Of gas turbines, for use in civil aircraft.

SPEED PROBE SUB ASSEMBLY. THIS IS PART OF…

SPEED PROBE SUB ASSEMBLY. THIS IS PART OF A PROBE WHICH GOES INTO A TRENT 500 GAS TURBINE USED IN CIVIL AIRCRAFT. THE TOP LEVEL PART MEASURES SPEED IN THE ENGINE.

Classification justification: CLASSIFICATION HAS BEEN DETERMINED IN ACCORDANCE WITH THE FOLLOWING:- GENERAL INTERPRETATIVE RULES (GIR)S GIR 1 HAS BEEN USED TO CLASSIFY THIS PRODUCT BY THE TERMS OF HEADING 8411 - TURBOJETS, TURBOPROPELLERS AND OTHER GAS TURBINES GIR 6 HAS BEEN USED TO CLASSIFY THE GOODS TO SUBHEADING LEVEL 841199 - PARTS TARIC CODE 8411990010 OF GAS TURBINES, FOR USE IN CIVIL AIRCRAFT

BTI Reference:
GB501489853.
Start date of validity:
.
End date of validity:
2019-05-08.

National keywords: FOR AIRCRAFT

METAL SPEED BODY ASSEMBLY. THIS IS PART OF…

METAL SPEED BODY ASSEMBLY. THIS IS PART OF PROBE WHICH MEASURES SPEED IN A PW1000 CIVIL AIRCRAFT GAS TURBINE ENGINE

BTI Reference:
GB501489167.
Start date of validity:
.
End date of validity:
2019-05-08.

National keywords: FOR AIRCRAFT

PARTS OF A GAS TURBINE ENGINE FOR USE IN…

PARTS OF A GAS TURBINE ENGINE FOR USE IN CIVIL AIRCRAFT OF AN UNLADEN WEIGHT OF OVER 8000 KG. BEING COMPRESSOR CASINGS.

Classification justification: CLASSIFICATION IS DETERMINED ACCORDING TO GIRS 1 AND 6 AS WELL AS THE TEXT OF CN CODE 841199 00.

BTI Reference:
GB116667068.
Start date of validity:
.
End date of validity:
2013-08-01.

BRACKET DESIGNED TO BE FITTED TO A SPECIFIC…

BRACKET DESIGNED TO BE FITTED TO A SPECIFIC AIRCRAFT ENGINE. THE BRACKET IS FITTED TO THE EXTERIOR OF THE ENGINE CASING TO RETAIN WIRING LOOM. IT IS MADE FROM INCONEL ALLOY 625 AND MEASURES APPROXIMATELY 41MM X 16MM.

Classification justification: GIR 1 TERMS OF HEADING 8411 TURBO-JETS,TURBO PROPELLERS AND OTHER GAS TURBINES.GIR 6 TERMS OF ONE DASH SUBHEADING- PARTS. TERMS OF TWO DASH SUBHEADING 8411.99 OTHER . TARIC CODE 84119900.10 OF GAS TURBINES , FOR USE IN CIVIL AIRCRAFT.

BTI Reference:
GB115418591.
Start date of validity:
.
End date of validity:
2012-05-12.

National keywords: FOR AIRCRAFT

SPACER DESIGNED TO BE FITTED TO A SPECIFIC…

SPACER DESIGNED TO BE FITTED TO A SPECIFIC AIRCRAFT ENGINE. IT FITS IN THE OUTER CASING ATTACHMENT OF COMPONENTS. IT IS MADE FROM TITANIUM AND MEASURES APPROXIMATELY 49MM X 14MM.

BTI Reference:
GB115490877.
Start date of validity:
.
End date of validity:
2012-05-12.

National keywords: FOR AIRCRAFT PLATES

PLATE BLANKING OUTER, IS FITTED TO THE RB21122B…

PLATE BLANKING OUTER, IS FITTED TO THE RB21122B ENGINE WHICH GOES INTO THE BOEING 747-400 CIVIL AIRCRAFT. IT IS MANUFACTURED FROM NICKEL BASED ALLOY. DESIGNED TO BE FITTED TO A SPECIFIC AIRCRAFT ENGINE

BTI Reference:
GB115475380.
Start date of validity:
.
End date of validity:
2012-05-10.

National keywords: PLATES FOR AIRCRAFT

BRACKET LOOP CLAMP GOES INTO THE TURBINE…

BRACKET LOOP CLAMP GOES INTO THE TURBINE ENGINE FOR AIRBUS SINGLE AISLE CIVIL AIRCRAFT. FITTED TO THE EXTERIOR OF THE ENGINE CASING TO RETAIN PIPE-WORK IN POSITION. MANUFACTURED FROM STAINLESS STEEL. MEASURES APPROXIMATELY 9.0CM BY 6.3CM

BTI Reference:
GB115412806.
Start date of validity:
.
End date of validity:
2012-05-10.

National keywords: FOR AIRCRAFT OF STAINLESS STEEL

PARTS OF GAS TURBINES FOR USE IN CIVIL AIRCRAFT.…

PARTS OF GAS TURBINES FOR USE IN CIVIL AIRCRAFT. COMPRISING COMBUSTION LINERS.

Classification justification: CLASSIFICATION IS DETERMINED BY THE PROVISIONS OF GENERAL INTERPRETATIVE RULES 1 AND 6 AS WELL AS THE TEXT OF HEADINGS 8411 AND SUBHEADING 841199.

BTI Reference:
GB115482287.
Start date of validity:
.
End date of validity:
2012-05-07.

GAS TURBINE PARTS FOR USE IN CIVIL AIRCRAFT.…

GAS TURBINE PARTS FOR USE IN CIVIL AIRCRAFT. COMPRISING COMPRESSOR/TURBINE BLADES AND STATORS.

BTI Reference:
GB115482189.
Start date of validity:
.
End date of validity:
2012-05-07.

PARTS OF GAS TURBINES FOR USE IN CIVIL AIRCRAFT.…

PARTS OF GAS TURBINES FOR USE IN CIVIL AIRCRAFT. COMPRISING ENGINE MODULES.

BTI Reference:
GB115482091.
Start date of validity:
.
End date of validity:
2012-05-07.