UAS OSC Volume 2

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Operator ID:
UAS Operating Safety Case Volume 2 - UAS Description:
Document reference number:
Document version and date:

Amendment record

Amendment Number	Date	Amended by	Details of changes

CAP722A Table 6

Aircraft and systems description

UAS Model	Mavic 3 Enterprise
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass	Weight: DJI Mavic 3E: 915 g DJI Mavic 3T: 920 g
Maximum Take-Off Mass (MTOM)	Max Takeoff Weight: DJI Mavic 3E: 1,050 g DJI Mavic 3T: 1,050 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded (without propellers): 221 x 96.3 x 90.3 mm (L x W x H) Unfolded (without propellers): 347.5 x 283 x 107.7 mm (L x W x H) Diagonal Distance: 380.1 mm
Width of aircraft body
Height of aircraft body
Propeller Configuration	Propeller Model: 9453F Propellers for Enterprise
Propeller Dimensions
Sound power level
Any other relevant information

CAP722A Table 7

UAS performance characteristics

Maximum airspeed	Max Flight Speed (at sea level, no wind): 15 m/s (Normal Mode) Forward: 21 m/s, Side: 20 m/s, Backward: 19 m/s (Sport Mode) [2]
Minimum airspeed to maintain safe flight
Normal/typical operating height	Max Take-off Altitude Above Sea Level: 6000 m (without payload)
Maximum operating height
Maximum flight time during normal operation	Max Flight Time: 45 mins [4]
Maximum flight time on an ISA day at cruising speed at normal/typical operating height.
Maximum flight range on an ISA day (normal and emergency conditions)	Max Flight Distance: 32 km
Glide distances
Maximum radio range of the C2 Link	Max Transmission Distance (unobstructed, free of interference) [7]: FCC: 15 km CE/SRRC/MIC: 8 km

CAP722A Table 8

UAS environmental limitations

Wind speed limits	Max Wind Speed Resistance: 12 m/s [3]
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature Range: -10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
In-flight icing condition limits
Any other relevant information

CAP722A Table 9

Construction

Type of material
Material characteristics or properties
Any other relevant information

CAP722A Table 10

Electrical power system

Batteries:
Battery type, model and manufacturer	Capacity: 5000 mAh Type: LiPo 4S Chemical System: LiCoO2
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Energy: 77 Wh Standard Voltage: 15.4 V
Electrical load shedding functionality
Power supply redundancy
Procedures to charge and discharge batteries.
Safety provisions with regards to hazards inherent to high-voltage storage devices:
Procedures in place for safe handling by any person who may come into contact with high-voltage storage devices
Means of identifying high-voltage storage
Safety provisions for any person discovering the UA following an accident.
Procedures and safety provisions to mitigate the risk of battery thermal runaway.
Procedures for monitoring high-voltage storage devices.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Charging Temperature: 5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)

CAP722A Table 11

Propulsion system

Propulsion type	Motor Model: 2008
Engines:
Type, model and manufacturer
Propeller type, model and manufacturer
Quantity
Arrangement
Power output
Propeller guards
In-flight restart functionality
Performance monitoring
Health monitoring
Safety features and redundancy in the system that allow maintaining flight after a failure or degradation has occurred in the propulsion system.
Fuel-powered propulsion system – Safety features to mitigate the risk of engine loss when the following hazards occur:
Fuel starvation
Fuel contamination
Failed signal input from the control station
Engine controller failure
Indication to the remote pilot
Electric-powered propulsion system:
Power source and supply management with regards to other systems in the UA
Redundant power sources
Maximum continuous power output of the motor
Maximum peak power output of the motor
Electrical distribution architecture
Electrical load shedding functionality
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 12

Fuel system

Fuel type
Safety provisions with regards to hazardous substances within the fuel system:
List of hazardous substances and their characteristics.
Procedures in place for safe handling of the UA by any person who may come into contact with the hazardous substances.
Means of identifying the hazardous substances.
Safety provisions for any person discovering the UA following an accident.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 13

