February 2026
Audible alert from the remote controller: “IMU not calibrated”
Remote controller display shows IMU1 / IMU2 not calibrated
Typically occurs after replacing the avionics assembly or interface board
May also occur if the aircraft has not been powered on for an extended period
Place the aircraft on a level surface
Ensure the environment is free of vibration and strong magnetic interference
On the remote controller, navigate to:Aircraft Settings → Advanced Settings → IMU Calibration, and perform IMU calibration
Audible Warnings:
Remote controller voice alert: “Dual-antenna heading abnormal”
Visual Warnings:
Weak GPS signal indication
Satellite icon turns red or yellow
Low number of satellites detected
Positioning status icon flashing (e.g., green → red)
Before Takeoff:
The Applicator View App by Ceres Air indicates “Insufficient satellites, unable to take off” or “GPS not ready”
During Flight:
Aircraft drifting
Unstable altitude
Tendency toward loss of control
Environmental Factors:
Signal obstruction around the aircraft (e.g., high-rise buildings, indoor environments, dense forest canopy)
Weather Interference:
Thunderstorms or ionospheric disturbances affecting signal transmission
Electromagnetic Interference:
Operation near high-voltage power lines, communication base stations, radar installations, or other strong electromagnetic sources
Hardware Factors:
Physical damage to antennas (e.g., impact damage from a crash)
Loose antenna connectors or damaged antenna cables
Before flight, confirm the operating area is open and unobstructed
Pause flight operations and wait for weather conditions to stabilize
Fly away from known interference sources
Inspect antenna condition and cable connections; replace damaged components as necessary
Rough or restricted rotation, accompanied by a grinding or scraping noise
Severe vibration during motor startup, with the motor unable to rotate normally
Visible motor housing deformation, leading to bearing wear or damage
Sand, dust, or foreign objects entering the motor interior
Impact, compression, or collision during flight or transportation, causing motor housing deformation
Troubleshooting Procedure:
Promptly clean foreign objects from the motor interior
Replace the motor if mechanical damage or deformation is detectedCauses of failure:
Motor housing is too hot to touch, with the remote controller indicating a temperature exceeding 140 °F (60 °C)
Presence of a burnt or scorched odor from the motor
Prolonged operation under overload conditions, such as heavy payloads, high RPM, or high ambient temperatures
Land immediately and allow the motor to cool down
Inspect the motor windings for discoloration or deformation
Reduce payload and monitor motor temperature during subsequent flights
Severe vibration during flight with a noticeable increase in noise
Unstable hover with irregular lateral drift
Visible propeller damage, including cracks, delamination, or deformation
Possible Causes:
Impact or compression during operation or transportation, resulting in propeller deformation
Improper installation, such as insufficient tightening of propeller clamp bolts, causing centrifugal imbalance
Surface contamination, including mud, pesticide residue, or corrosive chemical buildup
Replace propellers with new units
C31 propellers must be replaced in matched pairs Verify propeller clamp bolt torque
Clean propeller surfaces to remove dirt and chemical residue
After power-on, the ESC status LED on the affected arm displays a purple color
On the remote controller interface, under Propulsion System Status, the affected arm is shown as “Not Recognized”
(Example: Arm No. 2)
The flight controller is not receiving communication signals from the ESC
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
If the issue persists, replace the motor and/or ESC on the affected arm
This section describes typical fault symptoms caused by loose or disconnected wiring harnesses. Different harness faults may result in specific LED indications, system status messages, and subsystem recognition failures.
