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	Matrice 4T
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Takeoff Weight: 1229 g* * The standard weight of the aircraft (including the battery, propellers, and a microSD card). The actual product weight may vary due to differences in batch materials and external factors. Max Takeoff Weight: Standard Propellers: 1420 g Low-Noise Propellers: 1430 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded: 260.6 x 113.7 x 138.4 mm (L x W x H) Unfolded: 307.0 x 387.5 x 149.5 mm (L x W x H) Maximum dimensions excluding propellers. Diagonal Wheelbase: 438.8 mm
Width of aircraft body
Height of aircraft body
Propeller Configuration	Propeller Model: 1157F (standard propellers) 1154F (low noise propeller)
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): 21 m/s 21 m/s flying forward, 18 m/s flying backward, 19 m/s flying sideways* * No faster than 19 m/s with Sport mode in EU regions.
Minimum airspeed to maintain safe flight
Normal/typical operating height
Maximum operating height
Maximum flight time during normal operation	Max Flight Time: 49 min (standard propellers) 46 min (low-noise propellers) Measured with the aircraft flying at approximately 8 m/s without payloads in a windless environment until the battery level reached 0%. Data is for reference only. Actual usage time may vary depending on the flight mode, accessories, and environment. Please pay attention to reminders in the app.
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: 35 km (standard propellers) 32 km (low-noise propellers) Measured by the aircraft hovering in a windless environment at sea level, from 100% battery level until 0%.
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* * Max wind speed resistance during takeoff and landing.
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[1]: 6741 mAh
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Energy: 99.5 Wh
Electrical load shedding functionality	Discharge Rate: 4C
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

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 + Galileo + BeiDou + GLONASS* * GLONASS is supported only when the RTK module is enabled.
Quantity
Telemetry links
Method to determine current position.
Method to navigate to intended destination.
Automatic/automated navigation functions
Geo-awareness functions
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 a 3D infrared sensor at the bottom of the aircraft. Forward: Binocular Measurement Range: 0.4-22.5 m Measurement Range: 0.4-200 m Obstacle Avoidance Speed: Flight Speed <=21 m/s FOV: 90 Deg. (horizontal), 135 Deg. (vertical) Backward: Measurement Range: 0.4-22.5 m Measurement Range: 0.4-200 m Obstacle Avoidance Speed: Flight Speed <=21 m/sField of View (FOV)-90 Deg. (horizontal), 135 Deg. (vertical) Lateral: Measurement Range: 0.5-32 m Measurement Range: 0.5-200 m Obstacle Avoidance Speed: Flight Speed <=21 m/s FOV: 90 Deg. (horizontal), 90 Deg. (vertical) Downward: Measurement Range: 0.3-18.8 m Obstacle Avoidance Speed: Flight Speed <=10 m/s The FOV to the front and rear is 160 Deg. and 160 Deg. to the right and left.
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: Delicate texture on the surface, adequate light. Downward: The ground has rich textures and sufficient lighting conditions, with a diffuse reflection surface and a reflectivity greater than 20% (such as walls, trees, people, etc.). Sufficient lighting conditions refer to an illuminance not lower than that of a nighttime city light scene.
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
Transmission schemes
Operating frequencies
Details of frequency spectrum approvals
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	Max Payload: 200 g
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: DJI Matrice 4T Wide: 1/1.3-inch CMOS, Effective Pixels: 48 MP Medium Tele Camera: 1/1.3-inch CMOS, Effective Pixels: 48 MP Telephoto: 1/1.5-inch CMOS, Effective Pixels: 48 MP DJI Matrice 4E Wide: 4/3-inch CMOS Effective Pixels: 20 MP Medium Tele Camera: 1/1.3-inch CMOS, Effective Pixels: 48 MP Telephoto: 1/1.5-inch CMOS, Effective Pixels: 48 MP
Safety features to mitigate the risk of the payload affecting the flight of the UA:
Effects on aerodynamics
Effects of electro-magnetic interference.
Effects of electrical power and / or data connection failures on the UAS.
Effects of complete detachment of the payload from the UA (either caused by a failure or through intentional lowering / dropping of the payload).
Effects of partial detachment of the payload from the UA.
Distraction of the remote pilot generated by the payload during flight.
Procedures to verify the attachment points to the UA.
Procedures to verify the UA MTOM and CG location.
Procedures to detect and mitigate any failure of the payload in flight.
Safety provisions with regards to hazards inherent to the payload
Procedures in place for safe handling of the payload.
Means of identifying hazards.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