Flight Controls system

Design and operation of flight control units, surfaces, actuators, control linkages, etc.
Flight controller:
Type, model and manufacturer	Model: RM510B
Functions
Flight modes available
Automatic functions:
Take-off and landing
Stabilisation
Autopilot
Return to home
If functions are provided by COTS equipment, provide type, model and manufacturer.
Safety features and redundancy in the system which allow maintaining flight after a failure or degradation of the flight control system, including indication to the remote pilot.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 14

Navigation

Sensors
Type, model and manufacturer	GNSS: GPS+Galileo+BeiDou+GLONASS (GLONASS is supported only when the RTK module is enabled)
Quantity
Telemetry links
Method to determine current position.
Method to navigate to intended destination.
Automatic/automated navigation functions
Geo-awareness functions	RTK Positioning Accuracy: RTK Fix: Horizontal: 1 cm + 1 ppm; Vertical: 1.5 cm + 1 ppm
Containment functions
Safety features and redundancy in the system which allow maintaining flight after a failure or degradation has occurred in the navigation system:
Backup means of navigation
Detection of and response to loss of primary means and secondary means of navigation.
Indication to the remote pilot
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	GNSS: GPS+Galileo+GLONASS

CAP722A Table 15

Detect and Avoid (DAA) systems

DAA system functions	Forward: Measurement Range: 0.5-20 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <=15 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg. Backward: Measurement Range: 0.5-16 m Effective Sensing Speed: Flight Speed <=12 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg. Lateral: Measurement Range: 0.5-25 m Effective Sensing Speed: Flight Speed <=15 m/s FOV: Horizontal 90 Deg., Vertical 85 Deg. Upward: Measurement Range: 0.2-10 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Front and Back 100 Deg., Left and Right 90 Deg. Downward: Measurement Range: 0.3-18 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Front and Back 130 Deg., Left and Right 160 Deg. Type: Omnidirectional binocular vision system, supplemented with an infrared sensor at the bottom of the aircraft.
Devices used
Technology used
Interface between the DAA system and the flight control computer
Limitations of the DAA system	Operating Environment: Forward, Backward, Lateral, and Upward: Surface with a clear pattern and adequate lighting (lux >15) Downward: Diffuse reflective surface with diffuse reflectivity>20% (e.g. walls, trees, people) and adequate lighting (lux >15) Sensitivity: <=50 mk@F1.1
Evidence of equipment qualification and approval.
DAA event sequence:
Level of automation
Actions required by the remote pilot
Means to verify normal system operation.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 16

Other avionics systems

Command Unit (CU)

Power sources, supply management and redundancy.	Battery: Li-ion (5000 mAh @ 7.2 V) Rated Power: 12 W
Radio signal:
Determination of the signal strength and health value.
Threshold values which represent a critically degraded signal.
Control handover between two CUs
Safety features to mitigate the risk of inadvertent command activation:
List of critical commands
Mitigation means
Safety features to mitigate the risk of display or HMI lock-up.
Safety features to maintain flight-critical processing when multiple programs are running concurrently.
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Operating Temperature Range: -10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F) Operating Time: Approx. 3 hours

