Document ID: chunk:federal_register_of_legislation:F2024L01024:front:0:p235
Version: federal_register_of_legislation:F2024L01024
Segment Type: other
Provision Reference: 
Character Range: 670737–673794

or more; or
                b. Full load displacement exceeding 1,500 tonnes with a maximum design speed, fully loaded, exceeding 25 knots in a significant wave height of 4 m or more.
              Technical Note:
              For the purposes of 8E002.c.4., a 'small waterplane area vessel' is defined by the following formula: waterplane area at an operational design draft less than 2x (displaced volume at the operational design draft)2/3.

Category 9—Aerospace and propulsion
9. A  Systems, Equipment and Components
N.B.: For propulsion systems designed or rated against neutron or transient ionising radiation, see the Munitions List.
9. A. 001. Aero gas turbine engines having any of the following:
N.B.: SEE ALSO 9A101.
a. Incorporating any of the "technologies" specified by 9E003.a., 9E003.h. or 9E003.i.;
Note 1: 9A001 does not apply to aero gas turbine engines which meet all of the following:
                   a. Certified by the civil aviation authorities of one or more Wassenaar Arrangement Participating States; and
                   b. Intended to power non‑military manned "aircraft" for which any of the following has been issued by civil aviation authorities of one or more Wassenaar Arrangement Participating State for the aircraft with this specific engine type:
1. A civil type certificate; or
2. An equivalent document recognised by the International Civil Aviation Organisation (ICAO).
Note 2: 9A001 does not apply to aero gas turbine engines designed for Auxiliary Power Units (APUs) approved by the civil aviation authorities of one or more Wassenaar Arrangement Participating States.

b. Not used since 2022
9. A. 002. 'Marine gas turbine engines' designed to use liquid fuel and having all of the following, and specially designed assemblies and components therefor:
a.  Maximum continuous power when operating in "steady state mode" at standard reference conditions specified by ISO 3977‑2:1997 (or national equivalent) of 24,245 kW or more; and
b.  'Corrected specific fuel consumption' not exceeding 0.219 kg/kWh at 35% of the maximum continuous power when using liquid fuel.
Note: The term 'marine gas turbine engines' includes those industrial, or aero‑derivative, gas turbine engines adapted for a ship's electric power generation or propulsion.
Technical Note:
For the purposes of 9A002., 'corrected specific fuel consumption' is the specific fuel consumption of the engine corrected to a marine distillate liquid fuel having a net specific energy (i.e., net heating value) of 42MJ/kg (ISO 3977‑2:1997).

9. A. 003. Specially designed assemblies or components, incorporating any of the "technologies" specified by 9E003.a., 9E003.h. or 9E003i., or 9E003.k., for any of the following gas turbine engine propulsion systems:
a. Specified by 9A001; or
b. Whose design or production origins are either not from a Wassenaar Arrangement Participating State or unknown to the manufacturer.
9. A. 004. Space launch vehicles, "spacecraft", "spacecraft buses", "spacecraft payloads", "spacecraft" on-board systems or equipment,