Category 9--Aerospace and Propulsion

A. EQUIPMENT, ASSEMBLIES AND COMPONENTS

N.B.: For propulsion systems designed or rated against neutron or transient ionizing radiation, see the U.S. Munitions List, 22 CFR part 121.

9A001 Aero gas turbine engines having any of the following (see List of Items Controlled).

Note: 9A001.a. does not control aero gas turbine engines which meet all of the following:

a. Certified by the civil aviation authority in a country listed in Supplement No. 1 to Part 743; and

b. Intended to power non-military manned aircraft for which any of the following has been issued by a Participating State listed in Supplement No. 1 to Part 743 for the aircraft with this specific engine type:

b.1. A civil type certificate; or

b.2. An equivalent document recognized by the International Civil Aviation Organization (ICAO).

9A002 `Marine gas turbine engines' with an ISO standard continuous power rating of 24,245 kW or more and a specific fuel consumption not exceeding 0.219 kg/kWh in the power range from 35 to 100%, and specially designed assemblies and components therefor.

Items: The list of items controlled is contained in the ECCN heading.

9A003 Specially designed assemblies and components, incorporating any of the ``technologies'' controlled by 9E003.a, 9E003.h or 9E003.i, for any of the following gas turbine engine propulsion systems (see List of Items Controlled).

9A004 Space launch vehicles and ``spacecraft''.

Unit: Number

(1.) See also 9A104.

(2.) Space launch vehicles are under the jurisdiction of the Department of State.

(3.) Effective March 15, 1999, all satellites, including commercial communications satellites, are subject to the ITAR. Effective March 15, 1999, all license applications for the export of commercial communications satellites will be processed by the State Department, Directorate of Defense Trade Controls. Retransfer of jurisdiction for commercial communications satellites and related items shall not affect the validity of any export license issued by the Department of Commerce prior to March 15, 1999, or of any export license application filed under the Export Administration Regulations on or before March 14, 1999, and subsequently issued by the Department of Commerce. Commercial communications satellites licensed by the Department of Commerce, including those already exported, remain subject to the EAR and all terms and conditions of issued export licenses until their stated expiration date. All licenses issued by the Department of Commerce for commercial communications satellites, including licenses issued after March 15, 1999, remain subject to SI controls throughout the validity of the license. Effective March 15, 1999, Department of State jurisdiction shall apply to any instance where a replacement license would normally be required from the Department of Commerce. Transferring registration or operational control to any foreign person of any item controlled by this entry must be authorized on a license issued by the Department of State, Directorate of Defense Trade Controls. This requirement applies whether the item is physically located in the United States or abroad.

(4.) All other ``spacecraft'' not controlled under 9A004 and their payloads, and specifically designed or modified components, parts, accessories, attachments, and associated equipment, including ground support equipment, are subject to the export licensing authority of the Department of State unless otherwise transferred to the Department of Commerce via a commodity jurisdiction determination by the Department of State.

(5.) Exporters requesting a license from the Department of Commerce for ``spacecraft'' and their associated parts and components, other than the international space station, must provide a statement from the Department of State, Directorate of Defense Trade Controls, verifying that the item intended for export is under the licensing jurisdiction of the Department of Commerce. All specially designed or modified components, parts, accessories, attachments, and associated equipment for ``spacecraft'' that have been determined by the Department of State through the commodity jurisdiction process to be under the licensing jurisdiction of the Department of Commerce and that are not controlled by any other ECCN on the Commerce Control List will be assigned a classification under this ECCN 9A004.

(6.) Technical data required for the detailed design, development, manufacturing, or production of the international space station (to include specifically designed parts and components) remains under the jurisdiction of the Department of State. This control by the ITAR of detailed design, development, manufacturing or production technology for NASA's international space station does not include that level of technical data necessary and reasonable for assurance that a U.S.-built item intended to operate on NASA's international space station has been designed, manufactured, and tested in conformance with specified requirements (e.g., operational performance, reliability, lifetime, product quality, or delivery expectations). All technical data and all defense services, including all technical assistance, for launch of the international space station, including launch vehicle compatibility, integration, or processing data, are controlled and subject to the jurisdiction of the Department of State, in accordance with 22 CFR parts 120 through 130.