CAP722A Table 17

Command an Control (C2) link

RLOS
BRLOS
Antennas:
Type, model and manufacturer	Antenna: 4 Antennas, 2T4R
Locations on the UAS
Transceivers / Modems:
Power levels	Video Transmission Transmitter Power (EIRP): 2.4 GHz: <33 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.8 GHz: <33 dBm (FCC), <14 dBm (CE), ＜23 dBm (SRRC) Wi-Fi Transmitter Power (EIRP): 2.4 GHz: <26 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.1 GHz: <26 dBm (FCC), <23 dBm (CE/SRRC/MIC) 5.8 GHz: <26 dBm (FCC/SRRC), <14 dBm (CE) Bluetooth Transmitter Power (EIRP): < 10 dBm
Transmission schemes	Bluetooth Protocol: Bluetooth 5.1 Wi-Fi Protocol: 802.11 a/b/g/n/ac/ax Support 2 x 2 MIMO Wi-Fi
Operating frequencies
Details of frequency spectrum approvals	Video Transmission Operating Frequency [6]: 2.400-2.4835 GHz 5.725-5.850 GHz Wi-Fi Operating Frequency [6]: 2.400-2.4835 GHz 5.150-5.250 GHz 5.725-5.850 GHz Bluetooth Operating Frequency: 2.400-2.4835 GHz
Maximum power output/range
Type of signal processing
Datalink margin in terms of the overall link bandwidth at the maximum anticipated distance from the CU.
Operational C2 link management:
Frequency switchovers
Contingency situations
Third party link service provider
Radio signal:
Determination of the signal strength and health value
Threshold values which represent a critically degraded signal.
Minimum and average assured data rates
Minimum and average assured latencies
Design features and procedures to maintain availability, continuity, and integrity of the datalink:
RF or other interference
Flight beyond communications range
Antenna masking
Loss of CU functionality
Loss of UA functionality
Atmospheric attenuation
Safety features to mitigate the risk of loss of C2 link:
C2 links redundancy
Automatic triggering of an emergency recovery function
Automatic return to home
Safety features to mitigate the risk of harmful interference.
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 18

Communications

Antennas:
Type, model and manufacturer
Locations on the UAS
Communication method:
VHF
GSM network
Satellite
Safety features to mitigate the loss of communication function:
Primary communication means
Secondary / back-up communication means
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 19

Take-off and landing mechanisms

Wheels, skids, rails, launchers, etc.
If various mechanisms can be fitted:
Primary mechanism
Secondary mechanisms
Operational conditions/requirements for each mechanism.
Any other relevant information

CAP722A Table 20

Emergency recovery and safety systems

Mode of operation
Safety features which mitigate the risk of loss of control or situational awareness.
Means to verify normal system operation.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 21

External lighting

Type, model and manufacturer
Locations on the UA
Colour
Operation
Operating modes
Purpose
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 22

Payload

Types
Mass	Weight: 24±2 g Weight: 85±2 g
Interfaces with the UA:
Mechanical interface	Interface: USB-C Interface: USB-C
Electrical interface
Data interface
Release mechanism
Any other interface
Procedures to install the payload onto the UA.
Effects of the payload on the UA
Sensors	Sensor: 1/2-inch CMOS, Effective pixels: 12 MP Sensor: DJI Mavic 3E: 4/3 CMOS, Effective pixels: 20 MP DJI Mavic 3T: 1/2-inch CMOS, Effective pixels: 48 MP
Safety features to mitigate the risk of the payload affecting the flight of the UA:
Effects on aerodynamics
Effects of electro-magnetic interference.
Effects of electrical power and / or data connection failures on the UAS.
Effects of complete detachment of the payload from the UA (either caused by a failure or through intentional lowering / dropping of the payload).
Effects of partial detachment of the payload from the UA.
Distraction of the remote pilot generated by the payload during flight.
Procedures to verify the attachment points to the UA.
Procedures to verify the UA MTOM and CG location.
Procedures to detect and mitigate any failure of the payload in flight.
Safety provisions with regards to hazards inherent to the payload
Procedures in place for safe handling of the payload.
Means of identifying hazards.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Dimensions: 50.2 x 40.2 x 66.2 mm (L x W x H) Dimensions: 114.1 x 82.0 x 54.7 mm (L x W x H)

CAP722A Table 23

Ground support equipment

UAS launch and recovery systems
Power sources
Transportation equipment
Backup or emergency equipment
Procedures to transport UA, CU, battery/fuel, and other equipment between operation sites and from the loading/off-loading area to the take-off/landing area.
Storage of ground support equipment.
Suitability of the ground support equipment and transportation method with regards to the UAS components’ fragility, sensitivity or inherent hazards.
Ground support equipment standards
Ground support equipment manufacturer's recommendations.
Any other relevant information

