent level of safety. 

If the PIC has acquired the necessary knowledge of airspace requirements, the relevant issues 

are (1) where the aircraft will be flown, (2) the size of the aircraft relative to what is being used 

today to accomplish the same mission, and (3) what precautions will be taken to ensure the 

safety of those in the area of operation. We propose that the PIC is a pilot with an FAA airman 

certificate, has the necessary knowledge of airspace requirements and has the skill to 

masterfully operate the sUAS within all the manufacturers safety requirements; the aircraft be 

operated within a secure environment; and that no one be allowed to enter the secure 

environment unless they are part of the operation, have been fully briefed of the risks prior to 

operation of the sUAS, and have consented to the risks associated with being in the operating 

area. Should there be a mishap, the sUAS being flown pose significantly less of a threat than the 

helicopters and fixed wing aircraft now being employed because they are a fraction of the size, 

carry no flammable fuel, do not carry crew or passengers, and pose an infinitesimal risk to others. 

This is in stark contrast to conventional aircraft that are flown to the site, carry explosive fuel, 

carry passengers and crew, and operate in a much larger area. 

From a practical standpoint, there are relatively few licensed full-scale aircraft pilots who are also 

qualified to fly the type of sUAS that are utilized for assessment image-capture operations. There 

are even fewer commercial pilots that can fly these sUAS - to the point that to do both is 

considered rare. Assuming that it is unlikely for a company to find a pilot that has both 

qualifications, that company would either have to source a qualified sUAS pilot to train and obtain 

a commercial certificate, or find a commercial certificated pilot who would be willing to learn to fly 

a sUAS to the competency level required for professional use. 

5 
Minimum requirements for the PIC include: 

1. A pilot with an FAA airman certificate and minimum of a class Ill medical; 

2. A minimum of 200 flight cycles and 25 hours of total time as a sUAS rotorcraft pilot and 

at least 10 hours logged as a sUAS pilot with a similar sUAS type (single blade or 

m ultirotor ); 

3. A minimum of 5 hours as sUAS pilot with the make and model of sUAS to be utilized for 

operations under the exemption and 3 takeoffs and landings in the preceding 90 days; 

4. Have undergone a qualification process as specified in the Flight Operations & 

Procedures Manual consisting of a knowledge & skill test of the aircraft to be used. 

A-C-T intends to use commercially available sUAS Components for sUAS. These sUAS systems 

will be tested for quality and safety in our test facility before being deployed to the field. The 

sUAS is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, and operates 

exclusively within a secured area. We have a routine maintenance schedule to verify that the 

sUAS will remain in safe and operational condition. Please see Appendix B, for Specific Types 

ofsUAS. 

A-C-T Safety Operations & Procedures Overview: 

Technology Considerations: 

Best-in-class, tried and proven technologies that are in advanced iterations. Software from 

highly-reputable industry partners will include features: 

1. Auto descent (landing) if communication signal were to be severed. If the sUAS 

loses communications, the sUAS will have capability to return to a pre-determined 

location within the Security Perimeter and land. 

2. Auto descent (landing) if battery were to drop lower than nominal level. 

3. Flights will be terminated at 25% battery power reserve. 

4. Live video for operator gives real-time positioning feedback. In other words, we can 

monitor the scene from the vehicle's perspective for collision avoidance, and to 

maintain spatial orientation. 

5. The sUAS will have the capability to abort a flight in case of unpredicted obstacles 

or emergencies. 

6. On-Screen-Display (OSD) contains operating information to ascertain vehicle health 

at all times: speed, altitude, number of GPS satellites (when available), heading and 

voltage. 

7. GPS lock supplies for return-to-home (RTH). Should Command and Control (C2) 

link failures occur (highly improbable), vehicle returns automatically to the point of 

launch. 

8. Altitude information will be provided to the sUAS pilot via a digitally encoded 

telemetric data feed, which downlinks from the aircraft to a ground-based on-screen 

display. This altitude information will be generated by equipment installed on board 

the aircraft, using GPS triangulation, or digitally encoded barometric altimeter, or 

radio altimeter, or any combination thereof. Prior to each flight, a zero altitude 

initiation point will be established and confirmed for accuracy by the pilot. 

Mechanical/Physical: 

1. We will fly line-of-sight (LOS) only. The vehicle will always remain in direct LOS to 

the pilot, thus eliminating the concern of signal severance (flying behind 

objects/walls). 

2. The sUAS will weigh less than 55 lbs. and travel at less than 50 knots. 

3. Batteries should far exceed the capacity required for actual flight time. 

6 
4. Flights will be operated at an altitude of no more than 400 feet AGL. 

5. Fireproof bags for storage and charging of high capacity Lipo batteries on-site. 

6. UA operated under this exemption will be marked in accordance with 14 CFR part 

45 or as otherwise authorized by the FAA. 

Personnel: 

1. Spotters ensure safe operation and act as a redundant set of eyes for operators 

(pilot, gimbal op, director). 

2. Radio spectrum analysis for interference on the frequencies utilized for vehicle 

control/communication. 

3. A briefing will be conducted in regard to the planned sUAS operations prior to each 

day's activities. It will be mandatory that all personnel who will be performing duties 

within the boundaries of the safety perimeter be present for this briefing. 

4. The operator will obtain the consent of all persons involved in the sUAS operations 

and ensure that only consenting persons will be allowed within 100 feet of the flight 

operations. 

5. Observer and pilot will at all times be able to communicate by voice. 

6. Written and/or oral permission from the relevant property holders will be obtained. 

7. Pilot and observer will have been trained in operation of UAS generally and 

received up-to-date information on the particular UAS to be operated. 

Operations: 

1. The unmanned aircraft (UA) must weigh less than 55 pounds (25 Kg), including energy 

source(s) and equipment. Operations authorized by this petition of exemption are 

limited to the following aircraft described in Appendix B or equivalent. 

2. The UA may nat be flown at a ground speed exceeding 50 knots. 

3. Flights must 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 UA must be operated within visual line of sight (VLOS) of the PIC at all times. This 

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

corrective lenses. 

5. All operations must 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. The operator's manual included as Appendix C and this petition of exemption must be 

maintained and made available to the Administrator upon request. If a discrepancy 

exists between the conditions and limitations in this exemption and the procedures 

outlined in the operator's manual, the conditions and limitations herein take precedence 

and must be followed. Otherwise, the operator must follow the procedures as outlined 

in its operator's manual. 

The operator may update or revise its operator's manual. 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. If the operator determines that 

7 
any update or revision would affect the basis for which the FAA grants this petition for 

exemption, then the operator must petition for amendment to their exemption. The 

FAA's UAS Integration Office (AFS-80) may be contacted if questions arise regarding 

updates or revisions to the operator's manual. 

7. Prior to each flight the PIC must 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, must be included in the preflight inspection. All maintenance and 

alterations must be properly documented in the aircraft records. 

8. Any UAS that has undergone maintenance or alterations that affect the UAS operation 

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

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

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

The requirements and procedures for a functional test flight and aircraft record entry 

must be added to the operator's manual. 

9. The operator must 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 must be established and identified in the operator's manual. At a 

minimum, requirements for the following must be included in the operator's manual: 

a. Actuators I 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; 

10. The Pilot In Command (PIC} must possess an FAA airman certificate, at least a class 

Ill medical certificate and the necessary knowledge of airspace requirements and have 

the skill to masterfully operate the sUAS within all the manufacturers safety 

requirements. 

11 . Prior to operations conducted for the purpose of infrastructure inspections, the PIC 

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

minimum of 200 flight cycles and 25 hours of total time as a UAS rotorcraft pilot and at 

least 10 hours logged as a UAS pilot with a similar UAS type (single blade or 

multirotor}. Prior documented flight experience that was obtained in compliance with 

applicable regulations may satisfy this requirement. Training, proficiency, and 

experience-building flights can also be conducted under this petition of exemption to 

accomplish the required flight cycles and flight time. During training, proficiency, and 

experience-building flights, all persons not essential for flight operations are considered 

nonparticipants, and the PIC must operate the UA with appropriate distance from 

nonparticipants in accordance with 14 CFR § 91 .119. 

8 
12. Prior to operations conducted for the purpose of inspections, the PIC must have 

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

of five hours as UAS pilot operating the make and model of UAS to be utilized for 

operations under the exemption and three take-offs and three landings in the preceding 

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

flights can be conducted under this petition of exemption to accomplish the required 

flight time and 90 day currency. During training, proficiency, experience-building, and 

take·off and landing currency flights all persons not essential for flight operations are 

considered nonparticipants, and the PIC must operate the UA with appropriate distance 

from nonparticipants in accordance with 14 CFR § 91 .119. 

13. Prior to any flight operations authorized by this petition of exemption, the PIC and VO 

must have successfully completed a qualification process, as outlined in the operator's 

manual. As this is a requirement stipulated by the operator, the test must be developed 

and implemented by a qualified person designated at the sole discretion of the 

operator. A record of completion of this qualification process must be documented and 

made available to the Administrator upon request. 

14. Prior to operations conducted for the purpose of inspections, a flight demonstration, 

administered by an operator·approved and -qualified pilot must be successfully 

completed and documented. This documentation must be available for review upon 

request by the Administrator. Because the knowledge and airmanship test 

qualifications have been developed by the operator, and there are no established 

practical test standards that support a jurisdictional FAA FSDO evaluation and 

approval of company designated examiners, the petitioner will conduct these tests in 

accordance with the operator's manual. 

15. The UA 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. 

16. Regarding the distance from participating persons, the operator's manual has safety 

mitigations for authorized and consenting personnel. At all times, those persons 

must be essential to the operations. 

17. Regarding distance from nonparticipating persons, the operator must ensure that no 

persons are allowed within 200 feet of the area except those consenting to be 

involved and necessary for the infrastructure inspection operations. This provision 

may be reduced to no less than 1 00 feet if it would not adversely affect safety and 

the Administrator has approved it. For example, an equivalent level of safety may 

be determined by an aviation safety inspector's evaluation of the inspection area to 

note terrain features, obstructions, buildings, safety barriers, etc. Such barriers may 

protect nonparticipating persons (observers, the public, news media, etc.) from 

debris in the event of an accident. 

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

pre-determined location within the security perimeter and land or be recovered in 

accordance with the operator's manual. 

9 
19. The UAS must abort the flight in the event of unpredicted obstacles or emergencies 

in accordance with the operator's manual. 

20. Each UAS operation must be completed with 25% battery power remaining. 

21. The operator must obtain an Air Traffic Organization (ATO) issued Certificate of 

Waiver or Authorization (COA) prior to conducting any operations over 200 feet 

AGL under this petition of exemption. This COA will also require the operator to 

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

less than 48 hours prior to the operation. 

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

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

be as large as practicable. 

23. The operator must develop procedures to document and maintain a record of the 

UAS maintenance, preventative maintenance, alterations, status of 

replacement/overhaul component parts, and the total time in service of the UAS. 

These procedures must be added to the operator's manual. 

24. Each UAS operated under this exemption must comply with all manufacturer Safety 

Bulletins. 

25. The operator must develop UAS technician qualification criteria. These criteria must 

be added to the operator's manual. 

26. The preflight inspection section in the operator's manual must be amended to 

include the following requirement: The preflight inspection must account for all 

discrepancies, i.e. inoperable components, items, or equipment, not covered in the 

relevant preflight inspection sections of the operator's manual. 

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. At least three days before a scheduled inspection over 200 feet AGL, the operator of 

the UAS affected by this exemption must submit a written Plan of Activities to the 

local FSDO with jurisdiction over the area of proposed infrastructure inspection. The 

3-day notification may be waived with the concurrence of the FSDO or if it 

associated to emergency activities. The plan of activities must include at least the 

following: 

a. Dates and times for all flights; 

b. Name and phone number of the operator for the UAS infrastructure 

inspection operations conducted under this petition of exemption; 

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

operation of the UAS; 

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

e. Name and certificate number (if applicable) of UAS PIGs involved in the 

inspection event; 

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

10 
owners and/or local officials to conduct the infrastructure inspection 

event; the list of those who gave permission must be made available to 

the inspector upon request; 

g. Signature of exemption-holder or representative; and 

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

area, city, town, county, and/or state over which an inspection will be 

conducted and the altitudes essential to accomplish the operation. 

29. The documents required under 14 CFR §§ 91.9 and 91 .203 must be available to the 

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

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

enforcement official upon request. 

30. The UA must remain clear and yield the right of way to all other manned operations 

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

activities, parasailing activities, hang gliders, etc.). 

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

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

Flights under special visual flight rules (SVFR) are not authorized. 

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

33. 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. 

34. The UA may not operate in Class B, C, or D airspace without written approval from 

the FAA. The UA may not operate within 5 nautical miles of the geographic center of 

a non-towered airport as denoted on a current FAA-published aeronautical chart 

unless a letter of agreement with that airport's management is obtained, and the 

operation is conducted in accordance with a NOTAM as required by the operator's 

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

to the Administrator upon request. 

35. 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. Further flight 

operations may not be conducted until the incident, accident, or transgression is 

reviewed by AFS-80 and authorization to resume operations is provided. 

11 
Support for Petition for Exemption 

In accordance with the procedural requirements of 14 C.F.R. §11 .81, A-C-T provides the 

following information: 

Contact Information: 

Jeff Kincart 

Vice President 

American Compliance Technologies, Inc. 

1875 West Main Street 

Bartow, FL 33830 

(863) 533-2000 x246 

jkincart@A-C-T.com www.A-C-T.com 

Regulatory Provisions from which A-C-T seeks an Exemption 

A-C-T believes it may need an exemption from the following prov1s1ons to conduct the 

contemplated operations. In some instances, relief is needed because relief from another 

provision renders compliance with the regulation at hand infeasible. 

333 Aircraft Exemption Status 

14 C.F.R. §61 .3(a) and (c) 

14 C.F.R. §61 .113(a) and (b) 

14 C.F.R. §91 .109 

14 C.F.R. §91.119(b) and {c) 

14 C.F.R. §91.121 

14 C.F.R. §91 .151 

14 C.F.R. §91.405(a) 

14 C.F.R. §91 .407(a) 

14 C.F.R. §91.409(a)(1 )&(2) 

14 C.F.R. §91.417(a)&(b) 

A-C-T believes an exemption is only needed from the above-listed regulatory provisions. To the 

extent that the FAA believes that additional relief is required for A-C-T to conduct the operations 

described here, we request an exemption from any such regulatory provisions as well.4 

The Extent of Requested Relief and the Reasons Relief is Needed 

Section 333 Aircraft Exemption Status: 

Section 333 of the Modernization Act authorizes the FAA to exempt aircraft from the 

requirement for an airworthiness certificate based on a consideration of the size, weight, 

speed, operational capability of the particular UAS, as well as its proximity to airports and 

populated areas. An analysis of these criteria demonstrates that the sUAS operated without 

an airworthiness certificate in the areas and under the conditions contemplated by A-C-T will 

be at least as safe, or safer, than a conventional aircraft {fixed wing or rotorcraft) operating 

with an airworthiness certificate without the conditions proposed in this request. 

The sUAS is less than 55 lbs. fully loaded, carries neither a pilot nor passenger, and 

4 For example, 14 C.F.R. §91 .417{a) imposes certain maintenance record keeping requirements "as 

applicable". Since none of the underlying requirements {e.g., inspection intervals} can be met and will require 

an exemption, A-C-T believes a separate exemption should not be required for §91.417(a). 

12 
operates exclusively within a secured area. Unlike other civil aircraft, operations under this 

exemption will be tightly controlled and monitored by the operator and observer. Operations 

will be conducted in compliance with the FAA and with local public safety requirements to 

provide security for the area of operation as is now done during assessment and inspection 

activities. These safety enhancements provide an expanded degree of safety to the 

assessors over conventional operations. Lastly, application of these same criteria 

demonstrates that there is no credible threat to national security posed by the sUAS, due to 

its size, speed of operation, location of operation, lack of explosive materials and inability to 

carry a substantial external load. 