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 Matrice 4T

Aircraft
Takeoff Weight	1229 g* * The standard weight of the aircraft (including the battery, propellers, and a microSD card). The actual product weight may vary due to differences in batch materials and external factors.
Max Takeoff Weight	Standard Propellers: 1420 g Low-Noise Propellers: 1430 g
Dimensions	Folded: 260.6 x 113.7 x 138.4 mm (L x W x H) Unfolded: 307.0 x 387.5 x 149.5 mm (L x W x H) Maximum dimensions excluding propellers.
Max Payload	200 g
	10.8 in
Diagonal Wheelbase	438.8 mm
Max Ascent Speed	10 m/s
	6 m/s
Max Descent Speed	8 m/s
	6 m/s
Max Horizontal Speed (at sea level, no wind)	21 m/s 21 m/s flying forward, 18 m/s flying backward, 19 m/s flying sideways* * No faster than 19 m/s with Sport mode in EU regions.
	6000 m
	4000 m
Max Flight Time	49 min (standard propellers) 46 min (low-noise propellers) Measured with the aircraft flying at approximately 8 m/s without payloads in a windless environment until the battery level reached 0%. Data is for reference only. Actual usage time may vary depending on the flight mode, accessories, and environment. Please pay attention to reminders in the app.
Max Hover Time (without wind)	42 min (standard propellers) 39 min (low-noise propellers) Measured with the aircraft flying at approximately 8 m/s without payloads in a windless environment until the battery level reached 0%. Data is for reference only. Actual usage time may vary depending on the flight mode, accessories, and environment. Please pay attention to reminders in the app.
Max Flight Distance	35 km (standard propellers) 32 km (low-noise propellers) Measured by the aircraft hovering in a windless environment at sea level, from 100% battery level until 0%.
Max Wind Speed Resistance	12 m/s* * Max wind speed resistance during takeoff and landing.
Max Pitch Angle	35 Deg.
Operating Temperature	-10 Deg.C to 40 Deg.C (14 Deg.F to 104 Deg.F)
GNSS	GPS + Galileo + BeiDou + GLONASS* * GLONASS is supported only when the RTK module is enabled.
Hovering Accuracy Range	±0.1 m (with Vision System); ±0.5 m (with GNSS); ±0.1 m (with RTK)
	RTK Fix: 1 cm + 1 ppm (horizontal), 1.5 cm + 1 ppm (vertical)
Internal Storage	N/A
	E-Port interface x 1: Supports official accessories and third-party PSDK devices (hot-swapping is not supported) E-Port Lite interface x 1: supports USB connection to DJI tuning software and some third-party PSDK devices. Accessories or expansion modules must be installed before powering on.
Propeller Model	1157F (standard propellers) 1154F (low noise propeller)
Beacon	Built into the aircraft
Camera
