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	Air 2S
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Takeoff Weight: 595 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded: 180 x 97 x 77 mm (length x width x height) Unfolded: 183 x 253 x 77 mm (length x width x height) Diagonal Length: 302 mm
Width of aircraft body
Height of aircraft body
Propeller Configuration	Propellers: Quick release, low noise, folding
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): 19 m/s (S Mode) 15 m/s (N Mode) 5 m/s (C Mode)
Minimum airspeed to maintain safe flight
Normal/typical operating height
Maximum operating height	Max Service Ceiling Above Sea Level: 5000 m
Maximum flight time during normal operation	Max Flight Time: 31 minutes
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: 18.5 km
Glide distances
Maximum radio range of the C2 Link

CAP722A Table 8

UAS environmental limitations

Wind speed limits	Max Wind Speed Resistance: 10.7 m/s
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature Range: 0 Deg. to 40 Deg.C (32 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[1]: 3750 mAh / 3500 mAh Battery Type: LiPo 3S Built-in Battery: N/A
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Voltage: 11.04 V / 11.55 V Energy: 41.4 Wh / 40.42 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 Range: 5 Deg. to 40 Deg.C (41 Deg. to 104 Deg.F)

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	Model: RM330
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+GLONASS+GALILEO
Quantity
Telemetry links
Method to determine current position.
Method to navigate to intended destination.	Compass: Single Compass
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	Forward: Precision Measurement Range: 0.38-23.8 m Effective Sensing Speed: <=15 m/s Field of View (FOV): 72 Deg. (horizontal), 58 Deg. (vertical) Backward: Precision Measurement Range: 0.37-23.4 m Effective Sensing Speed: <=12 m/s Field of View (FOV): 57 Deg. (horizontal), 44 Deg. (vertical) Downward: ToF Measurement Range: 0.1-8 m Hovering Range: 0.5-30 m Vision Sensor Hovering Range: 0.5-60 m Left/Right: N/A Upward: Precision Measurement Range: 0.34-28.6 m Field of View (FOV): 63 Deg. (horizontal), 78 Deg. (vertical)
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 Life: 6 hours (4 hours when charging a mobile device)
Radio signal:
Determination of the signal strength and health value.
Threshold values which represent a critically degraded signal.
Control handover between two CUs	Multiple Controllers: N/A
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	Max Battery Life: Approx. 4 hours Operating Temperature: -10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F) Operating Temperature: 0 Deg. to 40 Deg.C (32 Deg. to 104 Deg.F)

CAP722A Table 17

Command an Control (C2) link

RLOS
BRLOS
Antennas:
Type, model and manufacturer
Locations on the UAS
Transceivers / Modems:
Power levels	Transmission Power (EIRP): 2.4 GHz: FCC: <=30 dBm CE: <=20 dBm SRRC: <=20 dBm MIC: <=20 dBm 5.8 GHz: FCC: <=30 dBm CE: <=14 dBm SRRC: <=29 dBm Transmitter Power (EIRP): 2.400-2.4835 GHz: <26 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.725-5.850 GHz: <26 dBm (FCC), <23 dBm (SRRC), <14 dBm (CE) Transmitter Power (EIRP): 2.400-2.4835 GHz: < 26 dBm (FCC), < 20 dBm (CE/SRRC/MIC) 5.725-5.850 GHz: < 26 dBm (FCC), < 23 dBm (SRRC), < 14 dBm (CE) Wi-Fi Transmitter Power (EIRP): 2.400-2.4835 GHz: < 23 dBm (FCC), < 20 dBm (CE/SRRC/MIC) 5.150-5.250 GHz: < 23 dBm (FCC/CE/SRRC/MIC) 5.725-5.850 GHz: < 23 dBm (FCC/SRRC), < 14 dBm (CE) Bluetooth Transmitter Power (EIRP): 2.400-2.4835 GHz: < 10 dBm
Transmission schemes	Remote Controller Transmission System: When used with different aircraft hardware configurations, DJI RC-N1 Remote Controllers will automatically select the corresponding firmware version for updating and support the following transmission technologies enabled by the hardware performance of the linked aircraft models: a. DJI Mini 2/ DJI Mavic Air 2: O2 b. DJI Air 2S: O3 c. DJI Mavic 3: O3+ Video Transmission System: DJI O3 Bluetooth Protocol: Bluetooth 4.2 Wi-Fi Protocol: 802.11 a/b/g/n
Operating frequencies
Details of frequency spectrum approvals	Operating Frequency: 2.4 GHz 5.8 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.	IMU: Single IMU
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	Downward Auxiliary Light: Single LED
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	Sensor: 1" CMOS Effective Pixels: 20 MP; 2.4μm Pixel Size
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 Air 2S