Given the size and limited operating area associated with the aircraft to be utilized by the 

Applicant, this meets the requirements of an equivalent level of safety under Part 11 and Section 

333 of the Reform Act. The Federal Aviation Act (49 U.S.C.§44701 (f)) and Section 333 of the 

Reform Act both authorize the FAA to exempt aircraft from the requirement for an airworthiness 

certificate, upon consideration of the size, weight, speed, operational capability, and proximity to 

airports and populated areas of the particular sUAS. In all cases, an analysis of these criteria 

demonstrates that the UAS operated without an airworthiness certificate, in the restricted 

environment and under the conditions proposed will be at least as safe, or safer, than a 

conventional aircraft (fixed wing or rotorcraft) operating with an airworthiness certificate without 

the restrictions and conditions proposed. 

14 C.F.R. §61.113(a) and (b) 

§61.113 Private pilot privileges and limitations: Pilot in command 

(a) Except as provided in paragraphs (b) through (h) of this section, no person who 

holds a private pilot certificate may act as pilot in command of an aircraft that is 

carrying passengers or property for compensation or hire; nor may that person, 

for compensation or hire, act as pilot in command of an aircraft. 

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

aircraft in connection with any business or employment if: 

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

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

A-C-T anticipates initially using a cadre of specially trained staff to conduct the sUAS operations. 

Some of these pilots may hold a private pilot license and not hold a commercial pilot licenses. 

The sUAS will not carry property for compensation or hire since they will be used solely to assist 

in the safe evaluation of emergency response operations, environmental and infrastructure 

assessments, and compliance audits for our clients; however, the employees' operation of the 

sUAS will not be incidental to their employment with A-C-T, and they will be compensated for 

such work. Without an exemption, the private pilot would be required to hold a commercial pilot 

certificate under §61.133. However, the risk associated with the contemplated operations is less 

than the risk posed by a traditional aircraft The sUAS will fly at altitudes well below the 

permissible limits for other civil aircraft, eliminating the risk to other aircraft, and within a 

geographical envelope under the sole control of A-C-T clients. Accordingly, the risk would be 

limited to A-C-T personnel, who will be appropriately outfitted in safety gear, and A-C-T client's 

property on the ground. Requiring a commercial pilot certificate would provide no appreciable 

safety benefrt and would needlessly impose additional cost on A-C-T. Because the contemplated 

operations would not comply with §61 .113(b )( 1) and none of the other exceptions to paragraph 

(a) apply, relief is needed from both paragraphs (a) and (b). 

13 
14 C.F.R. §91 .109 

§91.1 09 Flight Instruction; simulated instrument flight and certain test 

(a) No person may operate a civil aircraft (except a manned free balloon) that is 

being used for flight instruction unless the aircraft has fully functioning dual 

controls. 

(b) An airplane equipped with a single functioning control wheel that controls the 

elevator and ailerons ... 

(c) No person may operate a civil aircraft in simulated instrument flight unless ... 

(d) No person may operate a civil aircraft being used for a flight test. .. 

A-C-T requires relief from 14 C.F.R. §91.109 because aUASs, by their design, do not have fully 

functional dual controls. Flight control is accomplished through the use of a control box that 

communicates with the aircraft via radio communications. 

Aircraft being considered for use by A-C-T allow the UAS Instructor to place the aircraft into 

'loiter' mode (fixed altitude stationary hold). In the event of the student losing control, the UAS 

Instructor can quickly and via alternate equipment (equipment not in the hands of the student) 

place the aircraft into a mode that then allows the instructor to bring the aircraft back into 

control and back to the pre-determined and/or safe landing location. It is not applicable to the 

sUAS being operated for purposes of this exemption. There are not dual controls associated to 

sUAS operations so this section is not applicable to operation of the sUAS. 

14 C.F.R. 91.119{c) 

§91.119 Minimum safe altitudes: General 

Except when necessary for takeoff or landing, no person may operate an aircraft below 

the following altitudes ... 

(c) Over other than congested areas. An altitude of 500 feet above the surface, 

except over open water or sparsely populated areas. In those cases, the aircraft 

may not be operated closer than 500 feet to any person, vessel, vehicle, or 

structure ... 

A-C-T submits that it requires relief from §91.119 for the minimum altitudes listed in paragraph 

(b) and {c). Relief is required from paragraph (b) for flights over a congested area due to the 

potential response to hazardous materials emergency response operations or assessment 

activities at client owned facilities where there could be an assembly of many people. 

Operations of the sUAS will always take those situations into account in its flight operations plan 

for that event and notify the people in the area of any safety requirements. Relief is required 

from paragraph (c) because assessment activities conducted at 500 feet or higher is 

insufficiently distinct to be meaningful. Since operations at this altitude also pose a heightened 

risk of collision with another aircraft, safety can only be assured through the grant of an 

exemption. The anticipated rotorcraft operations should be adequately addressed by paragraph 

(d) (1 ). Additionally, relief should not be needed from paragraph (a} because an emergency 

landing of the aircraft due to a power failure will not create an undue hazard to persons or 

property on the surface. As noted in the explanation of why an exemption will not adversely 

affect safety, A-C-T clients typically have exclusive use of the land over which the sUAS will be 

operated, and public access is restricted in most situations, except potentially in emergency 

response situations. As such, the risk of injury is minimal. 

14 
14 C.F.R. 91 .121 

14 C.F.R. §91.121 Altimeter Settings 

This regulation requires each person operating an aircraft to maintain cruising altitude 

by reference to an altimeter that is set " .. . to the elevation of the departure airport or an 

appropriate altimeter setting available before departure." 

As the sUAS may not have a barometric altimeter, but instead a GPS altitude read out, an 

exemption may be needed. An equivalent level of safety will be achieved by the operator, 

pursuant to the Manual and Safety Check list, confirming the altitude of the launch site shown on 

the GPS altitude indicator before flight. Altitude information will be provided to the sUAS pilot 

via a digitally encoded telemetric data feed, which downlinks from the aircraft to a groundbased on-screen display. This altitude information will be generated by equipment installed 

on board the aircraft, using GPS triangulation, or digitally encoded barometric altimeter, or 

radio altimeter, or any combination thereof. Prior to each flight, a zero altitude initiation point 

will be established and confirmed for accuracy by the pilot. 

14 C.F.R. 91 .151 

§91.151 Fuel requirements for flight in VFR conditions 

(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 speed1. During the day, to fly after that for at least 30 minutes. 

(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 .. . 

Operating the sUAS in a pre-defined area with less than 30 minutes of reserve fuel does not 

raise the type of risk contemplated by §91 .151 , i.e., that an aircraft could run out of fuel in the 

event it has to be flown to an alternate airport or circle the planned airport in the event of 

unanticipated conditions. A-C-T does not intend to use the sUAS for point-to-point flights and 

will not operate the sUAS beyond visual line of sight. Nor will the sUAS require an airport in 

order to land. Rather, A-C-T will operate the sUAS using pre-planned flight paths (taking into 

account weather conditions) designed to allow the sUAS to fly to the point of intended landing. 

As such, there is no need for a time-based excess fuel requirement. Rather it should be 

sufficient to require only as much additional excess flight capacity as necessary to safely land 

the sUAS. We believe that a 25% battery reserve is more than sufficient to meet this objective. 

14 C.F.R. 91.405(a), 91 .407(a) (1). 14 C.F.R. 91.409(a) (1)&(2) and 14 C.F.R. 91.417(a) & (b) 

§91.405 Maintenance required 

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; ... 

§91.407 Operation after maintenance, preventive maintenance, rebuilding, or 

alteration 

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

rebuilding, or alteration unless15 
1. It has been approved for return to service by a person authorized under 

§43.7 of this chapter ... 

§91.409 Inspections 

{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 ... 

§91.417 (a) & (b) 

A-C-T believes that an exemption from these three maintenance requirements is appropriate 

because the FAA has not developed maintenance standards that would allow an operator to 

meet the part 91 maintenance requirements. In particular, there are no individuals authorized by 

the FAA to approve a sUAS for return to service under §91.407(a} or to conduct the initial 

airworthiness and annual return to service inspections required by §91.409(a}. A-C-T will 

maintain the aircraft as instructed in the owner's manual and ASTM F2909, where applicable, 

and will not operate the aircraft until it has reasonably determined that any needed repairs have 

been made. However, because of the technical impossibility of meeting the requirements of 

§§91.405(a), 407{a), 409(a) and 417(a)&(b), we believe an exemption from these provisions is 

appropriate. 

Please do not hesitate to contact me at the phone number or via the e-mail address provided 

above should you have any questions or concerns. 

ysubmitted, 

Kin cart 

V ce President 

American Compliance Technologies, Inc. 

16 
APPENDIX A 
Appendix A 

Summary for Federal Register Publication 

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

Register should the FAA determine that publication is needed. 

Petitioner: American Compliance Technologies, Inc. (A-C-T) 

Sections of 14 C.F.R. Affected: 333 Aircraft Exemption Status 14 C.F.R. §61.113(a) and (b) 

14 C.F.R. §91.109 

14 C.F.R. §91.119(b) and (c) 14 

C.F.R. §91.121 

14 C.F.R. §91.151 

14 C.F.R. §91.405(a) 

14 C.F.R. §91 .407(a) 

14 C.F.R. §91.409(a)(1 )&(2) 14 

C.F.R. §91.417(a)&(b) 

Description of Relief Sought: 

Petitioner seeks relief from the requirements of 333 Aircraft Exemption Status, 14 C.F.R. 

61 .113(a)&(b), 91 .109, 91 .119(a)&(c), 91 .121, 91.151, 91.405(a), 91.407(a), 91 .409(a), and 

91.417(a)&(b) to conduct sUAS operations over A-C-T's Client's owned or controlled land, 

solely during daylight hours, to assist in the evaluation of emergency response operations, 

environmental and infrastructure assessments, and compliance audits for our clients. In 

general, sUAS operations are typically intended to be conducted in areas remote from both 

congested areas and airports. The nature of operations anticipated by A-C-T requires that the 

sUAS be flown at relatively low altitudes. A-C-T expects that in most instances, the sUAS will 

be flown less than 200 feet along the path of the of the assessment area, and in no instances 

will be flown higher than 400 feet above the ground. Accordingly, the risk of interference with 

other aircraft is minimal. 
APPENDIX 8 
Appendix B 

Specific type, make, and model 

DJIINSPIRE 1 

1 Aircraft Dia{ilr~~ 

[f. 

Re·mote Controller o;agram 

[1) GPS 

f21 f!'ropcller (1"'17) r~.·, . 

,-

~. . [3, ,J Motor 

[4 l 

[!..j f4) Pron1 ~.l:D (P12') 

f5) LB. "'drng gear 

{61 Gimbal nr:::l Camero (P35) 

[3 [71 ln·~lltge-t Fl:g""llt Battery (~18) 

~~ ~i {8] A1rcrnft MiO"c-USB Port 

[9] Hear LlO.D W1 2) 

[10~ Ca•Tmr~ M cro-USB ~ort 

[11 1 Camera Mlcro-SD Gard Slo1 ~35) 

t t2j 

· 131 (12) Visio"t l~'tt::m: ng Sensors ld,116) 

:~131 Aircraft Sta'll;.~s ln:t cato~ (~';')13) 

1,) Antennas (P29) 

Relays a•!"Craf'; conlrol and video signal. 

[2) Mohjffil Oevlo9 Holder 

Mo.; nting pla~e for yo.Jt mobile oav ::e. 

lb~~;;t--r- -- ~ (3] Control Stick 

Gon-:rols ai?c a~ oriC" t.atior. .. 

!4] Re1urn Hor.r~e (RTt-1) EJutto:n (IP13) 

! •ross .and hold tho button to in'tta-e Ho· . .:m to 

t ;,T.'le (All ~). 

t51 Transformation Sw:itch (P27j 

·1 oggle the vw tch up o• down to •~Ji.; c or la!/'o"-Cr 

t'le la"''ding gea-. 
[61 Bauery l.evt<!l LEOt; 

D; splayb. the curtent bate y level. 

[7] Status LED 

o·splays the ro ... ver status. 

[10] Camera Senlngs D•al 

~8] P!'tWeJ B•i,~f\¢il 

u~b!d :a PO'•uer or1 o pow~· ·o"i the ~emote co·~bollw. 

(S] RTH LED 

Circule: l.CO arounci 1he RTii button displays Ri~·~ stat .IS. 

Turn f1e d1al ~o ad~u&t can:1era se~t~r.gs. 

Only fu~c~; • .::ms when !-:.a remnte oon~roller •~ 

con-:.:ctGo~ to a mobil~;: dfNIC(' rum ing the:' OJ I 

Pilo~aop. 

[111 Playback Button 

[15] ---+I~~:::J;.~=:r----'"'7~-~--[1~] [h) Atll---[11] 

Playback th13 cap:LJrad imRges or vidoos. 

[12] ShuUex Button 

r•ress to take a photo. If m burs': moue. the 

SQt nH'l1b~r of pho-':Os will bo taken with cma 

press. 

[13] FligL'lt Modo Switch 

Used to sw'tcll bt'l\.veen P, A a"'ld F mode. 

(14] Video Recording Biitton 

F,ress to start reoording video. Press ag:3ln to 

stop re(".ordt"'g. 

[1 5] Gimbal Dial 

Uoo this dial to oon•rol ~'le tilt of tr.e glrr.oal, 

(16] .Min,..I~DM] Pon 

Co:'"lnact an ~iD co'Tlpat;ble manito~ to tris 

port ''J ge~ a live HD video prev1ew o1 wh~ the 

cam0ra sees. 

[17] Micro-USB P·ort 

Fo~ connoctinH the rernclc controller to yo_.r 

computer. 

(18} CAN B11s Po:t 

Reserved for ~1JL; .. re .. !ie. 

[ 19} USB Port 

'----WJ] 

Con1act to mobile davies to access all of t"'a 

DJI P:lot app co:-ttrols a·1o features. 

[20} ClPS Module 

[2CJ USBd ~o pinpont the loc:aton o• tho romotc 

controUe•. 

i) 

See Attached Flight Manuals: 

DJIINSPIRE 1 User Manual V1.8 

[21] Back left Button 

Custo'nl:~ablc butt:m i, OJI Pilo: a.np, 

(~2J Power Port 

Con ·,~t:!t to a po.OJ.at :!Sou·ce \0 charge the 

rcma':C comrollcr s i~Jtomal ba~f'')', 

(231 Back Right Button 

Cu:;;;to'Tlizable button ir, DJII)ilc~ a.pp, 

DJI INSPIRE 1 Maintenance Manual_ v1.0 

2 
INSPIRE 1 

User Manual [vfaJ 

2075.9 
Using this manual 

Legend& 

0 Warning & Important {): Hints and Tips [;r;J Reference 

· Before Flight 

The following tutorials and manuals have been produced to ensure you to make full use of your Inspire 1. 

1 .Disclaimer 

2.1n the Box 

3.1nspire 1 Quick Start Guide 

4.Safety Guidelines 

S.lnspire 1 User Manual 

6.1ntelligent Flight Battery Safety Guidelines 

Watching all the tl1orial videos and reading the Disclaimer before flight is recommended. Afterwards, 

prepare for your first flight by using the Inspire 1 Quick Start Guide. Refer to this manual for more 

comprehensive information. 

: Watch the v1deo tutonals 

Please watch the tutorial video below to learn how to use Inspire 1 correctly and safely: 

www.dji.com/product/inspire-1Mdeo 

: Download the OJI GO app 

Download and install the DJI GO app before use. Scan the QR code or visit 

"http://m.dji.net/djigo" to download the app. 

raa ~ 

~ ~ For the best experience, use mobile device with Andriod V 4.1 .2 or above. Requires iOS 8.0 or later. 

