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PW4000-100 Engine
PW4000-100 Engine

PW4000-100 Engine

Brand:Pratt & Whitney Model:PW4000-100 Engine

Pratt & Whitney has taken its successful PW4000 100-inch engine for the Airbus A330 to new heights with the introduction of the PW4170 Advantage70™ program.
The Advantage70 is offered as a new engine and as an upgrade kit for existing engines. Advantage70 technology delivers superior engine performance, including a 2 percent thrust increase, more than 1 percent reduction in fuel consumption, increased durability, and reduced maintenance costs.
Developed specifically for the Airbus A330 twinjet and introduced in 1994, the PW4000 100-inch fan engine has thrust capability from 64,500 to 70,000 pounds at take-off. The engine was the first in aviation history to qualify for Extended-range Twin-engine Operations (ETOPS) prior to entering service. It is now approved for 180-minute ETOPS.
Pratt & Whitney supplies A330 customers the entire propulsion system - engine, nacelle, thrust reverser and accessories. This, along with superb service reliability, excellent performance retention and low cost of ownership, make the PW4000 100-inch engine an outstanding value.

Pratt & Whitney has taken its successful PW4000 100-inch engine for the Airbus A330 to new heights with the introduction of the PW4170 Advantage70™ program.

The Advantage70 is offered as a new engine and as an upgrade kit for existing engines. Advantage70 technology delivers superior engine performance, including a 2 percent thrust increase, more than 1 percent reduction in fuel consumption, increased durability, and reduced maintenance costs.

Developed specifically for the Airbus A330 twinjet and introduced in 1994, the PW4000 100-inch fan engine has thrust capability from 64,500 to 70,000 pounds at take-off. The engine was the first in aviation history to qualify for Extended-range Twin-engine Operations (ETOPS) prior to entering service. It is now approved for 180-minute ETOPS.

Pratt & Whitney supplies A330 customers the entire propulsion system - engine, nacelle, thrust reverser and accessories. This, along with superb service reliability, excellent performance retention and low cost of ownership, make the PW4000 100-inch engine an outstanding value.

Specs (7)

Fan Tip Diameter

100 In

Length, Flange To Flange

163.1 In

Takeoff Thrust

64,500–70,000 Lb

Flat Rated Temperature

86°F

Bypass Ratio

5.0

Overall Pressure Ratio (Takeoff)

32.0–35.4

Fan Pressure Ratio

1.75

Frequently Asked Questions

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    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%.
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    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.

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    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.

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    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.

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    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.

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    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.

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

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    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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