9A005 Liquid rocket propulsion systems containing any of the systems or components, controlled by 9A006. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121).

9A006 Systems and components, specially designed for liquid rocket propulsion systems. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121).

9A007 Solid rocket propulsion systems. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A008 Components specially designed for solid rocket propulsion systems. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A009 Hybrid rocket propulsion systems. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A010 Specially designed components, systems and structures, for launch vehicles, launch vehicle propulsion systems or ``spacecraft''. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121).

9A011 Ramjet, scramjet or combined cycle engines, and specially designed components therefor. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121).

9A012 Non-military ``unmanned aerial vehicles,'' (``UAVs''), unmanned ``airships'', associated systems, equipment and components, as follows (see List of Items Controlled).

a. ``UAVs'' or unmanned ``airships'', having any of the following:

a.1. An autonomous flight control and navigation capability (e.g., an autopilot with an Inertial Navigation System); or

a.2. Capability of controlled flight out of the direct visual range involving a human operator (e.g., televisual remote control);

b.1. Equipment specially designed for remotely controlling the ``UAVs'' or unmanned ``airships'', controlled by 9A012.a.;

b.2. Systems for navigation, attitude, guidance or control, other than those controlled in Category 7, specially designed to provide autonomous flight control or navigation capability to ``UAVs'' or unmanned ``airships'', controlled by 9A012.a.;

b.3. Equipment or components specially designed to convert a manned ``aircraft'' or a manned ``airship'' to a ``UAV'' or unmanned ``airship'', controlled by 9A012.a;

b.4. Air breathing reciprocating or rotary internal combustion type engines, specially designed or modified to propel ``UAVs'' or unmanned ``airships'', at altitudes above 50,000 feet (15,240 meters).

Note: 9A012 does not control model aircraft or model ``airships''.

9A018 Equipment on the Wassenaar Arrangement Munitions List.

(a) Parachute systems designed for use in dropping military equipment, braking military aircraft, slowing spacecraft descent, or retarding weapons delivery;

(b) Instrument flight trainers for combat simulation; and

(c) military ground armed or armored vehicles and parts and components specific thereto described in 22 CFR part 121, Category VII; and all-wheel drive vehicles capable of off-road use that have been armed or armored with articles described in 22 CFR part 121, Category XIII (See Sec. 770.2(h)--Interpretation 8) are all subject to the export licensing jurisdiction of the U.S. Department of State, Directorate of Defense Trade Controlss.

Related Definition: This entry controls parachute systems designed for use in dropping personnel only.

9A101 Turbojet and Turbofan Engines, Other Than Those Controlled by 9A001, as Follows (See List of Items Controlled

(1) Items controlled in 9A101.b are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls (see 22 CFR part 121).

(2) Engines designed or modified for missiles (except engines for non-military unmanned air vehicles [UAVs] or remotely piloted vehicles [RPVs]), regardless of thrust or specific fuel consumption, are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. (See 22 CFR part 121.)

Related Definitions: N/A

9A103 Liquid Propellant Tanks Specially Designed for the Propellants Controlled in ECCNs 1C011, 1C111 or Other Liquid Propellants Used in ``Missiles.'' (These Items Are Subject to the Export Licensing Authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A104 Sounding rockets, capable of a range of at least 300 km. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A105 Liquid propellant rocket engines. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A106 Systems or components, other than those controlled by 9A006, usable in ``missiles'', as follows (see List of Items Controlled), and specially designed for liquid rocket propulsion systems.

