U.S. Department of Transportation, Docket Operations 

West Building Ground Floor, Room W12-140 

1200 New Jersey Avenue, SE 

Washington, DC 20590

Paolo Wilczak 

Aerograph, LLC 

1715 Dogwood Ln 

Boulder, CO 80304 

303-960-2756 

wilczak.paolo@gmail.com 

October 3, 2015 

To whom it may concern, 

Aerograph, LLC respectfully requests exemptions from several provisions of Title 14 of the 

Code of Federal Regulations (C.F.R.) in order to permit the usage of small unmanned aerial 

systems (sUAS) to provide videography and photography services for real estate, agricultural 

surveillance, and infrastructure inspection. One motivation for this request is to demonstrate the 

safety awareness of Aerograph, LLC in aerial photography and videography. The exemption 

would allow Aerograph, LLC to satisfy the increasing demand from our clients safely. 

Background Information 

Aerograph, LLC is in the business of providing aerial digital content to our increasing number of 

potential clients. We have developed detailed operation procedures that speak to our 

understanding of safety. Our clients demand a high level of competence to minimize risks to their 

businesses due to the fact that flying sUAS can be dangerous unless done professionally and 

systematically. 

Operation Categories: 

 -Real Estate 

 -Agricultural Inspection 

 -Construction site inspection 

 -Utility Inspection 

Aerograph, LLC intends to use digital photographs and video capture to inspect such 

infrastructure. 

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, 

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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 the case of Aerograph, LLC an exemption would be in the 

public interest as it would allow for the development of new commercial applications of sUAS 

while maintaining a high level of safety in the emerging aerial imaging industry. The demand for 

aerial photography, videography, and infrastructure inspection is increasing rapidly. Using sUAS 

is far safer than using traditional aircraft. Reducing the number of traditional aircraft flying at 

low altitudes to capture photos is in the best interest of the public. Also, using sUAS can 

eliminate labor intensive and precarious jobs. For inspection and analysis of infrastructure, 

workers are required to go out on structures which can be a dangerous task. The job can be done 

just as effectively and much more safely using a sUAS. For example, a wind turbine blade can be 

examined for erosion and pitting using sUAS which would avoid the need for a person to climb 

out on the blades of a turbine. Structures can be analyzed much more frequently using sUAS. 

More frequent inspections can help eliminate problems before they become serious and 

potentially dangerous, ultimately adding to public safety. 

Additionally, the sheer amount of assets and the widely dispersed locations – in many instances 

far from sizable population centers – means that visual inspection in all 

instances by company personnel can be inefficient. 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 asset anomalies from such 

heights. Helicopters present better vantage points; however manned helicopters are much 

more costly, have increased human safety concerns, and carry highly explosive jet fuel, making 

them impractical for deployment. By using sUAS for asset evaluation, Aerograph, LLC will be 

able to significantly upgrade its capability to detect and address infrastructure issues. Granting an 

exemption would allow Aerograph, LLC to conduct infrastructure inspections commercially in a 

safe and reliable manner. 

Granting an Exemption will not Adversely Affect Safety 

Granting an Exemption will not adversely affect safety. Aerograph, LLC intends to operate over 

controlled land, during daylight hours, below 200 feet. Operations are intended to be held away 

from congested areas and airports in order to minimize risk. If an operation is inside a 4 mile 

radius of an airport or heliport, the control tower and airport management will be notified and 

Aerograph, LLC must comply with the requests of the airport personnel. If the personnel of the 

airport deny the request of Aerograph, LLC to conduct aerial operations in the location specified, 

the operation will be terminated. The area in which operations are held are owned by the client 

and are generally secured. For example, wind energy plants are secured from public access. 

