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 4 Pro
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Takeoff Weight: Approx. 1063 g Product weight may vary due to differences in batch materials and other factors.
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded (with propellers): 257.6 x 124.8 x 106.6 mm (L x W x H) Folded (without propellers): 257.6 x 124.8 x 103.4 mm (L x W x H) Unfolded (without propellers): 328.7 x 390.5 x 135.2 mm (L x W x H)
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 Horizontal Speed (at sea level, no wind): At sea level, in windless conditions: 25 m/s* (Sport Mode) 15 m/s (tracking status) At sea level, with 2 m/s tailwind, while flying in the same direction as the wind: 27 m/s* (Sport Mode) 15 m/s (tracking status) * Measured in a wind tunnel test environment with the aircraft taking off from an altitude of 0 m and ascending vertically by 1.5 m in Sport mode. Data is for reference only. Always pay attention to reminders on the camera view during your flight.
Minimum airspeed to maintain safe flight
Normal/typical operating height	Max Takeoff Altitude: 6000 m Maximum takeoff altitude is 3000 m with DJI Mavic 4 Pro Propeller Guards.
Maximum operating height
Maximum flight time during normal operation	Max Flight Time: 51 minutes Measured by the aircraft flying forward at a constant speed of 32.4 kph in a windless environment at sea level, with Obstacle Avoidance Action set to Brake, in photo mode, and from 100% battery level until 0%. Actual experience may vary depending on the environment, usage, and firmware version.
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: 41 km Measured by the aircraft flying forward at a constant speed of 54 kph in a windless environment at sea level, with Obstacle Avoidance Action set to Brake, in photo mode, and from 100% battery level until 0%. Actual experience may vary depending on the environment, usage, and firmware version.
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 (39.4 ft/s)
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature: -10 Deg.C to 40 Deg.C (14 Deg.F 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: 6654 mAh Battery Type: Li-ion 4S Chemical System: LiNiMnCoO2
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Nominal Voltage: 14.32 V Energy: 95.3 Wh
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) Charging Time: Using the DJI Mavic 240W Power Adapter with no other devices connected to the charger or the Charging Hub's USB-C port From 0% to 100%: 1 battery takes about 51 minutes, 3 batteries take about 90 minutes (200 V to 240 V input) or about 110 minutes (100 V to 127 V input) Using DJI 100W USB-C Power Adapter From 0% to 100%: 1 battery takes about 80 minutes Charging via the aircraft (65W max charging power) From 0% to 100%: 115 minutes Charging time is measured in a test environment with a temperature of 25 Deg.C. Actual charging time may increase due to higher ambient temperatures or variations in mains voltage between regions.

CAP722A Table 11

Propulsion system

Propulsion type
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
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	Global Navigation Satellite System: GPS + Galileo + BeiDou
Quantity
Telemetry links
Method to determine current position.
Method to navigate to intended destination.
Automatic/automated navigation functions
Geo-awareness functions
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

CAP722A Table 15

Detect and Avoid (DAA) systems

DAA system functions	Sensing Type: Omnidirectional binocular vision system, supplemented with forward-facing LiDAR and an infrared sensor at the bottom of the aircraft Forward: Measurement Range: 0.5-24 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <= 18 m/s FOV: Horizontal 180 Deg., Vertical 180 Deg. Backward: Measurement Range: 0.5-22 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <= 18 m/s FOV: Horizontal 180 Deg., Vertical 180 Deg. Lateral: Measurement Range: 0.5-21 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <= 18 m/s FOV: Horizontal 180 Deg., Vertical 180 Deg. Upward: Measurement Range: 0.5-18 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Horizontal 90 Deg., Vertical 90 Deg. Downward: Measurement Range: 0.5-17 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Horizontal 180 Deg., vertical 180 Deg.
Devices used
Technology used
Interface between the DAA system and the flight control computer
Limitations of the DAA system	Operating Environment: Forward, Backward, Left, Right, and Upward: Surfaces with discernible patterns, adequate lighting (lux > 0.1, urban lighting environment). Downward: Surfaces with discernible patterns, diffuse reflectivity > 20% (e.g. walls, trees, people), and adequate lighting (lux > 0.1, urban lighting environment).
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.
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