Technical Note: Examples of methods of achieving thrust vector control controlled by 9A106.c includes:

1. Flexible nozzle;

2. Fluid or secondary gas injection;

3. Movable engine or nozzle;

4. Deflection of exhaust gas steam (jet vanes or probes); or

5. Thrust tabs.

d. Liquid and slurry propellant (including oxidizers) control systems, and specially designed components therefor, designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2000 Hz.

9A107 Solid Propellant Rocket Engines, Usable in Rockets With a Range Capability of 300 Km or Greater, Other Than Those Controlled by 9A007, Having Total Impulse Capacity Equal to or Greater Than 8.41 x 10\5\ Ns, but less than 1.1 x 10\6\ (These Items are Subject to the Export Licensing Authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A108 Solid rocket propulsion components, other than those controlled by 9A008, usable in rockets with a range capability of 300 Km or greater. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A109 Hybrid rocket motors, usable in rockets with a range capability of 300 Km or greater, other than those controlled by 9A009, and specially designed components therefor. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A110Composite structures, laminates and manufactures thereof, other than those controlled by entry 9A010, specially designed for use in ``missiles'' or the subsystems controlled by entries 9A005, 9A007, 9A105.a, 9A106 to 9A108, 9A116, or 9A119.

9A111 Pulse jet engines, usable in ``missiles'', and specially designed components therefor. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A115 Apparatus, devices and vehicles, designed or modified for the transport, handling, control, activation and launching of rockets, missiles, and unmanned aerial vehicles capable of achieving a ``range'' equal to or greater than 300 km. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controlss. See 22 CFR part 121.)

9A116 Reentry vehicles, usable in ``missiles'', and equipment designed or modified therefor. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A117 Staging mechanisms, separation mechanisms, and interstages therefor, usable in ``missiles''. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controlss. See 22 CFR part 121.)

9A118 Devices to regulate combustion usable in engines which are usable in rockets with a range capability greater than 300 Km orgreater, controlled by 9A011 or 9A111. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A119 Individual rocket stages, usable in rockets with a range capability greater than 300 Km or greater, other than those controlled by 9A005, 9A007, 9A009, 9A105, 9A107 and 9A109. (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9A120 Complete unmanned aerial vehicles, not specified in 9A012, having all of the following:

Note: 9A120 does not control model aircraft, specially designed for recreational or competition purposes.

Technical Notes:

1. An aerosol consists of particulate or liquids other than fuel components, by-products or additives, as part of the payload to be dispersed in the atmosphere. Examples of aerosols include pesticides for crop dusting and dry chemicals for cloud seeding.

2. An aerosol dispensing system/mechanism contains all above devices (mechanical, electrical, hydraulic, etc.), which are necessary for storage and dispersion of an aerosol into the atmosphere. This includes the possibility of aerosol injection into the combustion exhaust vapor and into the propeller slip stream.

9A980 Nonmilitary mobile crime science laboratories; and parts and accessories, n.e.s.

9A990 Diesel engines, n.e.s., and tractors and specially designed parts therefor, n.e.s.

9A991 ``Aircraft'', n.e.s., and gas turbine engines not controlled by 9A001 or 9A101 and parts and components, n.e.s.

License Requirement Notes: There is no de minimis level for foreign-made aircraft described by this entry that incorporate commercial primary or standby instrument systems that integrate QRS11-00100-100/101 or commercial automatic flight control systems that integrate QRS11-00050-443/569 Micromachined Angular Rate Sensors (see Sec. 734.4(a) of the EAR).

Related Controls: QRS11 Micromachined Angular Rate Sensors are subject to the export licensing jurisdiction of the U.S. Department of State, Directorate of Defense Trade Controls, unless the QRS11-00100-100/101 is integrated into and included as an integral part of a commercial primary or standby instrument system of the type described in ECCN 7A994, or aircraft of the type described in ECCN 9A991 that incorporates such a system, or is exported solely for integration into such a system; or the QRS11-00050-443/569 is integrated into an automatic flight control system of the type described in ECCN 7A994, or aircraft of the type described in ECCN 9A991 that incorporates such a system, or are exported solely for integration into such a system. (See Commodity Jurisdiction requirements in 22 CFR Part 121; Category VIII(e), Note(1)) In the latter case, such items are subject to the licensing jurisdiction of the Department of Commerce. Technology specific to the development and production of QRS11 sensors remains subject to the licensing jurisdiction of the Department of State.