Therefore, while the operation is underway, everyone who has access to the area can be 

accounted for and notified to avoid certain areas where the sUAS is flying. The operations will 

generally be conducted under 100 feet above the highest structure in the flight area. Therefore, 

the risk of collision with a traditional aircraft is minimal. Also, interference with other sUAS is 

not an issue because Aerograph, LLC only allows for 1 sUAS to be in flight at a specific location 

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at a time. Moreover, since the area is secured, no other sUAS will be in the airspace of the 

operation. 

An approval of the exemptions stated in this document will increase safety by reducing risks. 

Traditional operations require that a jet or piston powered aircraft fly to the location and back 

carrying large amounts of weight and large amounts of combustable fuel. One of the lightest 

helicopters on the market, the Robinson R22, weighs in at around 1,000 lbs. Even as one of the 

lightest, the weight of the R22 is distinctively more than a sUAS weighing under 55 lbs. If a 

sUAS were to fail and crash, the damage would be orders of magnitude smaller than if a 

traditional helicopter were to have an emergency. The sUAS will carry no pilot or crew so the 

risks of manned human flight are eliminated. The sUAS don’t pose a threat to national security 

because of the small size and carrying capacity of the sUAS. The pilots of sUAS may be subject 

to screening by the Department of Homeland Security if it is believed that sUAS operated by 

Aerograph, LLC pose a threat to national security. 

The operation of small UASs, conducted in the strict conditions described in the Aerograph, LLC 

operations procedure and rules section, 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.

Aerograph, LLC Operations Procedure and Rules Overview 

Aerograph, LLC uses an operation procedure and a list of rules when conducting an operation. 

The rules and flight procedures are enforced by Aerograph, LLC management. Pilots who exhibit 

misjudgment or misunderstanding of these rules and flight procedures are suspended from active 

client duty until they are re-evaluated and show that they are worthy to pilot a sUAS under the 

Aerograph, LLC name. Pilots who exhibit misjudgment or misunderstanding a second time are 

subject to removal from pilot duty at Aerograph, LLC. 

Aerograph Pilot Training Procedures and Requirements 

Each person who is to become a pilot in command (PIC) of Aerograph, LLC sUAS, will have to 

complete a training program described below. 

Pilot Training Program Overview 

Pilots will have to demonstrate proficiency in the control of at least 2 different sUAS listed 

below though 3 phases of training 

• “The Electrohub” 

• DJI Phantom Professional

• DJI Inspire 1 

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*Specifications of the DJI Professional is given in Appendix B. 

*Specifications of the DJI Inspire 1 is given in Appendix C. 

Aircraft specifications and descriptions are located in Appendix B and Appendix C. Aerograph, 

LLC intends to solely own 3 different sUAS and operate 2 different sUAS commercially. An 

addition to this petition must be submitted if any additional sUAS are to be used in operation. 

Phase 1 Training 

The purpose of phase 1 training is to determine that pilots are capable of flying sUAS without 

flight automation features. The “Electrohub” is used solely as a training aircraft. The aircraft has 

the ability to turn off the advanced flight automation features. The “Electrohub” can simulate a 

failure of automation features. Pilots are trained on the “Electrohub” so that if either of the DJI’s 

flight automation were to fail during and operation, the pilot would be able to maintain control of 

the aircraft and bring it safely to the ground. Also, we strongly believe that pilots first must 

understand how the sUAS functions at its most basic operation settings before they can fly 

competently with the automated flight of the DJI Phantom and DJI Inspire. Pilots must complete 

a minimum time of 20 hours in the last 90 days before they are allowed to progress to Phase 2 of 

training. While 20 hours is the minimum, pilots who don’t show required levels of competency 

will not be authorized to progress to Phase 2 of training. 

Phase 2 Training 

The purpose of phase 2 training is to apply the flight skills learned in Phase 1 to meaningful 

inspection operations. Pilots who successfully progress through Phase 1 will begin training on 

the DJI Phantom Professional or the DJI Inspire. At our training facility, pilots in training will 

practice capturing inspection video capture and photographs of infrastructure. Pilots in training 

will complete a series of infrastructure inspections that involve different variables and vary in 

level of difficulty. Pilots in training must complete a minimum of 10 hours in the last 90 days on 

the DJI Phantom or DJI Inspire before they are considered to be advanced to Phase 3 of training. 

