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Geared turbofan with fan and core mounted accessory gearboxes
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Translatable cascade thrust reverser
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Integrated inlet fan case
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Gas turbine engine assembly including accessory components within the nacelle
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Systems and methods involving multiplexed engine control signals
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Pylon and engine mount configuration
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Reduced gearbox size by separate electrically powered engine oil system
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Generator with separate oil system for improved nacelle performance
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Tangential anti-swirl air supply
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Access door for gas turbine engine components
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Nacelle compartment plenum for bleed air flow delivery system
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