2 
Contents 

Using this manual 

Legends 

Before R ight 

Watch the video tutorials 

Download the DJI GO app 

Product Profile 

Aircraft 

Introduction 

Feature Highlights 

Assemble the Aircraft 

Aircraft Diagram 

Remote Controller Diagram 

Flight Controller 

Right Mode 

Flight Status Indicator 

Return to Home (RTH) 

Dynamic Home Point 

Vision Positioning System 

Flight Recorder 

Attaching and Detaching the Propellers 

DJI Intelligent R ight Battery 

Remote Controllers 

Remote Controller Profle 

Remote Controller Operations 

Dual Remote Controllers Mode 

Remote Controller Status LED 

Unking the Remote Controller 

Remote Controller Compliance Version 

2 

2 

2 

2 

2 

5 

6 

6 

6 

9 

9 

11 

12 

12 

12 

13 

15 

16 

17 

17 

18 

23 

24 

24 

29 

31 

32 

33 

3 
Gimbal and Camera 34 

Camera Profile 35 

Gimbal 36 

DJIGOApp 39 

Camera 40 

Library 43 

Explore 43 

Me 43 

Flight 44 

Flight Environment Requirements 45 

Flight Ll mils and Flig hi Restriction Area 45 

Preflight Checklist 49 

Calibrating the Compass 49 

Auto Take-off and Auto Landing 50 

Starting/Stopping the Motors 51 

Flight Test 51 

FAQ 53 

Appendix 56 

Specifications 57 

Intelligent Flight 60 

How to Update Firmware 61 

FCC Compliance 62 

4 
Product Pro1Ue 

This chapter describes the features of 

Inspire 1, instructs you to assemble the 

aircraft and explains the components on 

the aircraft and remote controllers. 
Product Profile 

: Introduction 

The Inspire 1 is brand new quadcopter capable of capturing 4K video and transmitting an HD video 

s!gnal {up to 21<m) to multiple devices stralght out of the box. Equipped with retractable landing gear, it 

can capture an unobstructed 360 degree view from its camera. The buit-in camera has an integrated 

g:mbal to maximize stability and weight efficiency while minimizing space. When no GPS signal is 

available, Vision Positioning technology provides hovering precision. 

:Feature Highlights . . .. 

Camera and Gimbal: vp to 4K video recording and 12 rnegapixel photo capture. Reserved ll1Cll-'1ting 

space fcr NO filters for better exposure control. New quick-release mount allows you to remove the 

camera with ease. 

HD Video Downlink: Loolatency, HD downlink powered by an enhanced version of the DJI Lightbrldge 

system. It also provides dual controllers mode. 

Landing gear: Retractable landing gear that enables an lJ'lObstructed panOI'amic view from the camera. 

DJI Intelligent Flight Battery: 4500 mAh DJI Intelligent Right Battery employs new battery cells and a 

battery management system. 

Fight Controller: The next generation fliltlt controller system provides a mOI'e reliable flight experience. 

A new flight reccrder stores the ffight data from each flight, and Vision Positioning enhances hovering 

precision when no GPS is available. 

· Assemble the Atrcraft 

Unlocking Travel Mode 

The alrcraft is in Travel Mode during delivery. Folloo these steps to change it to Landing Mode before 

your first flight: 

1. Insert the Intelligent Right Battery into the battery compartment. 

2. Power on the Remote Controller and the Intelligent Flight Battery. 

3. Toggle the Transformation Switch up and down at least four times. 

4. Pooer off the aircraft. 

Travel Mode Togglex4 Landmg Mode 

6 
INSPIRE 1 User Manual 

&. • Battery must be fully cha~ged before using it for lhe ~irst time. Refer to 'Charging t~e Intelligent 

Flight Battery' (P21) for more information . 

• If you have purchased the dual remote controller version, you must use the Master remote 

controller to deactivate Travel Mode. Refer to 'Setting Up Dual Remote Controllers Mode' (P30) 

section for more infromation about Master remote controller . 

• Be sure to remove the gimbal from the aircraft before switch from Landing Mode to Travel Mode . 

• Place the aircraft on the smooth and reflective surface (e.g. table or tile) before switching between 

the travel modes to the landing mode. Do not place the aircraft on the rough and sound-absorbing 

surface (e.g. carpet) before switchng between the travel modes and landing mode. 

lnstaUing Gimbal and camera 

1. Remove Gimbal Cover. 

2. Rotate the Gimbal Lock to the unlocked position (to the right when facing the nose of the aircraft). 

3. Insert the gimbal by aligning the white mark on the Gimbal. 

4. Rotate the Gimbal Lock back into the locked position. 

···•··•·· 

Ju., .... Gimbal Cover 

«i 

&. Ensure the Micro-SO card is correctly Inserted into the camera. 

Attaching Propellers 

Attach propellers with the black nut onto motors with the black dot and spin counter-clockwise to secure. 

Attach propellers with gray nut onto motors without a black dot and spin clockwise to secure . 

• or . . ,_.~u,.... m::1 r,, ,1 7 
INSPIRE 1 User Manual 

& Place all propellers onto the correct motor and tighten by hand to ensure security before flight. 

Attaching 1345s Quick-Release Propellers 

The 1345s Quick-Release propeller is the upgrade version of the propellers that greatly enhance the 

reliability of the propeller during the flight. Following the steps below to attach the 1345s Quick-Release 

propellers. 

1. Install the propelers with a white dot onto the ll'lOU1ting plates that have a white dot, and install the 

propellers without a white dot onto the mounting plates that do not have a white dot. 

2. Align the hook (A) on the propellers with the securing spring (B), then press down the propeller onto 

the mounting plate then rotate the propellers according to the lock direction until it is secured. 

Preparing Remote Controller 

Tilt the Mobile Device Holder to the desired position then adjust the antema as shown. 

1. Press the button on the side of the Mobile Device Holder to release the clamp, adjust it to fit then attach 

your mobile device. 

2. Connect your mobile device to the remote controller with a USB cable. 

3. Plug one end of the cable into your mobile device, and the other end into the USB port on the back of 

the remote controller. 

8 
A1rcraft D1agram 

- --·-·· [1] 

[6]--

[11] 

• Remote Controller D1ag_r~m 

INSPIRE 1 User Manual 

[1] GPS 

[2] Propel:er (P17) - - --- [2] 

. --. ·- [3] [3] Motor 

·---[4] 

[4] Front LED (P12) 

[5] Landing gear 

[6] Gimbal and Camera (P35) 

---[9] (7] Intelligent Flight Battery (P18) 

[10] (8] Aircraft Micro-USB Port 

[9] Rear LED (P12) 

[10] Camera Micro-USB Port 

[11) Camera Micro-SO Card Slot (P35) 

[13] [12] Vision Positioning Sensors (P16) 

[13] Aircraft Status Indicator (P13) 

[1] Antennas (P29) 

Relays aircraft control and video signal. 

[2] Mobile Device Holder 

Mounting place for your mobile device. 

[3] Conlrol Stick 

Controls aircraft orientation. 

[4] Return Home (RTH) Button (P13) 

Press and hold the button to initiate Return to 

Home(RTH). 

[5] Transformation Switch (P27) 

Toggle the switch up or down to raise or lower 

the landing gear. 

9 

-o 

0 

a. 

c 

~ 

-o 

g 

ro 
INSPIRE 1 User Manua! 

[6] Battery Level LEOs (6] Power Button 

Displays the current battery level. 

{7) Status LED 

Used to power on or power off the remote controUer. 

[9) RTH LED 

Displays the power status. Circular LED around the RTH button displays RTH status. 

[10) Camera Settings Dial 

Turn the dial to adjust camera settings. 

Only functions when the remote controller is 

comected to a mobile device running the OJI 

GOapp. 

[11] Playback Button 

Playback the captured images or videos. 

[12] Shutter Button 

Press to take a photo. If in burst mode, the 

set number of photos will be taken with one 

press. 

[13) Flight Mode Switch 

Used to switch between P, A and F mode. 

[14] Video Recording Button 

Press to start recording video. Press again to 

stop recording. 

[15] Gimbal Dial 

Use this dial to control the ti~ of the gimbal. 

[16] Mini·HDMI Port 

Connect an HD compatible monitor to this 

port to get a live HD video preview of what the 

camera sees. 

[17] Micro·USB Port 

For connecting the remote controller to your 

computer. 

.----------·-- {20] 

/ 

---- {21] 

[22]---

10 

[16] 117] [18] {19] 

1 1s1 _ _.(! , r-..r.;-nr:::;----'?i;r.;::'lt'l_ - [1o1 

[14] ·--- -- {1 1] 

[13 ] ·-

[18] CAN Bus Port 

Reserved for future use. 

(19] USB Port 

-- [12] 

Connect to mobile device to access all of the 

DJI GO app controls and features. 

[20] GPS Module 

Used to pinpoint the location of the remote 

controller. 

[21) Back Left Button 

Customizable button In OJI GO app. 

[22] Power Port 

Connect to a power source to charge the 

remote controller's internal battery. 

[23] Back Right Button 

C:.JStom:zable button in DJI GO app. 
Aircraft 

This chapter describes the features of 

the Flight Controller, Vision Positioning 

System and the Intelligent Flight Battery. 
Aircraft 

Flight Controller 

The Inspire 1 's flight controller is based on DJI flight controller with several enhancements such as new 

flight mode and new safe mode. Three safe modes are available: Failsafe, Return Home and Dynamic 

Heme Point. These features ensure the safe return of your aircraft if the cor.trol signal is lost. A flight 

recorder stores crucial flight data for each fUght. 

Flight Mode 

Three flight rrodes are available. The details of each flight mode are found in the section below: 

P mode (Positioning) : P mode works best Yklen GPS signal is strong. There are three different states of P 

rrode, which wil be automatically selected by the Inspire 1 depending on GPS signal strength and Vision 

Positioning sensors: 

P-GPS: GPS and Vision Positioning both are available, and the aircraft is using GPS for pos~lon ng. 

P-OPTI: Vision Positioning is available but the GPS signal is not. Aircraft is using only Vision 

Positioning for hovering 

P-ATII: Neither GPS or Vision Positioning available, aircraft is using only its barometer for positioning, 

so only altitude is controlled. 

A mode (Attitude): The GPS and Vision Positioning System is not used for holding position. The aircraft 

only uses its barometer to maintain altitude. If ~Is still receiving a GPS signal, the aircraft can automatically 

retum home if the Remote Controller signal Is lost and if the Home Point has been recorded sucoessfully. 

F mode (Function): Intelligent Orientation Control (lOC) is activated in this mode. For more Information 

about IOC, refer to the IOC in Appendix. 

,lj: Use the Flight Controller rrode switch to change the flight mode of the aircraft, refer to the "Flight 

Mode Switch" on P27 for more Information. 

: Flight Status Indicator 

The INSPIRE 1 comes with the Front LED, Rear LED and Aircraft Status Indicator. The positions of these 

LEOs are shoNn in the ftgure belo\N: 

,- ·-----"''craft Status Indicator 

Front LED Rear LED 

The Front and Rear LE~ show the orientation of the aircraft. The Front LED cftsplays solid red and the 

Rear LED displays solid green. 

Aircraft Status Indicator shows the system status of the flight oontroler. Refer to the table beloo for more 

ir:formation about the Aircraft Status Indicator: 

12 
Aircraft Status Indicator Descnpt1on 

Normal 

R G :Y. ······Red, Green and Yellow Rash 

Alternatively 

~ !'(: ... Green and Yellow Flash Alternatively 

::t;,. ······Green Flashes Slowly 

'(D(2 .. ·· Green Flashes Twice 

y. ······Yellow Flashes Slowly 

Wam1ng 

.'Y, ...... Fast Yellow Flashing 

:F'l· • · · Slow Red Flashing 

''R· ······ Fast Red Flashing 

.R·. ···· Red Flashing Alternatively 

.B -Solid Red 

INSPIRE 1 User Manual 

Power on and self-check 

A1rcrafi warm1ng up 

Safe to Fly (P mode with GPS and Vision Positioning) 

Safe 10 Ay (P rnode ''lith Vision Positioning but withoui GPS) 

Safe to Fly (A mode but No GPS and Vision Positioning) 

Remote Controller Signal Lost 

Low Battery Warning 

Critical Low Battery Warning 

IMU Error 

Critical Error 

~<.): · • · Red and Yellow Rash Alternatively Compass Calibration Required 

Return to Home (RTH) 

The Return to Home (RTH) brings the aircraft back to the last recorded Home Point. There are three cases 

that will trigger RTH procedure; they are Smart RTH, Low Battery RTH and Failsafe RTH. 

GPS 

Home Point 

Smart RTH 

Descnpt1on 

The Home Point is the location at which your aircraft takes off when the 

GPS signal is strong. You can view the GPS signal strength through 

the GPS icon ( ~lillt ). If you are using the Dynamic Home Point 

setting, the Home Point will be updated to your current position as you 

move around and when the Aircraft Status Indicator blinks green. 

Using the RTH button on the remote controller (refer to "RTH button" on P28 tor more information) or the 

RTH button in the DJI GO app when GPS is available to enables smart RTH. The aircraft return to the 

latest recorded Home Point, you may control the aircra~'s orientation to avoid collision during the Smart 

RTH. Press the Smart RTH button once to start the process, press the Smart RTH button again to ex!t 

Smart RTH and regain the control. 
INSPIRE 1 User Manual 

Low Battery RTH 

The low battery level failsafe is triggered when the DJI Intelligent Flight Battery is depleted to a point that 

may affect the safe return of the aircraft. Users are advised to return home or land the aircraft immediately 

when these warnings are shown. DJI GO app will advise user to return the aircraft to the Home Point 

when low battery warning is triggered. Aircraft will automatically return to the Home Point if no action is 

taken after 10 seconds COIJ1tdown. User can cancel the RTH by pressing once on the RTH button. The 

thresholds for these warnings are automatically determined based on the current aircraft altitude and its 

distance from the Hlome Point 

Aircraft will land automatically if the current battery level can only support the aircraft to land to the ground 

from the current altitude. User can use the remote controller to control the aircraft's orientation during the 

landing process. 

The Battery Level indicator is displayed In the DJI GO app, and is described below 

Critical Low banery level Suflte~<ont bar.~ 1· 

warning(Red) levei(Goeen) 

I ~~~ ~:,~~~ g l Remaining floght tirrb 

---L--··-----L---,-·- -~·····-:L . ?ewer 

to retum 

rc.qui~·es home 

~ 

Batleoy level indocator 

Battery Level Remark Arcraft Sldtus DJIGOapp Aght lnstrucbOns 

Wamng Indicator 

Tap "Go-horne" to have 

the aircraft return to the Fly the aircraft 

Home point and land back and land 

Low battery 

The battery Aircraft status automatically, or "Cancel" to it as soon as 

level warning power is low. indicator blinks resLme nonnal flight. II no possible, then Please land the action is taken, the aircraft 

aircraft. RED slowly. will automatically go home stop the motors 

and land after 1 0 seconds. and replace the 

Remote controller will sound battery. 

an alarm. 

Cntlcallow The ancrafi A1rcr aft siat\.os 

The [JJI GO app scrEltlf\ wjl The arrcrafl: 

batte>ry level musi land rndrcator blrn~'l flash red and alfCraft starts to '¥111 begtn to 

descend Remote controller descend a.nd land 

warnng mmedtaiely RED quiCkly Will sound an alatm automattcally 

Estimated Estimated 

remaining remai~g fig."t N/A N/A N/A 

based on et;rrent tlg,ttime battery level. 

14 
INSPIRE 1 User Manual 

'~ • When the c ritical battery level warning activates and the aircraft is descending to land 

automatically, you may push the throttle upward to hover the aircraft and navigate it to a more 

appropriate location for landing. 

