Part of Pratt & Whitney’s innovative PurePower® family, the PW800 demonstrates significantly improved fuel efficiency, emission levels, and operating costs. Designed to power long-haul business jets, regional aircraft, and narrowbodies, these engines are characterized by their advanced materials, design methods, and aerodynamics. Among the key components are an efficient fan, a compressor, a turbine, and the low-emission TALON™ combustor, which together ensure a marked reduction in fuel consumption and minimal environmental impact. The PW800 also harnesses the core technology of the Pratt & Whitney GTF™ engine family.
With its expertise in high-pressure compressors and low-pressure turbines, MTU is instrumental in the success of the PW800.
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.
Gas Turbine
Aircraft parts
