HS Code	Description	Primary rate
8501522010	For use in civil aircraft	0.00 %
8501522050	Ac synchronous servo motor with resolver and brake for a maximum speed of not more than 6 000rpm,with:<br>- an output of 340w or more but not more than 7,4kw,<br>- a flange of dimensions of not more than 180mm × 180mm, and<br>- a length from flange to extreme end of resolver of not more than 271mm	0.00 %
8501522070	Automotive-ready brushless permanently excited magnet synchronous alternating current motor with:<br>-a specified speed of not more than 7000 rpm,<br>-an output of 750 w or more but not more than 1,8 kw (at 12 v),<br>-a flange diameter of 80 mm or more, but not more than 200 mm,<br>-a maximum length of not more than 335 mm, measured from the beginning of the shaft to its outer end,<br>-a housing length of not more than 265 mm, measured from the flange to the outer end,<br>-a steel sheet or die-cast aluminium basic housing consisting of not more than two parts, including electrical components and a flange with two or more but not more than 11 holes, whether or not with a sealing connection (groove with o-ring and protective grease or liquid seal interface),<br>-a stator with single t-tooth design and single coil winding with 9/6 or 12/10 or 12/8 topology and surface magnets,<br>-whether or not with electronic power steering controller,<br>-whether or not with pulley or coupling,<br>-whether or not with rotor position sensor<br>	0.00 %
8501522080	Electric permanent magnet synchronous motor with:<br>-an output power of 850 w,<br>-a rotor containing 8 poles generated by permanent magnets composed mainly with neodymium-iron-boron (per gb/t 13560 standard) enclosed in polyethylene cover,<br>-an outer diameter of motor magnet shaft end with dimension of 10,001 mm or more but no more than 10,007 mm,<br>-terminals located across the radius 26,2 mm and separated by an angle 30,0°,<br>-a housing made of adc12 or ac46000 aluminium alloy die casting with composition of aluminium-silicon-copper (per jis h5302 or en1706 standard) and anodized coating (per astm b580 type e standard),<br>-a back electromotive force constant (ke) of 0,04009 v-sec/rad or more but no more than 0,04431 v-sec/rad,<br>-a back electromotive force harmonic order - 5th of no more than 0,36 % (of fundamental) and 7th of no more than 0,24 % (of fundamental),<br>-a cogging torque of no more than 20 mnm,<br>-a friction torque in ambient temperature of no more than 26,5 mnm,<br>-a maximum temperature of motor operation of no more than 200 °c<br>	0.00 %
8501522089	Other	0.00 %
8501523010	For use in civil aircraft	0.00 %
8501523090	Other	0.00 %
8501529010	For use in civil aircraft	0.00 %
8501529090	Other	0.00 %