Image Sensor	DJI Matrice 4T Wide: 1/1.3-inch CMOS, Effective Pixels: 48 MP Medium Tele Camera: 1/1.3-inch CMOS, Effective Pixels: 48 MP Telephoto: 1/1.5-inch CMOS, Effective Pixels: 48 MP DJI Matrice 4E Wide: 4/3-inch CMOS Effective Pixels: 20 MP Medium Tele Camera: 1/1.3-inch CMOS, Effective Pixels: 48 MP Telephoto: 1/1.5-inch CMOS, Effective Pixels: 48 MP
Lens	DJI Matrice 4T FOV: 82 Deg. Equivalent Focal Length: 24 mm Aperture: f/1.7 Focus: 1 m to ∞ DJI Matrice 4E FOV: 84 Deg. Equivalent Focal Length: 24 mm Aperture: f/2.8-f/11 Focus: 1 m to ∞ Medium Tele Camera FOV: 35 Deg. Equivalent Focal Length: 70 mm Aperture: f/2.8 Focus: 3 m to ∞ Tele camera FOV: 15 Deg. Equivalent Focal Length: 168 mm Aperture: f/2.8 Focus: 3 m to ∞
ISO Range	Normal Mode: ISO 100 to ISO 25600 Night Scene Mode: Matrice 4T: Wide Camera: ISO 100 to ISO 409600 Midum Tele Camera: ISO 100 to ISO 409600 Tele Camera: ISO 100 to ISO 819200 Matrice 4E: Wide Camera: ISO 100 to ISO 204800 Midum Tele Camera: ISO 100 to ISO 409600 Tele Camera: ISO 100 to ISO 409600
Shutter Speed	DJI Matrice 4T 2-1/8000 s DJI Matrice 4E Wide: Electronic Shutter: 2-1/8000 s Mechanical Shutter: 2-1/2000 s Medium Telephoto: 2-1/8000 s Telephoto: 2-1/8000 s
	DJI Matrice 4T Wide: 8064 x 6048 Medium Telephoto: 8064 x 6048 Telephoto: 8192 x 6144 DJI Matrice 4E Wide: 5280 x 3956 Medium Telephoto: 8064 x 6048 Telephoto: 8192 x 6144
	DJI Matrice 4T: 0.7 s DJI Matrice 4E: 0.5 s
Still Photography Modes	DJI Matrice 4T: Wide: Single: 12 MP/48 MP Interval: 12 MP/48 MP JPEG: 0.7/1/2/3/5/7/10/15/20/30/60 s Smart Shooting:12MP Panorama: 12 MP (raw image);100 MP (stitched image) Medium Tele Camera: Single: 12 MP and 48 MP Interval: 12 MP/48 MP JPEG: 0.7/1/2/3/5/7/10/15/20/30/60 s Smart Shooting: 12MP Telephoto: Single: 12 MP and 48 MP Interval: 12 MP/48 MP JPEG: 0.7/1/2/3/5/7/10/15/20/30/60 s Smart Shooting: 12MP DJI Matrice 4E: Single: 20 MP Interval: 20 MP JPEG: 0.5/0.7/1/2/3/5/7/10/15/20/30/60 s JPEG + RAW: 2/3/5/7/10/15/20/30/60 s Smart Shooting: 20 MP Panorama: 20 MP (raw image);100 MP (stitched image) Medium Tele Camera: Single: 12 MP and 48 MP Interval: 12 MP/48 MP JPEG: 0.5/0.7/1/2/3/5/7/10/15/20/30/60 s Smart Shooting: 12 MP Telephoto: Single: 12 MP and 48 MP Interval: 12 MP/48 MP JPEG: 0.5/0.7/1/2/3/5/7/10/15/20/30/60 s Smart Shooting: 12 MP
	Video Coding Format: H.264/H.265 Coding Strategy: CBR, VBR Resolution: 4K: 3840 x 2160@30fps FHD: 1920 x 1080@30fps
Max Video Bitrate	H.264: 60Mbps H.265: 40Mbps
Supported File System	exFAT
Photo Format	DJI Matrice 4T: JPEG DJI Matrice 4E: Wide: JPEG/DNG (RAW) Medium Tele Camera: JPEG Telephoto: JPEG
Video Format	MP4 (MPEG-4 AVC/H.264)
Digital Zoom	Telephoto: 16x (112x hybrid zoom)

