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.

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.