CAP722A Table 17

Command an Control (C2) link

RLOS
BRLOS
Antennas:
Type, model and manufacturer
Locations on the UAS
Transceivers / Modems:
Power levels	Transmitter Power (EIRP): 2.4 GHz: < 23 dBm (FCC) < 20 dBm (CE/SRRC/MIC) 5.8 GHz: < 23 dBm (FCC/SRRC) < 14 dBm (CE) Transmitter Power (EIRP): < 10 dBm
Transmission schemes	Protocol: 802.11 a/b/g/n/ac/ax
Operating frequencies
Details of frequency spectrum approvals	Operating Frequency[1]: 2.4000-2.4835 GHz 5.725-5.850 GHz Operating frequency allowed varies among countries and regions. Please refer to local laws and regulations for more information. Operating Frequency: 2.4000-2.4835 GHz Operating frequency allowed varies among countries and regions. Please refer to local laws and regulations for more information.
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
Interfaces with the UA:
Mechanical interface
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: Hasselblad Camera: 4/3 CMOS, Effective Pixels: 100 MP Medium Tele Camera: 1/1.3-inch CMOS, Effective Pixels: 48 MP Tele Camera: 1/1.5-inch CMOS, Effective Pixels: 50 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

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 4 Pro

Aircraft
Takeoff Weight	Approx. 1063 g Product weight may vary due to differences in batch materials and other factors.
Dimensions	Folded (with propellers): 257.6 x 124.8 x 106.6 mm (L x W x H) Folded (without propellers): 257.6 x 124.8 x 103.4 mm (L x W x H) Unfolded (without propellers): 328.7 x 390.5 x 135.2 mm (L x W x H)
Max Ascent Speed	10 m/s (Sport Mode) 6 m/s (Normal Mode) 6 m/s (Cine Mode)
Max Descent Speed	10 m/s (Sport Mode) 6 m/s (Normal Mode) 6 m/s (Cine Mode)
Max Horizontal Speed (at sea level, no wind)	At sea level, in windless conditions: 25 m/s* (Sport Mode) 15 m/s (tracking status) At sea level, with 2 m/s tailwind, while flying in the same direction as the wind: 27 m/s* (Sport Mode) 15 m/s (tracking status) * Measured in a wind tunnel test environment with the aircraft taking off from an altitude of 0 m and ascending vertically by 1.5 m in Sport mode. Data is for reference only. Always pay attention to reminders on the camera view during your flight.
Max Takeoff Altitude	6000 m Maximum takeoff altitude is 3000 m with DJI Mavic 4 Pro Propeller Guards.
Max Flight Time	51 minutes Measured by the aircraft flying forward at a constant speed of 32.4 kph in a windless environment at sea level, with Obstacle Avoidance Action set to Brake, in photo mode, and from 100% battery level until 0%. Actual experience may vary depending on the environment, usage, and firmware version.
Max Hovering Time	45 minutes Measured by the aircraft hovering in a windless environment at sea level, with Obstacle Avoidance Action set to Brake, in photo mode, and from 100% battery level until 0%. Actual experience may vary depending on the environment, usage, and firmware version.