:
Navigation LEDs on Arms 1–4 remain solid purple
Control signals lostRemote controller cannot connect to
the aircraft
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Navigation LEDs on Arms 1–4 remain solid purple
Remote controller cannot connect to the aircraft
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Remote controller connects normally
Radar System displays “Downward Radar Not Recognized”
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
ESC LED indicators:
Arm 1: Purple
Arm 2: Red
Arms 3 & 4: Green
Power System displays Motors No. 1 and No. 5 Not Recognized:
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
ESC LED indicators:
Arm 2: Purple
Arm 1: Red
Arms 3 & 4: Green
Power System displays Motors No. 2 and No. 6 Not Recognized
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
ESC LED indicators:
Arm 3: Purple
Arms 1 & 2: Red
Arm 4: Green
Power System displays Motors No. 3 and No. 7 Not Recognized
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
ESC LED indicators:
Arm 4: Purple
Arms 1 & 2: Red
Arm 3: Green
Remote controller connects normally
Power System displays Motors No. 4 and No. 8 Not Recognized
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Remote controller connects normally
Vision System displays “Front Camera Not Connected”
ESC status:
Arms 1–3: ESC fault
Arm 4: ESC normal
ESC LED indicators:
ESCs No. 1–6: Purple
ESCs No. 7 & 8: Green
Remote controller connects normally
Power System displays Motors No. 1–6 Not Recognized
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
ESC status:
Arm 4: ESC fault
Arms 1–3: ESC normal
ESC LED indicators:
Arms 1 & 2: Red
Arm 3: Green
Arm 4: Purple
Remote controller connects normally
Power System displays Motors No. 7 and No. 8 Not Recognized
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Remote controller connects normally
Vision System and Radar System not recognized
Vision System displays “Front Camera Not Recognized”
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Remote controller connects normally
Radar System displays “Rear Radar Not Recognized”
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Remote controller connects normally
Lifting System displays “Not Recognized”
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Remote controller connects normally
Radar System displays “Rotating Radar Not Recognized”
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
Battery cannot detect load
Aircraft cannot power on
Red indicator LED flashes briefly and then turns off
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
ESC indicators on the affected ports do not illuminate
Power System displays corresponding motors as “Not Recognized”
Verify that all related wiring harnesses are properly connected, fully seated, and undamaged
Check connectors for looseness, bent pins, or corrosion
The remote controller displays a warning: “Vision System Fault – Image Transmission Not Detected.”
Damaged image transmission antenna (bent, broken, or physically damaged)
Loose antenna connection or poor electrical contact
Inspect the image transmission antenna for damage
Tighten the antenna connection securely
Replace the image transmission antenna if damage is found
The remote controller displays a vision system warning: “Front Camera Not Detected.”
Blurred image, black screen, or snow/noise artifacts
Gimbal cannot rotate normally or video image shakes excessively
Physical damage caused by collision (loose or broken wiring harness)
Scratched lens or water ingress
Abnormal connection between the image transmission module and the camera
Ethernet connection failure
Inspect the connection path: front interface board → signal cables → cameraReplace the front interface board and/or camera if necessary2
Gently wiggle the camera cable connectors (power off before operation) to check for looseness. Replace the front camera if the issue persists
If hardware damage is confirmed (e.g., cracked lens or broken cable), replace the affected components immediately
After a crash, the lifting system is displayed as “Not Detected” on the aircraft or remote controller.
High-altitude crash resulting in damage to the lifting system or lifting module.
Inspect the payload control wiring harness and lifting module wiring connectors for abnormal conditions.
If looseness or poor contact is found, power off the aircraft before tightening the connectors.
If the issue cannot be resolved after reconnection, it is recommended to replace the lifting control wiring harness or the lifting module.
During lifting operations, the payload shows no anti-sway effect and continues to swing violently.
Power supply failure to the anti-sway module, preventing normal operation.
Software malfunction in the anti-sway module, causing failure to execute the anti-sway algorithm.
First, check whether the anti-sway module wiring harness is properly connected.
If the connection appears normal, power off the aircraft and re-plug the wiring harness to attempt recovery.
If reconnection does not resolve the issue, reinstall or update the anti-sway module software, or replace the anti-sway module if necessary.
After power-on, the system displays: “Operation System – Weighing Sensor Not Detected.”
High-altitude crash resulting in weighing sensor damage.
Water ingress causing sensor failure.
Replace the weighing sensor with a new unit.
The system displays a weighing calibration error.
Weighing calibration was not performed after replacing the anti-sway module.
Perform empty-load calibration or full-load calibration in the operation system interface.
The displayed weight value does not match the actual payload weight.
Calibration-related error.
Weighing sensor malfunction.
Perform empty-load calibration with no lifting rope or payload attached.
If the weight value remains incorrect after calibration, replace the weighing sensor.
The remote controller displays “Radar System Not Detected – Rotating Radar ESC.”
Radar ESC failure
Replace the rotating radar assembly
The remote controller displays: “Radar System Not Detected – Rotating Radar Altitude Hold.”
Failure of the radar internal PCB
Replace the rotating radar assembly
The remote controller displays: “Radar System Not Detected – Rotating Radar Obstacle Avoidance.”
Abnormal noise is heard during rotation, and intermittent radar errors are reported.
Loose radar mounting cover
Replace the rotating radar assembly
The remote controller displays: “Radar System Not Detected – Rear Obstacle Avoidance Radar.”