CAP722A Table 24

Maintenance

Maintenance manual:
Structure
Maintenance procedures:
Inspections
Overhaul
Repairs
Assurance of repair procedures
Batteries maintenance during storage periods
Origin of each procedure
Maintenance schedules
Procedures to record maintenance that has been carried out.
Storage of maintenance records
Staff qualification and levels of approval.
Procedures to use the manual by the Maintenance staff
Configuration control
Any other relevant information

CAP722A Table 25

Spare parts procurement

Sources of procurement
Process to confirm the suitability of the part.
Any other relevant information

CAP722A Table 26

Change Management and modifications to the system

Hardware, software, and firmware version control
Modification standards
Modification records storage
Safety assessment associated with the modification
Any other relevant information

CAP722A Table 27

Safety features of the UAS

Step 1 – Identify the main functions of the UAS.
Step 2 – Identify the sub-functions.
Step 3 – Consider the ways each function may fail.
Step 4 – Identify the failure conditions.
Step 5 – Select those failure conditions that may lead to mid-air collision or harm to uninvolved people on the ground. (Identified Hazard)
Step 6 – Assurance
Step 7 – Describe the consequence of the failure condition.
Step 8 – Describe the failure modes. (Unmitigated Failures)
Step 9 – Identify the single points of failure.
Step 10 – Describe the risk mitigation means.