Phase 3 Training 

Phase 3 training is a shadowing period. Pilots who complete Phase 1 and Phase 2 then shadow 

an operational pilot for a minimum of 5 operations. The purpose of phase 3 is to finally 

submerge the pilots into real operations in which the Operation Procedure must be carefully 

executed. 

Key Operational Procedure Steps 

(1) Aerograph, LLC requires that the area of operation be inspected a minimum of 3 days before 

the scheduled time of flight, and a maximum of 30 days before the scheduled time of flight. 

The PIC must be active and present at the inspection. Other personnel may attend to assist 

with the inspection. Personnel look for potential hazards such as proximity to congested 

areas and power lines. Additionally, takeoff and landing points must be established during 

the inspection. 

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(2) After the inspection, but before the flight, an intended flight plan must be drafted by the PIC 

in collaboration with the the visual observer. 

(3) Upon arrival to the flight area, a brief inspection of the flight path must be conducted to 

ensure that no new hazards have developed along the intended path of flight. 

(4) The PIC may commence the flight based on his/her discretion. The decision is mainly 

influenced by safety. Pilots are instructed to terminate all operations if either the visual 

observer or the PIC believes that the safety of any person, animal, or structure is jeopardized. 

(5) Once the sUAS gathers all of the required information, no additional flights will be 

conducted. The client and all of the area’s active personnel must be informed that flight 

operations have ceased and normal duty may continue. 

Key Operational Rules 

(1) The sUAS must not exceed 55 pound including energy sources and data collection 

equipment. 

(2) The sUAS must not be flown higher than 400 feet above ground level. 

(3) The sUAS must not be flown if wind gusts exceed 20 knots. 

(4) The sUAS must not be flown at speeds that exceed the manufacturer’s specifications. 

(5) Only one sUAS may be in flight at one specific time. 

(6) A visual observer must be present throughout the entire flight and maintain visual line of 

sight with the sUAS. 

(7) The PIC must make the fight information accessible to the client upon request. 

(8) The PIC must ensure that the sUAS is in full operational condition based upon the manual 

provided by the manufacturer. If the sUAS is not fully capable of flying safely, the PIC must 

terminate the operation until the problem is resolved. 

(9) If a sUAS is to be repaired, it must undergo a test flight prior to functioning in an operation. 

(10) All maintenance must be recorded in an Aerograph, LLC information storage system. 

(11) The sUAS may not be operated unless each and every person in the flight area is accounted 

for and is aware of the operation of the sUAS. 

(12) Each sUAS operation must have a planned completion with a minimum of 25% power 

remaining in the battery. 

(13) All batteries that are not mounted inside the sUAS must be stored in a fire-safe storage 

container. 

(14) The operator may not be in a moving vehicle 

(15) The operation must not be conducted during night 

(16) An operator must record in an Aerograph, LLC database prior to operation: 

 -Dates and times of all flights 

 -Name and contact information for PIC and visual observer

 -Proof of permission from the land owner to authorize sUAS operations 

 -Signature from exemption holder or representative 

 -Description of intended flight 

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Regulatory Provisions From Which Aerograph, LLC Seeks and Exemption 

Aerograph, LLC believes that it may need exemption from the following provisions in order to 

conduct the operations discussed. 

 333 Exemption Status 

 14 C.F.R. § 91.119 (c) 

 14 C.F.R. § 91.121 

 14 C.F.R. § 91.151 (a) and (b) 

 14 C.F.R. § 91.405 (a) 

 14 C.F.R. § 91.407 (a)(1) 

 14 C.F.R. § 91.409 (a)(2) 

 14 C.F.R. § 91.417(a) 

 14 C.F.R. § 61.113 (a) and (b) 

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 Aerograph, LLC will be at least 

as safe, if not 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 operates 

exclusively within a controlled 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 with conventional equipment. These safety 

enhancements provide an expanded degree of safety to the inspectors 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 

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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. § 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.

