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PT6E-66XT Engine
PT6E-66XT Engine

PT6E-66XT Engine

Brand:Pratt & Whitney Model:PT6E-66XT Engine

Introducing the new PT6E-66XT engine for the Daher TBM 960 aircraft – precise and consistent performance at every altitude, every temperature, on every flight.

The PT6 E-Series™ engine – the first engine family with a dual-channel integrated electronic propeller and engine control system in the General Aviation turboprop market.

The DNA you trust, pushing innovation to a new level.

Introducing the new PT6E-66XT engine for the Daher TBM 960 aircraft – precise and consistent performance at every altitude, every temperature, on every flight.

The PT6 E-Series™ engine – the first engine family with a dual-channel integrated electronic propeller and engine control system in the General Aviation turboprop market.

The DNA you trust, pushing innovation to a new level.

Simplified & Enhanced Pilot Experience

With digital intelligence at its heart, the PT6-66XT engine model offers the optimal combination of precision, performance and efficiency for an elevated flying experience.

More Flying Time

Improved design features and digital capabilities of the PT6E-66XT engine increase the time on wing of your engine, so you can enjoy more flying time. An easy engine to maintain just got even easier.

Data Intelligence

The intelligence behind the PT6E-66XT engine optimizes engine power, speed and fuel burn.
Feel the true digital experience knowing your engine provides the right performance at the right time by optimizing the power over your entire flight.

Frequently Asked Questions

  • What is the typical lead time for gas turbine overhaul services?
    The lead time for gas turbine overhaul services ranges from 6 to 14 weeks, depending on the damage assessment, parts availability, and whether hot-section repairs are required. Expedited options may reduce this by 30%.
  • Do you provide customizations for legacy turbine control systems?

    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.

  • How often should industrial gas turbines undergo performance testing?

    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.

  • Are your radiation-hardened (rad-hard) semiconductors compliant with MIL-PRF-38535?

    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.

  • What temperature ranges do your military-grade ICs support?

    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.

  • Are PMA parts interchangeable with OEM components?

    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.

  • What traceability standards do you follow for aircraft fasteners?

    All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.

  • How do you handle urgent AOG (Aircraft on Ground) requests?

    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.

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