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  2. Honeywell TPE331 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_TPE331

    The 715 shp TPE331-6 used in the Beech King Air B100 have a 400-hr. fuel nozzle cleaning interval, 1,800-hr. hot section inspection interval and a 5,400-hr. time between overhaul; approval is possible for 3,000-hr. HSIs and 6,000-hr. overhauls and engine reserves are cheaper than for the PT6A.

  3. Rolls-Royce AE 2100 - Wikipedia

    en.wikipedia.org/wiki/Rolls-Royce_AE_2100

    A variant proposed in 1995 and paired with Dowty R394 propellers to retrofit the Allison T56-powered Lockheed C-130 models E through H and Lockheed L-100-30, at a price after engine/propeller trade-in of USD$11 million per aircraft.

  4. General Electric H-Series - Wikipedia

    en.wikipedia.org/wiki/General_Electric_H-Series

    The H75-100 weighs 94 lb (43 kg) more than the equivalent PT6 but pioneers single lever electronic propeller and engine control in general aviation, for an initial TBO of 4,000 hr which could be increased with experience. [5] It promises 10% better fuel burn, 10% longer overhaul and lower maintenance costs than the PT6A-135 for the Nextant ...

  5. The cost of Prop. 1: Newsom's plan to transform ... - AOL

    www.aol.com/news/cost-prop-1-newsoms-plan...

    If Proposition 1 is approved by California voters, the bond to build more mental health facilities could cost $14 billion in debt and interest payments. The cost of Prop. 1: Newsom's plan to ...

  6. Pratt & Whitney Canada PT6 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PT6

    In October 2019 the PT6 E-Series was launched on the PC-12 NGX, the first general aviation turboprop with an electronic propeller and engine control system with a single lever and better monitoring for longer maintenance intervals, increased from 300 to 600 hours, and a TBO increased by 43% to 5,000 hours, reducing engine operating costs by at ...

  7. Pratt & Whitney Canada PW100 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_Canada_PW100

    Two PW150-based engines would be used to drive a single propeller. [23] The powerplant was eliminated from contention by Airbus in early June 1999, since it was short of providing the 9,000 shp (6,700 kW) required to drive the eight-bladed propeller at the time, and its specific fuel consumption (SFC) was excessive. [24] PW150B

  8. Prop. 32 would raise the minimum wage. But would it solve our ...

    www.aol.com/prop-32-raise-minimum-wage-170819225...

    Voters should reject Prop. 32, and, instead, advocate for their representatives to promote substantial housing development and other policies that would bring down or stabilize costs for everyday ...

  9. Allison Model 250 - Wikipedia

    en.wikipedia.org/wiki/Allison_Model_250

    Data from The Instrumentation Design And Control of a T63-A-700 Gas Turbine Engine General characteristics Type: Turboshaft Length: 40.5 in (1,029 mm) Diameter: 22.5 in (572 mm) Dry weight: 138.5 lb (63 kg) dry Components Compressor: 6-stage axial + 1-stage centrifugal compressors Combustors: Single can combustion chamber Turbine: 2-stage axial gas generator power turbine + 2-stage axial free ...

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