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.

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 3M
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass	Net Weight (with propellers and RTK module) [1]: 951 g
Maximum Take-Off Mass (MTOM)	Max Takeoff Weight: 1,050 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded (without propellers): 223 x 96.3 x 122.2 mm (Length x Width x Height) Unfolded (without propellers): 347.5 x 283 x 139.6 mm (Length x Width x Height) Diagonal Length: Diagonal: 380.1 mm
Width of aircraft body
Height of aircraft body
Propeller Configuration
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) Flying forward: 21 m/s, flying sideways: 20 m/s, flying backwards: 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 a payload)
Maximum operating height
Maximum flight time during normal operation	Max Flight Time: 43 minutes [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 [6]
Glide distances
Maximum radio range of the C2 Link

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: -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 Battery Type: LiPo 4S Chemical System: Lithium Cobalt
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Energy: 77 watt-hours 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
Engines:
Type, model and manufacturer	Motor Model Number: 2008
Propeller type, model and manufacturer	Propeller Model Number: 9453F Enterprise Edition
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 Number: 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 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 Position Accuracy: Fixed RTK: 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: Distance Measuring Range: 0.5 m to 20 m Detection Range: 0.5 m to 200 m Effective Obstacle Avoidance Speed: Flight Speed <=15 m/s FOV: Horizontal 90 Deg., vertical 103 Deg. Backward: Distance Measuring Range: 0.5 m to 16 m Effective Obstacle Avoidance Speed: Flight speed <=12 m/s FOV: Horizontal 90 Deg., vertical 103 Deg. Downward: Distance Measuring Range: 0.3 m to 18 m Effective Obstacle Avoidance Speed: Flight speed <=6 m/s FOV: Front and rear 130 Deg., left and right 160 Deg. Upward: Distance Measuring Range: 0.2 m to 10 m Effective Obstacle Avoidance Speed: Flight Speed <=6 m/s FOV: Front and rear 100 Deg., left and right 90 Deg. Operating Environment: Front, Rear, Left, Right, Above: Surfaces with clear patterns and adequate lighting (> 15 lux, environments with normal indoor fluorescent light exposure) Below: Surfaces with diffuse reflection material and a reflectivity of >20% (such as walls, trees, people, etc.); Adequate lighting (>15 lux, environments with normal indoor fluorescent light exposure) Sensing System Type: Omnidirectional binocular vision system, with an infrared sensor at the bottom of the aircraft Lateral: Distance Measuring Range: 0.5 m to 25 m Effective Obstacle Avoidance Speed: Flight speed <=15 m/s FOV: Horizontal 90 Deg., vertical 85 Deg.
Devices used
Technology used
Interface between the DAA system and the flight control computer
Limitations of the DAA system
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: Lithium-ion battery (5000 mAh, 7.2 V) Rated Power: 12 Watts
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: -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	Antennas: 4 antennas, 2 transmitting and 4 receiving
Locations on the UAS
Transceivers / Modems:
Power levels	Wi-Fi Operating Band and 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 Operating Band: 2.400-2.4835 GHz 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
Maximum power output/range	Max Effective Signal Distance (Unobstructed, No interference) [8]: FCC: 15 km CE: 8 km SRRC: 8 km MIC: 8 km
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
Interfaces with the UA:
Mechanical interface	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	Image Sensor: 4/3 CMOS Effective Pixels: 20 MP Image Sensor: 1/2.8-inch CMOS, effective pixels: 5 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 (Length x Width x Height)