Note: Specify make and model of aircraft and type of avionic equipment on aircraft.

Note: 9A991.c does not control aero gas turbine engines that are destined for use in civil ``aircraft'' and that have been in use in bona fide civil ``aircraft'' for more than eight years. If they have been in use in bona fide civil ``aircraft'' for more than eight years, such engines are controlled under 9A991.d.

9A992 Complete canopies, harnesses, and platforms and electronic release mechanisms therefor, except such types as are in normal sporting use.

B. TEST, INSPECTION AND PRODUCTION EQUIPMENT

9B001 Equipment, tooling and fixtures, specially designed for manufacturing gas turbine blades, vanes or "tip shroud" castings, as follows (See List of Items Controlled).

License Requirement Notes: See Sec. 743.1 of the EAR for reporting requirements for exports under License Exceptions.

9B002On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, having all of the following (See List of Items Controlled).

9B003 Equipment specially designed for the ``production'' or test of gas turbine brush seals designed to operate at tip speeds exceeding 335 m/s and temperatures in excess of 773 K (500[deg]C), and specially designed components or accessories therefor.

9B004 Tools, dies or fixtures, for the solid state joining of ``superalloy'', titanium or intermetallic airfoil-to-disk combinations described in 9E003.a.3 or 9E003.a.6 for gas turbines.

9B005 On-line (real time) control systems, instrumentation (including sensors) or automated data acquisition and processing equipment, specially designed for use with any of the following (see List of Items Controlled).

a. Wind tunnels designed for speeds of Mach 1.2 or more;

Note: 9B005.a does not control wind tunnels specially designed for educational purposes and having a `test section size' (measured laterally) of less than 250 mm.

Technical Note: `Test section size' in 9B005.a means the diameter of the circle, or the side of the square, or the longest side of the rectangle, at the largest test section location.

b. Devices for simulating flow-environments at speeds exceeding Mach 5, including hot-shot tunnels, plasma arc tunnels, shock tubes, shock tunnels, gas tunnels and light gas guns; or

c. Wind tunnels or devices, other than two-dimensional sections, capable of simulating Reynolds number flows exceeding 25 x 10 \6\.

9B006 Acoustic vibration test equipment capable of producing sound pressure levels of 160 Db or more (referenced to 20 uPa) with a rated output of 4 kW or more at a test cell temperature exceeding 1,273 K (1,000 deg.C), and specially designed quartz heaters therefor.

9B007 Equipment specially designed for inspecting the integrity of rocket motors and using Non-Destructive Test (NDT) techniques other than planar x-ray or basic physical or chemical analysis.

9B008 Direct measurement wall skin friction transducers specially designed to operate at a test flow total (stagnation) temperature exceeding 833 K (560[deg] C).

9B009 Tooling specially designed for producing turbine engine powder metallurgy rotor components capable of operating at stress levels of 60% of Ultimate Tensile Strength (UTS) or more and metal temperatures of 873 K (600[deg]C) or more.

9B105 Wind tunnels for speeds of Mach 0.9 or more, usable for rockets, missiles, or unmanned aerial vehicles capable of achieving a ``range'' equal to or greater than 300 km and their subsystems.

9B106 Environmental chambers usable for rockets, missiles, or unmanned aerial vehicles capable of achieving a ``range'' equal to or greater than 300 km and their subsystems, as follows (see List of Items Controlled).

a. Environmental chambers capable of simulating all of the following flight conditions:

a.1. Having any of the following:

a.1.a. Altitude equal to or greater than 15,000 m; or

a.1.b. Temperature range of at least -50 [deg]C to +125 [deg]C; and

a.2. Incorporating, or designed or modified to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured `bare table', between 20 Hz and 2 kHz imparting forces equal to or greater than 5 kN;

1. Item 9B106.a.2 describes systems that are capable of generating a vibration environment with a single wave (e.g., a sine wave) and systems capable of generating a broad band random vibration (i.e., power spectrum).