• Color zones and markers on the battery level indicator ~eflect estimated remaining flight time 

and are adjusted automatically, according to the aircraft's current status. 

Failsafe RTH 

Failsafe RTH is activated automatically if remote controller signal (including video relay signal) is lost for 

more than 3 seconds provided that Home Pont has been successfully recorded and compass is working 

normally. Return home process may be interrupted and the operator can regain oontrol over the aircraft if 

a remote controller signal is resumed. 

Failsafe Illustration 

1 Record Home P01nl (HP) 2 Confirm Home POint 3 Remote Controller Signal Losi 

y ,_,11111 

~ • 

Blinking Green Blinking Green Fast Blinking Yellow 

4 Signal Lost Lasts 3secs. 5 Go Home(20m can be set) 6 L.and1ng after Hovenng 15secs 

. ... 

·i~t;.;;~;,· ................. ~·.;.:;. Y , 

~ J :.r. Elt-' .. ltlf!t(, :!O:"Tiy 

IIJ) IW...Cll~ -"'" 1Lf'<• 20tll 

..,.... 

~ ~ Fast Blinking YeUow Fast Blinl<ing Ye!km Fast Blinking YePow 

& • Aircraft automatically descends and lands if RTH is triggered when the aircraft flies within a 20 

meter (65 feet) radius of the Home Point. 

• Aircraft cannot avoid obstruction during the Failsafe RTH, therefore it is ifll)Ortant to set an 

reasonable Failsafe altitude before each flight. LaLnCh the DJI GO app and enter "Camera" 

view and select "MODE" to set the Failsafe alt~ude . 

• Aircraft will stop ascending and immediately return to the Home Point if you move the throttle 

stick if the aircraft reaches 20 m altitudes or beyond during Failsafe. 

, -··· 

. Dynamic Home Pomt . . . 

Dynamic home point is useful in situations when you are in 

motion and require a Home Point that Is different from the 

takeoff point. GPS module is located at the position shown in 

the figure below: 

& Ensure the space above the GPS module is not 

obstructed when using Dynamic Home Point 

15 
INSPIRE 1 User Manual 

There are two options for Dynamic Home Point 

1. Set the aircraft current coordinate as the new Home Point. 

2. Set the remote controller's coordinate as the new Home Point. 

Setting Up Dynamic Home Point 

Follow the steps below to setup Dynamic Home Point: 

1. Connect to the mobile device and launch the OJI GO app and go to the "Camera• page. 

2. Tap''"and select"j,", to reset the remote controller's coord!nates as the new Home Point. 

3. Tap''"and select"4t", to reset the aircraft's coordinates as the new Home Point. 

4. The aircraft status indicator blinks green to show Home Point is set successfully. 

VISIOn PoSitiOning System 

DJI Vision Positioning is a positioning system that uses ultrasonic and image data to help the aircraft 

identify its current position. With the help of Vision Positioning, your Inspire 1 can hover in place more 

precisely and fly indoors or in other environments where there is no GPS signal available. The main 

canponents of DJI Vision Positioning are located on the bottom ot your lnspife 1, including [1]two sonar 

sensors and[2]one monocular camera. 

Using VISion Posnioning 

Vision Positioning is activated automatically when the Inspire 1 is powered on. No manual action is 

required. Vision Positioning is typically used in the indoor environment where no GPS Is available. By 

using the sensors on the Vision Positioning system, Inspire 1 can perform precision hovering even when 

no GPS is available. 

~ / 

-y- ~ 

''=/ 

__ / ~ '·....,_ 

16 
INSPIRE 1 User Manual 

Follow the steps below to use Vision Positioning: 

1. Toggle the switch to "P" as shown the figure to the right: 

2. Place the Inspire 1 on a flat surface. Notice that the Vision Positioning system 

cannot work properly on surfaces without pattern variations. 

3. Power on the Inspire 1. The aircraft status Indicator w~l flash twice in green light, 

which indicates the Vision Positioning sys1em is ready. Gently push the throttle up 

to lift off, and the Inspire 1 will hover in place. 

& The performance of your Inspire 1's Vision Positioning System is subject to the surface you are 

flying rNer. The ultrasonic waves may not be able to accurately measure the distance rNer SOU1d 

absort>ing materials, and the camera may not function correctly in suboptimal envirorments. The 

aircraft will switch from •p• mode to "A" mode automatically if both GPS and VISion Positioning 

System are not available. So operate the aircraft cautiously when in any of the following situations: 

• Flying rNer monochrome SlJ'faces (e.g. pure black, pure white, pure red, ptr"e green}. 

• Flying rNer a highly reflective SlJ'faces. 

• Flying at high speeds( over Bmts at 2 meters or over 4m/s at 1 meter). 

• Flying rNer water or transparent surfaces. 

• Flying over mrNi"lg surfaces or objects. 

• Flying in an area where the lighting changes frequently or drastically. 

• Flylng rNer extremely dark (lux< 10} or bright (lux> 1 0,000) surfaces. 

• Flying over surfaces that can absorb sound waves (e.g. thick carpet}. 

• Flying over surfaces without clear patterns or texture. 

• Flying over surfaces with identical repeating patterns or textures (e.g. tiles with same design). 

• Flying rNer inclined surfaces that will deflect sound waves away from the aircraft. 

• In the event of loss of remote controller's signal, the aircraft will hover for 8 seconds and then 

auto-land if it is in "P" mode. 

:ft- • Keep the sensors clean at all times. Dirt or other debris may adversely affect the effectiveness 

of the sensors. 

• The effective hovering altitudes of the aircraft is from 0 to 2.5 meters. 

• VIsion Positioning system may not function properly when the aircraft is flying rNer water. 

• Vision Positioning system may not be able to recognize pattern on the ground in low light 

conditions (less than 1 OOiux). 

• Do not use other lAtrasonlc devices with frBQJenCY of 40 KHz when Vision Positioning system is 

in operation. 

• Vision Positioning system may not be able to stabilize the aircraft when flylng close to the 

ground (below 0.5 meters) in fast speed. 

0 Keep the animals away from the aircraft when Vision Positioning system is activated. The sonar 

sensor emits high frequency sound that is only audible to some animals. 

.~~IQ~~- ~e~rder Flight data is automatically stored in the internal storage device of the aircraft. User can gain access to 

ttlese data through the DJI GO app. This includes flight duration, orientation, distance, aircraft status 

information, speed, and other parameters. 

; ~".a.~~~ ~d [)~t~c~~~. th& Pr~pe~~~~

use only DJI approved propellers with your inspire 1. The grey or black nut on the propeller i"ldicates 

the rotation drection ol the propeller and where it should be attached. To attach the propellers property, 

17 
INSPIRE 1 User Manual 

match the nut with the dots on the motors of your Inspire 1: 

Propelers Grey cap(1345) Bltl.ck cap(1345R) 

Figure ==::: c::= co:::=·•~ 

Attach On Motors without a black dot Motors wrth a black dot 

Legends a'l Lock :Tum the propeUers in the ndicated direction to mount and tighten 

'b""r Unlock :Tum the propellers in the indicated direction to loosen and remove 

Attaching the Propellers 

1. Attach the propellers with a grey nut onto a motor without a black dot and spin the propellers clockwise 

to secure them in place. Attach the propellers with a black nut onto a motor with a black dot and spin 

the propellers counter clockwise to secure its position. Be sure to completely tighten each propeller by 

hand before flight. 

& · Ensure propellers are attached to its corresponding motors, otherwise the aircraft camd take off. 

• Handlilg the propellers with care. 

• Manually tighten each of the propellers on the corresponding rrotors to ensure l is attached fimiy. 

Detaching the Propellers 

Hold the motor still. Then spin the propeller in the unlock direction indicated on the propeller itself. 

Detaching 1345s Quick-Release Propelers 

Press the 1345s Quick-Release propellers downward firmly then rotate the propeller in the unlock 

direction to unlock the propellers. 

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

• Ensure that al! propellers are in good condition before each tnght. DO NOT use old, chipped, 

or broken propellers. 

• To avoid injury, STAND CLEAR of and DO NOT touch propellers or rrotors when they are spinning. 

• ONLY use orig!nal DJI propellers for a better and safer flight experience. 

~~ 1 l_nteiDgent_ ~~~~h! ~~ry _ 

The DJI Intelligent Right Battery has a capacity of 4500mAh, votage of 22.2V, and smart chargedischarge fulctionality. It can only be charged with an appropriate OJI approved charger. 

lntellogent Flig ht Battery Charger 
INSPIRE 1 User Manual 

& Battery must be fully charged before using !t for the first time. Refer to 'Charging the l:1telligent 

Right Battery' P21 for more information . 

OJ! Intelligent Right Battery Functions 

1. Battery Level Display: LEOs display the current battery level. 

2. Battery Life Display: LEDs display the current battery power cycle. 

3. Auto-discharging Function: The battery automatically discharges to below 65% of total power when it 

is idle (press the power button to check battery level will cause battery to exit idle state) for more than 

10 days to prevent swelling. It takes around 2 days to discharge the battery to 65%.1t is normal to feel 

moderate heat emitting from the battery during the discharge process. Discharge thresholds can be 

set n the DJI GO app. 

4. Balanced Charging: Automatically balances the voltage of each battery cell when charging. 

5. Over charge Protection: Charging automatically stops when the battery is fully charged. 

6. Temperature Detection: The battery will only charge when the temperature is between 0 •C(32•F) and 

4o•c (104"F). 

7. Over Current Protection: Battery stops charging Ykoen high amperage (more than 10A) is detected. 

8. Over Discharge Protection: Discharging automatically stops when the battery voltage reaches 18V to 

prevent over-discharge damage 

9. Short Circuit Protection: Automatically cuts the power supply when a short circuit is detected. 

10. Battery Cell Damages Protection: DJI GO app shows warning message when damaged battery cell 

is detected. 

11. Battery Information History: Show the last 32 entries of battery information records that ilclude wamng 

messages and so on. 

12. Sleep Mode: Sleep mode is entered after 10 minutes of inactivity to save power. 

13. Communication: Battery voltage, capacity, current, and other relevant information is provided to the 

aircraft's to the main controller. 

& Refer to Disclaimer and Intelligent Right Battery Safety Guide/ins before use. Users take full 

responsibility for all operations and usage. 

Using the Battery 

Powering ON/OFF 

Powering On: Press the Power Button once, then press agaJn and hold for 2 seconds to power on. The 

Power LED wili turn red and the Battery Level Indicators will display the current battery level. 

Powering OH: Press the Power Button once, then press aga n and hold for 2 seconds to power olf. 
INSPIRE 1 User Manual 

Low Temperature Notice: 

1. The performance of the intelligent Flight Battery is sign\ficantly reduced when flying In a low 

temperature environments (those with air temperatures below 5•C). Ensure that the battery Is fully 

charged and the cell voltage is at 4.35 V before each flight. 

2. Using the Intelligent Flight Battery In extremely low temperature environments (those with air 

temperatures below -10°C) is r.ot recorrrnended. When flying in environments with temperatures 

between 5•c and -1o•c, the Intelligent Rlgrt Battery should be able to achieve the appropriate voltage 

levels (above 4.2 \f), but it is recommended that you apply the included instAation sticker to the battery 

n order to prevent a rapid drop in temperatures. 

3. If the DJI GO app displays the "Critical Low Battery Level Waming" when flying in low temperal1Xe 

environments, stop flying and land the aircraft lrrmediately. Yoo will stil be able to control the aircraft's 

movement when this wamng is triggered. 

4. Store the Intelligent Riltlt Battery in a room temperature environment and ensure that its temperature 

exceeds s•c before using it in the low terTl)erature environment 

5. When using the Inspire 1 in a low temperall.Je envirorment, begin by alowing the aircraft to hOver at a 

low altitude, tor approxmately one minute, to heat 1he battery. 

6. To ensure optinum performance, keep the Intelligent Flight Battery's core temperature above 20•c 

when in use. 

&:. In cold environments, insert the battery into the battery compartment and allow the aircraft to 

warm up for approximately 1-2 minutes before taking off. 

Checking the battery level 

The Battery Level Indicators display how much remaining power the battery has. When the battery is 

powered off, press the Power Button once. The Battery Level Indicators will light l.P to display the current 

battery level. See below for details. 

EJ!) The Battery Level Indicators will also show the current battery level during charging and 

discharging. The indicators are defined below. 

~ : LED is on. ~ : LED is flashing. 

~ : LED is off. 

Battery Level 

LED1 LED2 LED3 LED4 Battery Level 

~ ~ <t ~ 87.5%-100% 

~ ~ ~ ~- 75%-87 5% 

~ ~ ~ ~ 62.5%-75% 

... ~ ~ : ~ 50%-625% 

~ ~ ~ ~ 37.5%-50",{, 

~ ~: ~ <( 25%-375% 

~ ~ <t <t 12.5%-25% 

~ <t <t 0%- 125% 

<t ~ ~ ~ =D"k 

20 
INSPIRE 1 User Manual 

Battery life 

The battery life indicates how many more times the battery can be discharged and recharged before 

it must be replaced. When the battery is powered off, press and hold 1he Power Button for 5 seconds 

to check the battery life. The Battery Level Indicators will light up and/or blink as described below for 2 

seconds: 

Battery Life 

LED1 LED2 LED3 LED4 Battery Life 

~ ~ ~ ~ 90%-100% 

-4: ~ ~ ~-- 80%-90% .. 

~ ~ ~ ~ 70%-80% 

·'· ~ ~ ~: ~ 60%-70% 

~ ~ ~ ~ 50%-60% 

~ ~: ~ ~ 40%-50% 

~ ~ ~ ~ 30%-40% 

~- ~ ~ ~ 20%-30% ... 

~ ~ ~ ~ below20% 

.& When battery life reaches 0%, it can no longer be used. 

1:1::J For rrore information about the battery, launch DJI GO app and check 1he infoonation under the 

battery tab. 

Charging the Intelligent Flight Battery 

1. Connect Battery Charger to a power source (10G-240V 50/60Hz). 

2. Open the Protection Cap and connect the Intelligent Flight Battery to 1he Battery Charger. If the battery 

level is above 95%, turn on the battery before charging. 

3. The Battery Level Indicator will display the current battery level during charging. 

4. The Intelligent Flight Battery is fully charged when Battery Level Indicators are all off. 

5. Air cool the Intelligent Right Battery after each flight. Allow its temperature to drop to room temperature 

before storing it for an extended period. 

& • Do not charge the Intelligent Flight Battery and remote controller with standard charger (model: 

A 14-100P1A) at the same time, o1herwise the charger may overheat. 

• Always turn off the battery before inserting it or removing it from the Inspire 1. Never insert or 

remove a battery when it is powered on. 

Power Outlet 

Intelligent Flight Banery Charger 

21 

)> 

~r 

~ 
INSPIRE 1 User Manual 

Battery Level lndll:'ators wh1le Charg1ng 

LED1 LED2 

~-- • • + • ~ ~ 

~-- ~-~ 

·'· ... ~-- ~--

'•' ' •' 

~-- ~--

-=t ~ 

LED3 

~ 

~ 

... 

~--

.. . 

