GAS TURBINE BLADES. PRODUCED FROM A NICKEL BASED SUPER ALLOY. THE PRODUCTS ARE CAST AND MACHINED DURING THEIR MANUFACTURING PROCESS, BEFORE THE APPLICATION OF VARIOUS CORROSION AND HEAT RESISTANT COATINGS. EACH TURBINE BLADE INCLUDES A SERIAL NUMBER ENGRAVED INTO EACH BLADE. THE TURBINE BLADES FORM PART OF A GAS TURBINE POWERED TURBOPROPELLOR ENGINE, TO BE FITTED ONTO A CIVIL AIRCRAFT.

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. GIR6 HAS BEEN USED TO CLASSIFY THE GOODS TO SUBHEADING LEVEL 841199 - PARTS. TARIC CODE 8411990090 - OTHER THAN OF GAS TURBINES, FOR USE IN CIVIL AIRCRAFT. ALSO CLASSIFIED IN ACCORDANCE WITH:- SECTION NOTE 2(B) TO SECTION XVI. HSEN NOTE (C) TO HEADING 8411 CNENS TO 84119900 INCLUDES BLADES FOR GAS TURBINES