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 2 Enterprise Series
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Takeoff Weight: Zoom Edition:905 g Dual Edition:899 g Max Takeoff Weight: 1100 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded: 214 x 91 x 84 mm Unfolded: 322 x 242 x 84 mm Unfolded+Spotlight: 322 x 242 x 114 mm Unfolded+Beacon: 322 x 242 x 101 mm Unfolded+Speaker: 322 x 242 x 140 mm Diagonal Length: 354 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 Speed (near sea level, no wind): 72 kph (S-mode，without wind) 50 kph (P-mode，without wind)
Minimum airspeed to maintain safe flight
Normal/typical operating height
Maximum operating height	Max Service Ceiling Above Sea Level: 6000 m
Maximum flight time during normal operation	Max Flight Time: 31 min (at a consistent speed of 25 kph)
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)
Glide distances
Maximum radio range of the C2 Link	Max Transmission Distance (unobstructed, free of interference): 2.400 - 2.483 GHz; 5.725 - 5.850 GHz FCC: 10000 m CE: 6000 m SRRC: 6000 m MIC: 6000 m

CAP722A Table 8

UAS environmental limitations

Wind speed limits	Max Wind Speed Resistance: 29-38 kph
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature Range: -10 Deg.C to 40 Deg.C
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]: 3850 mAh Battery Type: LiPo
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Voltage: 15.4 V Energy: 59.29 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	Net Weight: 297 g Charging Time: 90 min Charging Temperature: 5 Deg.C - 40 Deg.C Operating Temperature Range: -10 Deg.C to 40 Deg.C Heating Methods: Manual Heating；Auto Heating Heating Temperature: -20 Deg.C to 6 Deg.C Heating duration: 600s (Max) Heating Power: 35W (Max)

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	GNSS: GPS+GLONASS
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	Forward: Precision Measurement Range:0.5 - 20 m Detectable Range: 20 - 40 m Effective Sensing Speed: <= 14m/s FOV: Horizontal: 40 Deg., Vertical: 70 Deg. Backward: Precision Measurement Range: 0.5 - 16 m Detectable Range: 16 - 32 m Effective Sensing Speed: <= 12m/s FOV: Horizontal: 60 Deg., Vertical: 77 Deg. Downward: Precision Measurement Range: 0.5 - 11 m Detectable Range: 11 - 22 m Upward: Precision Measurement Range: 0.1 - 8 m Operating Environment: Forward, Backward and Sides: Surface with clear pattern and adequate lighting (lux > 15) Upward: Detects diffuse reflective surfaces (>20%) (walls, trees, people, etc.) Downward: Surface with clear pattern and adequate lighting (lux > 15) Detects diffuse reflective surfaces (>20%) (walls, trees, people, etc.) Sensing System: Omnidirectional Obstacle Sensing [3] Sides: Precision Measurement Range:0.5 - 10 m Effective Sensing Speed: <= 8m/s FOV: Horizontal: 80 Deg., Vertical: 65 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: 3950mAh
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: 0 Deg.C to 40 Deg.C

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): 2.400 - 2.4835 GHz FCC: <=26 dBm CE: <=20 dBm SRRC: <=20 dBm MIC: <=20 dBm5.725-5.850 GHz FCC: <=26 dBm CE: <=14 dBm SRRC: <=26 dBm Transmitter Power (EIRP): 2.4 - 2.4835 GHz FCC: <=26 dBm；CE: <=20 dBm；SRRC: <=20 dBm MIC: <=20 dBm 5.725 - 5.850 GHz FCC: <=26 dBm；CE: <=14 dBm；SRRC: <=26 dBm
Transmission schemes
Operating frequencies
Details of frequency spectrum approvals	Operating Frequency: 2.400 - 2.4835 GHz 5.725 - 5.850 GHz Operating Frequency: 2.400 - 2.483 GHz; 5.725 - 5.850 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
Interfaces with the UA:
Mechanical interface
Electrical interface	Port Type: USB Micro-B Port Type: USB Micro-B
Data interface
Release mechanism
Any other interface
Procedures to install the payload onto the UA.
Effects of the payload on the UA
Sensors	Sensor: 1/2.3" CMOS; Effective pixels: 12M Sensor: Uncooled VOx Microbolometer Sensor: 1/2.3" CMOS； Effective pixels:12 Megapixels
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).	Port Type: USB Micro-B
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 2 Enterprise Series

