- Latest available (Revised)
- Original (As adopted by EU)
Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items (Recast)
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There are currently no known outstanding effects for the Council Regulation (EC) No 428/2009, Division [9B].
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NB:
SEE ALSO 2B226
Directional solidification or single crystal casting equipment designed for "superalloys";
Casting tooling, specially designed for manufacturing gas turbine engine blades, vanes or "tip shrouds", manufactured from refractory metals or ceramics, as follows:
Cores;
Shells (moulds);
Combined core and shell (mould) units;
[F2Directional-solidification or single-crystal additive-manufacturing equipment designed for “superalloys”;]
Textual Amendments
Specially designed for the "development" of gas turbine engines, assemblies or components; and
Incorporating any of the "technologies" specified in 9E003.h. or 9E003.i.
Textual Amendments
F3Word in Annex 1 Entry 9B004 substituted (31.3.2023) by The Export Control (Military and Dual-Use Lists) (Amendment) Regulations 2023 (S.I. 2023/302), regs. 1, 5(2)(i)(v)
NB:
SEE ALSO 9B105.
Wind tunnels designed for speeds of Mach 1,2 or more;
Note:
9B005.a. does not [F4apply to] wind tunnels specially designed for educational purposes and having a ‘test section size’ (measured laterally) of less than 250 mm.
Technical Note:
[F5For the purposes of the Note in 9B005.a., ‘test] section size’ 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.
=
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
Wind tunnels or devices, other than two-dimensional sections, capable of simulating Reynolds number flows exceeding 25 × 106.
Textual Amendments
F4Words in Annex 1 Entry 9B005.a substituted (20.4.2022) by The Trade in Dual-Use Items (Council Regulation (EC) No 428/2009) (Amendment) Regulations 2022 (S.I. 2022/410), regs. 1, 2(2)(e)(i)
F5Words in Annex 1 Entry 9B005.a substituted (13.7.2023) by The Export Control (Amendment) Regulations 2023 (S.I. 2023/695), regs. 1(1), 3(2)(l)(viii)
NB:
SEE ALSO 9B106.
Designed to operate at stress levels of 60 % of Ultimate Tensile Strength (UTS) or more measured at a temperature of 873 K (600 °C); and
Designed to operate at 873 K (600 °C) or more.
Note:
9B009 does not control tooling for the production of powder.
Textual Amendments
F6Word in Annex 1 Entry 9B010 substituted (1.4.2024) by The Export Control (Amendment) Regulations 2024 (S.I. 2024/346), regs. 1(1), 3(21)
NB:
SEE ALSO 9B005.
Note:
9B105 does not control wind-tunnels for speeds of Mach 3 or less with dimension of the ‘test cross section size’ equal to or less than 250 mm.
Technical Notes:
1.
In 9B105 ‘aerodynamic test facilities’ includes wind tunnels and shock tunnels for the study of airflow over objects.
2.
In Note to 9B105, ‘test cross section size’ means the diameter of the circle, or the side of the square, or the longest side of the rectangle, or the major axis of the ellipse at the largest ‘test cross section’ location. ‘Test cross section’ is the section perpendicular to the flow direction.
3.
In 9B105 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Environmental chambers having all of the following:
Capable of simulating any of the following flight conditions:
Altitude equal to or greater than 15 km; or
Temperature range from below 223 K (– 50°C) to above 398 K (125°C); and
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 while imparting forces equal to or greater than 5 kN;
Technical Notes:
1.
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.
In 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 2B116.
3.
In 9B106.a.2., ‘bare table’ means a flat table, or surface, with no fixture or fittings.
Environmental chambers capable of simulating the following flight conditions:
Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 μPa) or with a total rated acoustic power output of 4 kW or greater; and
Altitude equal to or greater than 15 km; or
Temperature range from below 223 K (– 50°C) to above 398 K (125°C).
An electrical power supply equal to or greater than 5 MW; or
A gas supply total pressure equal to or greater than 3 MPa.
Technical Notes:
1.
‘Aerothermodynamic test facilities’ include plasma arc jet facilities and plasma wind tunnels for the study of thermal and mechanical effects of airflow on objects.
2.
In 9B107 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
Technical Note:
In 9B116 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
The capacity to handle more than 68 kN of thrust; or
Capable of simultaneously measuring the three axial thrust components.]
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