	DJI Matrice 4T: FOV: 5.7 Deg.±0.3 Deg.
Laser Module
	Measurement Range: 1800 m (1 Hz) @20% reflectivity target* Oblique Incidence Range (1:5 Oblique Distance): 600 m (1 Hz) Blind Zone: 1 m Distance Measurement Accuracy: 1-3 m: System Error <0.3 m, Random Error <0.1 meters @1σ Other Distances: ±(0.2+0.0015D) (D represents the measurement distance in meters) * Performance degradation may occur in rainy or foggy conditions

	DJI Matrice 4T: uncooled vanadium oxide (VOx) DO NOT expose the infrared camera lenses to strong sources of energy such as the sun, lava, or a laser beam. Otherwise, the camera sensor may be burned leading to permanent damage.
	DJI Matrice 4T: 640 x 512
	DJI Matrice 4T: 12 μm
	DJI Matrice 4T: 30 Hz
	DJI Matrice 4T DFOV: 45 Deg.±0.3 Deg. DJI Matrice 4T equivalent focal length: 53 mm DJI Matrice 4T Aperture: f/1.0 DJI Matrice 4T Focus: 5 m to ∞
	DJI Matrice 4T: <=50mk@F1.0
	DJI Matrice 4T: Spot Meter, Area Measurement
	DJI Matrice 4T: High Gain Mode: -20 Deg.C to 150 Deg.C (-4 Deg.F to 302 Deg.F) () Low Gain Mode: 0 Deg.C to 550 Deg.C (32 Deg.F to 1022 Deg.F)
	DJI Matrice 4T: White Hot/Black Hot/Tint/Iron Red/Hot Iron/Arctic/Medical/Fulgurite/Rainbow 1/Rainbow 2
	DJI Matrice 4T: JPEG (8bit)、 R-JPEG (16bit)
	DJI Matrice 4T: 1280 x 1024@30fps (Super Resolution enabled, Night Mode not activated) Other conditions: 640 x 512@30fps
	DJI Matrice 4T: 6.5Mbps (H.264 640 x 512@30fps) 5Mbps (H.265 640 x 512@30fps) 12Mbps (H.264 1280 x 1024@30fps) 8Mbps (H.265 1280 x 1024@30fps)
	DJI Matrice 4T: MP4
	DJI Matrice 4T: Single: 1280 x 1024/640 x 512 Interval: 1280 x 1024/640 x 512 JPEG: 0.7/1/2/3/5/7/10/15/20/30/60 s
	DJI Matrice 4T: Infrared: 1280 x 1024 (Super Resolution on) 640 x 512 (Super Resolution off)
	DJI Matrice 4T: 28x
	DJI Matrice 4T: 8um to 14um
	DJI Matrice 4T: High Gain: ±2 Deg.C or ±2%, whichever is greater DJI Matrice 4T: Low Gain: ±5 Deg.C or ±3%, whichever is greater
Gimbal
Stabilization System	DJI Matrice 4T: 3-axis (tilt, roll, pan) DJI Matrice 4E: 3-axis (tilt, roll, pan)
Mechanical Range	DJI Matrice 4T Gimbal Mechanical Limits: Tilt: -140 Deg. to 113 Deg. Roll: -52 Deg. to 52 Deg. Pan: -65 Deg. to 65 Deg. Soft Limits: Tilt: -90 Deg. to 35 Deg. Roll: -47 Deg. to 47 Deg. Pan: -60 Deg. to 60 Deg. DJI Matrice 4E Gimbal Mechanical Limits: Tilt: -140 Deg. to 50 Deg. Roll: -52 Deg. to 52 Deg. Pan: -65 Deg. to 65 Deg. Soft Limits: Tilt: -90 Deg. to 35 Deg. Roll: -47 Deg. to 47 Deg. Pan: -60 Deg. to 60 Deg.
	DJI Matrice 4T DJI Matrice 4T Pan: ±-90 Deg. to 35 Deg. Pan: Not controllable DJI Matrice 4E Tilt: -90 Deg. to 35 Deg. Pan: Not controllable
Max Control Speed (tilt)	100 Deg./s
Angular Vibration Range	±0.007 Deg.
	Manual operation is uncontrollable The MSDK interface program is controllable.
	No Standard Protection Level
	Standard: -10 Deg.C to 40 Deg.C (14 Deg.F to 104 Deg.F)
Sensing
Sensing Type	Omnidirectional binocular vision system, supplemented with a 3D infrared sensor at the bottom of the aircraft.
Forward	Binocular Measurement Range: 0.4-22.5 m Measurement Range: 0.4-200 m Obstacle Avoidance Speed: Flight Speed <=21 m/s FOV: 90 Deg. (horizontal), 135 Deg. (vertical)
Backward	Measurement Range: 0.4-22.5 m Measurement Range: 0.4-200 m Obstacle Avoidance Speed: Flight Speed <=21 m/sField of View (FOV)-90 Deg. (horizontal), 135 Deg. (vertical)
Lateral	Measurement Range: 0.5-32 m Measurement Range: 0.5-200 m Obstacle Avoidance Speed: Flight Speed <=21 m/s FOV: 90 Deg. (horizontal), 90 Deg. (vertical)
Downward	Measurement Range: 0.3-18.8 m Obstacle Avoidance Speed: Flight Speed <=10 m/s The FOV to the front and rear is 160 Deg. and 160 Deg. to the right and left.
Operating Environment	Forward, Backward, Left, Right, and Upward: Delicate texture on the surface, adequate light. Downward: The ground has rich textures and sufficient lighting conditions, with a diffuse reflection surface and a reflectivity greater than 20% (such as walls, trees, people, etc.). Sufficient lighting conditions refer to an illuminance not lower than that of a nighttime city light scene.
Video Transmission
Video Transmission System	O4 Enterprise
Live View Quality	Remote Controller: 1080p/30fps
Operating Frequency	2.400-2.4835 GHz 2.400-2.4835 GHz 5.725-5.850 GHz 5.150-5.250 GHz (CE) Operating frequency allowed varies among countries and regions. Refer to local laws and regulations for more information.
Transmitter Power (EIRP)	2.4 GHz: <=33 dBm (FCC), <=20 dBm (CE/SRRC/MIC) 5.8 GHz: <33 dBm (FCC), <30 dB (SRRC) , <14 dBm (CE) 5.15-5.25: < 23 dBm (FCC/CE)
Max Transmission Distance (free of interference)	Strong Interference - City Centers (approx. 1.5-5 km) Medium Interference - Suburban Areas (approx. 5-15 km) Micro interference: Suburbs/Seasides (approx. 15-25 km) * Data is tested under FCC standards in unobstructed environments of typical interference. Only to serve as a reference and provides no guarantee as to the actual flight distance.
Max Download Speed	20 MB/s The above data was measured under conditions where the aircraft and remote controller were in close proximity without interference.
Latency (depending on environmental conditions and mobile device)	130 ms Under near-field interference-free conditions, the Latency performance when shooting with a 1x lens.
Antenna	8 antennas, 2T4R
	Cellular Dongle Compartment