Aircraft
Takeoff Weight	Zoom Edition:905 g Dual Edition:899 g
Max Takeoff Weight	1100 g
Dimensions	Folded: 214 x 91 x 84 mm Unfolded: 322 x 242 x 84 mm Unfolded+Spotlight: 322 x 242 x 114 mm Unfolded+Beacon: 322 x 242 x 101 mm Unfolded+Speaker: 322 x 242 x 140 mm
Diagonal Length	354 mm
Max Ascent Speed	5 m/s (S-mode[1]) 4 m/s (P-mode) 4 m/s (S-mode with accessories[1]) 4 m/s (P-mode with accessories)
Max Descent Speed	3 m/s (S-mode[1]) 3 m/s (P-mode)
Max Speed (near sea level, no wind)	72 kph (S-mode，without wind) 50 kph (P-mode，without wind)
Max Service Ceiling Above Sea Level	6000 m
Max Flight Time	31 min (at a consistent speed of 25 kph)
Max Hovering Time	29 min 27 min (with beacon turned on) 28 min (with beacon turned off) 22 min (with spotlight turned on) 26 min (with spotlight turned off) 25 min (with speaker turned on) 26 min (with speaker turned off)
Max Wind Speed Resistance	29-38 kph
Max Tilt Angle	35 Deg. (S-mode, with remote controller) 25 Deg. (P-mode)
Max Angular Velocity	200 Deg./s（S-Mode) 100 Deg./s（P-Mode) 200 Deg./s（S-Mode) 100 Deg./s（P-Mode)
Operating Temperature Range	-10 Deg.C to 40 Deg.C
GNSS	GPS+GLONASS
Hovering Accuracy Range	Vertical: ±0.1 m (with Vision Positioning) ±0.5 m (with GPS Positioning) Horizontal: ±0.3m (with Vision Positioning) ±1.5 m (with GPS Positioning)
Operating Frequency	2.400 - 2.4835 GHz 5.725 - 5.850 GHz
Transmission Power (EIRP)	2.400 - 2.4835 GHz FCC: <=26 dBm CE: <=20 dBm SRRC: <=20 dBm MIC: <=20 dBm5.725-5.850 GHz FCC: <=26 dBm CE: <=14 dBm SRRC: <=26 dBm
Internal Storage	24 GB
M2ED Visual Camera
Sensor	1/2.3" CMOS; Effective pixels: 12M
Lens	FOV: approx. 85 Deg. 35 mm format equivalent:24 mm Aperture: f/2.8 Focus: 0.5 m to ∞
ISO Range	Video: 100-12800 (auto) Photo: 100-1600 (auto)
Max Image Size	4056 x 3040（4:3) ；4056 x 2280（16:9)
Still Photography Modes	Single shot Burst shooting: 3/5/7 frames Interval (2/3/5/7/10/15/20/30/60 s)
Video Recording Modes	4K Ultra HD: 3840 x 2160 30p 2.7K: 2688 x 1512 30p FHD: 1920 x 1080 30p
Max Video Bitrate	100 Mbps
Photo	JPEG
Video Format	MP4，MOV (MPEG-4 AVC/H.264)
Gimbal
Mechanical Range	Tilt: -135 - +45 Deg. Pan: -100 - +100 Deg.
Controllable Range	Tilt: -90 - +30 Deg. Pan: -75 - +75 Deg.
Stabilization	3-axis (tilt, roll, pan)
Max Control Speed (tilt)	120 Deg./s
Angular Vibration Range	±0.005 Deg.
Remote Controller
Operating Frequency	2.400 - 2.483 GHz; 5.725 - 5.850 GHz
Max Transmission Distance (unobstructed, free of interference)	2.400 - 2.483 GHz; 5.725 - 5.850 GHz FCC: 10000 m CE: 6000 m SRRC: 6000 m MIC: 6000 m
Operating Temperature Range	0 Deg.C to 40 Deg.C
Transmitter Power (EIRP)	2.4 - 2.4835 GHz FCC: <=26 dBm；CE: <=20 dBm；SRRC: <=20 dBm MIC: <=20 dBm 5.725 - 5.850 GHz FCC: <=26 dBm；CE: <=14 dBm；SRRC: <=26 dBm
Battery	3950mAh
Charging Time	2 hours 15 min
