TDA LTT CR 2.2 16V
High-altitude performance
The TDA-LTT CR 2.2 16V is a high-performance aircraft diesel engine developed to deliver consistent power across demanding altitude conditions.
Its twin-turbo architecture, combined with Common Rail direct injection and Dual FADEC engine control, provides 172 kW take-off power and 155 kW maximum continuous power, with continuous power maintained up to 18,000 ft.
Designed as a flexible propulsion platform, the engine can be configured to meet different aircraft integration and mission requirements.
Built for altitude
FULL CONTINUOUS POWER UP TO 18,000 FT
The TDA-LTT CR 2.2 16V is designed to retain power as altitude increases.
At 3,800 rpm, maximum continuous power remains at 155 kW up to 18,000 ft, with 148 kW available at 20,000 ft, 125 kW at 25,000 ft and 102 kW at 30,000 ft.
Looking for a propulsion solution for your aircraft application?
Our engineering and sales teams can support configuration and integration from the first technical assessment to the complete propulsion system.