CAP722A Table 28

ANNEX - Manufacturer supplied data forDJI Mavic 3 Enterprise

Aircraft
Weight	DJI Mavic 3E: 915 g DJI Mavic 3T: 920 g
Max Takeoff Weight	DJI Mavic 3E: 1,050 g DJI Mavic 3T: 1,050 g
Dimensions	Folded (without propellers): 221 x 96.3 x 90.3 mm (L x W x H) Unfolded (without propellers): 347.5 x 283 x 107.7 mm (L x W x H)
Diagonal Distance	380.1 mm
Max Ascent Speed	6 m/s (Normal Mode) 8 m/s (Sport Mode)
Max Descent Speed	6 m/s (Normal Mode) 6 m/s (Sport Mode)
Max Flight Speed (at sea level, no wind)	15 m/s (Normal Mode) Forward: 21 m/s, Side: 20 m/s, Backward: 19 m/s (Sport Mode) [2]
Max Wind Speed Resistance	12 m/s [3]
Max Take-off Altitude Above Sea Level	6000 m (without payload)
Max Flight Time	45 mins [4]
Max Hover Time (without wind)	38 mins
Max Flight Distance	32 km
Max Tilt Angle	30 Deg. (Normal Mode) 35 Deg. (Sport Mode)
Max Angular Velocity	200 Deg./s
GNSS	GPS+Galileo+BeiDou+GLONASS (GLONASS is supported only when the RTK module is enabled)
Hovering Accuracy	Vertical: ±0.1 m (with Vision System); ±0.5 m (with GNSS); ±0.1 m (with RTK) Horizontal: ±0.3 m (with Vision System); ±0.5 m (with High-Precision Positioning System); ±0.1 m (with RTK)
Operating Temperature Range	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Internal Storage	N/A
Motor Model	2008
Propeller Model	9453F Propellers for Enterprise
Beacon	Built into the aircraft
Wide Camera
Sensor	DJI Mavic 3E: 4/3 CMOS, Effective pixels: 20 MP DJI Mavic 3T: 1/2-inch CMOS, Effective pixels: 48 MP
Lens	DJI Mavic 3E: FOV: 84 Deg. Format Equivalent: 24 mm Aperture: f/2.8-f/11 Focus: 1 m to ∞ DJI Mavic 3T: FOV: 84 Deg. Format Equivalent: 24 mm Aperture: f/2.8 Focus: 1 m to ∞
ISO Range	DJI Mavic 3E: 100-6400 DJI Mavic 3T: 100-25600
Shutter Speed	DJI Mavic 3E: Electronic Shutter: 8-1/8000 s Mechanical Shutter: 8-1/2000 s DJI Mavic 3T: Electronic Shutter: 8-1/8000 s
Max Image Size	DJI Mavic 3E: 5280 x 3956 DJI Mavic 3T: 8000 x 6000
Still Photography Modes	DJI Mavic 3E: Single: 20 MP Timed: 20 MP JPEG: 0.7/1/2/3/5/7/10/15/20/30/60 s JPEG+RAW: 3/5/7/10/15/20/30/60 s Smart Low-light Shooting: 20 MP Panorama: 20 MP (raw image) DJI Mavic 3T: Single: 12 MP/48 MP Timed: 12 MP/48 MP JPEG: 2/3/5/7/10/15/20/30/60 s* Panorama: 12 MP (raw image); 100 MP (stitched image) Smart Low-light Shooting: 12 MP * Shooting 48MP photo does not support 2s interval
Video Resolution	H.264 4K: 3840 x 2160@30fps FHD: 1920 x 1080@30fps
Bitrate	DJI Mavic 3E: 4K: 130 Mbps FHD: 70 Mbps DJI Mavic 3T: 4K: 85 Mbps FHD: 30 Mbps
Supported File Formats	exFAT
Photo Format	DJI Mavic 3E: JPEG/DNG (RAW) DJI Mavic 3T: JPEG
Video Format	MP4 (MPEG-4 AVC/H.264)
Tele Camera
Sensor	1/2-inch CMOS, Effective pixels: 12 MP
Lens	FOV: 15 Deg. Format Equivalent: 162 mm Aperture: f/4.4 Focus: 3 m to ∞
ISO Range	DJI Mavic 3E: 100-6400 DJI Mavic 3T: 100-25600
Shutter Speed	Electronic Shutter: 8-1/8000 s
Max Image Size	4000 x 3000
Photo Format	JPEG
Video Format	MP4 (MPEG-4 AVC/H.264)
Still Photography Modes	DJI Mavic 3E: Single: 12 MP Timed: 12 MP JPEG: 0.7/1/2/3/5/7/10/15/20/30/60 s Smart Low-light Shooting: 12 MP DJI Mavic 3T: Single: 12 MP Timed: 12 MP JPEG: 2/3/5/7/10/15/20/30/60 s Smart Low-light Shooting: 12 MP
Video Resolution	H.264 4K: 3840 x 2160@30fps FHD: 1920 x 1080@30fps
Bitrate	DJI Mavic 3E: 4K: 130 Mbps FHD: 70 Mbps DJI Mavic 3T: 4K: 85 Mbps FHD: 30 Mbps
Digital Zoom	8x (56x hybrid zoom)
Thermal Camera [5]
Thermal Imager	Uncooled VOx Microbolometer
Pixel Pitch	12 μm
Frame Rate	30 Hz
Lens	DFOV: 61 Deg. Format Equivalent: 40 mm Aperture: f/1.0 Focus: 5 m to ∞
Sensitivity	<=50 mk@F1.1
Temperature Measurement Method	Spot Meter, Area Measurement