	U3/Class10/V30 or above is required, or use a memory card from the recommended list.
	Lexar 1066x 64GB U3 A2 V30 microSDXC Lexar 1066x 128GB U3 A2 V30 microSDXC Lexar 1066x 256GB U3 A2 V30 microSDXC Lexar 1066x 512GB U3 A2 V30 microSDXC Kingston Canvas GO! Plus 64GB U3 A2 V30 microSDXC Kingston Canvas GO! Plus 128GB U3 A2 V30 microSDXC Kingston Canvas GO! Plus 256GB U3 A2 V30 microSDXC Kingston Canvas GO! Plus 512GB U3 A2 V30 microSDXC
Intelligent Flight Battery
Capacity[1]	6741 mAh
Standard Voltage	14.76 V
Max Charging Voltage	17.0 V
	Li-ion 4S
Energy	99.5 Wh
Weight	401 g
	5 Deg.C to 40 Deg.C (41 Deg.F to 104 Deg.F)
Discharge Rate	4C
Max Charging Power	1.8C
	Not supported
	200

	100-240 V (AC), 50-60 Hz, 2.5 A
	Max. 100 W (total) When both ports are used, the max output power of one port is 82 W, and the charger will dynamically allocate the output power of the two ports according to the power load.
	100 W
Charging Hub
Input	USB-C: 5-20 V, max 5 A
Output	Battery Interface: 11.2 V to 17 V
Rated Power	100 W
	4 batteries charging in sequence Support Standard Mode (100% SOC) and Standby Mode (90% SOC)
	DJI Matrice 4E/T Series Intelligent Flight Battery
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg.F to 104 Deg.F)