Max Flight Distance	41 km Measured by the aircraft flying forward at a constant speed of 54 kph in a windless environment at sea level, with Obstacle Avoidance Action set to Brake, in photo mode, and from 100% battery level until 0%. Actual experience may vary depending on the environment, usage, and firmware version.
Max Wind Speed Resistance	12 m/s (39.4 ft/s)
Max Pitch Angle	35 Deg.
Operating Temperature	-10 Deg.C to 40 Deg.C (14 Deg.F to 104 Deg.F)
Global Navigation Satellite System	GPS + Galileo + BeiDou
Hovering Accuracy Range	Vertical: ±0.1 m (with vision positioning) ±0.5 m (with satellite positioning) Horizontal: ±0.3 (with vision positioning) ±0.5 m (with satellite positioning)
Internal Storage	Mavic 4 Pro: 64GB (available storage space is approximately 42GB) Mavic 4 Pro 512GB (Creator Combo): 512GB (available storage space is approximately 460GB)
	C2 (EU)
Camera
Image Sensor	Hasselblad Camera: 4/3 CMOS, Effective Pixels: 100 MP Medium Tele Camera: 1/1.3-inch CMOS, Effective Pixels: 48 MP Tele Camera: 1/1.5-inch CMOS, Effective Pixels: 50 MP
Lens	Hasselblad Camera FOV: 72 Deg. Format Equivalent: 28 mm Aperture: f/2.0 to f/11 Focus: 2 m to ∞ Medium Tele Camera FOV: 35 Deg. Format Equivalent: 70 mm Aperture: f/2.8 Focus: 3 m to ∞ Tele Camera FOV: 15 Deg. Format Equivalent: 168 mm Aperture: f/2.8 Focus: 3 m to ∞
ISO Range	Hasselblad Camera Video Normal: 100-12800 (Normal) 400-6400 (D-Log) 100-6400 (D-Log M) 100-6400 (HLG) Slow Motion: 100-6400 (Normal) 400-3200 (D-Log) 100-3200 (D-Log M) 100-3200 (HLG) Photo 100-6400 (25 MP) 100-3200 (100 MP) Medium Tele Camera and Tele Camera Video Normal: 100-12800 (Normal) 400-3200 (D-Log) 100-3200 (D-Log M) 100-3200 (HLG) Slow Motion: 100-6400 (Normal) 400-3200 (D-Log) 100-3200 (D-Log M) 100-3200 (HLG) Photo 100-6400 (12 MP) 100-3200 (48 MP and 50 MP)
Shutter Speed	Hasselblad Camera 25MP Single Shot: 1/16000-16 s (over 2 s for simulated long exposure) 100MP Single Shot: 1/8000-8 s 25 MP Auto Exposure Bracketing (AEB)/Burst Shooting/Timed: 1/16000-8 s 100 MP Auto Exposure Bracketing (AEB)/Burst Shooting/Timed: 1/8000-8 s Medium Tele Camera 12 MP Single Shot: 1/16000-8 s (over 2 s for simulated long exposure) 48 MP Single Shot: 1/8000-2 s 12 MP Auto Exposure Bracketing (AEB)/Burst Shooting/Timed: 1/16000-2 s 48 MP Auto Exposure Bracketing (AEB)/Burst Shooting/Timed: 1/8000-2 s Tele Camera 12.5 MP Single Shot: 1/16000-8 s (over 1 s for simulated long exposure) 50 MP Single Shot: 1/16000-2 s 12.5 MP Auto Exposure Bracketing (AEB)/Burst Shooting/Timed: 1/16000-2 s 50 MP Auto Exposure Bracketing (AEB)/Burst Shooting/Timed: 1/16000-2 s
Max Image Size	Hasselblad Camera: 12288 x 8192 Medium Tele Camera: 8064 x 6048 Tele Camera: 8192 x 6144
