Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p248
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 705955–709086

Specially designed to predict aero thermal, aeromechanical and combustion conditions in aero gas turbine engines; and
2. Theoretical modelling predictions of the aero thermal, aeromechanical and combustion conditions, which have been validated with actual aero gas turbine engine (experimental or production) performance data.
9. D. 005. "Software" specially designed or modified for the operation of items specified by 9A004.e. or 9A004.f.
N.B.: For "software" for items listed in 9A004.d. that are incorporated into "spacecraft payloads", see the appropriate Categories.
9. D. 101. "Software" specially designed or modified for the "use" of goods specified by 9B105, 9B106, 9B116 or 9B117.
9. D. 103. "Software" specially designed for modelling, simulation or design integration of the space launch vehicles specified by 9A004 or sounding rockets specified by 9A104, or the subsystems specified by 9A005, 9A007, 9A105, 9A106.c., 9A107, 9A108.c., 9A116 or 9A119.
Note 1: "Software" specified by 9D103 remains controlled when combined with specially designed hardware specified by 4A102.
Note 2: Certain items specified in 9D103 may be subject to the MTCR Guidelines for Sensitive Missile‑Relevant Transfers.
9. D. 104. "Software" specially designed or modified for the "use" of goods specified by 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A008.d., 9A009.a., 9A010.d., 9A011, 9A101, 9A102, 9A105, 9A106.c., 9A106.d., 9A107, 9A108.c., 9A109, 9A111, 9A115.a., 9A116.d., 9A117 or 9A118.
Note: Certain items specified in 9D104 may be subject to the MTCR Guidelines for Sensitive Missile‑Relevant Transfers.
9. D. 105. "Software" which coordinates the function of more than one subsystem, specially designed or modified for "use" in 'missiles', space launch vehicles specified by 9A004 or sounding rockets specified by 9A104.
Note: For a manned aircraft converted to operate as an unmanned aerial vehicle, 9D105 includes "software", as follows:
a. "Software" specially designed or modified to integrate the conversion equipment with the aircraft system functions;
b. "Software" specially designed or modified to operate the aircraft as an unmanned aerial vehicle.
Technical Note:
In 9D105, 'missile' means complete rocket systems and "unmanned aerial vehicles" capable of a range exceeding 300km.
9. E.  Technology
Note: "Development" or "production" "technology" specified by 9E001 to 9E003 for gas turbine engines remains controlled when used for repair or overhaul. Excluded from control are: technical data, drawings or documentation for maintenance activities directly associated with calibration, removal or replacement of damaged or unserviceable line replaceable units, including replacement of whole engines or engine modules.
9. E. 001. "Technology" according to the General Technology Note for the "development" of equipment or "software", specified by 9A004 to 9A012, 9A350, 9B or 9D.
Note: Certain items specified in 9E001 may be subject to the MTCR Guidelines for Sensitive Missile‑Relevant Transfers.
9. E. 002. "Technology" according to the General Technology Note for the "production" of equipment specified by 9A004