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MATRICE 30

SERIES Maintenance Manual

Flight Controller

1. After the aircraft is powered on and self-check is complete, there are no error prompts in the app

related to the ight controller.

2. In outdoor open environments, the GNSS signal reaches “Strong” level within 1 minute of powering

on the aircraft, indicating that the Home Point can be recorded automatically, and the RTK data

meets the heading measurement standard.

3. In outdoor open environments, the interference of the compass after calibration is less than 50.

4. Sensor bias is less than 0.05 after the IMU calibration.

Aircraft Structure

Type Inspection Process Illustrations

Aircraft

Appearance

1. The aircraft body is clean and not damaged.

2. Clean the aircraft body with a clean and soft

cloth, especially for the lenses of the infrared

sensing and vision systems and the heat

dissipation vents.

Screws

1. All the screws on the aircraft body are

tightened, especially the screws connecting the

motor and the carbon tube.

Frame Arms

1. The 12 screws on the four frame arms are

secure.

2. The screw nuts attached on the shaft screws

are secure when rotating the frame arms.

3. The arm junctions are not damaged or

cracked.

4. The frame arm folding buttons can pop out

smoothly so that the frame arms are unfolded

and locked rmly.

5. The frame arm folding buttons can be pressed

down smoothly when the arms are folded.

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General

Max Flight Time	41 minutes
Max Service Ceiling	7000 m
Max Ascent Speed	6 m/s
Max Descent Speed	5 m/s
Ingress Protection Rating	IP55
Max Speed	23 m/s
Operating Temperature Range	-20°C to 50°C (-4°F to 122°F)
Operating Frequency	2.400-2.4835 GHz, 5.725-5.850 GHz
Max Tilt Angle	35°
GNSS	GPS, GLONASS, BeiDou, Galileo
Hovering Accuracy Range (P-mode with GPS)	±0.5 m (Vertical), ±1.5 m (Horizontal)
Operating Temperature (Battery)	-20°C to 50°C (-4°F to 122°F)
Battery Charging Temperature	5° to 40° C (41° to 104° F)
Transmission Range	15 km