Temperature Measurement Range	-20 Deg. to 150 Deg. C (-4 Deg. to 302 Deg. F, High Gain Mode) 0 Deg. to 500 Deg. C (32 Deg. to 932 Deg. F, Low Gain Mode)
Palette	White Hot/Black Hot/Tint/Iron Red/Hot Iron/Arctic/Medical/Fulgurite/Rainbow 1/Rainbow 2
Photo Format	JPEG (8-bit) R-JPEG (16-bit)
Video Resolution	640 x 512@30fps
Bitrate	6 Mbps
Video Format	MP4 (MPEG-4 AVC/H.264)
Still Photography Modes	DJI Mavic 3T: Single: 640 x 512 Timed: 640 x 512 JPEG: 2/3/5/7/10/15/20/30/60 s
Digital Zoom	28x
Infrared Wavelength	8-14 μm
Infrared Temperature Measurement Accuracy	±2 Deg. C or ±2% (using the larger value)
Gimbal
Stabilization	3-axis (tilt, roll, pan)
Mechanical Range	DJI Mavic 3E: Tilt: -135 Deg. to 100 Deg. Roll: -45 Deg. to 45 Deg. Pan: -27 Deg. to 27 Deg. DJI Mavic 3T: Tilt: -135 Deg. to 45 Deg. Roll: -45 Deg. to 45 Deg. Pan: -27 Deg. to 27 Deg.
Controllable Range	Tilt: -90 Deg. to 35 Deg. Pan: Not controllable
Max Control Speed (tilt)	100 Deg./s
Angular Vibration Range	±0.007 Deg.
Sensing
Type	Omnidirectional binocular vision system, supplemented with an infrared sensor at the bottom of the aircraft.
Forward	Measurement Range: 0.5-20 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <=15 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg.
Backward	Measurement Range: 0.5-16 m Effective Sensing Speed: Flight Speed <=12 m/s FOV: Horizontal 90 Deg., Vertical 103 Deg.
Lateral	Measurement Range: 0.5-25 m Effective Sensing Speed: Flight Speed <=15 m/s FOV: Horizontal 90 Deg., Vertical 85 Deg.
Upward	Measurement Range: 0.2-10 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Front and Back 100 Deg., Left and Right 90 Deg.
Downward	Measurement Range: 0.3-18 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Front and Back 130 Deg., Left and Right 160 Deg.
Operating Environment	Forward, Backward, Lateral, and Upward: Surface with a clear pattern and adequate lighting (lux >15) Downward: Diffuse reflective surface with diffuse reflectivity>20% (e.g. walls, trees, people) and adequate lighting (lux >15)
Video Transmission
Video Transmission System	DJI O3 Enterprise Transmission
Live View Quality	Remote Controller: 1080p/30fps
Operating Frequency	2.400-2.4835 GHz 5.725-5.850 GHz
Max Transmission Distance (free of interference)	Strong Interference (dense buildings, residential areas, etc.): 1.5-3 km (FCC/CE/SRRC/MIC) Medium Interference (suburban areas, city parks, etc.): 3-9 km (FCC), 3-6 km (CE/SRRC/MIC) Low Interference (open spaces, remote areas, etc.): 9-15 km (FCC), 6-8 km (CE/SRRC/MIC)
Max Download Speed	15 MB/s (with DJI RC Pro Enterprise)
Latency (depending on environmental conditions and mobile device)	Approx. 200 ms
Antenna	4 Antennas, 2T4R
Transmission Power (EIRP)	2.4 GHz: <33 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.8 GHz: <33 dBm (FCC), ＜30 dBm (SRRC), <14 dBm (CE)
DJI RC Pro Enterprise
Video Transmission System	DJI O3 Enterprise Transmission
Max Transmission Distance (unobstructed, free of interference) [7]	FCC: 15 km CE/SRRC/MIC: 8 km
Video Transmission Operating Frequency [6]	2.400-2.4835 GHz 5.725-5.850 GHz
Antenna	4 Antennas, 2T4R
Video Transmission Transmitter Power (EIRP)	2.4 GHz: <33 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.8 GHz: <33 dBm (FCC), <14 dBm (CE), ＜23 dBm (SRRC)
Wi-Fi Protocol	802.11 a/b/g/n/ac/ax Support 2 x 2 MIMO Wi-Fi
Wi-Fi Operating Frequency [6]	2.400-2.4835 GHz 5.150-5.250 GHz 5.725-5.850 GHz
Wi-Fi Transmitter Power (EIRP)	2.4 GHz: <26 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.1 GHz: <26 dBm (FCC), <23 dBm (CE/SRRC/MIC) 5.8 GHz: <26 dBm (FCC/SRRC), <14 dBm (CE)
Bluetooth Protocol	Bluetooth 5.1