Still Photography Modes	Hasselblad Camera Single Shot: 25 MP, 100 MP Automatic Exposure Bracketing (AEB): 25 MP, 3/5/7 frames at 0.7 EV step; 100 MP, 3/5 frames at 0.7 EV step Burst Shooting: 25 MP, 3/5/7 frames; 100 MP, 3/5 frames Timed: 25 MP, 1 (Mavic 4 Pro 512GB)/2/3/5/7/10/15/20/30/60 seconds; 100 MP, 2 (Mavic 4 Pro 512GB)/3 (Mavic 4 Pro 512GB)/5 (Mavic 4 Pro 512GB)/7 (Mavic 4 Pro 512GB)/10/15/20/30/60 seconds Medium Tele Camera Single Shot: 12 MP, 48 MP Automatic Exposure Bracketing (AEB): 12 MP, 3/5/7 frames at 0.7 EV step; 48 MP, 3/5/7 frames at 0.7 EV step Burst Shooting: 12 MP, 3/5/7 frames; 48 MP, 3/5/7 frames Timed: 12 MP, 1 (Mavic 4 Pro 512GB)/2/3/5/7/10/15/20/30/60 seconds; 48 MP, 1 (Mavic 4 Pro 512GB)/2 (Mavic 4 Pro 512GB)/3 (Mavic 4 Pro 512GB)/5/7/10/15/20/30/60 seconds Tele Camera Single Shot: 12.5 MP, 50 MP Auto Exposure Bracketing (AEB): 12.5 MP, 3/5/7 frames at 0.7 EV step; 50 MP, 3/5/7 frames at 0.7 EV step Burst Shooting: 12.5 MP, 3/5/7 frames; 50 MP, 3/5/7 frames Timed: 12.5 MP, 1 (Mavic 4 Pro 512GB)/2/3/5/7/10/15/20/30/60 seconds; 50 MP, 1 (Mavic 4 Pro 512GB)/2 (Mavic 4 Pro 512GB)/3 (Mavic 4 Pro 512GB)/5/7/10/15/20/30/60 seconds
Photo Format	JPEG DNG (RAW)
Video Resolution	Hasselblad Camera H.264 ALL-I/H.265 Standard* 6K: 6016 x 3384@24/25/30/48/50/60fps DCI 4K: 4096 x 2160@24/25/30/48/50/60/120fps 4K: 3840 x 2160@24/25/30/48/50/60/120fps FHD: 1920 x 1080@24/25/30/48/50/60fps 4K Vertical Shooting: 2160 x 3840@24/25/30/48/50/60fps H.264 Standard FHD: 1920 x 1080@24/25/30/48/50/60fps Medium Tele Camera H.264 ALL-I/H.265 Standard* 4K: 3840 x 2160@24/25/30/48/50/60/120*fps FHD: 1920 x 1080@24/25/30/48/50/60fps 2.7K Vertical Shooting: 1512 x 2688@24/25/30/48/50/60fps H.264 Standard FHD: 1920 x 1080@24/25/30/48/50/60fps 2.7K Vertical Shooting: 1512 x 2688@24/25/30/48/50/60fps Tele Camera H.264 ALL-I/H.265 Standard 4K: 3840 x 2160@24/25/30/48/50/60/100*fps FHD: 1920 x 1080@24/25/30/48/50/60fps 2.7K Vertical Shooting: 1512 x 2688@24/25/30/48/50/60fps H.264 Standard FHD: 1920 x 1080@24/25/30/48/50/60fps 2.7K Vertical Shooting: 1512 x 2688@24/25/30/48/50/60fps Only Mavic 4 Pro 512GB (Creator Combo) supports H.264 ALL-I recording. ** Recording frame rates. The corresponding video plays as a slow-motion video.
Video Format	MP4 (H.264 ALL-I/H.264 Standard/H.265 Standard) Only Mavic 4 Pro 512GB (Creator Combo) supports H.264 ALL-I recording.
Max Video Bitrate	H.264 Standard Bitrate: 90 Mbps H.265 Standard Bitrate: 180 Mbps H.264 ALL-I Bitrate: 1200 Mbps Only Mavic 4 Pro 512GB (Creator Combo) supports H.264 ALL-I recording.
Supported File System	exFAT
Color Mode and Sampling Method	Hasselblad Camera Normal Color: 10-bit 4:2:2 (H.264 ALL-I) 10-bit 4:2:0 (H.265 Standard) 8-bit 4:2:0 (H.264 Standard) HLG/D-Log M/D-Log: 10-bit 4:2:2 (H.264 ALL-I) 10-bit 4:2:0 (H.265 Standard) Medium Tele Camera Normal Color: 10-bit 4:2:2 (H.264 ALL-I) 10-bit 4:2:0 (H.265 Standard) 8-bit 4:2:0 (H.264 Standard) HLG/D-Log M/D-Log: 10-bit 4:2:2 (H.264 ALL-I) 10-bit 4:2:0 (H.265 Standard) Tele Camera Normal Color: 10-bit 4:2:2 (H.264 ALL-I) 10-bit 4:2:0 (H.265 Standard) 8-bit 4:2:0 (H.264 Standard) HLG/D-Log M/D-Log: 10-bit 4:2:2 (H.264 ALL-I) 10-bit 4:2:0 (H.265 Standard) Only Mavic 4 Pro 512GB (Creator Combo) supports H.264 ALL-I recording.
