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	Flip
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Takeoff Weight: ‌< 249 g ‌Standard aircraft weight (including the Intelligent Flight Battery and a microSD card). Actual product weight may vary due to differences in batch materials and other factors. Training or examination is not required for flying this product in most countries and regions. Always check local laws and regulations before use. Always check and strictly abide by local laws and regulations before flying.
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: Folded: 136 x 62 x 165 mm (L x W x H) Unfolded: 233 x 280 x 79 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: 12 m/s* (Sport mode) 12 m/s (tracking status) At sea level, with 4 m/s tailwind, while flying in the same direction as the wind: 16 m/s* (Sport mode) 12 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: 3000 m In a windless environment, a fully charged aircraft can take off from an altitude of 3000 m, ascend vertically by 500 m, and fly in Sport mode until the battery level drops to 20%. Data is for reference only. Always pay attention to reminders on the camera view during your flight.
Maximum operating height
Maximum flight time during normal operation	Max Flight Time: 31 minutes Measured when flying forward at a constant speed of 6 m/s in a windless environment 20 m above sea level, 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: 14 km Measured when flying forward at a constant speed of 9 m/s in a windless environment 20 m above sea level, 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: 10.7 m/s (Level 5)
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature: -10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
In-flight icing condition limits
Any other relevant information

CAP722A Table 9

Construction

Type of material
Material characteristics or properties
Any other relevant information

CAP722A Table 10

Electrical power system

Batteries:
Battery type, model and manufacturer	Capacity: 3110 mAh Battery Type: Li-ion Chemical System: LiNiMnCoO2
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Nominal Voltage: 7.16 V Energy: 22.3 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: When Charging via Aircraft (30W max charging power): From 0% to 100%: Approx. 70 minutes* When Using the Battery Charging Hub for Charging One Battery (48W max charging power): From 0% to 100%: Approx. 45 minutes When Using the Battery Charging Hub for Parallel Charging Two Batteries (65W max charging power):  Two batteries from 0% to 100%: Approx. 70 minutes*  * Using the DJI 30W USB-C Charger or a charger that supports the PD protocol with a power output higher than 30 W. Using the DJI 65W USB-C Charger or a charger that supports the PD protocol with a power output higher than 48 W. * Using the DJI 65W USB-C Charger or a charger that supports the PD protocol with a power output higher than 65 W.

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: Downward: one visual sensor and an infrared sensor, Forward: 3D Infrared Sensing System Forward: 3D Infrared Sensing System Measurement Range: 0.3-8 m (reflectivity > 10%) FOV: Horizontal 60 Deg., Vertical 60 Deg. Downward: Measurement Range: 0.3-8 m (reflectivity > 10%) Precise Hovering Range: 0.5-10 m FOV: Horizontal 60 Deg., Vertical 60 Deg.
Devices used
Technology used
Interface between the DAA system and the flight control computer
Limitations of the DAA system	Operating Environment: Downward: Surfaces with discernible patterns, diffuse reflectivity > 20% (such as cement pavement), and adequate lighting (lux > 15)
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: <20 dBm（FCC/CE/SRRC/MIC) 5.8 GHz: <20 dBm（FCC/SRRC) <14 dBm （CE) Transmitter Power (EIRP): ＜10 dBm
Transmission schemes	Protocol: 802.11a/b/g/n/ac
Operating frequencies
Details of frequency spectrum approvals	Operating Frequency[1]: 2.4000 GHz-2.4835 GHz 5.7250 GHz-5.850 GHz Operating frequency allowed varies among countries and regions. Refer to local laws and regulations for more information. Operating Frequency: 2.4000-2.4835 GHz Operating frequency allowed varies among countries and regions. 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: 1/1.3-inch image sensor
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 Flip

