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  2. Time between overhauls - Wikipedia

    en.wikipedia.org/wiki/Time_between_overhauls

    Time between overhauls (abbreviated as TBO or TBOH) is the manufacturer's recommended number of running hours or calendar time before an aircraft engine or other component requires overhaul. [ 1 ] On rotorcraft , many components have recommended or mandatory TBOs, including main rotor blades , tail rotor blades and gearboxes .

  3. 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.

  4. Honeywell HTF7000 - Wikipedia

    en.wikipedia.org/wiki/Honeywell_HTF7000

    Honeywell maintenance program is $447 for two engines per hour. [5] Borescope inspections extends time between overhaul and some engines have remained installed for up to 10,000 hr. [3] It has line replaceable components installed with hand tools and is designed for condition-based maintenance. [2]

  5. Aircraft maintenance - Wikipedia

    en.wikipedia.org/wiki/Aircraft_maintenance

    In 2017, of the $70 billion spent by airlines on maintenance, repair and overhaul (MRO), 31% were for engines, 27% for components, 24% for line maintenance, 10% for modifications and 8% for the airframe; 70% were for mature airliners (Airbus A320 and A330, Boeing 777 and 737NG), 23% were for “sunset” aircraft (McDonnell Douglas MD-80 ...

  6. General Electric CF34 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_CF34

    The General Electric CF34 is a civilian high-bypass turbofan developed by GE Aviation from its TF34 military engine. The CF34 is used on a number of business and regional jets, including the Bombardier CRJ series, the Embraer E-Jets, and Comac ARJ21. [2] [3] In 2012, there were 5,600 engines in service.

  7. Vedeneyev M14P - Wikipedia

    en.wikipedia.org/wiki/Vedeneyev_M14P

    The Vedeneyev M14P is a Russian nine-cylinder, four-stroke, air-cooled, petrol-powered radial engine. Producing 360 hp (268 kW), its design dates from the 1940s (Kotelnikov 2005), and is itself a development of the Ivchenko AI-14 engine. The engine has been used extensively by the Yakovlev and Sukhoi Design Bureaus.

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