Aircraft
Takeoff Weight	595 g
Dimensions	Folded: 180 x 97 x 77 mm (length x width x height) Unfolded: 183 x 253 x 77 mm (length x width x height)
Diagonal Length	302 mm
Max Ascent Speed	6 m/s (S Mode) 6 m/s (N Mode)
Max Descent Speed	6 m/s (S Mode) 6 m/s (N Mode)
Max Service Ceiling Above Sea Level	5000 m
Max Flight Time	31 minutes
Max Hovering Time	30 minutes * * The flight time was measured in a controlled test environment. Specific test conditions are as follows: No wind, at sea level, constant flight speed of 32.4 kph, APAS off, AirSense off, camera parameters set to 1080p/24fps, video mode off, and flying from 100% battery to 0% battery. Results may vary depending on environment, usage scenario, and firmware version.
Max Flight Distance	18.5 km
Max Flight Speed (at sea level, no wind)	19 m/s (S Mode) 15 m/s (N Mode) 5 m/s (C Mode)
Max Wind Speed Resistance	10.7 m/s
Max Tilt Angle	35 Deg. (S Mode) Front: 30 Deg., Back: 20 Deg., Left: 35 Deg., Right: 35 Deg. (N Mode)
Max Angular Velocity	250 Deg./s (S Mode) 90 Deg./s (N Mode) 60 Deg./s (C Mode)
Operating Temperature Range	0 Deg. to 40 Deg.C (32 Deg. to 104 Deg.F)
Operating Frequency	2.4 GHz 5.8 GHz
Transmission Power (EIRP)	2.4 GHz: FCC: <=30 dBm CE: <=20 dBm SRRC: <=20 dBm MIC: <=20 dBm 5.8 GHz: FCC: <=30 dBm CE: <=14 dBm SRRC: <=29 dBm
Hovering Accuracy Range	Vertical: ± 0.1 m (with vision positioning) ± 0.5 m (with GNSS positioning) Horizontal: ± 0.1 m (with vision positioning) ± 1.5 m (with GNSS positioning)
Propellers	Quick release, low noise, folding
Aircraft Arms	Foldable
GNSS	GPS+GLONASS+GALILEO
Compass	Single Compass
IMU	Single IMU
Internal Storage	8 GB
Intelligent Flight Battery
Capacity[1]	3750 mAh / 3500 mAh
Voltage	11.04 V / 11.55 V
Max Charging Voltage	12.6 V / 13.2 V
Battery Type	LiPo 3S
Energy	41.4 Wh / 40.42 Wh
Weight	198 g
Charging Temperature Range	5 Deg. to 40 Deg.C (41 Deg. to 104 Deg.F)
Max Charging Power	38 W
Built-in Battery	N/A
Camera
Sensor	1" CMOS Effective Pixels: 20 MP; 2.4μm Pixel Size
Lens	FOV: 88 Deg. 35 mm Format Equivalent: 22 mm Aperture: f/2.8 Shooting Range: 0.6 m to ∞
ISO Range	Video: 100-3200 (Auto) 100-6400 (Manual) 10-Bit Dlog-M Video: 100-800 (Auto) 100-1600 (Manual) Photo: 100-3200 (Auto) 100-12800 (Manual)
Still Image Size	20 MP 5472 x 3648 (3:2) 5472 x 3078 (16:9)
Still Photography Modes	Single shot: 20 MP Burst shooting: 20 MP (continuous burst) Auto Exposure Bracketing (AEB): 20 MP, 3/5 bracketed frames at 0.7 EV bias Timed: 20 MP, 2/3/5/7/10/15/20/30/60s SmartPhoto (including HDR and HyperLight): 20 MP HDR Panorama[2]: Vertical (3 x 1): 3328 x 8000 (width x height) Wide-angle (3 x 3): 8000 x 6144 (width x height) 180 Deg. (3 x 7): 8192 x 3500 (width x height) Sphere (3 x 8+1): 8192 x 4096 (width x height) JPEG/DNG (RAW)
Video Resolution	5.4K: 5472 x 3078 @ 24/25/30 fps 4K Ultra HD: 3840 x 2160 @ 24/25/30/48/50/60 fps 2.7K: 2688x1512 @ 24/25/30/48/50/60 fps FHD: 1920 x 1080 @ 24/25/30/48/50/60/120 fps MP4/MOV (H.264/MPEG-4 AVC, H.265/HEVC)
Max Video Bitrate	150 Mbps
Supported File System	FAT32/exFAT Supports a microSD card with a capacity of up to 256 GB.
Digital Zoom	Zoom recording is not available while recording 10-bit videos and 120fps videos. 4K/30fps: 4x; 2.7K/60fps: 4x; 2.7K/30fps: 6x; 1080p/60fps: 6x; 1080p/30fps: 8x
Gimbal
Stabilization	3-axis (tilt, roll, pan)
Mechanical Range	Tilt: -135 Deg. to 45 Deg. Roll: -45 Deg. to 45 Deg. Pan: -100 Deg. to 100 Deg.
Pan Axis	Not Controllable
Controllable Range	Tilt: -90 Deg. to 0 Deg.(default); -90 Deg. to 24 Deg. (extended)
Max Controllable Speed (tilt)	100 Deg./s
Angular Vibration Range	±0.01 Deg.
Sensing System
Forward	Precision Measurement Range: 0.38-23.8 m Effective Sensing Speed: <=15 m/s Field of View (FOV): 72 Deg. (horizontal), 58 Deg. (vertical)