Aircraft
Takeoff Weight	‌< 249 g ‌Standard aircraft weight (including the Intelligent Flight Battery and a microSD card). Actual product weight may vary due to differences in batch materials and other factors. Training or examination is not required for flying this product in most countries and regions. Always check local laws and regulations before use. Always check and strictly abide by local laws and regulations before flying.
Dimensions	Folded: 136 x 62 x 165 mm (L x W x H) Unfolded: 233 x 280 x 79 mm (L x W x H)
Max Ascent Speed	5 m/s (Sport mode) 5 m/s (Normal mode) 2 m/s (Cine mode)
Max Descent Speed	5 m/s (Sport mode) 5 m/s (Normal mode) 1.5 m/s (Cine mode)
Max Horizontal Speed (at sea level, no wind)	At sea level, in windless conditions: 12 m/s* (Sport mode) 12 m/s (tracking status) At sea level, with 4 m/s tailwind, while flying in the same direction as the wind: 16 m/s* (Sport mode) 12 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	3000 m In a windless environment, a fully charged aircraft can take off from an altitude of 3000 m, ascend vertically by 500 m, and fly in Sport mode until the battery level drops to 20%. Data is for reference only. Always pay attention to reminders on the camera view during your flight.
Max Flight Time	31 minutes Measured when flying forward at a constant speed of 6 m/s in a windless environment 20 m above sea level, 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	28 minutes Measured when hovering in a windless environment 20 m above sea level, 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	14 km Measured when flying forward at a constant speed of 9 m/s in a windless environment 20 m above sea level, 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	10.7 m/s (Level 5)
Operating Temperature	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Global Navigation Satellite System	GPS + Galileo + BeiDou
Internal Storage	2 GB
	C0 (EU)
Camera
Image Sensor	1/1.3-inch image sensor
Lens	FOV: 82.1 Deg. Format Equivalent: 24 mm Aperture: f/1.7 Focus: 1 m to ∞
ISO Range	Video Normal/Slow Motion: 100-6400 (Normal) 100-1600 (D-Log M) Photo 12MP Photo: 100-6400 48MP Photo: 100-3200
Shutter Speed	12MP Photo: 1/16000-2 s (2.5-8 s for simulated long exposure) 48MP Photo: 1/8000-2 s
Max Image Size	48MP Photo 8064 x 6048
Still Photography Modes	Single Shot: 12 MP and 48 MP Burst Shooting: 12 MP, 3/5/7 frames Automatic Exposure Bracketing (AEB): 12 MP, 3/5/7 frames at 2/3 EV step Timed: 12 MP, 2/3/5/7/10/15/20/30/60 s
Photo Format	JPEG DNG/RAW
Video Resolution	4K: 3840 x 2160@24/25/30/48/50/60/100fps FHD: 1920 x 1080@24/25/30/48/50/60/100fps 2.7K Vertical Shooting: 1512 x 2688@24/25/30fps FHD Vertical Shooting: 1080 x 1920@24/25/30fps
Video Format	MP4
Max Video Bitrate	150Mbps
Supported File System	exFAT
Color Mode	Normal D-Log M
Digital Zoom	4K: 3x FHD: 4x 2.7K Vertical Shooting: 3x FHD Vertical Shooting: 4x 12 MP Photo: 3x
Gimbal
Stabilization	3-axis mechanical gimbal (tilt, roll, pan)
Mechanical Range	Tilt Axis: -130 Deg. to +63 Deg. Roll Axis: -47 Deg. to +47 Deg. Pan: -30 Deg. to +30 Deg.
Controllable Range	Tilt Axis: -90 Deg. to +35 Deg.
Max Control Speed (tilt)	100 Deg./s
Angular Vibration Range	±0.01 Deg.
Sensing
Sensing Type	Downward: one visual sensor and an infrared sensor, Forward: 3D Infrared Sensing System
Forward	3D Infrared Sensing System Measurement Range: 0.3-8 m (reflectivity > 10%) FOV: Horizontal 60 Deg., Vertical 60 Deg.
Downward	Measurement Range: 0.3-8 m (reflectivity > 10%) Precise Hovering Range: 0.5-10 m FOV: Horizontal 60 Deg., Vertical 60 Deg.
Operating Environment	Downward: Surfaces with discernible patterns, diffuse reflectivity > 20% (such as cement pavement), and adequate lighting (lux > 15)
