TP400-D6
Design, development, and manufacturing activities of the TP400-D6 engine are carried out by the Europrop International (EPI) consortium, established by MTU Aero Engines, Snecma, Rolls-Royce, and ITP Aero. TEI participates in the project as a risk and revenue-sharing partner alongside ITP Aero.
The engine performed its first flight on the A400M aircraft in Seville, Spain, in late 2009, and entered into service at the end of 2013. As of March 2026, the engine has surpassed 1,000,000 flight hours.
As of 2022, all 10 A400M (ATLAS) aircraft procured
by the Turkish Air Force have been delivered.
As of 2022, all 10 A400M (ATLAS) aircraft procured
by the Turkish Air Force have been delivered.
TEI is responsible for design, development, prototype production, assembly, testing, mass production and post-sales support of the following work packages:
- Front Bearing Structure Module,
- Propeller Gearbox Supporting Bars,
- Primary Exhaust Nozzle,
- Exhaust Cone,
- Special to Project Test Equipment - SPTE
- Preparation of the Component Maintenance Manual (CMM) as necessary to perform the maintenance activities for the Front Bearing Structure Module at TEI MRO
- Service support engineering activities to resolve any problems arising in the post-sales process with respect to the modules under TEI's responsibility
Technical Specifications
- Engine Type: Turboprop
- Engine Power: Approx. 11,000 shp (sea level)
- Pressure Ratio: 25
- Weight: Approx. 1,900 kg (dry)
- Length: 3,5 m
- Diameter: 0,92 m
- Compressor: 5 intermediate-pressure stages, 6 high-pressure stages
- Turbine: 1 high-pressure stage, 1 intermediate-pressure stage, 3 low-pressure stages
General Specifications
- The most powerful turboprop engine of the Western Europe
- High growth potential
- Low lifecycle cost
- Component technology endurable for military and commercial applications
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