 ———-

The relief that Aerograph ,LLC requires is from the minimum altitudes in § 91.119 (c). Relief is 

required because operations of multi-rotor sUAS and fixed wing sUAS shall not be conducted 

above 500 feet because operation above 500 feet is impractical and poses higher risk for collision 

with traditional aircraft and potential loss of line of sight between the spotter and the sUAS. 

Additionally, The land on which the operation will be conducted is owned by the client and is 

secured so that all personnel and infrastructure are accounted for before the flight of the sUAS. 

Therefore, the risk of injury or damage to property is minimal. Aerograph, LLC does not plan to 

operate sUAS in congested areas so exemption from paragraph (b) is not required. 

14 C.F.R. § 91.121 

§ 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.”

 ——— 

The sUAS does not contain a barometric altimeter, but instead a GPS. Therefore an exemption 

from § 91.121 is needed. Safety will not be compromised because the operator of the sUAS will 

confirm that the GPS readout is set to zero before each and every flight and that the system is 

fully functional in order to ensure that the safety of the operation is not compromised. The sUAS 

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has an onboard digital GPS that sends a downlink to the pilot through a digitally encoded 

telemetric data feed. 

14 C.F.R. § 91.151 (a) and (b) 

§ 91.151 (a) and (b) - 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 speed, 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.

 ——— 

Aerograph, LLC does not intend to fly beyond line of sight and therefore doesn’t need a time 

based excess fuel requirement. The flights are preplanned and take into account weather 

conditions which will allow the sUAS to arrive at the planned landing spot with a percentage of 

electric fuel remaining in the battery. Aerograph, LLC flight policy requires that all flights must 

have a planned finish with a minimum of 25% power remaining in the battery of the sUAS so 

that there is plenty of reserve power to safely bring the sUAS to a landing in case of and 

emergency. 

14 C.F.R. § 91.405(a), § 91.407(a) (1), § 91.409(a)(2), § 91.417(a)

§ 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 unless –

 (1) It has been approved for return to service by a person authorized under §43.7 of this 

 chapter. 

 ———— 

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§ 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.

Aerograph, LLC believes that exemptions from these three maintenance requirements is 

necessary because the FAA has not established maintenance standards for sUAS. Also, there are 

no persons authorized by the FAA to conduct maintenance on sUAS. All maintenance of the 

sUAS will be conducted by Aerograph, LLC. The aircraft will not be flown if there is any factor 

that jeopardizes the airworthiness of the sUAS. The sUAS undergoes a examination prior to 

every flight, as stated in the flight operation procedure. 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.

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.

 ———- 

Aerograph, LLC specially trains pilots for the operation of our sUAS. These persons will not 

hold commercial pilot licenses. Without an exemption, the pilot would be required to hold a 

commercial pilot certificate under § 61.113. However, operation of the sUAS is far safer than 

traditional aircraft. The sUAS is operated far below altitudes than traditional aircraft operate. In 

addition, the area in which the sUAS operates is controlled solely by Aerograph, LLC and its 

client. The sUAS will not carry property for compensation or hire. 

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I respectfully submit this petition on behalf of Aerograph, LLC 

Please don’t hesitate to contact me with any questions, concerns, or updates. 

