1/24/2022 | 8310000000 | PLATE B/N BAC27DLG0144, MADE OF ALUMINUM ALLOYS (DURALUMINUM, CHEMICAL COMPOSITION OF THE MATERIAL: ALUMINUM 93.2%, COPPER 4.5%, MAGNESIUM 1.6%, MANGANESE 0.7%), MANUFACTURING METHOD - STAMPING, WITH FURTHER PROCESSING - GRINDING, WITHOUT BASE, THICKNESS 0.18 MM, SODER | 0.07 | 599.81 | United States of America | GOODYEAR | PJSC AIRLINE UTair |
1/4/2022 | 8310000000 | PLATE H/N BAC27DLG0145, FROM ALUMINUM ALLOYS (DURALUM, CHEMICAL COMPOSITION OF THE MATERIAL: ALUMINUM 93.2%, COPPER 4.5%, MAGNESIUM 1.6%, MANGANESE 0.7%), MANUFACTURING METHOD: STAMPING, WITH FURTHER PROCESSING - GRINDING, WITHOUT BACKING, SELF-ADHESIVE, THICKNESS 0, | 0.01 | 96.69 | United States of America | GOODIER | PJSC AIRLINE UTair |
1/17/2022 | 8302300009 | CLAMP B/N 82-47-113-15 FASTENING, MADE OF ALUMINUM ALLOYS (DURALUMINUM-ALUMINUM ALLOY AL (BASE) WITH COPPER CU (1.4-1.3%), MAGNESIUM MG (0.4-2.8% ) AND MANGANESE MN (0.2-1%), PROCESSING METHOD - TURNING WITH GRINDING, FOR FASTENING PANELS IN THE AIR CONDITION, | 0.01 | 9.58 | United States of America | HOUNSLOW | PJSC AIRLINE UTair |