•' • 

~~~ 

~ 

LED4 

~ 

~ 

~ 

· ' · ~--

~ 

Battery Level 

0%-25% 

25%-50% 

50%-75% 

75%-100% 

Fully Charged 

Charging Protection LED Display 

The table below shows battery protection mechanisms and corresponding LED patterns. 

Battery Level Indicators while Charg1ng 

LED1 LED2 LED3 LED4 Blmk•ng Pattern Battery Protection Item 

~ ~-- '•' ~ ~ LED2 blinks twice per second Over current detected 

~ ~: < ~ LED2 blinks .tlree <mes per second Shari circun detected .,. 

~ ~ ~-- ... ~ LED3 blinks twice per second Over charge detected 

~ ~ ~: ~ u:o3 blinks thr!le i1mes per second O"er-voltage charger detected .. 

~ ~ ~ ~-- LED4 blinks twice per second Charging temperature is too low ... (<0°C) 

~ ~ ~ ~- LED4 hlinl<.s three ~mes per second Charg•ng temperaLure 1s too high 

'•' (>40°C) 

After any of the above mentioned protection issues are resolved, press the button to turn ott the Battery 

Level Indicator. Unplug the Intelligent Flight Battery from the charger and plug it back in to resume 

charging_ Note that you do not need to unplug and plug the charger in the event of a room temperature 

error, the charger will resume charging when the temperature falls within the normal range. 

& OJI does not take any responsibility for damage caused by third-party chargers. 

~ How to discharge your Intelligent Right Battery: 

22 

To effectively calibrate the battery capacity, it is recommenced to charge and discharge the 

battery thoroughly for every 1 0 charge-and-discharge cycle. User should install the battery onto 

the aircraft and then power on the aircraft to initiate the discharge process, discharge the battery 

until the aircraft is powered off automatically. User should then fully charge the battery to ensure 

the battery is working at its optimal. 

Slow : Place the Intelligent Flight Battery into the Inspire 1 's Battery Compartment and power it 

on. Leave it on u~l there is less than 5% of power left, or until the battery can no lo~ger 

be turned on. Launch the DJI GO app to check battery level. 

Rapid: Ay the Inspire 1 outdoo~s until there is less than 5% of power left, or until the battery can 

no longer be turned on. 
Remote Controllers 

This chapter describes the features 

of the remote controller that includes 

aircraft and remote controller operations 

and dual remote controller mode. 

~ l C'J1 ,.11 '' r~,. 23 
::0 

(!) 

3 

0 

$' 

0 

0 

;a. 

Q. 

co 

til 

Remote Controller 

Remote Controller Profile 

The Inspire 1 Remote Controller is a multi-function wireless communication device that integrates the 

video downlink ground system and aircraft Remote Controller system. The video downiink and aircraft 

Remote Cootroller system operate at 2.4 GHz with maximum transmissioo distance of 5 km. The remote 

controller features a nurrber of camera flTICtions, such as taking and previewing photos and video, and 

controlling gimbal motions. The remote controller is powered by a 2S rechargeable battery. The current 

battery level is displayed by LEOs on the front panel of the remote control. 

Eel 

& 

• Compliance Version: The Remote Controller is compliant with both CE and FCC regulations. 

• Operating Mode: Control can be set to~ 1 , Mode 2. 

• Mode 1: The right stick serves as the throttle. 

• Mode 2: The left stick serves as the throttle. 

Do not operate more than 3 aircrafts within in the same area (size equivalent to a soccer field) to 

prevent transmission interference. 

Remote Controller Operations . . .... 

Powering On And Off The Remote Controller 

The Inspire 1 remote controller is powered by a 2S rechargeable battery with a capacity of 6000mAh. The 

battery level is indicated by the Battery Level LEOs on the front panel. Follow the steps below to power on 

your remote controller: 

1. When powered off, press the Pcmer Button once and the Battery Level LEOs will display the current 

battery level. 

2. Then, press and hold the Pcmer Button to pavo~er on the remote controller. 

3. The Remote Controller will beep when it powers on. The Status LED will blink green (slave remote 

controller blinks solid purple) rapidly, Indicating that the remote controler is lili<Jng to the aircraft. The 

Status LED will show a solid green light when linking is completed. 

4. Repeat step 2 to power off the remote controller after finish usi:-~g it. 

Charging Remote Controller 

Charge the remote controiler via supplied charger. 
INSPIRE 1 User Manual 

rr=--~~:¢,.8 

PonM Outlet 

Power Button 

Controlling Camera 

Shoot videos or images and adjust camera settings via the Shutter Button, Camera Settings Dial, Playback 

Button and Video Recording Button on the remote control. 

--- {1) 

{4) - ·- - ---- {2) 

[1] Camera Settings Dial 

Tum the dial to quickly adjust camera settings such as ISO and shutter speed without letting go of the 

remote controller. Move the dial button to left or right to view the pictures or videos in playback mode. 

[2] Playback Button 

Press to view images or videos that have already been captured. 

[3] Shutter Button 

Press to take a photo. If bli'SI mode is activated, mtJtiple photos will be taken with a single press. 

[4] Reooding Button 

Press once to start recording video, then press again to stop recording. 

Controlling Aircraft 

This section explains how to use the various features of the remote controller. The Remote Controller is set 

to Mode 2 by default 

25 
INSPIRE 1 User ~anua! 

f!)!J Stick NeutraV mid point: Control sticks of the Remote ControRer are p!aced at the central position. 

26 

Move the Stick: The control stick is pushed away from the central position. 

Remote 

Controller 

(Mode2) 

Aircraft 

( o 1ncfJCales nose direction) Remarks 

Moving the left stick up and down changes the 

aircraft's elevation. 

Push the stick up to ascend and down to descend. 

Push the throttle stick up to takeoff. 

When both sticks are centered, the Inspire 1 will 

hover in place. 

The more the stick is pushed away from the 

center position, the faster the Inspire 1 will change 

elevation. Always push the stick gently to prevent 

sudden and unexpected elevation changes. 

Moving the left stick to the left or right controls the 

rudder and rotation of the aircraft. 

Push the sick left to rotate the aircraft counter 

clock-wise, and push the stick right to rotate the 

aircraft clockwise. If the stick Is centered, the 

I 

Inspire 1 will stay facing its current direction. 

The more the stick is pushed away from the center 

position, the faster the Inspire 1 will rotate. 

Moving the right stick up and down changes the 

--;:,~~~~~~p:;-1 aircraft's forward and backward pitch. 

• Push the stick up to fly fOIWard and down to fly 

0 

backward. The Inspire 1 will hover in place if the stick 

is centered. 

Push the stick fu1her away from the center position for 

a larger plch angle (maximum 35') and faster flight. 

l 

Moving the right stick control left and right changes 

the aircraft's left and right pitch. 

Push left to fly left and right to fly right The Inspire 1 

I 

will hover in place if the stick is centered. 

Push the stick further away from the center position for 

a larger p~ch angle (maximum 35") and faster flight. 

Gimbal Dial: Tum the dial to the right, and the 

camera will shift to porn upwards. Tum the 

dial to the left, and the camera will shift to point 

\ downwards. The camera will remain in its current 

position when dial is static. 
Flight Mode Switch 

Toggle the switch to select the desired flight mode. 

You may choose between: P mode, F mode and A 

mode. 

F19ure AghtMode 

F 4b Frnode 

A cL-S F. mode 

~ Pmode 

INSPIRE 1 User Manual 

P mode (Positioning) : P mode works best when GPS signal is strong. There are three different states of P 

mode, which wift be automatically selected by the Inspire 'i depending on GPS signal strength and Vision 

Positioning sensors: 

P-GPS: GPS and Vision Positioning both are avaiable, and the aircraft is using GPS for positioning. 

P-OPTI: Vision Positioning is available but the GPS signal is not. Aircraft is using only Vision 

Positioning for hoverng 

P-ATTI: Neither GPS Of Vision Positioning available, aircraft Is using only its barometer for positioring, 

so only alt~ude is controlled. 

A mode (Attitude): The GPS and Vision Positioning System is not used for holding pos~ion. The aircraft 

only uses ~s barometer to maintain altitude. If~ is stil receiving a GPS signal, the aircraft can automatically 

return home if the Remote Controller signal is lost and if the Home Pont has been recorded successfully. 

F mode (Function): Intelligent Orientation Control (IOC) is activated in this mode. For more information 

about IOC, refer to the IOC in Appendx. 

The Flight Mode Switch is locked in P mode by default. To unlock the switch, launch the DJI GO app, 

enter the ·camera' page, tap 'MODE', and then activate "Multiple Right Mode" . 

Transformation Switch I RTH Button 

The Transformation Switch I RTH Button combilation serves two functions. Toggle the sw~ch up or down 

to raise or lower the landing gear. Or, press the button to activate the Return to Home (RTH) procedure. 

Transformation Switch 

This switch has two positions. The effect of toggling the switch to any of these positions is defined below: 

Lower Rei&e 

1. Raise: Raise the landing gear to its upper most position. 

27 

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INSPIRE 1 User Manual 

2. Lower: The landing gear will lower to its lowest position for landi'lg. 

~,~ 

,.--- ~~ --- -~~~,"[] 

.1:, Do not raise the landing gear when the aircraft is on the ground. Ensure the landing gear is 

lowered before landing. 

RTH button 

Press and hold this button to start the Return to Horne (RTH) procedure. The LED around the RTH Button 

will blink white to indicate the aircraft is entering RTH mode. The aircraft will then return to the last recorded 

Home Point Press this button again to cancel the RTH procedure and regain the control of the aircraft 

Connecting Mobile Device 

Tilt the Mobile Device Holder to the desired position. Press the button on the side of the Mobile Device Holder 

to release the clamp, and then place you- mobile device into the clamp. Adjust the clarnp to secL.re your 

mobile device. Then comect your mobile device to the remote controller with a USB cable. Plug one end of 

the cable into you- rrobile deW:e, Md the othe:' end ln1o the USB port on the back of the rerrde controler. 

28 
INSPIRE 1 User Manual 

Optimal Transmission Range 

The signal transmission between aircraft and remote controller perform best within the range that 

displayed in the picture shown below: 

Optimal Tram:misSIOfl Range 

Strong Weak 

, , 

·, 

Ensure the aircraft is flying within the optimal transmission range. Adjust the distance and position 

between the operator and the aircraft to achieve optimal transmission performance. 

: Dual Remote Controllers Mode 

More than one remote controller can connect to the same aircraft in Dual Remote Controller mode. In 

Dual Controllers mode, the "Master" remote controller operator controls the orientation of the aircraft, while 

the "Slave" remote controller controls the movement of the gimbal and camera operation. When multiple 

"slave" remote controllers (max of 6) are connect to the aircraft, only the first connected "slave" remote 

controller is able to control the gimbal, the remaining "slave" remote controller can view the live feed video 

from the aircraft and set the camera parameters, but they cannot control the gimbal . 

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INSPIRE 1 User Manual 

.1:, Use the gimbal dial on the remote controller to control the pitch movement of the camera in the 

s:ngle remote controller mode, however, you camot control the pari movement of the camera. 

Setting Up Dual Remote Controllers Mode 

Dual Remote Controllers mode is disabled by default. Users must enable this feature on the "Master" 

remote controller by through the DJI GO app. Follow the steps below for setup: 

"Master" Remote Controller: 

1. Connect the remote controller to your mobile device and launch the DJI GO app. 

2. Go to the Camera page, and tap ~~ ,ull to enter the remote controller setti'lgs window. 

3. Tap "Set RC Status" to enable Master-and-Slave mode. 

4. Select "Master" in the "Set RC Status" section to set the remote controller as "Master" remote controller . 

• ,t •• ,_ •• ' 

[ RC Control Settings >I Mnw onc1 Slave 

Set RC Status ! OFF Ril Sl•ve ) 

RC Name ! T12254 l Connection Password I 1234 l 

SloveRC List 

5. Enter the connection password for the "Slave" remote controller. 

"Slave" Remote Controller: 

1. Tap "Search for Master Controller" to search the "Master" remote controller. 

· '--" Ufl - I 

[ RC Control Setting >I Muter and Slave 

Sat RC Status I OFF I Master •• 

RCName ! $88642 l 

Request Control 

Sear~ for Master Controller 

Moster RC Ll&t 
INSPIRE 1 User Manual 

Lt. Rern:>te controller cannot link to the aircraft if the rern:>te controller is set as "Slave". Meanwhile, 

the "Slave• remote controller cannot control the orientation of the aircraft. Reset the remote 

controller to "Master" in DJ I GO app If you wish to link the remote controller to the aircraft. 

2. Search the "Master" rern:>te controller in the surrounding area 1

n the "Request Control" section. 

R -,r•l' ' •J . 

I RC Control Settings >I 

Ma-andSiowl 

Set RC Status I OFF I Ma&tar ~'l 

RC Name I S88642 ) 

Request Control 

Search for Master Controller 

Master RC lilt 

[ V' T12254 ) 

3. Select the "Master" remote controller from the "Master RC Ust" and input the connection password to 

connect to the desired "Master· remote controller. 

v T12254 Connection Password 1234 

IAaster RC List 

; Remote Controller Status LED . . 

The Status LED reflects connection status between Remote Controller and aircraft. The RTH LED shows 

the Return to Horne status of the aircraft. The table below contains details on these indicators. 

·--·- ··- RTH LED 

Status LED - - - -· 

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Status LED Alarm 

:1'1' -Solid Red f chime 

·G; -Solid Green f chime 

.:J'j -Solid Purple 

B -Solid Blue D-O-/chime 

. iij': ······Slow Blinking Red 0-D-D· .... · 

:.R ~r·R. y ... Red and Green/ Red and None 

Yellow Alternate Bliri<s 

RTH LED Sol.rld 

~ - Solid Wh~e f chime 

W - Blinking White D · · 

. !if· ...... Blinking White 

Remote Controller Status 

The rerrote controller set as 'Master' but it is not 

connected with the aircraft. 

The remote controller set as 'Master' and 1t IS connected 

with the aircraft 

The remote controler set as 'Slave' but it is not 

connected with the aircraft. 

The remote controller set as 'Slave' and It is connected 

with ·the aircraft . 

Remote controller error. 

HD Downlink IS disrupted 

Remote Controller Si:aius 

Aircraft is returning home. 

Send1ng Return to Home command <o the aircraft . 

Aircraft Retum to Home in progress. 

Lt The Remote Status Indicator will bliri< red, SOU'ld an alert, when the battery level is criticaly low. 

Linkrng the Remote Controller 

The remote controller is linked to your aircraft before delivery. Linking is only required when using a new 

remote controller for the first time. Follow these steps to link a new remote controller: 

1. Power on the remote controller and connect to the mobile device. Launch DJI GO app. 

2. Power on the Intelligent Flight Battery. 

3. Enter "Camera" view and tap on and then tap "Linking Remote Controller" button as shown below. 

32 

Remote Control Calibration > 

Stick Mode > 

Default sUck mode I& Mode 2, changing stick model alters the way the aircraft is controlled. 

Do not change lJI'iess familiar with your new mode. 

C1 I Gimbal PictVYaw C2 I Reset ginbal yaw 

You can customize the C 1 Wld C2 buttons on the back 

of the remota contrOller. 
INSPIRE 1 User Manual 

4. The remote controller is ready to link. The Remote Controller Status Indicator blinks blue and 'beep" 

sound is emitted. 

Remote Control Calibration 

Stick Mode 

Dofau II stic~ mode is Mode 

DonO! 

;1 _1_ II ' I !...• !' l 

> 

> 

Soarc:llltlg tor al~~:raft ~oquency, 

timeout In 54 seconds ircraft is controHe d. 

change unless femili Press the linking button on the aircraft 

C1 I Gimbal Pile 

to link this remote controller 

Cancel 

bal yaw I 

You can customize the C"1 and C2 buttons on the beck 

of the remote controllar. 

5. Locate the Linking button on the front of the aircraft, as shown in the figure shown below. Press the 

Linking button to start linking. The Remote Controller Status Indicator will display solid green if Link is 

succeed. 

& • Remote coreroller cannot link to the aircraft if the remote controller is set as "Slave". Meanwhile, 

the "Slave" remote controller cannot control the orientation of the aircraft. Reset the remote 

controller to "Master" in DJI GO app if you wish to link the remote controller to the aircraft. 

• Remote controller will disconnect from the linked aircraft if a new remote controller is linked to 

the same aircraft . 

.. Remote Controller Compll~nce VerSIOf1 

The remote controller is compliant with both CE and FCC requiremer.ts. 

33 
Gimbal and Camera 

This chapter provides the technical 

specifications of the camera and explains 

the working mode of the gimbal. 
Camera and Gimbal 

·Camera Profrle 

The on-board camera supports 4K video capture up to 4096x2160p24 and 12M pixel photos capture by 

using the 1/2.3 inch CMOS sensor. You may export the video in either MOV or MP4 format for eciting. 

Available picture shooting modes include burst, continuous, and timer mode. A "ve preview of what the 

camera is seeing before you shoot videos and pictures is supported through the DJI GO App. 

Camera Micro-SO Card Slot 

To store your photos and videos, plug in the micro-SO card into the slot shown bela.v before powering on 

the Inspire 1. The Inspire 1 comes with a 16GB micro-SO card and supports up to a 64GB micro-SO card. 

A UHS-1 type micfo-SD card is reccmmended, because the fast read and write capabnity of these cards 

enables you to store high-resolution video data. 

0 Do not remove micro-SO card from the Inspire 1 when ~ is powered on. 

Camera Data Port 

Power on the Inspire 1 and then connect a USB cable to the Camera Data Port to download photos or 

videos from the camera to your computer. 

I 

·-~-

;:~~ .. ~ .. ~ 

- t::" ..=·. 

& Power on the aircraft before atterr.pt:ng to doNnload the files. 

35 
INSPIRE 1 User Manual 

Camera Operation 

Use the Shutter and Record button on the remote controller to shoot the images or the videos through the 

DJI GO app. For more information about how to use these buttons, refer to "Controlling Camera" P25. 

NO Filter 

Attach an ND mer to the front of the camera to reduce over-exposure and "jello" effect. 

.Gimbal 

Gimbal Profile 

The 3-axis Gimbal pr<:Mdes a steady platform for the attached camera, allowing you to capture stabilized 

images and video. The Gimbal can tilt the camera up to 120 degrees and rotate 360 degrees. 

Use the gimbal dial on the remote controller to control pitch movement of the camera by default. Note that 

you cannot control the pan motion of the camera by defau~ . Enable the "Master-and-Slave" mode and 