2. The term `bare table' means a flat table, or surface, with no fixture or fittings.

3. In Item 9B106.a.2, designed or modified means the environmental chamber provides appropriate interfaces (e.g., sealing devices) to incorporate a shaker unit or other vibration test equipment as specified in this Item.

9B115 Specially designed ``production equipment'' for the systems, sub-systems and components controlled by 9A004 to 9A009, 9A011, 9A101, 9A104 to 9A109, 9A111, 9A116 to 9A119.

9B116 Specially designed ``production facilities'' for the systems, sub-systems, and components controlled by 9A004 to 9A009, 9A011, 9A012, 9A101, 9A104 to 9A109, 9A111, 9A116 to 9A119.

9B117 Test Benches and Test Stands for Solid or Liquid Propellant Rockets, Motors or Rocket Engines, Having Either of the Following Characteristics (see List of Items Controlled)

9B990 Vibration test equipment and specially designed parts and components, n.e.s.

9B991 Specially designed equipment, tooling or fixtures, not controlled by 9B001, as described in the List of Items Controlled, for manufacturing or measuring gas turbine blades, vanes or tip shroud castings.

C. MATERIALS

9C110 Resin impregnated fiber prepregs and metal coated fiber preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilizing fibrous or filamentary reinforcements having a ``specific tensile strength'' greater than 7.62 x 10\4\ m and a ``specific modulus'' greater than 3.18 x 10\6\ m.

D. SOFTWARE

9D001 ``Software'' specially designed or modified for the ``development'' of equipment or ``technology'', controlled by 9A (except 9A018, 9A990 or 9A991), 9B (except 9B990 or 9B991) or 9E003.

License Requirement Notes: See Sec. 743.1 of the EAR for reporting requirements for exports under License Exceptions.

9D002 ``Software'' specially designed or modified for the ``production'' of equipment controlled by 9A (except 9A018, 9A990, or 9A991) or 9B (except 9B990 or 9B991).

License Requirement Notes: See Sec. 743.1 of the EAR for reporting requirements for exports under License Exceptions.

(1) ``Software'' ``required'' for the ``production'' of items controlled by 9A004 is subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. (See 22 CFR part 121.)

(2) ``Software'' ``required'' for the ``production'' of equipment or ``technology'' subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls is also subject to the same licensing jurisdiction. (See 22 CFR part 121.)

9D003 ``Software'' incorporating ``technology'' specified by 9E003.h and used in ``FADEC Systems'' for propulsion systems controlled by 9A (except 9A018, 9A990 or 9A991) or equipment controlled by 9B (except 9B990 or 9B991).

Related Definitions: N/A

9D004 Other ``software'' as follows (see List of Items Controlled).

9D018 ``Software'' for the ``use'' of equipment controlled by 9A018.

9D101 ``Software'' specially designed or modified for the ``use'' of commodities controlled by 9B105, 9B106, 9B116, or 9B117.

9D102 ``Software'' specially designed for the ``use'' of items controlled by 9A012 (for MT controlled items only), 9A101, 9A106, and 9A110.

9D103 ``Software'' specially designed for modelling, simulation or design integration of ``missiles'', or the subsystems controlled by 9A005, 9A007, 9A105.a, 9A106, 9A108, 9A116 or 9A119. (This entry is subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. See 22 CFR part 121.)

9D104 ``Software'' specially designed and modified for the ``use'' of equipment controlled by 9A001, 9A005, 9A006.d, 9A006.g, 9A007.a, 9A008.d, 9A009.a, 9A010.d, 9A011, 9A012 (for MT controlled items only), 9A101, 9A105, 9A106.c and .d, 9A107, 9A108.c, 9A109, 9A111, 9A115.a, 9A116.d, 9A117, or 9A118.

