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OverviewTARIC NomenclatureClassification GuideBTIEU Classification RulingsCJEU Case Law - Tariff ClassificationMarket IntelligenceOrigin of GoodsExport ControlCBAM CalculatorEUDR CheckerClassifyAI SHCustoms ValueIncoterms® 2020
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Binding Tariff Information (BTI)

MT0013-169031803805

Fibre optic gyroscope is opto-electronic sensor for meusuring angular rate based on the sagnac effect. Each fibre optic gyroscope consists of the following main components: fibre optic winding on a bobbin, light source in the form of a super luminescent diode, optic couplers, optical polarizer, piezoceramic modulator photo-diode and processing electronics. The gyroscope is normally packed individually and are for use in civil aircrafts.

MT0014-169031803805

Fibre optic gyroscope is opto-electronic sensor for measuring angular rate based on the sagnac effect. Each fibre optic gyroscope consists of the following main components: fibre optic winding on a bobbin, light source in the form of a super luminescent diode, optic couplers, optical polarizer, piezoceramic modulator photo-diode and processing electronics. The gyroscope is normally packed individually and are not for use in civil aircrafts.

GB5028600789031803805

SENSOR FOR BOEING 737 CIVIL AIRCRAFT. THE ANGLE OF AIRFLOW SENSOR CAN ALSO BE IDENTIFIED AS THE STALL WARNING SENSOR OR AS A SENSOR FOR THE STALL WARNING. TNE ANGLE OF AIRFLOW SENSOR FOR EACH SYSTEM PROVIDES A SIGNAL WHICH REPRESENTS AIRPLANE ANGLE ATTACK. THE SENSORS ARE LOCATED ON THE OUTSIDE OF THE FUSELAGE BELOW EACH PILOT'S SIDE WINDOW. THE SENSOR CONSISTS OF AN AERODYNAMIC VANE WHICH PIVOTS TO POSITION THREE INTERNAL SYNCHRO TRANSMITTERS. IN FLIGHT THE VANE TAKES A POSITION PARALLEL TO THE AIRFLOW PASSING OVER IT. THE SENSOR PROVIDES SEPERATE OUTPUTS TO THE SMALL MANAGEMENT COMPUTER AND TO THE AUTOPILOT. MADE IN THE USA

GB1176325799031803805

UNIVERSAL LOGIC CARD FOR USE IN CIVIL AIRCRAFT.THE PRODUCT IS A PRINTED CIRCUIT INSTALLED IN THE MODULARISED AVIONICS AND ELECTRONICS WARNING ASSEMBLY. IT IS A MULTIFUNCTION UNIT THAT CAN BE USED AS A MASTER MONITOR, CONFIGURATION ,STALL WARNING OR CREW ALERTING MODULE.

GB1176338709031803805

MONITORING SYSTEM FOR USE IN CIVIL AIRCRAFT. THIS PRINTED WIRING ASSEMBLY COMPRISES TWO IDENTICAL SYSTEMS( ONE AS A FAILSAFE) TO MONITOR AND TEST WARNING AND INDICATION SIGNALS SUCH AS FIRE, NACELLE OVERHEAT,TURBINE OVERHEAT,STRUT OVERHEAT,CARGO SMOKE AND DUCT LEAKE OVERHEAT.

See also

TARIC Nomenclature

25 000+ codes

Classification Guide

1 095 HS4

BTI

1 000 000+ BTI