Product overview
The TINTEC TL2S is a payload-release accessory for the Autel EVO Max 4T, intended for planned lightweight delivery and field-support tasks. Its integrated architecture provides one release channel and one hook, with an external manual hook-loading button for preparation before take-off. PSDK supplies payload communication and control without a separate third-party controller. The device occupies ≤ 60 × 40 × 20 mm and weighs 50 ± 5 g. Fast onboard or belly mounting avoids modifying the original drone structure, and the housing is waterproof and dustproof.
The rated load capacity is up to 1 kg, while the recommended routine payload is within 500 g. Permitted mission loading must follow aircraft limits, installation condition, battery status, flight environment and applicable regulations. Each application requires individual assessment of payload dimensions, attachment method, wind conditions, release height, landing area, personnel safety and aviation rules. Before take-off, the hook and payload connection require manual checks, and the load must be securely attached. The single-hook configuration provides one controlled release point for missions requiring one lightweight item.
Specifications
| Specification | Value & conditions |
|---|---|
| Model | TL2S |
| Applicable platform | Max4T |
| Control method | PSDK |
| Release channels | 1 |
| Number of hooks | 1 |
| Dimensions | ≤ 60 × 40 × 20 mm |
| Device weight | 50 ± 5 g |
| Maximum load capacity | Up to 1 kgProduct rated load capacity; permitted mission payload must follow aircraft limits, installation condition, battery status, flight environment and applicable regulations. |
| Recommended routine payload | Within 500 gRoutine operation. |
| Mounting method | Fast onboard / belly mounting |
| Payload loading | External manual hook-loading button |
| Protective structure | Waterproof and dustproof housing |
| Controller integration | PSDK payload communication and control without a separate third-party controller.Max4T platform. |
| Structural installation | Belly mounting without modifying the original drone structure. |
| Payload attachment requirements | Secure payload attachment and manual checks of the hook and payload connection.Before take-off; payload within permitted aircraft limits and suitable for planned flight conditions. |
| Mission suitability factors | Payload dimensions, attachment method, wind conditions, release height, landing area, personnel safety and aviation rules.Individual application assessment. |