9D105 ``Software'' that coordinates the function of more than one subsystem, specially designed or modified for ``use'' in ``missiles.'' (These items are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controlss. See 22 CFR part 121.)

9D990 ``Software'', n.e.s., for the ``development'' or ``production'' of equipment controlled by 9A990 or 9B990.

9D991 ``Software'', for the ``development'' or ``production'' of equipment controlled by 9A991 or 9B991.

E. TECHNOLOGY

Note: "Development" or "production" "technology" controlled by 9E001 to 9E003 for gas turbine engines remains controlled when used for repair or overhaul. Excluded from 9E001 to 9E003 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.

9E001 ``Technology'' according to the General Technology Note for the ``development'' of equipment or ``software'', controlled by 9A001.b, 9A004 to 9A012, 9B (except 9B990 or 9B991), or 9D (except 9D990 or 9D991)

License Requirement Notes: See Sec. 743.1 of the EAR for reporting requirements for exports under License Exceptions.

(1) See also 9E101 and 1E002.f (for controls on ``technology'' for the repair of controlled structures, laminates or materials).

(2) The ``technology'' required for the ``development'' of equipment controlled by 9A004 is subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls. (See 22 CFR part 121.)

(3) ``Technology'', required for the ``development'' of equipment or ``software'' subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controls, is also subject to the same licensing jurisdiction. (See 22 CFR part 121)

Related Definitions: N/A.

Items: The list of items controlled is contained in the ECCN heading

9E002 ``Technology'' according to the General Technology Note for the ``production'' of equipment controlled by 9A001.b, 9A004 to 9A011 or 9B(except 9B990 or 9B991).

License Requirement Notes: See Sec. 743.1 of the EAR for reporting requirements for exports under License Exceptions.

9E003 Other ``technology'' as follows (see List of Items Controlled).

License Requirement Notes: See Sec. 743.1 of the EAR for reporting requirements for exports under License Exceptions.

Technical Note: The term `steady state mode' defines engine operation conditions, where the engine parameters, such as thrust/power, rpm and others, have no appreciable fluctuations, when the ambient air temperature and pressure at the engine inlet are constant.

Technical Note: ``Damage tolerant''components are designed using methodology and substantiation to predict and limit crack growth.

N.B.: For ``FADEC systems'', see 9E003.h.

N.B.: For adjustable flow path geometry, see 9E003.i.

c. ``Technology'' ``required'' for manufacturing cooling holes, in gas turbine engine components incorporating any of the ``technologies'' specified by 9E003.a.1, 9E003.a.2 or 9E003.a.5, and having any of the following:

Note: 9E003.c does not apply to ``technology'' for manufacturing constant radius cylindrical holes that are straight through and enter and exit on the external surfaces of the component.

Technical Notes:

1. For the purposes of 9E003.c, the `cross-sectional area' is the area of the hole in the plane perpendicular to the hole axis.

2. For the purposes of 9E003.c, `hole shape ratio' is the nominal length of the axis of the hole divided by the square root of its minimum `cross-sectional area'.

3. For the purposes of 9E003.c, `incidence angle' is the acute angle measured between the plane tangential to the airfoil surface and the hole axis at the point where the hole axis enters the airfoil surface.