Video Transmission
Video Transmission System	O4
Live View Quality	Remote Controller: Up to 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. Refer to local laws and regulations for more information.
Transmitter Power (EIRP)	2.4 GHz: <30 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. 0-0.5 km Low Interference and Obstructed by Trees: Approx. 0.5-2 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: DJI RC-N3 Remote Controller: 10 MB/s DJI RC: 10 MB/s Wi-Fi 5: 30 MB/s Measured in a laboratory environment with little interference in countries/regions that support both 2.4 GHz and 5.8 GHz. Download speeds may vary depending on the actual conditions.
Lowest Latency	Approx. 120 ms Depending on the actual environment and mobile device.
Antenna	4 antennas (2.4 GHz: 1T2R; 5.2/5.8 GHz: 2T2R)
Wi-Fi
Protocol	802.11a/b/g/n/ac
Operating Frequency[1]	2.4000 GHz-2.4835 GHz 5.7250 GHz-5.850 GHz Operating frequency allowed varies among countries and regions. Refer to local laws and regulations for more information.
Transmitter Power (EIRP)	2.4 GHz: <20 dBm（FCC/CE/SRRC/MIC) 5.8 GHz: <20 dBm（FCC/SRRC) <14 dBm （CE)
	50 m Measured in an open environment free of interference. Actual transmission distance may vary by the operating environment.
Bluetooth
Protocol	Bluetooth 5.0
Operating Frequency	2.4000-2.4835 GHz Operating frequency allowed varies among countries and regions. Refer to local laws and regulations for more information.
Transmitter Power (EIRP)	＜10 dBm
Battery
Capacity	3110 mAh
Weight	Approx. 83.5 g
Nominal Voltage	7.16 V
Battery Type	Li-ion
Chemical System	LiNiMnCoO2
Energy	22.3 Wh
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Charging Time	When Charging via Aircraft (30W max charging power): From 0% to 100%: Approx. 70 minutes* When Using the Battery Charging Hub for Charging One Battery (48W max charging power): From 0% to 100%: Approx. 45 minutes When Using the Battery Charging Hub for Parallel Charging Two Batteries (65W max charging power):  Two batteries from 0% to 100%: Approx. 70 minutes*  * Using the DJI 30W USB-C Charger or a charger that supports the PD protocol with a power output higher than 30 W. Using the DJI 65W USB-C Charger or a charger that supports the PD protocol with a power output higher than 48 W. * Using the DJI 65W USB-C Charger or a charger that supports the PD protocol with a power output higher than 65 W.
Battery Charging Hub
Input	5 V, 4.3 A 9 V, 4.3 A 12 V, 4.3 A 15 V, 4.3 A
Output	15 V, 2 A 12 V, 2 A 9 V, 3 A 5 V, 3 A
Rated Power	65 W
Charging Type	2 batteries charged simultaneously or in sequence
Compatibility	DJI Flip Intelligent Flight Battery
Charger
Recommended Charger	DJI 65W Portable Charger* USB Power Delivery chargers * When you charge the battery mounted to the aircraft, the maximum charging power supported is 30 W. * When you charge the battery inserted into the Parallel Charging Hub, the maximum charging power supported is 65 W.
Storage
Recommended microSD Cards	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 Lexar Professional 1066x 64GB U3 A2 V30 microSDXC Lexar Professional 1066x 128GB U3 A2 V30 microSDXC Lexar Professional 1066x 256GB U3 A2 V30 microSDXC Lexar Professional 1066x 512GB U3 A2 V30 microSDXC

	Without Charging Any Mobile Device: 3.5 hours When Charging a Mobile Device: 1.5 hours
	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
	180 x 86 x 10 mm (L x W x H)
APP
Mobile Device App	DJI Fly
Required Operating System	iOS 13.0 or later Android 7.0 or later

Data source: https://www.dji.com/uk/flip/specs

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