DJI Matrice 400 OEM Body Casing / Body Cover Shell

DJI Matrice 400 OEM Body Casing / Body Cover Shell

Replacement exterior body casing for the DJI Matrice 400 enterprise aircraft. This component forms a major portion of the aircraft’s protective outer enclosure and is intended for repair of cracked, impact-damaged, heavily scratched, warped, or otherwise compromised body shell sections.

The body casing protects internal flight-control, power-distribution, sensing, cooling, and payload-interface hardware from direct exposure and helps restore the aircraft’s original structural fit and serviceability after body damage.

Compatibility

Designed for: DJI Matrice 400.

Compatibility should be verified against the removed component and aircraft configuration before installation. This listing is for the body casing / body cover shell shown, not a complete aircraft.

Typical Replacement Reasons

• Crash or impact damage
• Cracked or deformed outer shell
• Damaged mounting tabs or screw locations
• Severe cosmetic damage during professional fleet refurbishment
• Reassembly following internal Matrice 400 repairs

Repair Notes

Body-shell replacement may require substantial disassembly of the Matrice 400 and transfer of existing internal components, seals, fasteners, vents, sensors, and related hardware. Professional installation is recommended for aircraft used in mission-critical enterprise operations.

What Is Included

One replacement DJI Matrice 400 body casing / body cover shell as represented by the selected product configuration. Internal electronics, batteries, payloads, landing gear, arms, and unrelated hardware are not included unless explicitly shown or stated.

Use Cases

Suitable for enterprise drone repair centers, public-safety fleets, inspection operators, survey teams, mapping providers, utilities, infrastructure contractors, and Matrice 400 owners maintaining spare repair inventory.

Important

Confirm the exact housing section and mounting geometry before ordering. DJI aircraft components can be position- and revision-specific. Installation should be followed by a complete aircraft inspection and operational verification before return to service.