Digital Zoom	Hasselblad Camera: 1x to 2.5x Medium Tele Camera: 2.5x to 6x Tele Camera: 6x to 24x
Gimbal
Stabilization	3-axis mechanical gimbal (tilt, roll, pan)
Mechanical Range	Tilt: -164 Deg. to 160 Deg. Roll: -90 Deg. to 450 Deg. Pan: -22 Deg. to 22 Deg.
Controllable Range	Tilt: -90 Deg. to 70 Deg. Roll: -40 Deg. to 400 Deg.
Max Control Speed (tilt)	Tilt: 100 Deg./s Roll: 100 Deg./s
Angular Vibration Range	Hovering Without Wind: ±0.001 Deg. Normal Mode: ±0.003 Deg. Sport Mode: ±0.005 Deg.
Sensing
Sensing Type	Omnidirectional binocular vision system, supplemented with forward-facing LiDAR and an infrared sensor at the bottom of the aircraft
Forward	Measurement Range: 0.5-24 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <= 18 m/s FOV: Horizontal 180 Deg., Vertical 180 Deg.
Backward	Measurement Range: 0.5-22 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <= 18 m/s FOV: Horizontal 180 Deg., Vertical 180 Deg.
Lateral	Measurement Range: 0.5-21 m Detection Range: 0.5-200 m Effective Sensing Speed: Flight Speed <= 18 m/s FOV: Horizontal 180 Deg., Vertical 180 Deg.
Upward	Measurement Range: 0.5-18 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Horizontal 90 Deg., Vertical 90 Deg.
Downward	Measurement Range: 0.5-17 m Effective Sensing Speed: Flight Speed <=6 m/s FOV: Horizontal 180 Deg., vertical 180 Deg.
	Forward-Facing LiDAR Measurement Range (nighttime): 0.5-25 m (reflectivity > 10%) FOV: Up and Down 60 Deg., Left and Right 60 Deg. Downward-Facing Infrared Sensor Measurement Range: 0.3-8 m (reflectivity > 10%) FOV: Front and Back 60 Deg., Left and Right 60 Deg.
Operating Environment	Forward, Backward, Left, Right, and Upward: Surfaces with discernible patterns, adequate lighting (lux > 0.1, urban lighting environment). Downward: Surfaces with discernible patterns, diffuse reflectivity > 20% (e.g. walls, trees, people), and adequate lighting (lux > 0.1, urban lighting environment).
Video Transmission
Video Transmission System	O4+
Live View Quality	Remote Controller: 1080p/30fps, 1080p/60fps
Operating Frequency	2.4000-2.4835 GHz 5.170-5.250 GHz 5.725-5.850 GHz Operating frequency allowed varies among countries and regions. Please refer to local laws and regulations for more information.
Transmitter Power (EIRP)	2.4 GHz: < 33 dBm (FCC) < 20 dBm (CE/SRRC/MIC) 5.1 GHz: < 23 dBm (CE) 5.8 GHz: < 33 dBm (FCC) < 14 dBm (CE) < 30 dBm (SRRC)
Max Transmission Distance (free of interference)	Low Interference and Obstructed by Buildings: Approx. 0-0.7 km Low Interference and Obstructed by Trees: Approx. 0.7-4.5 km Measured under FCC standard in obstructed environments with typical low interference. Used for reference purposes only and provides no guarantee for actual transmission distance.
