1988 Ed.]
Import and Export (Strategic Commodities) Regulations
[CAP. 60
G 51
[Subsidiary]
(c) "Helicopter power transfer systems" and technology therefor, except:
(i) Those "helicopter power transfer systems" destined for use in "civil helicopters" only, as follows:
(1) Those which have been in civil use in bona fide "civil helicopters" for more than eight years;
(2) Those which it is considered do not contain, and were not fabricated utilizing, any of the technologies shown in Note 9;
(3) Those for replacement in or servicing of specific, previously exported helicopters;
(ii) Data not in the public domain resulting from "helicopter power transfer system" performance and installation design studies; fabrication technology, or overhaul and refurbishing technology for specific "helicopter power transfer systems" in civil use in bona fide "civil helicopters" for more than eight years, unless they remain listed in Note 9;
Note:
"Helicopter power transfer system" performance and installation design data do not include technology for: computer-aided design (CAD); computer-aided design/manufacturing (CAD/CAM); or parametric performance analysis, engine analysis and selection, or component design utilizing unpublished technical data.
(d) Gas turbine engines and auxiliary power units (APUs) for use in aircraft or helicopters and technology therefor, except:
(1) Those destined for use in "civil aircraft" or "civil helicopters" only, as follows: (1) Jet, turboprop and turboshaft aircraft engines in civil use in bona fide "civil aircraft" or "civil helicopters" for more than eight years, or which it is considered do not contain, and were not fabricated utilizing, any of the technologies shown in Note 8;
(2) Gas turbine powered aircraft APUs in civil use in bona fide "civil aircraft" or "civil helicopters" for more than eight years, or where it is considered do not contain, and were not fabricated utilizing, any of the technologies shown in Note 8;
(ii) Data not in the public domain resulting from aircraft performance and installation design studies; fabrication technology, or overhaul and refurbishing technology for specific gas turbine aero-engines or gas turbine powered aircraft APUs in civil use in bona fide "civil aircraft" or "civil helicopters" for more than twelve years, unless they remain listed in Note 8;
Note:
Aircraft performance and installation design data do not include technology for computer-aided design (CAD); computer-aided design/manufacturing (CAD/CAM); or parametric engine performance analysis, engine cycle analysis and selection, or component aerodynamic design utilizing unpublished technical data.
(e) Specially designed components for gas turbine engines, APUs and "helicopter power transfer systems", embargoed by (c) and (d) above, as follows:
(1) Embodying technologies listed under Notes 8 or 9;
(2) Hot-section components;
(3) Engine control system components;
(4) Gas turbine engine or APU rotor system components (including bearings);
Note:
(Aero-engines, APUs or "helicopter power transfer systems" which have any special feature designed for a military application are embargoed by the Munitions List. See also Items IL1485 and 1501. For technology relating to industrial gas turbine engines, see Item IL1372; for marine gas turbine engines and related technology, Item IL1431.)
see
1988 Ed.]
Import and Export (Strategic Commodities) Regulations
[CAP. 60
G 51
[Subsidiary]
(c) "Helicopter power transfer systems" and technology therefør, except:
(i) Those "helicopter power transfer systems" destined for use in "civil
helicopters" only, as follows:
(1) Those which have been in civil use in bona fide "civil helicopters" for
more than eight years;
(2) Those which it is considered do not contain, and were not fabricated
utilizing, any of the technologies shown in Note 9;
(3) Those for replacement in or servicing of specific, previously exported
helicopters;
(ii) Data not in the public domain resulting from "helicopter power transfer system" performance and installation design studies; fabrication technology, or overhaul and refurbishing technology for specific "helicopter power transfer systems" in civil use in bona fide "civil helicopters" for more than eight years, unless they remain/listed in Note 9;
Note:
"Helicopter power transfer system" performance and installation design data do not include technology for: computer-aided design (CAD); computer-aided design/manufacturing (CAD) CAM); or parametric performance analysis, engine analysis and selection, or component design utilizing unpublished technical data.
(d) Gas turbine engines and auxiliary power units (APUs) for use in aircraft or
helicopters and technology therefor, except:
(1) Those destined for use in "civil aircraft” or “civil helicopters" only, as follows: (1) Jet, turboprop and turboshaft aircraft engines in civil use in bona fide “civil aircraft" or "civil helicopters" for more than eight years, or which it is considered do not contain, and were not fabricated utilizing, any of the technologies shown in Note 8;
(2) Gas turbine powered aircraft APUs in civil use in bona fide "civil aircraft" or "civil helicopters" for more than eight years, or where it is considéred do not contain, and were not fabricated utilizing, any of the technologies shown in Note 8;
(ii) Data not in the public domain resulting from aircraft performance and installation design studies; fabrication technology, or overhaul and refurbishing technology for specific gas turbine aero-engines or gas turbine powered aircraft APUs/in civil use in bona fide “civil aircraft" or "civil helicopters” for more than twelve years, unless they remain listed in Note 8;
Note:
Aircraft performance and installation design data do not include technology for computer-aided design (CAD); computer-aided design/manufacturing (CAD/CAM); or parametric engine performance analysis, engine cycle analysis and selection, or component aerodynamic design utilizing unpublished technical data.
(e) Specially designed components for gas turbine engines, APUs and "helicopter
power transfer systems", embargoed by (c) and (d) above, as follows:
(1) Embodying technologies listed under Notes 8 or 9;
(2) Hot-section components;
(3) Engine control system components;
(4) Gas turbine engine or APU rotor system components (including bearings);
Note:
(Aero-engines, APUs or "helicopter power transfer systems" which have any special feature designed for a military application are embargoed by the Munitions List. See also Items IL 1485 and 1501. For technology relating to industrial gas turbine engines, see Item IL 1372; for marine gas turbine engines and related technology, Item IL 1431.)
see
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