Operating Current/Voltage	1800mA ⎓ 3.83V
Mobile Device Holder	Thickness Supported:6.5-8.5 mm，Max length: 160 mm
RC Size	Folded: 145 x 80 x 48 mm (L x W x H) Unfolded: 190 x 115 x 100 mm (L x W x H)
Supported USB Port Types	Lightning, Micro USB (Type-B), USB Type-C™
Charger
Input	100-240V， 50-60Hz， 1.8A
Output	Main: 17.6V ⎓ 3.41A or 17.0V⎓3.53 USB: 5 V ⎓ 2 A
Voltage	17.6±0.1V
Rated Power	60W
M2E Spotlight
Dimensions	68x60x41 mm
Port Type	USB Micro-B
Operating Range	30 m
Power	Max 26W
Illuminance	FOV17 Deg., Max: 11lux @ 30m Straight
App / Live View
Video Transmission System	OcuSync 2.0
Mobile App	DJI PILOT
Live View Quality	Remote Controller: 720p@30fps / 1080p@30fps
Max Live View Bitrate	40 Mbps
Latency	120 - 130 ms
Required Operating Systems	ios 10.0 or later Android 5.0 or later
Footnotes:
Footnotes	[1] Remote controller required. [2] Due to real-time digital enhancements, the photo and video size of the thermal data is larger than the sensor's native resolution. [3] Omnidirectional Obstacle Sensing includes left/right, up/down, and forward/backward obstacle sensing. Sensing for left/right directions is only available in ActiveTrack or Tripod Mode. Omnidirectional Obstacle Sensing does not fully cover the circumference of a 360-degree arc. And left and right obstacle sensing system only works in specific modes and environments. DJI warranty does not cover any loss caused by crashing when flying left or right, even when ActiveTrack or Tripod mode is activated. Please be aware of your surroundings and App notifications when operating the Mavic 2 to ensure safety. These specs have been determined through tests conducted with the latest firmware. Firmware updates can enhance performance, so updating to the latest firmware is highly recommended." [4]These specs have been determined through tests conducted with the latest firmware. Firmware updates can enhance performance, so updating to the latest firmware is highly recommended."
	The terms HDMI, HDMI High-Definition Multimedia Interface, HDMI Trade dress and the HDMI Logos are trademarks or registered trademarks of HDMI Licensing Administrator, Inc.
M2ED Thermal Camera
Sensor	Uncooled VOx Microbolometer
Lens	HFOV: 57 Deg. Aperture: f/1.1
Sensor Resolution	160 x 120
Pixel Pitch	12 μm
Spectral Band	8-14 μm
Image Size [2]	640 x 480 (4:3); 640 x 360 (16:9)
Still Photography Modes	Single shot Burst shooting: 3/5/7 frames
Video Recording Modes	640 x 360 @8.7fps
Accuracy	High Gain: Max ±5% (typical) Low Gain: Max ±10% (typical)
Scene Range	High Gain: -10 Deg. to +140 Deg.C Low Gain: -10 Deg.to +400 Deg.C
Photo	JPEG
Video	MP4, MOV (MPEG-4 AVC/H.264)
M2E Camera
Sensor	1/2.3" CMOS； Effective pixels:12 Megapixels
Lens	FOV: 82.6 Deg.(24 mm)；47.8 Deg.(48 mm) Format equivalent: 24-48 mm Aperture: f/2.8(24 mm)-f/3.8(48 mm) Auto focus at : 0.5 - ∞