	O4 Enterprise
	25 km (FCC) 12 km (CE) 12 km (SRRC) 12 km (MIC) Measured in an unobstructed environment free of interference. The above data shows the farthest communication range for one-way, non-return flights under each standard. During your flight, please pay attention to RTH reminder on the DJI Pilot 2 app.
	2.4000-2.4835 GHz 5.725 - 5.850 GHz 5.1GHz (receive only) Operating frequency allowed varies among countries and regions. Refer to local laws and regulations for more information.
	2T4R, built-in multi-beam high-gain antenna
	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)
	DJI Cellular Dongle 2
	Wi-Fi Direct, Wireless Display, IEEE 802.11a/b/g/n/ac/ax Support 2 x 2 MIMO Wi-Fi, Dual Band Simultaneous (DBS) with dual MAC, up to 1774.5 Mbps data rate (2 x 2 + 2 x 2 11ax DBS)
	2.4000-2.4835 GHz 5.150-5.250 GHz 5.725-5.850 GHz 5.8 and 5.2GHz frequencies are prohibited in some countries. In some countries, the 5.2GHz frequency is only allowed for use in indoor.
	2.4 GHz: ＜26 dBm (FCC), ＜20 dBm (CE/SRRC/ MIC) 5.1 GHz: <23 dBm (FCC) 5.8 GHz ＜23 dBm (FCC/SRRC), ＜14 dBm (CE)
	Bluetooth 5.2
	2.400-2.4835 GHz
	<10 dBm
	1920 x 1200
	7.02 inches
	60 fps
	1400 nits
	10 Points Multi-touch
	2S2P High Energy Density 18650 Lithium-ion Battery (6500 mAh @ 7.2 V) 46.8 Wh
	Optional, WB37 (4920 mAh @ 7.6 V) 37 Wh
	Supports PD fast charging, with a maximum specification of 20 V/3.25 A USB Type-C charger.
	ROM 128 G + expandable storage via microSD card
	2 hrs for internal battery or internal and external battery. When remote controller is powered off and using a standard DJI charger.
	3.8 hrs
	3.2 hrs
	HDMI 1.4
	Status light & power light & permission light, three-color light, brightness can be adjusted according to ambient brightness.
	Supports buzzer
	Array MIC
	-20 Deg. to 50 Deg. C (D228 (-4 Deg.F to 122 Deg.F)
	Within one month: -30 Deg. to 45 Deg. C (-22 Deg.F to 113 Deg.F) One to three months: -30 Deg. to 35 Deg. C (-22 Deg.F to 95 Deg.F) Three months to one year: -30 Deg. to 30 Deg. C (-22 Deg.F to 86 Deg.F)
	5 Deg. to 40 Deg. C (41 Deg.F to 104 Deg.F)
	Support for Matrice 4T/4E
	GPS, Galileo, and BeiDou triple-mode, supports dynamic Home Point refresh.
	268 x 163 x 94.5 mm (L x W x H) Width including external antenna folded, thickness including handle and controller sticks.
	1.15 kg (without external battery)
	TKPL 2
	Android 11
	HDMI 1.4, SD3.0, Type-C supports OTG, supports PD charging, maximum power 65W, USB-A supports USB 2.0 interface.
	Optional strap/waist support

	99 g (including bracket) Approx. 91 g (excluding bracket)
	95 x 164 x 30 mm (L x W x H,including bracket) 79 x 164 x 28 mm (L x W x H, without bracket)
	32 W
	4.3±0.2 lux @ 100 meters, 17±0.2 lux @ 50 meters The data was measured in a laboratory environment with the spotlight installed separately on the aircraft at an ambient temperature of 25 Deg.C.
	23 Deg. (10% relative illumination)
	1,300 square meters @ 100 meters (10% relative illumination, Normal Mode) 2,200 square meters @ 100 meters (10% central illuminance, Wide fov Mode)
	Supports always-on and strobe modes.
	Tilt: -140 Deg. to 50 Deg.
	Tilt: -90 Deg. to 35 Deg.
	120 Deg./s
	±0.1 Deg.
	-20 Deg.C to 50 Deg.C (-4 Deg.F to 122 Deg.F)
	Quick-release hand-tightened screws

	92.5 g (including bracket) Approx. 90 g (excluding bracket)
	73 x 70 x 52 mm (L x W x H,including bracket) 73 x 70 x 47 mm (L x W x H, without bracket)
	15 W
	At 1 meter, it can reach 114 decibels (114dB@1m). Data measured in a laboratory environment at 25 Deg.C. Actual conditions may vary slightly due to software version, audio source, specific environment, and other factors. The final effect is subject to actual use.
	300 m Data measured in a laboratory environment at 25 Deg.C. Actual conditions may vary slightly due to software version, audio source, specific environment, and other factors. The final effect is subject to actual use.
	Real-time broadcasting (supports echo suppression), recorded broadcasting, media import (supports simultaneous transmission and playback), text-to-speech* * Need to upgrade to the latest firmware. ** Currently only supports Chinese and English.
	-20 Deg.C to 50 Deg.C (-4 Deg.F to 122 Deg.F)
	Quick-release hand-tightened screws

Data source: https://enterprise.dji.com/matrice-4-series/specs

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Source data acquired 2025-01-09 12:23:43