Cheers,

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: Aerograph, LLC 

Sections of 14 C.F.R. Affected: 

 333 Exemption Status 

 14 C.F.R. § 91.119 (c) 

 14 C.F.R. § 91.121 

 14 C.F.R. § 91.151 (a) and (b) 

 14 C.F.R. § 91.405 (a) 

 14 C.F.R. § 91.407 (a)(1) 

 14 C.F.R. § 91.409 (a)(2) 

 14 C.F.R. § 91.417(a) 

 14 C.F.R. § 61.113 (a) and (b) 

Description of Relief Sought: 

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

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

and 61.113(a) and (b)) to conduct sUAS operations over Aerograph, LLC client’s owned or 

controlled land, solely during daylight hours, to assist in the safe evaluation and analysis of 

infrastructure and operations. In general, sUAS operations are intended to be conducted in areas 

remote from both congested areas and airports. Aerograph, LLC expects that in most instances, 

the sUAS will be flown less than 100 feet above the highest structure along the path of the sUAS 

and in no instances will be flown higher than 400 feet above the ground. Accordingly, the risk of 

interference with other aircraft is minimal.

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Appendix B

Specifications of the DJI Phantom Professional 

AircraftAircraft Weight (Including Battery And Propellers): 1280g 

Diagonal Size (Including Propellers): 590 mm 

Max Ascent Speed: 5 m/s 

Max Descent Speed: 3 m/s 

Hover Accuracy: Vertical: +/- 0.1 m (when Vision Positioning is active) or +/- 0.5 m 

 Horizontal: +/- 1.5 m Max Speed 16m/s (ATTI mode, no wind) 

Max Altitude Above Sea Level: 6000 m 

Operating Temperature: 0°C to 40°C 

GPS Mode: GPS/GLONASS 

CameraCamera Sensor: Sony EXMOR 1/2.3” Effective pixels: 12.4 M (total pixels: 12.76 M) 

Lens: FOV 94° 20 mm (35 mm format equivalent) f/2.8, focus at ∞

ISO Range: 100-3200 (video) 100-1600 (photo) 

Shutter Speed: 8s -1/8000s 

Image Max Size: 4000 x 3000 

Still Photography Modes: Single Shot 

Burst Shooting: 3/5/7 shots 

Auto Exposure Bracketing (AEB): 3/5Bracketed Frames at 0.7EV Bias 

Time-lapse Video Recording Modes: UHD: 4096x2160p 24/25, 3840x2160p 24/25/30 

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 FHD: 1920x1080p 24/25/30/48/50/60 

 HD: 1280x720p 24/25/30/48/50/60 

Supported SD Card Types: 

Micro SD: Max capacity: 64 GB. Class 10 or UHS-1 rating required 

Max Bitrate of Video Storage: 60 Mbps 

Supported File Formats: Photo: JPEG, DNG 

 Video: MP4, MOV (MPEG-4 

Operating Temperature: 0°C to 40°C 

GimbalGimbal Controllable Range: Pitch -90° to +30° 

Stabilization: 3-axis (pitch, roll, yaw) Vision Positioning 

Max Velocity: Less than 8 m/s (when 2 m above ground) 

Altitude Range: 30 cm-300 cm 

Operating Range: 30 cm-300 cm 

Operating Environment: Surface with clear pattern and adequate lighting (Lux > 15) 

RemoteRemote Controller Operating Frequency: 2.400 GHz-2.483 GHz 

Max Distance: 2000m (outdoors and unobstructed) 

Battery: 6000 mAh LiPo 2S 

Receiver Sensitivity (1%PER): -101 dBm ±2 dBm 

Transmitter Power (EIRP): FCC: 20 dBm 

 CE: 16 dBm 

Working Voltage: 1.2 A @7.4 V 

Battery Charger Voltage: 17.4 V 

Rated Power: 100 W 

BatteryIntelligent Flight Battery Capacity: 4480 mAh 

Voltage: 15.2 V 

Battery Type: LiPo 4S 

Energy: 68 Wh 

Net Weight: 365 g 

Max Flight Time: Approximately 23 minutes 

Operating Temperature: -10°C to 40°C

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Appendix C

Specifications of the DJI Inspire 1 

AircraftWeight (Battery Included): 2935 g

Hovering Accuracy (GPS Mode): Vertical: 0.5 m/Horizontal: 2.5 m

Max Angular Velocity: Pitch: 300°/s Yaw: 150°/s

Max Tilt Angle: 35°

Max Ascent Speed: 5 m/s

Max Descent Speed: 4 m/s

Max Speed: 22 m/s (ATTI mode, no wind)