4. Techniques for manufacturing holes in 9E003.c include ``laser'', water jet, Electro-Chemical Machining (ECM) or Electrical Discharge Machining (EDM) methods.

d. ``Technology'' ``required'' for the ``development'' or ``production'' of helicopter power transfer systems or tilt rotor or tilt wing ``aircraft'' power transfer systems;

Technical Note: `Box volume' is the product of three perpendicular dimensions measured in the following way:

Length: The length of the crankshaft from front flange to flywheel face;

Width: The widest of any of the following:

a. The outside dimension from valve cover to valve cover;

b. The dimensions of the outside edges of the cylinder heads; or

c. The diameter of the flywheel housing;

Height: The largest of any of the following:

a. The dimension of the crankshaft center-line to the top plane of the valve cover (or cylinder head) plus twice the stroke; or

b. The diameter of the flywheel housing.

f. ``Technology'' ``required'' for the ``production'' of specially designed components for high output diesel engines, as follows:

g. ``Technology'' ``required'' for the development'' or ``production'' of `high output diesel engines' for solid, gas phase or liquid film (or combinations thereof) cylinder wall lubrication and permitting operation to temperatures exceeding 723 K (450[deg]C), measured on the cylinder wall at the top limit of travel of the top ring of the piston;

Technical Note: `High output diesel engines' are diesel engines with a specified brake mean effective pressure of 1.8 MPa or more at a speed of 2,300 r.p.m., provided the rated speed is 2,300 r.p.m. or more.

h. ``Technology'' for gas turbine engine ``FADEC systems'' as follows:

h.1. ``Development'' ``technology'' for deriving the functional requirements for the components necessary for the ``FADEC system'' to regulate engine thrust or shaft power (e.g., feedback sensor time constants and accuracies, fuel valve slew rate);

h.2. ``Development'' or ``production'' ``technology'' for control and diagnostic components unique to the ``FADEC system'' and used to regulate engine thrust or shaft power;

h.3. ``Development'' ``technology'' for the control law algorithms, including ``source code'', unique to the ``FADEC system'' and used to regulate engine thrust or shaft power.

Note: 9E003.h does not apply to technical data related to engine-aircraft integration required by the civil aviation certification authorities to be published for general airline use (e.g., installation manuals, operating instructions, instructions for continued airworthiness) or interface functions (e.g., input/output processing, airframe thrust or shaft power demand).

Note: 9E003.i does not apply to ``development'' or ``production'' ``technology'' for any of the following:

a. Inlet guide vanes;

b. Variable pitch fans or prop-fans;

c. Variable compressor vanes;

d. Compressor bleed valves; or

e. Adjustable flow path geometry for reverse thrust.

j. ``Technology'' not otherwise controlled in 9E003.a.1 through a.8, a.10, and .h and used in the ``development'', ``production'', or overhaul of hot section parts and components of civil derivatives of military engines controlled on the U.S. Munitions List.

9E018 ``Technology'' for the ``development'', ``production'', or ``use'' of equipment controlled by 9A018.

9E101 ``Technology'' according to the General Technology Note for the ``development'', ``production'', or ``use'' of commodities or software controlled by 9A012, 9A101, 9A104 to 9A111, 9A115 to 9A119, 9C110, 9D101, 9D103, 9D104 or 9D105.

Related Controls: ``Technology'' controlled by 9E101 for items in 9A012, 9A101.b, 9A104, 9A105, to 9A109, 9A110 that are specially designed for use in missile systems and subsystems, 9A111, 9A115, 9A116 to 9A119, 9D103, and 9D105 are subject to the export licensing authority of the U.S. Department of State, Directorate of Defense Trade Controlss (see 22 CFR part 121).

9E102 ``Technology'' according to the General Technology Note for the ``use'' of space launch vehicles specified in 9A004, or commodities or software controlled by 9A005 to 9A012, 9A101, 9A104 to 9A111, 9A115 to 9A119, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101, 9D103, 9D104 or 9D105.

9E990 ``Technology'', n.e.s., for the ``development'' or ``production'' or ``use'' of equipment controlled by 9A990 or 9B990.

9E991 ``Technology'', for the ``development'', ``production'' or ``use'' of equipment controlled by 9A991 or 9B991.

9E993 Other ``technology'', not described by 9E003, as follows (see List of Items Controlled)

EAR99 Items subject to the EAR that are not elsewhere specified in this CCL Category or in any other category in the CCL are designated by the number EAR99.