CN code 9032 89 00 Other

One TARIC code carries a different end-use rate.

TARIC codes (10 digits): 5

Origin, preferential duty and next steps ›

Examples from the EU database of Binding Tariff Information (BTI). A ruling binds only its holder and many have expired — read them as guidance, not as a decision for your product.

• CURRENT MONITORING PULSED DC CONTROLLER, BRINGS TOGETHER POWERFUL LONG-RANGE IONISATION; CLOSED-LOOP FEEDBACK; SELF-MONITORING AND REMOTE REPORTING. A COMPLETE PACKAGE, SELF-MONITORING AND ADJUSTMENT OF PERFORMANCE ALLOWS OPTIMUM CONTROL OF STATIC FOR MUCH LONGER PERIODS THAN PREVIOUSLY POSSIBLE. LOCAL DISPLAY AND OUTPUT SIGNALS ALERT OPERATORS TO THE NEED TO CLEAN THE EQUIPMENT.

  9032 89 00 · GB 2020 · GBBTI504664162

• A GENERATOR CONTROL UNIT (GCU), USED TO MONITOR AND CONTROL THE INTEGRATED DRIVE GENERATORS WHEN THEY ARE POWERING AIRCRAFT LOAD BUSES. IT HAS TWO MAIN AIRCRAFT TASKS: CONTROL AND PROTECTION; TO MONITOR AND CONTROL THE QUALITY OF ELECTRIC POWER SUPPLIED TO THE AIRCRAFT AND BUILT-IN TEST EQUIPMENT (BITE); TO COLLECT AND ANALYSE FAULT DATA AND SAVE THIS FOR LATER RETRIEVAL BY MAINTENANCE PERSONNEL.

  9032 89 00 · GB 2018 · GBBTI504000621

• PROBE HEAT COMPUTER (PHC), USED IN CONJUNCTION WITH AN AIRCRAFT ANTI-ICING SYSTEM OF PROBES AND SENSORS. THE PHC IS A RECTANGULAR UNIT WHICH HAS A BOX ASSEMBLY WITH PRINTED CIRCUIT BOARDS. THE CPU PERMANENTLY MONITORS THE PROBE ANTI-ICING OPERATION. THE PHC PROVIDES AN ANTI-ICING FUNCTION WITH DATA PROCESSING. THE FUNCTIONS INCLUDE: POWER SUPPLY, ANTI ICING OF THE TOTAL PRESSURE PROBE, OUTER AIR…

  9032 89 00 · GB 2018 · GBBTI503975538

• A HYDROMECHANICAL UNIT (HMU), A COMPONENT OF AN AIRCRAFT ENGINE SYSTEM. THE HMU RESPONDS TO ELECTRICAL SIGNALS FROM AN EEC TO METER ENGINE FUEL FLOW AND MODULATE MOTIVE FLOW TO SIX EXTERNAL HYDRAULIC SYSTEMS. A COMPONENT IN THE HMU CAUSES SERVO POSITIONING OF THE UNIT MV. THE MV POSITION ESTABLISHES THE PROPER METERED FUEL DELIVERY ORIFICE FOR THE COMMANDED FUEL FLOW. A MECHANICAL OVERSPEED…

  9032 89 00 · GB 2017 · GB125138004

• A VEHICLE DYNAMIC CONTROL . IT IS A DRIVER / VEHICLE AID TO CONTROL AND ASSIST THE DRIVER TO SAFELY CONTROL THE VEHICLE IN A STABLE AND OPTIMISED CONDITION. IT MONITORS DRIVER INPUT AND CONDITIONS EFFECTING THE VEHICLE BY MEANS OF ELECTRICAL CIRCUITS AND SENSORS, MAKING ADJUSTMENTS AND APPLYING THE BRAKES DURING MANOEUVRES THAT ENDANGER THE SAFETY OF THE DRIVER AND VEHICLE. IT MANAGES STABILITY…

  9032 89 00 · GB 2017 · GB503427577

• IGBT GATE DRIVER ASSEMBLY PN 51020195 IS PART OF STARTER GENERATOR CONTROL UNIT THAT CONTROLS THE OPERATION OF THE STARTER GENERATOR SYSTEM. FOR USE IN AIRCRAFT.

  9032 89 00 · GB 2016 · GB503276766

• GENERATOR CONTROL UNIT (GCU) FOR AIRBUS A340 CIVIL AIRCRAFT. THE UNIT CONSISTS OF A COMPACT CAST ALUMINIUM HOUSING CONTAINING A SERIES OF PRINTED CIRCUIT BOARDS. THE UNIT CONTROLS THE VOLTAGE COMING FROM THE GENERATOR KEEPING IT AT A CONSTANT AND PROVIDING OVER VOLTAGE PROTECTION. IT IS ALL PERFORMED ELECTRONICALLY WITH THE UNIT SENSING VARIOUS PARAMETERS AND COMPARING THEM WITH A STANDARD. IT…

  9032 89 00 · GB 2016 · GB502985932

• SWITCH ALTITUDE FOR AIRBUS A320 CIVIL AIRCRAFT. FUNCTIONAL DESCRIPTION : THE ALTITUDE SWITCH 16WR, WHICH IS INSTALLED IN THE AVIONICS COMPARTMENT, STARTS THE AUTOMATIC OPERATION OF THE PASSENGER EMERGENCY-OXYGEN SYSTEM. IF THE ALTITUDE SWITCH DOES NOT WORK YOU CAN PUSH THE 'MAN ON' PUSHBUTTON SWITCH 14WR. THE ALTITUDE SWITCH CLOSES WHEN THE CABIN PRESSURE DECREASES TO A PRESSURE EQUIVALENT TO…

  9032 89 00 · GB 2016 · GB502983350