Home > Media > Media library MEDIA LIBRARY All our photos and videos PHOTOS SHOW ALLA400MFLIGHT CENTERTP400-D6 +LOAD MORE Terms and conditions to use the photos The pictures may be used solely for press applications. They may under no circumstances be put to any commercial or promotional use, nor may they be sold or transferred to a third party. Users agree to comply with all legislation and regulations governing intellectual property and literary and artistic property, notably compulsory inclusion of the photo credits. VIDEOS DISCOVER ALSO NEWS AND EVENTS OUR PUBLICATIONS OUR COMPANY LEGAL TERMS AND CONDITIONS & PRIVACY POLICY FOLLOW US ON LINKEDIN By continuing your navigation, you consent to our use of cookies for services and statistics. OK, I AGREENO, LEARN MORE

Home > TP400-D6 engine TP400-D6 ENGINE THE MOST POWERFUL TURBOPROP ENGINE IN PRODUCTION A STRONG PARTNERSHIP FACTS & FIGURES THE TP400-D6, A KEY TO THE A400M'S UNRIVALED CAPABILITIES HIGH SPEED Delivering an output of more than 11,000 shaft horsepower at sea level and a three-shaft configuration combining state-of-the-art engine modules LONG RANGE With a high autonomy of 4,800 nm (8900 km), the TP400-D6 can power extended round trip sorties from its main operating base HIGH TECHNOLOGY To optimise engine utilization and enable post-flight troubleshooting, the engine benefits from a dual Full Authority Digital Engine Control (FADEC) HIGH ALTITUDE Operating up to 40,000 ft MODULAR DESIGN Interchangeable modules improve engine availability for operational support and efficiency for all maintenance activities CIVIL CERTIFICATION First military engine to be fully civil certified from the outset by EASA in 2011. THE TP400-D6 HAS COMPLETED MORE THAN 400,000 ENGINE FLYING HOURS (EFH) IN MAY 2021. HOW DOES IT WORK Video Player 00:00 00:25 TP400-D6 ENGINE SPECIFICATIONS ENGINE CHARACTERISTICS Type of Engine: three-shaft turboprop Power output: 11,000 shp at sea level Pressure ratio: 25 Weight approx.: 1,900kg (dry) Length: 3,5m Diameter: 0,92m Compressor: 5 intermediate pressure stages, 6 high pressure stages Turbine: 1 high pressure stage, 1 intermediate pressure stage, 3 low pressure stages ARCHITECTURE High Pressure Compressor: pressure ratio 7 6 stages to ensure growth margin Intermediate Pressure Compressor: pressure ratio 3.5 5-stage unit with no variables to reduce complexity Single stage High Pressure Turbine Single stage Intermediate Turbine Three stage Low Pressure Turbine Two modes of engine rotation right-handed with common casing left-handed with additional gear train ©Photos DISCOVER ALSO OUR SERVICES OUR COMPANY OUR MAINTENANCE CONCEPT LEGAL TERMS AND CONDITIONS & PRIVACY POLICY FOLLOW US ON LINKEDIN By continuing your navigation, you consent to our use of cookies for services and statistics. OK, I AGREENO, LEARN MORE