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HS code / TARIC details
8501522010 - For use in civil aircraft
DeclarableNo supplementary unitDuty hint: 0.000%Official TARIC lookup
Definition & language versions
For use in civil aircraft
Tip: confirm material, use and finished-product form first, then compare hierarchy and declarable candidates below.
ZH
用于民用飞机
DE
für zivile Luftfahrzeuge
EN
For use in civil aircraft
Classification hints
This code appears to be a directly declarable leaf candidate and can be used for the next customs-filing step.
Please check validity dates and duty effective dates, as the applicable rule may depend on the filing date.
Trade measures and restrictions
This block shows a filing-oriented summary first, then imported TARIC measures including scope, add. codes, order numbers, duty expressions and legal bases.
Open official TARIC
Measure
Current value
Notes / validity
Reference import duty
0.000%
Effective from Mon Jan 01
Legal base
Regulation 1549/06
-
Supplementary unit
Not required
Validity: Sun Jan 01 - -
Imported TARIC measures
No detailed TARIC measures are available for this code in the current import yet. Use the summary above and verify against the official TARIC page.
Siblings
8501522050
AC synchronous servo motor with resolver and brake for a maximum speed of not more than 6 000rpm,With: - an output of 340W or more but not more than 7,4kW, - a flange of dimensions of not more than 180mm × 180mm, and - a length from flange to extreme end of resolver of not more than 271mm
8501522070
Automotive-ready brushless permanently excited magnet synchronous alternating current motor with: -a specified speed of not more than 7000 rpm, -an output of 750 W or more but not more than 1,8 kW (at 12 V), -a flange diameter of 80 mm or more, but not more than 200 mm, -a maximum length of not more than 335 mm, measured from the beginning of the shaft to its outer end, -a housing length of not more than 265 mm, measured from the flange to the outer end, -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), -a stator with single T-tooth design and single coil winding with 9/6 or 12/10 or 12/8 topology and surface magnets, -whether or not with electronic power steering controller, -whether or not with pulley or coupling, -whether or not with rotor position sensor
8501522080
Electric permanent magnet synchronous motor with: -an output power of 850 W, -a rotor containing 8 poles generated by permanent magnets composed mainly with neodymium-iron-boron (per GB/T 13560 standard) enclosed in polyethylene cover, -an outer diameter of motor magnet shaft end with dimension of 10,001 mm or more but no more than 10,007 mm, -terminals located across the radius 26,2 mm and separated by an angle 30,0°, -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), -a back electromotive force constant (Ke) of 0,04009 V-sec/rad or more but no more than 0,04431 V-sec/rad, -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), -a cogging torque of no more than 20 mNm, -a friction torque in ambient temperature of no more than 26,5 mNm, -a maximum temperature of motor operation of no more than 200 °C
8501522089
Other
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TARIC change hints
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für zivile Luftfahrzeuge
Type: newSource lang: EN+DE
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