Max Flight Altitude: 4500 m

Max Wind Speed Resistance: 10 m/s

Max Flight Time: Approximately 18 minutes

Motor Model: DJI 3510

Propeller Model: DJI 1345

Indoor Hovering: Enabled by default

Operating Temperature Range: -10° to 40° C

Diagonal Distance: 559 to 581 mm

Dimensions: 438x451x301 mm

Power Spectral Density: 9.06mW/MHz

GimbalModel: ZENMUSE X3

Operating Current: Station: 750 mA/Motion: 900 mA

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Angular Vibration Range: ±0.03°

Mounting: Detachable

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

Mechanical Range: Pitch: -125° to +45°/Pan: ±330°

Max Controllable Speed: Pitch: 120°/s Pan: 180°/s

 CameraModel: FC350

Total Pixels: 12.76M

Effective Pixels: 12.4M

Image Max Size: 4000x3000

ISO Range: 100-3200 (video)/100-1600 (photo)

Electronic Shutter Speed: 8s - 1/8000s

FOV (Field Of View): 94°

CMOS: Sony EXMOR 1/2.3”

Lens: 20mm (35mm format equivalent)f/2.8 focus at ∞ - 9 Elements in 9 groups - Anti-distortion

Still Photography Modes: Single shoot - Burst shooting: 3/5/7 frames - Auto Exposure - 

Bracketing (AEB): 3/5 bracketed frames at 0.7EV Bias - Time-lapse

Video Recording Modes: UHD (4K): 4096x2160p24/25, 3840x2160p24/25/30 

FHD: 1920x1080p24/25/30/48/50/60 

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

Max Bitrate Of Video Storage: 60 Mbps

Supported File Formats: FAT32/exFAT - Photo: JPEG, DNG - Video: MP4/MOV (MPEG-4 

AVC/H.264)

Supported SD Card Types: Micro SD - Max capacity: 64 GB. Class 10 or UHS-1 rating required.

Operating Temperature Range: 0° to 40° C

Remote ControllerOperating Frequency: 5.725~5.825 GHz - 2.400~2.483 GHz

Transmitting Distance (Outdoor And Unobstructed): 2 km

EIRP: 10dBm@900m, 13dBm@5.8G, 20dBm@2.4G

Video Output Port: USB, mini-HDMI

Power Supply: Built-in battery

Charging: DJI charger

Dual User Capability: Host-and-Slave connection

Mobile Device Holder: Tablet or Phone

Max Mobile Device Width: 170mm

Output Power: 9 W

Operating Temperature Range: -10° to 40° C

Storage Temperature Range: Less than 3 months: -20° to 45° C - More than 3 months: 22° to 28° 

Charging Temperature Range: 0-40° C

Battery: 6000 mAh LiPo 2S

ChargerModel: A14-100P1A

Voltage: 26.3 V

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Rated Power: 100 W

Battery(Standard)- 

Name: Intelligent Flight Battery

Model: TB47

Capacity: 4500 mAh

Voltage: 22.2 V

Battery Type: LiPo 6S High voltage battery

Energy: 99.9 Wh

Net Weight: 570 g

Operating Temperature Range: -10° to 40° C

Storage Temperature Range: Less than 3 months: -20° to 45° C - More than 3 months: 22° C to 

28° C

Charging Temperature Range: 0° to 40° C

Max Charging Power: 180 W

Vision PositioningVelocity Range: Below 8 m/s (2 m above ground)

Altitude Range: 5-500 cm

Operating Environment: Brightly lit (lux > 15) patterned surfaces

Operating Range: 0-250 cm

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