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 3M

Aircraft
Net Weight (with propellers and RTK module) [1]	951 g
Max Takeoff Weight	1,050 g
Dimensions	Folded (without propellers): 223 x 96.3 x 122.2 mm (Length x Width x Height) Unfolded (without propellers): 347.5 x 283 x 139.6 mm (Length x Width x Height)
Diagonal Length	Diagonal: 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) Flying forward: 21 m/s, flying sideways: 20 m/s, flying backwards: 19 m/s (Sport mode) [2]
Max Wind Speed Resistance	12 m/s [3]
Max Take-off Altitude Above Sea Level	6000 m (without a payload)
Max Flight Time	43 minutes [4]
Max Hover Time (without wind)	37 minutes [4]
Max Flight Distance	32 km [6]
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 RTK module is enabled)
Hovering Accuracy Range	Vertical: ±0.1 m (Vision Positioning enabled); ±0.5 m (GNSS Positioning enabled); ±0.1 m (D-RTK enabled) Horizontal: ±0.3 m (Vision Positioning enabled); ±0.5 m (HD Positioning enabled); ±0.1 m (RTK enabled)
Operating Temperature	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Internal Storage	N/A
Motor Model Number	2008
Propeller Model Number	9453F Enterprise Edition
Light Sensor	Built-in module
RGB Camera
Image Sensor	4/3 CMOS Effective Pixels: 20 MP
Lens	FOV: 84 Deg. Equivalent focal length: 24 mm Aperture: f/2.8 to f/11 Focus: 1 m to ∞
ISO Range	100-6400
Shutter speed	Electronic shutter: 8-1/8000 s Mechanical shutter: 8-1/2000 s
Max Image Size	5280 x 3956
Photo Shooting Mode	Single shot: 20 MP Timelapse: 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 Panorama: 20 MP (original material)
Video Resolution	H.264: 4K: 3840 x 2160@30fps FHD: 1920 x 1080@30fps
Max Video Bitrate	4K: 130Mbps FHD: 70Mbps
Supported File System	exFAT
Image Format	JPEG/DNG (RAW)
Video Format	MP4 (MPEG-4 AVC/H.264)
Multispectral Camera
Image Sensor	1/2.8-inch CMOS, effective pixels: 5 MP
Lens	FOV: 73.91 Deg. (61.2 Deg. x 48.10 Deg.) Equivalent focal length: 25 mm Aperture: f/2.0 Focus: Fixed Focus
Multispectral Camera Band	Green (G): 560 ± 16 nm; Red (R): 650 ± 16 nm; Red Edge (RE): 730 ± 16 nm; Near infrared (NIR): 860 ± 26 nm;
Gain Range	1x-32x
Shutter Speed	Electronic Shutter: 1/30~1/12800 s
Max Image Size	2592 x 1944
Image Format	TIFF
Video Format	MP4 (MPEG-4 AVC/H.264)
Photo Shooting Mode	Single shot: 5 MP Timelapse: 5 MP TIFF: 2/3/5/7/10/15/20/30/60 s
Video Resolution	H.264 FHD: 1920 x 1080@30fps Video content: NDVI/GNDVI/NDRE
Max Video Bitrate	Stream: 60 Mbps
Gimbal
Stabilization System	3-axis mechanical gimbal (tilt, roll, pan)
Mechanical Range	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: Uncontrollable
Max Control Speed (tilt)	100 Deg./s
Angular Vibration Range	±0.007 Deg.
Sensing System
Sensing System Type	Omnidirectional binocular vision system, with an infrared sensor at the bottom of the aircraft
Forward	Distance Measuring Range: 0.5 m to 20 m Detection Range: 0.5 m to 200 m Effective Obstacle Avoidance Speed: Flight Speed <=15 m/s FOV: Horizontal 90 Deg., vertical 103 Deg.
Backward	Distance Measuring Range: 0.5 m to 16 m Effective Obstacle Avoidance Speed: Flight speed <=12 m/s FOV: Horizontal 90 Deg., vertical 103 Deg.
Lateral	Distance Measuring Range: 0.5 m to 25 m Effective Obstacle Avoidance Speed: Flight speed <=15 m/s FOV: Horizontal 90 Deg., vertical 85 Deg.
Upward	Distance Measuring Range: 0.2 m to 10 m Effective Obstacle Avoidance Speed: Flight Speed <=6 m/s FOV: Front and rear 100 Deg., left and right 90 Deg.
Downward	Distance Measuring Range: 0.3 m to 18 m Effective Obstacle Avoidance Speed: Flight speed <=6 m/s FOV: Front and rear 130 Deg., left and right 160 Deg.
Operating Environment	Front, Rear, Left, Right, Above: Surfaces with clear patterns and adequate lighting (> 15 lux, environments with normal indoor fluorescent light exposure) Below: Surfaces with diffuse reflection material and a reflectivity of >20% (such as walls, trees, people, etc.); Adequate lighting (>15 lux, environments with normal indoor fluorescent light exposure)
Video Transmission
Video Transmission System	DJI O3 Image Transmission Industry Edition
Live View Quality	Remote Controller: 1080p/30fps
Operating Band [7]	2.400-2.4835 GHz 5.725-5.850 GHz
Max Effective Signal Distance (Unobstructed, No interference) [8]	FCC: 15 km CE: 8 km SRRC: 8 km MIC: 8 km
Max Transmission Distance (free of interference)	Strong Interference (urban landscapes, residential areas, etc.): 1.5-3 km (FCC/CE/SRRC/MIC) Medium Interference (suburban landscapes, city parks, etc.): 3-9 km (FCC), 3-6 km (CE/SRRC/MIC) Weak Interference (remote fields, open farmland, etc.): 9-15 km (FCC), 6-8 km (CE/SRRC/MIC)
Max Download Speed	15 MB/s (with DJI RC Pro Industry Edition)
Latency (depending on environmental conditions and mobile device)	Approximately 200 milliseconds
Antennas	4 antennas, 2 transmitting and 4 receiving
Transmitter 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)
Other	Supports the DJI Cellular module
DJI RC Pro Enterprise Edition
Image Transmission System	DJI O3 Image Transmission Industry Edition
Max Effective Signal Distance (Unobstructed, No interference) [8]	FCC: 15 km CE: 8 km SRRC: 8 km MIC: 8 km
