TDA CR 2.2 16V
Next-Generation Diesel Propulsion for AviationThe TDA-L CR 2.2 16V is a next-generation aviation diesel engine developed from proven automotive technology and specifically optimized for aircraft applications.
Featuring a 2.2 L four-cylinder Common Rail architecture, Single Turbo configuration and Dual FADEC control, the engine delivers up to 172 kW take-off power with high fuel efficiency, reliability and excellent power-to-weight ratio.
Designed for fixed-wing, UAV and rotorcraft applications, the TDA-L CR 2.2 16V can be supplied as a complete propulsion system, including gearbox, engine control, accessories and dedicated integration support.
EASA Certification 2026
- Optimized 2.2 L Single Turbo architecture for efficiency and reliability
- Dual FADEC engine control for enhanced safety and redundancy
- Designed for fixed-wing, UAV and rotorcraft applications
- Dedicated engineering, calibration and aircraft integration support