set the remote controller to "stave" state if you wish to control both the pan and p~ch movement of the 

camera. 

& Use the gimbal dial on the remote controller to control the p~ch movement of the camera in the 

single remote controller mode, however, you cannot control the pan movement of the camera. 

Pan Control 

Follow the instructions below to use the gimbal dial to control the pan movement of the gimbal: 

1. Power on the aircraft and rerrote control, launch DJI GO app and enter "C;;vnera" page. 

2. Tap "RC Control Settings" icon and select either C1 or C2 customizable button as the gimbal p~ch/ 

yaw switching button. 

3. Select "Gimbal Pitclw'Yaw" from the dropdown lis:. 

36 
INSPIRE 1 User Manual 

;; - ,· f'' .':::·''Jt I 

Remote Control CalibraUon > 

Stick Mode > 

Dolaull Slick mode i• Mode 2, changing Slick modes aHers the way the aircraft is controled. 

Do 1\ClC change unless am~i8f whh your f'l6W mode. 

C1 I G!mbal Pitch/Yaw C2 I Reset gimbal yaw 

You can customize 1ho C1 and C2 bullons on the back 

of the remote contrOller. 

Press C1 or C2 button to switch from pitch mode to 'f8'N mode. You may use the girrtlal dial to Pl¥'1 the 

gimbal under yaw mode. Press C1 or C2 again to exit yaw mode.'vVIile pressing the C2 button, tun the 

camera settings dial to fine tune the rol axis ot the gimbal. 

Using DJI GO App to Control Gimbal 

Follow the steps below to use DJI GO app to control the gimbal orientation: 

1. Launch DJI GO app, enter "Camera" page. 

2. Tap and press on the screen until a blue circle is shown. 

3. Slide to control the gimbal orientation within the "Camera" page as shown below. 

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INSPIRE 1 User Manual 

Gimbal Operation Modes 

Three Gimbal operation modes are available. Switch between the different operation modes on the 

Camera page of the DJI GO App. Note that your mobile device must be connected to the remote 

controller for changes to take effect. Refer to the table below for details: 

Follow Mode 

<.1J I 

Pan 

The angle between Gimbal's orientation and aircraft's nose remains 

constant at all times. One user alone can control the pitch motion of the 

Girrbal, but a second user is required to control the pan rrotion using a 

second remote controller. 

The Gimbal will lock to the movements of the aircraft to provide a FlrstPerson-Vlew flying experience. 

The Gimbal's motion is independent of the aircraft's orientation. One user 

alone can control the pitch motion of the Gimbal, but a second user is 

required to control the pan motion using a second remote controller. 

Tap to force the Gimbal orientation to re-align with aircraft's orientation 

by panning from gimbal's current orientation. Pitch angle will remain 

unchanged during the re-alignment. 

&, • Gimbal motor error may occur in these situations: (1) Gimbal is placed on uneven ground. (2) 

Gimbal has received an excessive external force, e.g. a collision. Please take off from flat, open 

ground and protect the gimbal after powering up. 

38 

• Flying in heavy fog or cloud may make the gimbal wet, leading to a temporary failure. The 

gimbal will recover when it dries out. 
DJI GO App 

This chapter describes the four main 

GUI of the OJI GO app. 

39 
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DJI GO App 

The DJI GO app is a new mobile app designed specifically for the Inspire 1. Use this app to control the 

gimbal, camera and other features of your flight system, The app also comes with Map, Store a User Center, 

for configuring your aircraft and sharing your content with friends. It is recommended that you use a tablet 

tor the best experience. 

INSPIRE 1 

•.camera 

The Camera page contains a live HD video feed from the Inspire 1's camera You can also configure 

various camera parameters from the Camera page. 

[10] 

40 
INSPIRE 1 User M anual 

[1) Flight Mode 

~: The text next to this icon indicates the current flight mode. 

Tap to configure the MC (Main Controller) Settings. These sef.ings allow you to modify flight limits and 

set the gain values. 

[2] GPS Signal Strength 

~IIIII: This icon shows the current strength of GPS signals. Green bars indicate adequate GPS 

strength. 

[3) IOC Settings 

~ CL: This icon displays the IOC setting v.tlen the aircraft has entered F-mode. Tap to view the IOC 

setmgs menu and select the desired IOC setting. 

[4] System Status 

*'"'Rot<GPSI : This icon indicates the current aircraft system status and GPS signal strength. 

[5) Battery Level Indicator 

- - • : The battery level indicator provides a dynamic display of the battery level. The colored 

zones on the battery level indicator represent the power levels needed to carry out different functions. 

[6) Remote Controller Signal 

fi'Jo ,1

111: This icon shows the strength of remote controller's signal. 

[7) HD Video Unk Signal Strength 

~ ,ul~ This icon shows the strength of the HD video downlink connection between the aircraft and 

the remote controller. 

[8) Battery Level 

& 100%: This icon shows the current battery level. 

Tap to view the battery information menu, set the various battery warning ttv"esholds, and view the 

battery warning history. 

[9) General Settings 

:: : Tap this icon to view the General Settings page. Fronn this page, you can set fig,! parameters. 

reset the camera, enable the quick view feature, adjust the gimbal roll value. and toggle the flight 

route display. 

[1 0) Camera Operation Bar 

Shutter and Recording Settings 

9: Tap to enter various camera value settings, including color space for the recording, resolution 

IX the videos, image size ar.d so on. 

Shutter 

e : Tap this button to take a single photo. Press and hold this button to select single shot, triple shot 

or time-lapsed shooting modes. 

41 

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INSPIRE 1 User Manual 

Record 

0 : Tap once to start recording video, then tap again to stop recording. You can also press the 

Video Recording Button on the remote controller, which has the same functionality. 

Playback 

[8 : Tap to enter the playback page. You can preV.ew pho!os and videos as soon as they are 

captured. 

Camera Settings 

~;::Tap to set ISO, shutter and auto exposure values of the camera. 

[11 ) Map 

Display the ffight path of the current fight. Tap to switch from the Camera GUI to tf1e Map GUI. 

[12] Aircraft Distance 

I. : The distance of the aircraft from the Horne Point. When the aircraft is near the gound, this icon 

will change to.& to display the height the Vision Position System's sensors from the ground. 

[13] Flight Telemetry 

The Vision Positioning Status icon Is highlighted when the Vision Positioning Is In operation. 

Right attitude is indicated by the flight attitude icon. 

(1) The red arrow shows which direction the aircraft is facng. 

(2) light blue and dark blue areas indicate pitch. 

(3) The angle of the boundary between the light blue and dark blue areas Indicates the roll angle. 

[14] Home Point Settings 

f : Tap this button to reset the current home point. You may choose to set the aircraft takfH)ff 

location, the remote controler's current position, or the aircraft's current position as the Home Point. 

[15] Return to Home (RTH) 

£ : Initiate RTH home procedure. Tap to have the aircraft return to the latest home point. 

(16] Gimbal Operation Mode 

Refer to "Gimbal Operation Mode" P38 for more information. 

[17] Auto Takeoff/Landing 

i t:f: : Tap to init!ate auto takeoff or landing. 

42 
INSPIRE 1 User Manual 

[1 8) Livestream 

«:) : Livestream icon Indicates the current video feed is broadcasting live on YouTube. Be sure the 

mobile data service is available on the mobile device. 

(19) Back 

~ :Tap to return to the main GUI. 

Library 

View, edit and share your artwork all in one place. The Library has a range of simple but powerful tools 

that let you edit your videos and photos before sharing them online, minutes after they are captured. 

Explore 

Rnd out about our latest events, featured products and trending Skypixel t.ploads in the Explore page. 

Me 

If you already have a OJI account, you will be able to participate in forum discussions, earn Credits in the 

OJI Store, and share your artwork with the community 

43 

0 

c... 
Flight 

This chapter describes the flight safety 

and flight restrictions. 

« 
Flight 

Once pre-flight preparation is complete, It Is recommended to use the flight simulator to learn how to fly 

safely. Ensure that all flights are carried out In a suitable location. 

Fhght Environment Requirements 

1. Do not use the aircraft in severe wea~her conditions. These include wind speed exceeding 10l"TVs 

snow, rain and smog. 

2. Oriy fly in open areas. Tal buildings and steel struct11es may affect the accuracy of the on-board 

compass and GPS signal. 

3. Avoid from obstacles, cruwds, ligh voltage power lines, trees or txxies of water. 

4. Minimize electromagnetic interference by not flying in area with high levels of electromagnetism, 

including mobile phone base stations or radio transmission towers. 

5. Aircraft and battery performance is subject to environment factor such as air density and temperature. 

Be very careful when flying 14700 feet (4500 meters) or more above sea level as battery and aircraft 

performa1ee may be reduced. 

6. The Inspire 1 cannot operate within the polar areas in "P" mode. 

1- • •• 

. Flight Limits and Flight Restriction Area 

Aight limits on height and distance can be set. The details of these flight limits are described in the following 

section. 

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

the ICAO (International Civil Aviation Organization), FAA and their own national airspace regulations. For 

safety reasons, the flight limits function is enabled by defaut to help users use this product safely and 

legaly. The flight limits function includes height limits, distance linits and No Ay Zones. 

When operating in P Mode, height, distance Mmits and No Ay Zones work together to ma."lage fUght. In A 

mode only height lmits work and fMQhts cannot go higlerthan 120 meters. 

Max Height & Radius Linits 

Max Height & Radius limit flying height and a1stance, and the user may change these settings in the 

DJI GO App. Once cOI'fl)lete. your Inspire 1 will fly in a restricted cylinder that is determined by these 

settings. The tables below show the details of these limits. 

Max Height Max Radius 

Home Point 

....1.1....._.---+- Height ol aircratt 

when powered on 

45 
:!! 

INSPIRE 1 User Manual 

GPS S1gnaiStrong ·G. • Blinking G1een 

Max Height 

Max Radius 

Flighl Umits 

Flight altli:ude muse be und~r 

the set height. 

Flight distance must be within 

the max radius. 

DJI GOApp 

Warning He~ght 

limrt reached 

Warning: Distance 

limit reached. 

GPS Signal Weak ·Y • • • Bllnkmg Yelow 

Flight Umits DJI GOApp 

Max Height Aight he1gh< restriCted to 

120m anc under 

Wam1ng Height lmti 

reached 

Aircraft Status Indicator 

None 

Rapid red flashing r, 

······when close to the 

max radius limit 

Aircraft Status Indicator 

None. 

ce· Max Radius No limits 

::r 

&. • If you fly out of the limtt, you can still corrtrol the Inspire 1, but cannot fly it further. 

• If the Inspire 1 flies out of the max radius In Ready to Fly (non-GPS} mode, it will fly back within 

range automatically. 

No-Fly Zones 

All No-Ay Zones are listed on the DJI official website at http://flysafe.dji.corn'l'l<rfly. N~ Zones are 

divided into Airports and Restricted Areas. Ai"ports include major airports and flying fields where manned 

aircraft operate at low altitudes. Restricted Areas include borders between countries or sensitive sites. 

The details of the No-Aiy Zones are explained bebw: 

Airport: 

{1) Airport No-Fly Zones are comprised of Takeoff Restricted Zones and Restricted-Altitude Zones. Each 

zone features circles of various size. 

(2) R1 depends on the size and shape of the airport, and is an area around the airport that is a Takeoff 

Restricted Zone, Inside of which tai<EKlff and flight is prevented. 

(3) From R1 to R1 + 1 mile around the airport, the flight altitude is limited on a 15 degree Incline, starting at 

65 feet (20 meters) from the edge of airport and radiating outward. The flight altitude is limited to 1640 

feet (500 meters) at R1+1 mile. 

(4) When the aircraft is within 320 feet (100 meters) of the No-Fly Zones, a warning message will appear 

n the DJI GO app. 

46 
-i 

1640 

feet 

1 

Airports 

1 

16feet 

::i 

L .1- 1 mile --+1+-- R1 -~ ~----- R2-----. 

Restricted Areas: 

(1) Restricted Areas oo not have a fig,! altitude restriction. 

INSPIRE 1 User Manual 

Rellrtct.cHftllude lllaht zone W•mlng zone 

(2) R around the designated Restricted Area is a Take-off Restricted area. Aircraft cannot takeoff within 

this zone. The value of R varies depending on the definition of the Restricted Area. 

(3) A "warning zone" has been set around each Restricted Area. When the aircraft is within 0.6 miles (1 

km) of this zone, a warning message will appear in the DJI GO app. 

1- Restricted Areas -1 

No-tty ~ne 'Warning zone Free zone 

47 
INSPIRE 1 User Manual 

GPS Srgnal Strong G· Blrnklng Green 

Aircraft 

Zone Restriction OJI GO App Prompt Status 

Indicator 

Motors will not start. Warning: You are in a No-fly 

zone. Take off prohibited. 

No-fly Zone If the aircraft enters the 

I 

... restricted area in A mode but Warning: You are in a No-fly .. P mode activates the aircraft zone, automatic landing has 

will automatically descend to begun. (II you are within 1.5 mile 

land then stop its motors after radius) 

landing. 

Warning: You are in a restricted ·A······ zone. Descending to safe Red flashing 

RestrictedIf the aircraft enters the altitude. (If you are between the 

altitude flight restricted area in A mode but P range ol1 .5 mile and 5 mile 

mode activates, it will descend radius) zone to a safe attitude and hover 15 Warning: You are In a restricted 

feet below the safe altitude. zone. Max flight height restricted 

to between 1 O.Sm and 120m. Fly 

Cautiously. 

Warning zone No flight restricijon applies, but Warning: You are approaching a 

there will be warning message. restricted zone, Fly Cautiously. 

Free zone No restrictions. None. None. 

!!1:1 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. 

&, • When flying in the safety zone, aircraft status indcator wiU bliti< red quickly and contirue 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. 

• For safety reasons, please do not fly close to airports, highways, railway statiions, railway lines, 

city centers and other special areas. Try to ensure the aircraft is visible. 
INSPIRE 1 User Manual 

Preflight Checklist 

1. Remote controller, aircraft battery, and mobile device are fully charged. 

2. Propellers are mounted correctly and finnly. 

3. Micro-SO card has been inserted if necessary. 

4. Gimbal is functioning as normal. 

5. Motors can start and are functioning as normal. 

6. DJI GO app connected to the aircraft. 

Calibrating the Compass 

IMPORTANT: Make sure to calibrate the compass in every new flight location. The compass is very 

sensitive to electromagnetic interference, which can cause abnormal compass data leading to poor flight 

perfonnance or even failure. Regular calibration is required for optimum performance. 

0 . DO NOT calibrate your compass where there is a chance of strong magnetic interference, such 

as magnetite, parking structures, and steel reinforcements underground. 

• DO NOT carry ferromagnetic materials with you during calibration such as keys or cellular 

phones. 

• DO NOT calibrate beside massive metal objects. 

Calibration Procedures 

Choose an open space to carry out the following procedures. 

1. Ensure that the compass is calibrated. If you did not calibrate the compass as part of your pre-flight 

preparations. or if you have moved to a new location since the last calibration, tap Aircraft Status 

Indicator bar in the app and select "Calibrate", then follow the on-screen inst11.1ctions. 

2. Hold and rotate the aircraft horizontally 360 degrees, and the Aircraft Status Indicator will display a 

solid green light. 

49 
INSPIRE 1 User tvlanual 

3. Hold the aircraft vertically with rose pointing d<1M1Ward, a'ld rotate it 360 degrees around the cerrter 

axis. Recalibrate the compass if the Aircraft Status Indicator show solid red. 

& If the Aircraft Status Indicator blinks red and yellow after the calibration, move your aircraft to a 

different location to carry out compass calibration. 

~; Calibrate the compass before each flight. Launch DJI GO App, fo!lcm the on-screen instruction 

to calibrate the compass. 

When to Recalibrate 

1. \\'hen COITlJ8SS data is abnormal, and the Aircraft Status Indicator is blinkilg red and yella.v. 

2. When flying in a new location, or a location that is different from your last flight. 

3. When the mechanical structure of the Inspire 1 has changed, i.e. changed mounting position of the 

compass. 

4. \\'hen severe drifti)g occurs in flight. i.e. the Inspire 1 does not fly in straight lines. 

Auto Take-off and Auto Landin~ 

Auto Take-off 

Use auto takEH>ff to take off your aircraft automatically if the Aircraft Status Indicator displays blinking 

green. Follcm the steps below to use auto takEH>ff: 

1. Launch DJI GO app, enter "Camera" page. 

2. Ensure the aircraft is in •p• mode. 

3. Go t'1rough the pre-ftight checklist. 

4. Tap".t.", and confirm flight condition. Slide to confirm a'1d take-off. 

5. Aircraft takes off and hovers at 1.2 meters above ground. 

50 
INSPIRE 1 User ~anua l 

Auto-Landing 

Use auto-landing to land your aircraft automatically if the Aircraft Status Indicator displays blinking green. 

Follow the steps below to use auto-landing: 

1. Ensure the aircraft is in "P" mode. 

2. Check the landing area condition before tapping "!.", to perform landing. 

3. Aircraft lowers the landing gear and proceed to land automatically. 

(j: Landing gear wil automatically raise when the aircraft reaches an altitude ol 1.2m for the first 

time, and atmnaticaly lower every time it descends to 0.8m. Users can tum this feature ON/OFF 

in the GO app. 

: Start1ng/Stopp1ng the Motors 

Starting Motors 

The Combination Stick Command (CSe) listed below are used to start the motors instead of simply pushing the stick up. Ensure that you pertorm the esc in one motion. :!! 

OR 

Stopping Motors 

There are two methods to stop the motors. 

Method 1: When the Inspire 1 has landed, push the throttle down (i), then conduct esc <2>. Motors will stop 

immediately. Release both sticks once motors stop. 

Method 2: When the aircraft has landed, push the throttle down and tdd. The motors will stop after 3 

seconds. 

OR 

Lt. Do not perform esc when aircraft Is In midair, otherwise the motors will be stopped. 

·Right Test -······ .. --

Take off/landing Procedures 

1. Place the aircraft on open, flat grolJ"'d wi+..h battery ind!cato!'s facing towards you. 

2. Power on the rerrote controller and yrxx mobile device, then the lnteligent Right Battery. 

3. Launch the OJI GO App and enter the camera page. 

4. Wait n l the Aircraft Indicator blinks green. This means the Home Poirt is recorded and ills safe to fly 