ISO Range	Video: 100-3200 Photo: 100-1600(Auto) 100-12800(Manual)
Shutter Speed	8-1/8000s
Still Image Size	4000 x 3000
Still Photography Modes	Single shot Burst shooting: 3/5/7 frames Auto Exposure Bracketing (AEB): 3/5 bracketed frames at 0.7 EV Bias Interval (JPEG: 2/3/5/7/10/15/20/30/60s RAW:5/7/10/15/20/30/60s)
Video Resolution	4K: 3840 x 2160 24/25/30p 2.7K: 2720 x 1530 24/25/30/48/50/60p FHD: 1920 x 1080 24/25/30/48/50/60/120p
Max Video Bitrate	100 Mbps
Supported File System	FAT32(<= 32 GB )；exFAT(> 32 GB)
Photo Format	JPEG，DNG (RAW)
Video Format	MP4 / MOV (MPEG-4 AVC/H.264)
Sensing System
Sensing System	Omnidirectional Obstacle Sensing [3]
Forward	Precision Measurement Range:0.5 - 20 m Detectable Range: 20 - 40 m Effective Sensing Speed: <= 14m/s FOV: Horizontal: 40 Deg., Vertical: 70 Deg.
Backward	Precision Measurement Range: 0.5 - 16 m Detectable Range: 16 - 32 m Effective Sensing Speed: <= 12m/s FOV: Horizontal: 60 Deg., Vertical: 77 Deg.
Upward	Precision Measurement Range: 0.1 - 8 m
Downward	Precision Measurement Range: 0.5 - 11 m Detectable Range: 11 - 22 m
Sides	Precision Measurement Range:0.5 - 10 m Effective Sensing Speed: <= 8m/s FOV: Horizontal: 80 Deg., Vertical: 65 Deg.
Operating Environment	Forward, Backward and Sides: Surface with clear pattern and adequate lighting (lux > 15) Upward: Detects diffuse reflective surfaces (>20%) (walls, trees, people, etc.) Downward: Surface with clear pattern and adequate lighting (lux > 15) Detects diffuse reflective surfaces (>20%) (walls, trees, people, etc.)
Intelligent Flight Battery
Capacity[1]	3850 mAh
Voltage	15.4 V
Max Charging Voltage	17.6 V
Battery Type	LiPo
Energy	59.29 Wh
Net Weight	297 g
Charging Temperature	5 Deg.C - 40 Deg.C
Operating Temperature Range	-10 Deg.C to 40 Deg.C
Heating Methods	Manual Heating；Auto Heating
Heating Temperature	-20 Deg.C to 6 Deg.C
Heating duration	600s (Max)
Heating Power	35W (Max)
Charging Time	90 min
Max Charging Power	80W
M2E Beacon
Dimensions	68x40x27.8 mm
Port Type	USB Micro-B
Power	Avg. 1.6W
Controllable Range	5000 m
Light intensity	Min Angle: 55 cd； Light intensity: 157 cd
M2E Speaker
Dimensions	68x55x65 mm
Port Type	USB Micro-B
Power	Max 10W
Decibel	100 db @ 1 meter distance
Bitrate	16 kbps
Supported SD Cards
Supported SD Cards	Micro SD™ Supports a microSD with capacity of up to 128 GB. A UHS-I Speed Grade 3 rating microSD card is required.

Data source: https://www.dji.com/mavic-2-enterprise/info#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 2 Enterprise Series

Aircraft

M2ED Visual Camera

Gimbal

Remote Controller

Charger

M2E Spotlight

App / Live View

Footnotes:

M2ED Thermal Camera

M2E Camera

Sensing System

Intelligent Flight Battery

M2E Beacon

M2E Speaker

Supported SD Cards