Bluetooth Operating Frequency	2.400-2.4835 GHz
Bluetooth Transmitter Power (EIRP)	< 10 dBm
Screen Resolution	1920 x 1080
Screen Size	5.5 inches
Screen	60 fps
Brightness	1,000 nits
Touchscreen Control	10-point multi-touch
Battery	Li-ion (5000 mAh @ 7.2 V)
Charging Type	Recommended to be charged with the included DJI USB-C Power Adapter (100W) or USB charger at 12 V or 15 V
Rated Power	12 W
Storage Capacity	Internal Storage (ROM): 64 GB Supports a microSD card for expanded capacity.
Charging Time	Approx. 1 hour 30 minutes (with the included DJI USB-C Power Adapter (100W) only charging the remote controller or a USB charger at 15 V) Approx. 2 hours (with a USB charger at 12 V) Approx. 2 hours 50 minutes (with the included DJI USB-C Power Adapter (100W) charging the aircraft and remote controller simultaneously)
Operating Time	Approx. 3 hours
Video Output Port	Mini-HDMI port
Operating Temperature Range	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Storage Temperature	-30 Deg. to 60 Deg. C (-22 Deg. to 140 Deg. F) (within one month) -30 Deg. to 45 Deg. C (-22 Deg. to 113 Deg. F) (one to three months) -30 Deg. to 35 Deg. C (-22 Deg. to 95 Deg. F) (three to six months) -30 Deg. to 25 Deg. C (-22 Deg. to 77 Deg. F) (more than six months)
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Supported DJI Aircraft[10]	DJI Mavic 3E DJI Mavic 3T
GNSS	GPS+Galileo+GLONASS
Dimensions	Antennas folded and controller sticks unmounted: 183.27 x 137.41 x 47.6 mm (L x W x H) Antennas unfolded and controller sticks mounted: 183.27 x 203.35 x 59.84 mm (L x W x H)
Weight	Approx. 680 g
Model	RM510B
Storage
Supported Memory Cards	Aircraft: U3/Class10/V30 or above is required. A list of recommended microSD cards can be found below.
Recommended microSD Cards	Remote Controller: SanDisk Extreme PRO 64GB V30 A2 microSDXC SanDisk High Endurance 64GB V30 microSDXC SanDisk Extreme 128GB V30 A2 microSDXC SanDisk Extreme 256GB V30 A2 microSDXC SanDisk Extreme 512GB V30 A2 microSDXC Lexar 667x 64GB V30 A2 microSDXC Lexar High-Endurance 64GB V30 microSDXC Lexar High-Endurance 128GB V30 microSDXC Lexar 667x 256GB V30 A2 microSDXC Lexar 512GB V30 A2 microSDXC Samsung EVO Plus 64GB V30 microSDXC Samsung EVO Plus 128GB V30 microSDXC Samsung EVO Plus 256GB V30 microSDXC Samsung EVO Plus 512GB V30 microSDXC Kingston Canvas Go! Plus 128GB V30 A2 microSDXC Kingston Canvas React Plus 128GB V90 A1 microSDXC Aircraft: SanDisk Extreme 32GB V30 A1 microSDHC SanDisk Extreme PRO 32GB V30 A1 microSDHC SanDisk Extreme 512GB V30 A2 microSDXC Lexar 1066x 64GB V30 A2 microSDXC Kingston Canvas Go! Plus 64GB V30 A2 microSDXC Kingston Canvas React Plus 64GB V90 A1 microSDXC Kingston Canvas Go! Plus 128GB V30 A2 microSDXC Kingston Canvas React Plus 128GB V90 A1 microSDXC Kingston Canvas React Plus 256GB V90 A2 microSDXC Samsung PRO Plus 256GB V30 A2 microSDXC
Battery
Capacity	5000 mAh
Standard Voltage	15.4 V
Max Charging Voltage	17.6 V
Type	LiPo 4S
Chemical System	LiCoO2
Energy	77 Wh
Weight	335.5 g
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Charger
Input	100-240 V (AC Power), 50-60 Hz, 2.5 A
Output Power	100 W
Output	Max. 100 W (total) When both ports are used, the maximum output power of each interface is 82 W, and the charger will dynamically allocate the output power of the two ports according to the load power.
Charging Hub
Input	USB-C: 5-20 V, 5.0 A
Output	Battery Port: 12-17.6 V, 8.0 A
Rated Power	100 W
Charging Type	Three batteries charged in sequence
Charging Temperature Range	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
RTK Module
Dimensions	50.2 x 40.2 x 66.2 mm (L x W x H)
Weight	24±2 g
Interface	USB-C