ocm. If tt flashes yefoN, it means Home Poir.t is not recorded, and you shotJd not take ott. 

5. Push the throttle up slowly to take off or using Auto i ake-off to take off. 

51 

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INSPIRE 1 User Manual 

6. Shoot photos and videos using the DJI GO app. 

7. To land, hover over a level surface and gently pull da.vn on the ti-Jrottle slowly to descend. 

B. After landing, execute the CSC command or hold the throttle at its lowest position for 3 seconds or 

more until the motors stop. 

9. Tum off the Intelligent Flight Battery first, followed by the Remote Controller. 

& • When 1he Ai'craft Status k1dicator bl'nks yetJw rapidly d.mg fig-t, the aircraft has eriered Falsafe 

mode. 

• A low battery level warning is indicated by the Aircraft Status Indicator blinking red slowly or 

rapidly during flight. 

• Watch video tutorials about flight for more fight information. 

VIdeo Suggestions and lips 

1. Work through the checklist before each flight. 

2. Select desired gimbal working mode in the DJI GO app. 

3. Ain to shoot when flying in P mode only. 

4. Nways fly in good weather, such as sunny or windess days. 

5. Change camera settings to suit you. These include photo format and exposure compensation. 

6. Perform flight tests to establish flight routes and scenes. 

7. Push the sticks gently to make aircraft movements stable and smooth. 

52 I ' 
FAQ 
Troubleshooting (FAQ) 

1. How can I put a Go Pro camera on the Inspire 1 ? 

The Inspire 1 does not currently support GoPro attachments. The gimbal is designed to hold DJI 

cameras only. 

2. When will ground station functionality be available? 

The Inspire 1 does not currently support ground station. Ground station will be available with future 

firmware updates. 

3. Is the camera's exposure automatic? 

The exposure can be set to Auto, for automatic changes, or Manual, if you wish to use a specific setting. 

4. Can I see the size of images through the app? 

Yes, you can preview image or video sizes through the DJI GO app. 

5. How much weight can the Inspire 1 carry without its included camera? 

We do not recommend flying with any payload other than the included DJI gimbal and camera. 

6. Do you have an LCD monitor available for the Inspire 1 ? 

No, DJl does not sell LCD or HD monitors for the Inspire 1. However, you can output the live streaming 

video to a compatible monitor or mobile device of your own. 

7. How long does it take to charge the battery? Does it comes with a charger? 

Yes, all Inspire 1 units come with standard TB47 charger. 

With the standard TB47100W charger, it takes 85min to fully charge a 4500mAh battery. 

B. Are the two remote controllers the same? Should I setup the remote controllers in the app or 

somewhere else to control the camera and aircraft separately? 

The two remote controllers are physically identical. You can set the remote controllers to either 'Master" 

or 'Slave' through the DJI GO app if you wish to use dual controller mode. 

9. Where can l find info on the simulation application that plugs into the trainer port? Can you suggest a 

simulation program? 

There is no trainer port on the remote controller for the Inspire 1. 

1 0. Can the mobile device holder be used on the Phantom 2 series remote controller? 

No, it cannot. The mobile device holder can only be used with the Inspire 1 remote. 

11. Does the Inspire 1 have a SD card included? 

The Inspire 1 comes with a 16GB micro-SO card. It supports SD cards up to 64GB. 

12. Can I upgrade and buy a second remote controller if l only buy a single remote controller now? 

Yes. 

13. How big is the Inspire 1? 

Its length x heightx width dimensions without the propellers attached are 44 x 30 x 45cm (17.3 x 11.8 x 17.7in). 

54 
INSPIRE 1 User Manual 

14. What !fight conlroler does the Inspire 1 use? 

The Inspire 1 uses its own new flight controler. 

15. Which motors and propellers does the Inspire 1 come with? 

The Inspire 1 uses 3510 motors and 1345 propellers. 

16. Aircraft frame arm joints appear loosen, is that normal? 

The space of the joins shown in the belo.v figure is normal and it will not affect the performance of 

aircraft, do not adjust the position of the screws on your o.vn. 

17. Failed to complete seW-check? 

Place the aircraft on the flat surface before powering on. Do not move the aircraft du'ing the selfcheck. 

55 
Appendix 
Appendix 

Specifications 

Aorcraft 

Model 

Weoght (Battery Included) 

Hovering Accuracy (P Mode) 

Max Angular Velocity 

Max Tilt Angle 

Max Ascent Speed 

Max Descent Speed 

Max Speed 

Max Service Ceiling Above Sea Level 

Max Wind Speed Resistance 

Max Flight Time 

Motor Model 

Propeller Model 

Indoor Hovenng 

Operating Temperature Range 

Diagonal Distanctt 

Dimensions 

Gombal 

Model 

Ot•tput Power (With Camera) 

Operating Current 

Angt•lar Vibrl!.tiOil Range 

Mounting 

Controllable RangE 

Mechanical Range 

~ax Controllable Speed 

T600 

2935g 

Vertical: 0.5 m 

Horizontal: 2.5 m 

?itch 300" /s 

Yaw 150"/s 

as• 

5 mis 

4 m/s 

22 m/s (A TTl mode, no wond) 

4,500 m (Software altitude limit: 120m above takeoff point) 

iO on/s 

Approximately 18 minutes 

DJI3510 

DJI1345 

Enabled by deffl.ult 

-to• to 40• C 

559 to 581 mno 

438x451x301 mm 

ZENMUSEX3 

Static 9 W. In MOliOol 11 W 

Station: 750 mA; Motion: 900 mA 

::t:003° 

Detachable 

Pitch .go• to +30" 

Pan :t320" 

Pitch: -125° to +45• 

Pan: ±330" 

Potch 120"/s 

Pan teo•ts 

57 
INSPIRE 1 User Manual 

Camera 

Name 

Model 

Total Pixels 

Effective P1xels 

Image Max Size 

ISO Range 

Electronic Shutter Speed 

FOV (Reltl Oi View) 

CMOS 

Lens 

Still Photography Modes 

V1deo i'lec.ord1ng Mode<> 

Max Bitrate Of Video Storage 

Supported File Rlrmat!o 

Supported SD Card Types 

Operating T11mperature Range 

Remote Coniroller 

Name 

Operating Frequency 

Transmitting Distance 

EIRP 

Video Output Port 

58 

X3 

FC350 

12.76M 

124M 

4000x3000 

100.3200 (video) 100-1600 (photo) 

8 s to 1/8000 s 

94< 

Sony EXMOR 1/2.3• 

20mm (35mm format equivalent) f/2.8 focus al oo) 

9 Elements 1n 9 groups 

Anti-distortion 

Single shoot 

Burst shooting: 3/5{7 frames 

Auto Exposure Bracketing (AEB): 3/5 bracketed frames ~~ 

0.7EV Bias 

Time-lapse 

UHD (4K) 4096x2160p24/25 3840x2160p24/25/30 

FHD 1920x1080p2'f/25/30/48/50/f30 

HD 1 ~80;:720p24/25/30/48/50/60 

60 Mbps 

FAT32iflxFAT 

Photo JPEG. DNG 

Video ~~P4/MOV (MPEG-4 AVCIH 204) 

Micro SO 

Max capacity: 64GB. Class 10 or UHS-1 rating required. 

0' to ®• c 

C1 

922 7MHz-927 7 Mt-:z (Japan Only) 

5 725-5 825 GH:z '2 "00-2 183 GH£ 

Up to 5.0 km or 3.1 miles (unobstructed, free of interferences 

and FCC compliant) when it is FCC compliant. 

Up to 3.5 km or 2.1 miles (unobstructed, free of interferences) 

when it is CE compliant 

'iOdBm0900m. 13d8m@5 8G. 20dBm02 4G 

USB, Mini-H:::lMI 
INSPIRE 1 User Manual 

Power Supply Built-in battery 

Charging DJI charger 

Dual User Capability Ho~t-and Siave connection 

Mobile Device Holder Tablet or Smart Phone 

Output Power 9W 

Operating Temperature Range -10" to 40" C 

Storage Temperature Range 

Less than 3 months. -20" to 45" C 

More than 3 month~ 22" to 28" C 

Charging Temperature Range 0-40" c 

Battery 6000 mAh LiPo 2S 

Charger 

Model A14-100P1A 

Voltage 263¥ 

Rated Power 100W 

Battery (Standard) )> 

Name Intelligent Flight Battery "C 

"C 

(1) 

~~odel T8~7 ::J 

c. 

)(' 

Capacity 4500 mAh 

Voltage 222\1 

Battery Type UPo 6S High voltage battery 

Energy 99 91.\'h 

Net Weight 570g 

IJperatrng Temperature Range -·ro• to 40' \J 

Storage Temperature Range 

Less than 3 months: -20" to 45" C 

More than 3 months: 22" C to 28" C 

Chargrng Temperature R!lnge o• to ~o·c 

Max Charging Power 180W 

Battery (Optronal) 

Name Intelligent Flight Battery 

Model TB4B 

Capacity 5700 mAh 

llol18.ge 228V 

9attery Type LiPo 6S 

Energy 'i2996Wh 

Net Weight 670g 

Operatrng T3mperature Range -10 io -10' C 

59 
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INSPIRE 1 User Manuel 

Storage Temperature Range 

Charg1ng Temperature Range 

Max Charging Power 

VISIOn Pos1t1omng 

Velocity Range 

Altitude Range 

Operating Environment 

(),Jerat1ng Range 

DJI GOApp 

Mobile Device System Requirements 

Supported Mobil& DeviCes 

Less than 3 months: -20 to 45° C 

More than 3 months: 22" to 28• C 

o• to 40• C 

1BOW 

Below 8 m/s (2 m above ground) 

5-500cm 

Brightly lit (lux> 15) patterned surfaces 

0-300cm 

lOS version 7.1 or later; Android version 4.1.2 or later 

• 1Phone 6 Plus. 1Phone 6, iPhone SS, iPad Air 2, 1Pad Mint 

3 1Pad AJr. 1Pad M1n1 2, iPad 4:• 5amsung Note~ Samsung 

SS. Sony Z3 EXPERI.·~· Note It IS recommended that you 

use e tablet for the best expenence 

~ ! Intelligent Fltght 

x· Intelligent Right mode includes Course Lock, Home Lock, Point of Interest (POl), Follow Me and 

Waypoints features to assist users to create professional shoots during the fUght. Course Lock and Home 

Point lock helps to lock the orientation of aircraft so that the user can focus more on other operations. 

Point of Interest, Follow Me and Waypoints mode enable aircraft to fly automatically according to the preset flight f'TBleiNers. 

Course Loci\ 

Horne Lock 

Potni of lnt10>res< 

Waypoints 

Lock ·(he curreni. nose d1rect1on as lhe aircraft's forward d 1rect1on. The a1rcrafi: 

1'1111 .nove n i:he locked d1re..;t1ooe regardleRs of liB onentallon (yaw angle). 

Pull the pitch stick backward to move the aircraft toward its recorderd Home 

Point. 

The a1rcraft 'VIII orbti around (he subJect automatiCally to allow (he operator 

08-n be more focus on fram1ng ihe1r shoot on the subj9ct 1n P01nt of lnierest 

Record a flign path, then the aircraft will fly along the sa-ne path repeatedly 

while you control the camera and orientation. The flight path can be saved 

and re-apply in the future. 

Enable Multiple Right Mode by launching the DJI GO app > Camera Vif!W > ~ > Advanced Settings > 

Mulitple Flight Mode before using the Intelligent Fight :-.1ode for the first time. 

60 ~ I r ... 
INSPIRE 1 User Manual 

. How to Update Firmware 

FoiiCM' the process described below to upgrade the aircraft, r~ controller and battery. 

Updating the Aircraft Firmware 

Step 1- Check Battery and SD Card Capacity 

Ensure the Intelligent Flight Battery has at least 50% power and there is at least 100 MB of free space on 

theSDcard. 

Step 2- Prepare the Firmware Update Package 

1. Download the firmware update package from the official DJI website (http://wWW.dji.com/producV 

phantom-3/download). 

2. Insert the SD card into your PC. Extract the all downloaded files into the root directory of the SD card. 

Remove the SD card from your PC. Ensure the aircraft is powered off then insert the SD card into the 

SD card slot on the camera. 

Step 3- Update the Aircraft 

1. Ensure the remote controller is powered off and then power on the aircraft. Upgrade will begin 

automatically after aircraft is powered on. 

2. It will take approximately 25 minutes to complete the firmware update. The ca'Tlera status indicator 

will blink green and red to indicate the upgrade is In progress and stop blinking when the update is 

complete with success. 

3. Check the upgrade status by opening the ".txt" file that is automatically generated after the update. 

The update is successful If the text "result: successful" is in the document. Try upgrading the firmware 

again if the text resu~: failed" is found or the camera status indicator shows solid red. 

Updating the Remote Controller Firmware 

Ensure the DJI GO app has been updated to v1 .2.0 before updating the remote controller. The 

System Status bar in Camera View of the DJI GO App will flash several times if a firmware update is 

available. Fonow these steps to update the firmware via the DJI GO App. 

Step 1- Check Batte!)' and SD Card Capacity 

1. The remote controller has at least 50% battery level. 

2. Ymx mobile device is able to access !he internet. 

3. There is at least 30 MB of free space on your mobile device. 

Step 2- Download and Update the Firmware 

1. Go to the DJI GO App >Camera View> System Status bar> Overall Status. Tap Download the 

firmware update package to download and update the firmware. Track the update progress from 

progress bar in the DJI GO App. The status LED on the remote controller will blink blue during update 

and blink green when update is complete with success. 

Firmware update through the DJI GO app will not work with older versions of the remote controller 

firmware. If the firmware update fails, follow the Instructions below to update the firmware using the 

traditional method: 

a. Update the latest firmware package files from DJI official web s:te. 

61 
INSPIRE 1 User Manual 

b. Extract all doWnloaded flies into the root directory of an SO card or USB f!ash drive. 

c. Turn off the remote cont~oller, Insert the SO card into a SO card reader or the USB cfisk onto the 

remote controller USB port when remote controller is turned off. 

d. Power on the remote controller and wait 60 seconds until the upgrade begins. Do not power off 

the remote controller during the update. 

e. It ml take approximately 10 minutes to complete the fimnware update. The camera will sound 

a beeping sound and the Status LED on the remote controller shows solid blue to indicate the 

update is in progress. The Status LED on remote controller shows solid green and beeping 

sound will stop if the upgrade is completed with success. 

f . If you do not have a SO card reader, you may insert the SO card into the gimbal and connect the 

gimbal with remote controller to upgrade the remote controller. 

& You wil only be able to update the remote controller firmware through the D.JI GO app from 

this point onwards. 

Updating Intelligent FOght Battery Firmware 

The Intelligent Aight Battery is upgraded dlJing the aircraft firmware upgrade process. It is recommended 

to keep the upgrade package files in your SD card. The upgrade will start automatically after power 

cycling the aircraft. 

& • Ensure there Is only one tinware package file stored on your SO card. 

• Only storage devices that are foonatted for FAT32 and exFAT file systems are supported for 

aircraft and remote controler firmware updates. 

• Ensure the internet connection of your mobile device is stable when downloading the firmware 

update package. 

• Turn on Airplane Mode on your mobile device before updating the firmware, as any incoming 

calls may disrupt the update process. 

• Do not perform firmware update while the aircraft is stil flying in the air. Only carry out firmware 

update when the aircraft is landed. 

• Be sure to update the remote controller's firmware to the latest version after you upgrade the 

aircraft's firmware. 

• The remote controller may become unlinked from the aircraft after updating. Re-link the remote 

controller and aircraft. 

• Confirm the update results based on the blinking pattern of camera status indicator or gimbal 

sound. It is normal for the aircraft to sound or the LED to bli"lk during the update process. 

FC_C Camphane~ 

FCC Complance 

This device comp~ies with part 15 of the FCC Rules. Operation is subject to the foUowng two conditions: 

( 1) This device may not cause harmful interference, and 

(2) Th s device must accept any interference received, including interference that may cause undesired 

operation. 

Changes or r."'Odifications not expressly roved by the party responsible for complil¥1Ce could void the 

user's authority to operate the equipment. 

62 
INSPIRE 1 User Manual 

Compliance Information 

FCC Warning Message 

Any Changes or modifications not expressly roved by the party responsible for compliance could void the 

user's authority to operate the equipment. 

This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: 

(I} This device may not cause harmful interference, and (2} this device must accept any interference 

received, including interference that may cause undesired operation. 

FCC Radiation ExposLXe Statement: 

This equipment complies with FCC radiation exposure limits set forth for an uncontrolled environment. 

This equipment should be installed and operated with minimum distance 20cm between the radiator& 

your body. This transmitter IDJSt not be co-located or operating in conjunction with any other antenna or 

transmitter. 

Note: This equipment has been tested and found to comply with the limits for a Class B digital device, 

pursuant to part 15 of the FCC Rules. These limits are designed to provide reasonable protection against 

harmful interference in a residential installation. This eqlipment generates uses and can radiate radio 

frequency energy and, ~ not installed and used in accordance with the instructions, may cause harmful 

interference to radio communications. However, there is no guarantee that Interference will not occur in 

a partictAar installation. If this equipment does cause harmful Interference to radio or television reception, 

which can be detemined by ILJ"ning the eql.ipment off and on, the user is en<:oll'aged to try to correct 

the interference by one or more of the following measures: 

- Reorient or relocate the receiving antenna. 

-Increase the separation between the equipment and receiver. 

-Connect the eqlipment into an ouUet on a circtit different from that to which the receivef is connected. 

--Consu~ the dealer or an experienced radio/TV technician for help. 

IC RSS warning 

This device complies with Industry Canada licence-exempt ASS standard (s). Operation is subject to the 

following two conditions: ( 1) this device may not cause interference, and (2) this device rrust accept any 

interference, including interference that may cause undesired operation of the device. 

Le prllsent areil est conforme aux CNR d'lndustrle Canada licables aux areils radio exempts de licence. 

L'exploitation est autorislle aux deux concitions suivantes: 

(1) l'areil ne doit pas prorure de brouilage, et 

(2)1'utilisateur de l'areil dolt accepter tout brouillage radi~lectrique subl, mame si le brouillage est 

susceptible d'en compromettre le fonctionnement. 

IC Radiation Exposure Statement: 

This equipment compl!es wi~h IC R!" rad:ation exposure limi!s set forth for an uncomrolled environment. 

This transmitter must not be co-located or operating in conjunction with any other antenna or transmitter. 

This equipment should be instaled and operated with min!mu;n dis+.ance 20cm between the radiator& 

your body. 

Any Changes or mod~icatior.s not expressly roved by the party responsible for compliance could void the 

user's authority to operate the equipment. 

63 

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INSPIRE 1 User Manual 

KCC Warning Message 

ii!I~Ji!~~l::ll~ ~§ ~ ~lll-~~ 7rg~OI ~.2..E!S!. ~~~~j!j- ~~~ A-ll::ll~e 'It* i;!irtL..IQ .• 

"!II~ .lf-~~l::l e ~~ ~ ~ll~~~ 7Hs-:9ol ~8· 

NCC Warning Message 

ifWJ.liD&t.i~11!E~fhr.! 

~+=W!I!~:it~ml%mzf~~1!m•ll. ~~~afDJ, ~~ ill~ifm~:ffrutEIRI!lml.ll, JJr: :;tl1.J$~1!W"~~ZW&l1.J1!~. 

~+l!!lillflWJ$t-j~•~~m:ff3~11~bl.~l%i!ll~; ~~m~Tm~~~. AI!&~~$.\ 

TliB~iJf!JUll!Jf.l . i~iJl~l%l!~fS. m~tli8i!WEf~1!ft~ililm. ifWJ*M3fiU~Te.~l%i! 