Backward	Precision Measurement Range: 0.37-23.4 m Effective Sensing Speed: <=12 m/s Field of View (FOV): 57 Deg. (horizontal), 44 Deg. (vertical)
Downward	ToF Measurement Range: 0.1-8 m Hovering Range: 0.5-30 m Vision Sensor Hovering Range: 0.5-60 m
Left/Right	N/A
Upward	Precision Measurement Range: 0.34-28.6 m Field of View (FOV): 63 Deg. (horizontal), 78 Deg. (vertical)
Downward Auxiliary Light	Single LED
Video Transmission
Transmission System	O3 2.4 GHz/5.8 GHz Auto-Switching (compatible with OcuSync 2.0) 4-antenna 2T4R
Max Transmission Distance (free of interference)	12 km (FCC), 8 km (CE) 8 km (SRRC), 8 km (MIC)
Live View Quality/Latency	Drone + Remote Controller: 1080p/30fps 12 Mbps 120 ms Drone + DJI Smart Controller: 1080p/30fps 12Mbps 130 ms
Max Transmission Bitrate	44 Mbps (download bitrate) 16 Mbps (live video bitrate)
Operating Frequency	2.4 GHz 5.8 GHz
DJI RC-N1 Remote Controller
Multiple Controllers	N/A
DJI Smart Controller	Supported
Remote Controller Transmission System	When used with different aircraft hardware configurations, DJI RC-N1 Remote Controllers will automatically select the corresponding firmware version for updating and support the following transmission technologies enabled by the hardware performance of the linked aircraft models: a. DJI Mini 2/ DJI Mavic Air 2: O2 b. DJI Air 2S: O3 c. DJI Mavic 3: O3+
Battery Life	6 hours (4 hours when charging a mobile device)
Supported Mobile Device Connectors	Lightning, Micro USB, USB-C
Max Supported Mobile Device Size	180 x 86 x 10 mm (length x width x height)
Operating Temperature	0 Deg. to 40 Deg.C (32 Deg. to 104 Deg.F)
Transmitter Power (EIRP)	2.400-2.4835 GHz: <26 dBm (FCC), <20 dBm (CE/SRRC/MIC) 5.725-5.850 GHz: <26 dBm (FCC), <23 dBm (SRRC), <14 dBm (CE)
DJI RC
Model	RM330
Video Transmission System	DJI O3
Transmitter Power (EIRP)	2.400-2.4835 GHz: < 26 dBm (FCC), < 20 dBm (CE/SRRC/MIC) 5.725-5.850 GHz: < 26 dBm (FCC), < 23 dBm (SRRC), < 14 dBm (CE)
Storage Capacity	DJI RC's storage capacity can be increased by using a microSD card. Users can store images and videos on the card and export them to a computer or other devices.
Video Output Port	N/A
Max Battery Life	Approx. 4 hours
Operating Temperature	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Supported SD Cards	UHS-I Speed Class 3 or above is required. A list of recommended microSD cards can be found below.
Recommended microSD Cards	SanDisk Extreme 64GB V30 A1 microSDXC SanDisk Extreme 128GB V30 A2 microSDXC SanDisk Extreme 256GB V30 A2 microSDXC SanDisk Extreme 512GB V30 A2 microSDXC SanDisk Extreme Pro 64GB V30 A2 microSDXC SanDisk Extreme Pro 256GB V30 A2 microSDXC SanDisk Extreme Pro 400GB V30 A2 microSDXC SanDisk High Endurance 64GB V30 microSDXC SanDisk High Endurance 256GB V30 microSDXC Kingston Canvas Go!Plus 64GB V30 A2 microSDXC Kingston Canvas Go!Plus 256GB V30 A2 microSDXC Lexar High Endurance 64GB V30 microSDXC Lexar High Endurance 128GB V30 microSDXC Lexar 633x 256GB V30 A1 microSDXC Lexar 1066x 64GB V30 A2 microSDXC Samsung EVO Plus 512GB microSDXC
Wi-Fi Transmitter Power (EIRP)	2.400-2.4835 GHz: < 23 dBm (FCC), < 20 dBm (CE/SRRC/MIC) 5.150-5.250 GHz: < 23 dBm (FCC/CE/SRRC/MIC) 5.725-5.850 GHz: < 23 dBm (FCC/SRRC), < 14 dBm (CE)
Bluetooth Protocol	Bluetooth 4.2
Bluetooth Transmitter Power (EIRP)	2.400-2.4835 GHz: < 10 dBm
Wi-Fi Protocol	802.11 a/b/g/n
Charger
Charging Input	100-240V, 50/60 Hz, 1.3 A
Charging Output	Charging Port: 13.2 V⎓2.82 A USB Port: 5 V⎓2 A
Voltage	13.2 V
Rated Power	38 W
Footnotes:
	2. To ensure the Panorama quality, the aircraft will crop the panoramic photos made out of multiple images. Therefore, the photo resolution may vary in different shooting scenarios.

Data source: https://www.dji.com/air-2s/specs

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Source data acquired 2023-01-23 19:03:42