Max Download Speed	O4+: 10 MB/s* Wi-Fi 6: 80 MB/s* * Measured in a laboratory environment with little interference in countries/regions that support both 2.4 GHz and 5.8 GHz, with footage saved to the internal storage. Download speeds may vary depending on the actual conditions.
Lowest Latency	Compatible with DJI RC 2/ DJI RC Pro 2 Remote Controller: approx. 130 ms Depending on the actual environment and mobile device.
Antenna	6 antennas, 2T4R
Wi-Fi
Protocol	802.11 a/b/g/n/ac/ax
Operating Frequency[1]	2.4000-2.4835 GHz 5.725-5.850 GHz Operating frequency allowed varies among countries and regions. Please refer to local laws and regulations for more information.
Transmitter Power (EIRP)	2.4 GHz: < 23 dBm (FCC) < 20 dBm (CE/SRRC/MIC) 5.8 GHz: < 23 dBm (FCC/SRRC) < 14 dBm (CE)
Bluetooth
Protocol	Bluetooth 5.1
Operating Frequency	2.4000-2.4835 GHz Operating frequency allowed varies among countries and regions. Please refer to local laws and regulations for more information.
Transmitter Power (EIRP)	< 10 dBm
Battery
Capacity	6654 mAh
Weight	Approx. 332 g
Nominal Voltage	14.32 V
Max Charging Voltage	17.2 V
Battery Type	Li-ion 4S
Chemical System	LiNiMnCoO2
Energy	95.3 Wh
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Charging Time	Using the DJI Mavic 240W Power Adapter with no other devices connected to the charger or the Charging Hub's USB-C port From 0% to 100%: 1 battery takes about 51 minutes, 3 batteries take about 90 minutes (200 V to 240 V input) or about 110 minutes (100 V to 127 V input) Using DJI 100W USB-C Power Adapter From 0% to 100%: 1 battery takes about 80 minutes Charging via the aircraft (65W max charging power) From 0% to 100%: 115 minutes Charging time is measured in a test environment with a temperature of 25 Deg.C. Actual charging time may increase due to higher ambient temperatures or variations in mains voltage between regions.
Battery Charging Hub
Input	USB-C Port: 5 V to 20 V, max 5 A Mini SDC Port: 11.2 V to 17.6 V, max 15 A
Output	Battery Port: 10 V to 17.2 V, max 12 A
Rated Power	USB-C Port: Supports up to 100 W Mini SDC Port: Supports up to 240 W/15 A
Charging Type	When used with the DJI Mavic 240W Power Adapter: Supports parallel charging of three batteries (The Parallel Charging Hub will prioritize the battery with the lowest charge and switch to parallel charging once all three batteries reach the same charge level.) When used with the DJI 100W USB-C Power Adapter: Charges three batteries in sequence.
Compatibility	DJI Mavic 4 Pro Intelligent Flight Battery
Storage
Recommended microSD Cards	Lexar Silver plus 64GB A2 V30 microSDXC Lexar Silver plus 128GB A2 V30 microSDXC Lexar Silver plus 256GB A2 V30 microSDXC Lexar Silver plus 512GB A2 V30 microSDXC Lexar Silver plus 1TB A2 V30 microSDXC Kingston CANVAS GO! Plus 64GB A2 V30 microSDXC Kingston CANVAS GO! Plus 128GB A2 V30 microSDXC Kingston CANVAS GO! Plus 256GB A2 V30 microSDXC Kingston CANVAS GO! Plus 512GB A2 V30 microSDXC

Data source: https://www.dji.com/uk/mavic-4-pro/specs

Generated using dronespec.info
Source data acquired 2023-01-23 13:14:42