Power	Approx. 1.2 W
RTK Positioning Accuracy	RTK Fix: Horizontal: 1 cm + 1 ppm; Vertical: 1.5 cm + 1 ppm
Speaker
Dimensions	114.1 x 82.0 x 54.7 mm (L x W x H)
Weight	85±2 g
Interface	USB-C
Rated Power	3 W
Max Volume [11]	110 dB @ 1 m
Effective Broadcast Distance [11]	100 m @ 70 dB
Bit Rate	16 Kbps/32 Kbps
Operating Temperature Range	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Other
Notes	[1] The standard weight of the aircraft (including the battery, propellers, and a microSD card). The actual product weight may vary due to differences in batch materials and external factors. [2] Maximum speed in Sport mode is 19m/s when operating in EU regions. [3] Max wind speed resistance during takeoff and landing. [4] Measured with Mavic 3 Enterprise Series flying at a constant speed of 32.4 kph in a windless environment at sea level until the battery reached 0%. Data is for reference only. Please pay attention to RTH reminders in the DJI Pilot 2 app during flight. [5] DO NOT expose the infrared camera lenses to strong sources of energy such as the sun, lava, or laser beams. Otherwise, the camera sensor may be burned, leading to permanent damage. [6] In some countries and regions, the 5.8 and 5.1GHz frequencies are prohibited, or the 5.1GHz frequency is only allowed for indoor use. Check local laws and regulations for more information. [7] Measured in an unobstructed environment free of interference. The above data shows the farthest communication range for one-way, non-return flights (with no payload) under each standard. During your flight, please pay attention to RTH reminders in the DJI Pilot 2 app. [8] Data tested under different standards in unobstructed environments with typical interference. Uses for reference purposes only and provides no guarantee as to the actual flight distance. [9] Measured in a laboratory environment with little interference in countries/regions that support both 2.4 GHz and 5.8 GHz. With footage saved on the officially recommended microSD cards. Download speeds may vary depending on actual conditions. [10] Will support more DJI aircraft in the future. Visit the official website for the latest information. [11] Data was measured in a controlled environment and is for reference only. Actual use experience may vary depending on software version, sound source, specific environment, and other conditions.

Data source: https://www.dji.com/mavic-3-enterprise/specs

Generated using dronespec.info
Source data acquired 2023-01-23 19:03:42

UAS OSC Volume 2

WARNING: This document was generated automatically and may contain errors and/or ommissions. You MUST review the data and satisfy yourself that it is complete and accurate. There is a link to the original source of the data below to help you do that.

Amendment record

Aircraft and systems description

UAS physical characteristics

UAS performance characteristics

UAS environmental limitations

Construction

Electrical power system

Propulsion system

Fuel system

Flight Controls system

Navigation

Detect and Avoid (DAA) systems

Other avionics systems

Command Unit (CU)

Command an Control (C2) link

Communications

Take-off and landing mechanisms

Emergency recovery and safety systems

External lighting

Payload

Ground support equipment

Maintenance

Spare parts procurement

Change Management and modifications to the system

Safety features of the UAS

ANNEX - Manufacturer supplied data forDJI Mavic 3 Enterprise

Aircraft

Wide Camera

Tele Camera

Thermal Camera [5]

Gimbal

Sensing

Video Transmission

DJI RC Pro Enterprise

Storage

Battery

Charger

Charging Hub

RTK Module

Speaker

Other