Defence Production Act — D-1 5
5 (1) Subject to subsection (2) and section 6, goods set out in Group 6 of the Guide, other than those described in any of the following items, are controlled goods: (a) item 6-1.C; (b) item 6-2.C; (c) items 6-3.A.1, 6-3.A.6, 6-3.A.7, 6-3.A.9, 6-3.B.3 or 6-3.C; (d) items 6-4.A, 6-4.B.3 or 6-4.C.1, 6-4.C.2.c to 6-4.C.2.f, 6-4.C.3, 6-4.C.4.a.2, 6-4.C.4.b.1, 6-4.C.4.b.3 or 6-4.C.4.b.5, 6-4.C.5.c, 6-4.C.6.b or 6-4.C.6.d, 6-4.C.6.e.1 or 6-4.D; (e) item 6-5; (f) items 6-6.B, 6-6.C.1 to 6-6.C.4, 6-6.C.6 to 6-6.C.9, 6-6.D or 6-6.E.2 or 6-6.E.3; (g) items 6-7 to 6-11; (h) items 6-12.A.3, 6-12.A.5.a, 6-12.A.6, 6-12.B or 6-12.C or 6-12.D.2; (i) items 6-13 to 6-15; (j) items 6-16.B or 6-16.C; (k) items 6-18.A.1 or 6-18.B to 6-18.D; (l) items 6-19.A.3 or 6-19.C; (m) item 6-20.C. (2) The following modifications apply to the controlled goods set out in Group 6 of the Guide: (a) the heading of item 6-2 of the Guide is to be read as follows: 6-2 COMPLETE SUBSYSTEMS SPECIALLY DESIGNED FOR COMPLETE DELIVERY SYSTEMS (b) the portion of item 6-2.A.1 of the Guide before item 6-2.A.1.a is to be read as follows: 1 Complete subsystems specially designed for the systems specified in 6-1.A., as follows: (c) items 6-2.A.1.b.1 and 6-2.A.1.b.2 of the Guide are to be read as follows: 1 Heat shields fabricated of ceramic or ablative materials; 2 Heat sinks fabricated of light-weight, high heat capacity materials; (d) the portion of item 6-2.A.1.c of the Guide before the “Note” is to be read as follows: c Solid propellant rocket motors, hybrid rocket motors or liquid propellant rocket engines, specially designed for the systems specified in 6-1.A., having a total impulse capacity equal to or greater than 1.1 x 10 6 Ns; (e) the portion of item 6-2.A.1.d of the Guide before the “Technical Notes” is to be read as follows: d ‘Guidance sets’, specially designed for the systems specified in 6-1.A., capable of achieving system accuracy of 3.33% or less of the “range” (e.g., a ‘CEP’ of 10 km or less at a “range” of 300 km), except as provided in the Note at the end of 6-2.A.1. for those designed for missiles with a “range” under 300 km or manned aircraft; (f) the portion of item 6-2.A.1.e of the Guide before the “Technical Note” is to be read as follows: e Thrust vector control sub-systems, specially designed for the systems specified in 6-1.A., except as provided in the Note at the end of 6-2.A.1. for those designed for rocket systems that do not exceed the “range”/“payload” capability of systems specified in 6-1.A.; (g) the portion of item 6-2.A.1.f of the Guide before the “Note” is to be read as follows: f Weapon or warhead safing, arming, fuzing, and firing mechanisms, specially designed for the systems specified in 6-1.A., except as provided in the Note at the end of 6-2.A.1. for those designed for systems other than those specified in 6-1.A. Note A: For the purposes of the schedule to the Defence Production Act , the “Note” at the end of item 6-2.A.1.f. of the Guide does not apply. (h) the portion of item 6-3.A.2 of the Guide before the “Technical Note” is to be read as follows: 2 Ramjet/scramjet/pulse jet/combined cycle engines, including devices to regulate combustion, specially designed for the systems specified in 6-1.A. or 6-19.A.2, and specially designed components therefor. (i) the portion of item 6-3.A.3 of the Guide before the “Technical Note” is to be read as follows: 3 Rocket motor cases and nozzles therefor, specially designed for the systems specified in 6-1.A. or 6-19.A.1. Note A: For the purposes of the schedule to the Defence Production Act , the “Technical Note” and “Note” at the end of item 6-3.A.3. of the Guide do not apply. (j) item 6-3.A.4 of the Guide is to be read as follows: 4 Staging mechanisms, separation mechanisms, and interstages therefor, specially designed for the systems specified in 6-1.A. (k) the portion of item 6-3.A.5 of the Guide before the “Notes” is to be read as follows: 5 Liquid and slurry propellant (including oxidisers)