Operating Band of Image Transmission [7]	2.400-2.4835 GHz 5.725-5.850 GHz
Antennas	4 antennas, 2 transmitting and 4 receiving
Operating Band of Image Transmission and 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 Band [7]	2.400-2.4835 GHz 5.150-5.250 GHz 5.725-5.850 GHz
Wi-Fi Operating Band and 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 Band	2.400-2.4835 GHz
Bluetooth Transmitter Power (EIRP)	<10 dBm
Screen Resolution	1920 x 1080
Screen Size	5.5 inches
Screen Frame Rate	60 fps
Screen Brightness	1,000 nits
Touch-Screen	10-point multi-touch
Battery	Lithium-ion battery (5000 mAh, 7.2 V)
Charging Type	100W Battery Charging Hub or USB charger with 12V or 15V specifications is recommended
Rated Power	12 Watts
Storage Capacity	Internal Memory (ROM): 64 GB Supports microSD card usage to increase storage capacity
Charging Time	Approx. 1.5 hours (measured when only using the 100W Battery Charging Hub to charge the remote control, or when using a 15V USB charger) Approximately 2 hours (measured using a 12V USB charger) Approximately 2 hours and 50 minutes (measured using the 100W Battery Charging Hub to charge the aircraft and remote control at the same time)
Operating Time	Approx. 3 hours
Video Output Port	Mini-HDMI Port
Operating Temperature	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg.F)
Storage Temperature Range	<1 month: -30 Deg. to 60 Deg. C (-22 Deg. to 140 Deg. F) One to three months: -30 Deg. to 45 Deg. C (-22 Deg. to 113 Deg. F) Three to six months: -30 Deg. to 35 Deg. C (-22 Deg. to 95 Deg. F) More than six months: -30 Deg. to 25 Deg. C (-22 Deg. to 77 Deg. F)
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Supported DJI Aircraft [10]	DJI Mavic 3E DJI Mavic 3T DJI Mavic 3M
GNSS	GPS + Galileo + GLONASS
Dimensions	Antenna is folded and no control sticks are installed: 183.27 x 137.41 x 47.6 mm (Length x Width x Height) Antenna unfolded and control sticks are installed: 183.27 x 203.35 x 59.84 mm (Length x Width x Height)
Weight	Approx. 680 g
Model Number	RM510B
Storage
Supported microSD Cards	Aircraft: Please use a memory card with a speed rating of V30 or higher, or use a memory card from the recommended list
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
Battery Type	LiPo 4S
Chemical System	Lithium Cobalt
Energy	77 watt-hours
Weight	335.5 g
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Battery Charger
Input	100V to 240V (AC), 50Hz to 60Hz, 2.5A
Output Power	100 Watts
Output	Maximum output power of 100 Watts (total) When both the ports are used, the maximum output power of one interface is 82 W, and the charger will dynamically allocate the output power of the two interfaces according to load power.
Charging Hub
Input	USB-C: 5V to 20V, 5.0A
Output	Battery Port: 12V to 17.6V, 8.0A
Rated Power	100 Watts
Charging Type	3 batteries on charging rotation
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
RTK Module
Dimensions	50.2 x 40.2 x 66.2 mm (Length x Width x Height)
Weight	24±2 g
Interface	USB-C
Power	Approximately 1.2 watts
RTK Position Accuracy	Fixed RTK: Horizontal: 1 cm + 1 ppm; Vertical: 1.5 cm + 1 ppm
Notes
Footnotes	1. Standard weight of the aircraft (including battery, propellers, and microSD card). The actual product weight may vary due to differences in batch materials and external factors. Use for reference only. 2. The max speed in the EU cannot exceed 19 m/s. 3. Max wind resistance during takeoff and landing. 4. Data measured using the DJI Mavic 3M in a wind-free environment while flying at sea level at a constant speed of 36 kph until there was 0% power remaining. For reference only. Please pay attention to Return to Home prompts in the DJI Pilot 2 app when flying. 5. Data measured using the DJI Mavic 3M in a wind-free environment hovering over the sea level until there was 0% power remaining. For reference only. Please pay attention to Return to Home prompts in the DJI Pilot 2 app when flying. 6. Data measured using the DJI Mavic 3M in a wind-free environment while flying at sea level at 57.6 kph until there was 0% power remaining. For reference only. Please pay attention to Return to Home prompts in the DJI Pilot 2 app when flying. 7. In some countries, the 5.1/5.8GHz frequencies are prohibited, or the 5.1GHz frequency is only allowed for indoor use. Please refer to local laws and regulations before use. 8. Data measured flying in an unobstructed outdoor environment free of interference. It shows the farthest communication range for one-way, non-Return to Home flights under each standard. Please pay attention to Return to Home prompts in the DJI Pilot 2 app when flying. 9. Data measured in an unobstructed environment with typical interference under various standards. The actual flight distance may vary and is for reference only. 10. The DJI RC Plus will support more DJI aircraft in the future.

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

Generated using dronespec.info
Source data acquired 2023-01-23 19:03:43

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 3M

Aircraft

RGB Camera

Multispectral Camera

Gimbal

Sensing System

Video Transmission

DJI RC Pro Enterprise Edition

Storage

Battery

Battery Charger

Charging Hub

RTK Module

Notes