Rear obstacle avoidance radar failure
Replace the rear obstacle avoidance radar module
The remote controller displays: “Radar System Not Detected – Downward Radar.”
Downward-facing radar failure
Replace the downward radar module
After powering on the aircraft, the system displays: “Radar System Fault – Radar Not Rotating.”
Firmware version mismatch between the aircraft and the newly installed radar module
Upgrade to the latest firmware version
Ensure the remote controller firmware version matches the aircraft firmware version
Intermittent radar faults with various abnormal error reports
Excessive aircraft vibration causing unstable radar connections
Adjust propeller clamp tightness to ensure consistency
Secure radar connectors using adhesive (yellow glue)
Radar system not detected, accompanied by a front camera fault
Excessive aircraft vibration causing Ethernet communication instability
Inspect and secure Ethernet connections
The remote controller announces: “Radar System Fault – Rear Obstacle Avoidance Not Detected.”
Firmware version mismatch between the radar and aircraft
Radar malfunction
Rear radar hardware failure
Possible causes include incompatible radar firmware, a poor connection to the rear radar, or a faulty radar unit.
Inspect rear radar connections
Verify aircraft firmware and remote controller firmware versions
Upgrade to the latest firmware
If the rear radar is still not detected, replace the rear radar assembly
After the battery is powered on, the flight controller does not power up (wiring harness connections are confirmed to be normal)
Battery communication failure on the front interface board
Inspect the battery communication wiring
If wiring is normal, replace the front interface board
After powering on the aircraft, the propulsion system is not recognized, and the ESC indicator lights display purple
- ESC signal interface damage (e.g., bent or broken connector pins)
- Replace the front interface board
After powering on the aircraft, the system displays: Frame Module Fault – Barometer Error.”
Barometer malfunction or failure within the frame module
Inspect barometer connections
Replace the barometer module or the affected frame module component if necessary
The propulsion system is not recognized, and the ESC indicator lights display
Communication failure in the corresponding arm module
Inspect the communication wiring harness of the affected arm
If the wiring is normal, replace the front interface board
After powering on the aircraft, multiple faults are reported simultaneously, such as:“Vision System Fault,” “Radar System Fault,” and other related errors
CAN bus short circuit within the aircraft
Disconnect all external payloads and accessories
Retain only the following connections:
Avionics (flight controller)
Ethernet
Battery communication
Power distribution board (PDB) signal harness
Power on the aircraft:
If the aircraft powers on normally, reconnect additional devices one by one until the shorted device is identified
If the aircraft still fails to power on with only the above connections:
Troubleshoot sequentially following this order:Front interface board → wiring harness → avionics
Continue troubleshooting until the aircraft powers on normally, then resume the above isolation procedure
After powering on the aircraft, the status LED flashes red slowly and then turns off
Battery load not detected
Load detection module failure
Inspect the battery signal wiring connection
Attempt to power on using Battery No. 2
If the aircraft powers on normally, replace the upper cover assembly of Battery No. 1
If the issue persists:
Inspect the PDB signal wiring
If wiring is normal, replace the power distribution board assembly
The remote controller announces: “Power System Fault – Battery Cells Not Detected.”
Battery communication failure
Power distribution board (PDB) communication failure
Replace the battery and attempt to power on the aircraft
If the issue persists, replace the power distribution board
The remote controller announces: “Power System Fault – Abnormal Cell Voltage Difference, Please Land Immediately.”
Excessive voltage imbalance between battery cells
Upload the battery log
Await analysis results from engineering support
Abnormal voltage jumps occur during charging or discharging(e.g., voltage suddenly increases during charging, or drops suddenly when installed on the aircraft)
Excessive voltage imbalance between battery cells
Upload the battery log
Await analysis results from engineering support
The remote controller displays “Flight Authorization Error”
The remote controller is logged in with a non-owner aircraft account
Aircraft unlocking is restricted
Log in to the Ceres Aviation platform
Grant control authorization to the relevant account under Flight Control Authorization
The remote controller displays “Pilot Authorization Error”
The pilot has not completed official Ceres training
Pilot credentials have not been approved or verified
Contact the authorized dealer or Ceres technical support
Complete required pilot training and certification review
Fault Symptom:
The current operating area does not permit aircraft unlocking (e.g., restricted or no-fly area outside the dealer’s authorized operating region) outside the dealer’s authorized operating region)
Submit required documentation to request area unlocking
Coordinate with Ceres technical support to add an approved test flight zone for the aircraft