~~~~~-N~&~~m~~~~~ZTm. 
The content is subject to change. 

I Download tha latest version from I 

www.dji.com/support 

@> 2015 OJ I. All Rights Reserved. 
Inspire 1 

Maintenance Manual 
NSPiRE 1 

Maintenance tv1anual 

[ V1.0) 2015.2 

To ensure that your aircraft continues to offer optimal performance and to ensure flight safety, 

it is recommended that comprehensive maintenance be performed after every 200 flights or 50 

flight hours. This manuat is intend to hetp users maintain their aircraft and maximize its continued 

reliability. 

I. Checking the Battery 

1 . Check the battery for dam age and deformities. If 

there are any signs of damage to the battery, stop 

using it and discharge the battery to 10% or below 

for disposal. Do not disassemble the battery for any 

reason. 

2. Check the battery pins and rub them clean with an 

eraser if any residue is observed. This will help to 

ensure a more reliable connection. 

3. Check the metal battery power connectors for 

damage. If the connectors appear burnt, try to clear 

them. This can be done by inserting a piece of 

sandpaper ( 1 mm thick) into the connectors to polish 

the metal. 

4. Check the contact pins in the battery compartment to 

ensure that the pins are clear. They should be able 

to establish easy contact with the battery connectors 

and should not be bent. 

5. Check the electrodes on the battery. If they appear 

burnt. polish them with sandpaper. If there is serious 

erosion, send the battery in for repairs. 

6. Check the plastic components of the battery bracket 

to see it is in good condition and that all screws are 

secure. This prevents the battery from becoming 

loose during flight. 

7. Check the power cables between the arms and the 

center plate, if the cables are worn, contact DJ I to 

arrange repairs, 

8. For long term storage, please refer to the "Intelligent 

Flight Battery Safety Guidelines" and check the 

battery once a month to prevent the battery cell from 

being damaged. 

9. Run the DJI Pilot App to confirm !hat al: battery cells 

are at similar voltage levels and stay at the same level 

when the battery is fully charged. If all cel!s maintain 

voltage levels above 3. 7V but any cell is a .2V higher 

or lower than the others, contact DJI for ana:ysis. You 

can also check the battery cell warning history. If any 

warning are reported, contact DJI. 

11. Checking the Transformation System 

1. Check the servomotor cables for wear. Also confirm 

that the connection points are sti II in good condition. 

2. Check the lead screws and contact DJ I Support 

to arrange repairs if any bending or damage is 

discovered. Clean the lead screws with WD-40 spray 

if they show signs of rust. 

3. Listen to the servomotors during the transformation, 

if there is abnormal noise, it may indicate that the 

servomotors worn. 

4. After the landing gear rises, check the lead screws 

and bearings. If any dirt or dust is found, clean and 

grease the bearings. 

5. Check the lead screws. lf there is any scratches, 

dents, or plastic particles underneath them. contact 

DJ I Support to arrange repairs. 

Ill. Checking the Aircraft 

t. Confirm that all the screws are still adequately 

tightened. 

2. Check the aircraft for breaks or damage. If there is 

any reason to believe that detectable damage might 

affect flight safety, consult with DJI Support. 

3. Check the carbon tubes of the arms for damage. 

4. Check the dampers on the landing gears. If they are 

loose, secure them with 502 glue. 

5. Ensure that there are no obstacles on or around the 

GPS module or around the antennas on the landing 

gear. Remove any obstacles (such as tapes with 

conductive material) that might affect or block the 

signal. 

6. Check that the right and left !anding gear rest at the 

same tin angle. 
IV. Checking the Motors 

1. Check the rotors to confirm that they have not 

become loose. 

2. Detach the propellers and start the motors. Listen 

carefully. If there is any abnormal noise. please 

replace the motors. This may be a sign that the 

bearings have been worn out 

3. Detach the propellers and start the motors. Carefully 

examine the edge of the rotor and confirm that the 

shaft is perfectly centered on the motor. Check 

for any abnormal or excessive vibration. If any 

problems are detected, contact DJI Support to order 

replacement motors. 

4. Check for deformities by confirming that the gap 

between the motor and motor base is even. If not 

contact DJI Support to order replacement motors. 

5. Ensure that the screws used to secure the motor 

base are tight and the plastic components around 

the motors are in good condition. If not please 

tighten the screws and contact DJI to repair any 

broken plastic components. 

V. Checking the Propellers 

1. Check the propellers. If there is any bending, 

breakage or cracking on a propeller, do not use it. 

2. Attach the propeller to the motor. turn on the aircraft, 

and place it on the ground. Stand 1 meter away from 

the aircraft and observe the rotating propellers. If you 

can see two distinct propeller outline layers, when 

looking at a spinning propeller from the side, this 

propeller is damaged and should not be used. 

VI. Checking the IMU 

1. Open DJI Pilot app to check the condition of the JMU 

and perform an advanced IMU calibration. Please 

place the aircraft in a cool environment and on a 

flat. stable surface (if the landing gear is damaged, 

support the aircraft with four objects of equal 

height). Do not touch the craft during the calibration. 

2. Turn on the aircraft and listen for any abnormal noise 

or vibration from the fan located on the front of the 

aircraft. If any irregularity is detected, replace the 

fan. 

VII. Checking the Control and VIdeo Transmission System 

1. Check the 4 antennas on the landing gear to ensure 

that they are secure. Also check for any bending or 

damage. 

2. Check the antennas of the remote controller for 

damage 

3. Check the neck strap for damage or wear, replace 

if necessary. 

VIII. Checking the Gimbal and Camera 

1. The quick-mount connector for the camera is a 

particularly vulnerable component. If the gimbal 

fails to initialize when turned on, fails to work after 

initialization, or fails to transmit video to the app 

(while OSD data is displayed). the quick-mount 

connector may be worn. In this case, replace the 

rubber mat, circuit board, and/or connector on the 

gimbal quick-mount 

2. Check the metal contacts on the quick mount 

connector board, if any contact is bent. replace 

the quick-mount connector. 

3. Check the contact pins on the quick-mount 

connector board, if there is any dirt, rub it clean 

with an eraser. II any contact pins are worn out it 

should be replaced. 

4. Confirm that the gimbal is able to properly stabilize 

itself. If its stabilizing performance deteriorates, 

contact DJI to arrange repairs. 

5. Listen for any abnormal noise from the fan when 

the gimbal is turned on. This may indicate unusual 

vibration and the fan should be replaced. 

IX. Checking the Vision Positioning System 

1. Check the lens of the camera. If any dirt or residue 

is detected, genlly clean the lens. 

2. Check for and remove objects that might block the 

sensors. 

3. Ensure that the Vision Positioning System is securely 

installed on the aircraft. 

4. Detach the propellers and turn on the aircraft. Hold 

the aircraft 1-2 meters above a surface with rich 

patterns. under good lighting conditions. Change 

the Flight Mode switch to P Mode on the controller 

and check the DJI Pilot app. If the app displays an 

altitude value and indicates that P-OPTI mode is 

active. the Vision Positioning System should function 

normally. 

Support Center Contact Info: 

http://www.dji.com/support 

The content is subJect to change. 

Download the latest version from 

http:ltwww.dji.com/productlinspire-1/download 
APPENDIX C 
Appendix C 

Please see the attached Confidential & Proprietary: 

American Compliance Technologies, Inc. 

Flight Operation & Procedures Manual (FOPM)