Document ID: chunk:federal_register_of_legislation:F2024L01100:clause:1_34
Version: federal_register_of_legislation:F2024L01100
Segment Type: clause
Provision Reference: sch 1 cl 34
Character Range: 32013–34395

34        ML10.d                              "Classified" items as follows not integrated into a complete engine:
                                               1.    Digital engine control systems (e.g., Full Authority Digital Engine Controls (FADEC) and Digital Electronic Engine Controls (DEEC)) specially designed for the following gas turbine engines.
                                               1.         Turbofan and Turbojet engines capable of 15,000 lbf (66.7 kN) of thrust or greater, having any of the following:
                                               1.             With or specially designed for thrust augmentation (afterburner);
                                               1.             Thrust or exhaust nozzle vectoring;
                                               2.             Specially designed for sustained 30 second inverted flight or negative g maneuver; or
                                               3.             Specially designed for high power extraction (greater than 50 percent of engine thrust at altitude) at altitudes greater than 50,000 feet.
                                               1.        Turboshaft and Turboprop engines having any of the following:
                                               1.             Capable of 2000 mechanical shp (1491 kW) or greater and specially designed with oil sump sealing when the engine is in the vertical position; or
                                               1.             Capable of a specific power of 225 shp/(lbm/sec) or greater and specially designed for armament gas ingestion and non-civil transient maneuvers, where specific power is defined as maximum takeoff shaft horsepower (shp) divided by compressor inlet flow (lbm/sec).
                                               1.         Gas turbine engines specially designed for uncrewed aerial vehicle, cruise missiles, or target drones.
                                               2.        GE38, AGT1500, CTS800, T55, HPW3000, GE3000, T408, and T700 engines.
                                               1.    Specially designed components for the following U.S.-origin engines: F101, F107, F112, F118, F119, F120, F135, F136, F414, F415, and J402;
                                               2.    "Hot section" components specially designed for gas turbine engines specified in this section.