| 1/21/2022 | 8306290009 | COPPER DECORATIVE HORN, : | 11 | 37553.3 | United States of America | MOSCOW RUSSIA | CENTRALIZED RELIGIOUS ORGANIZATION RELIGIOUS ASSOCIATION OF THE CHURCH OF JESUS CHRIST LAST DAY SAINTS IN RUSSIA |
| 1/8/2022 | 8308200000 | EXHAUST RIVET, TUBULAR, CONSISTING OF A SLEEVE AND A ROD INSERTED INTO IT, FOR FASTENING THE FUSELAGE PANELS OF A321 CIVIL AVIATION ACFT, MATERIAL - MONEL (65% - NICKEL, 35% - COPPER), DIAMETER - 3.2 MM. | 0.2 | 654.66 | United States of America | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
| 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 |
| 1/16/2022 | 8310000000 | MARKER H/N BACM10L00-1BJV, IS AN INFORMATION PLATE, MADE OF ALUMINUM FOIL (Duraluminium, CHEMICAL COMPOSITION OF THE MATERIAL: ALUMINUM 93.2%, COPPER 4.5%, MAGNESIUM 1.6%, MANGANESE 0.7%). SELF-ADHESIVE, WITHOUT BACKING, 0.18 MM THICK. SOD | 0 | 45.7 | United States of America | SITAK | PJSC AIRLINE UTair |
| 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 |
| 1/17/2022 | 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 |
| 1/28/2022 | 8308200000 | DRAWING RIVET, TUBULAR, WITH SUNSUND HEAD AND EXTENDED CORRULATED SHAFT, FASTENING THE PASSENGER AC WING LIP TRIM EMBRAER170. MATERIAL - SLEEVE - MONEL - NICKEL BASED ALLOY (70% NICKEL; 23% COPPER; 4% ALUMINUM; 2% IRON; 1% | 0.17 | 57 | United States of America | MIAMI | S 7 ENGINEERING LLC |
| 1/19/2022 | 8308200000 | EXHAUST RIVET, TUBULAR, CONSISTING OF A SLEEVE AND A ROD INSERTED INTO IT. USED FOR FASTENING PANELS AND STRUCTURAL ELEMENTS OF THE FUSELAGE OF THE EMBRAER170 PASSENGER AIRCRAFT. DIAMETER: 3 MM. MATERIAL: MONEL ALLOY (65% NICKEL; 32% COPPER; 2% IRON | 0.01 | 114.64 | United States of America | MIAMI | S 7 ENGINEERING LLC |
| 1/26/2022 | 8308200000 | EXHAUST RIVET, TUBULAR, CONSISTING OF A SLEEVE AND A ROD INSERTED INTO IT. USED FOR FASTENING PANELS AND STRUCTURAL ELEMENTS OF THE FUSELAGE OF PASSENGER AIRCRAFT EMBRAER170. DIAMETER: 4 MM. MATERIAL: MONEL ALLOY (65% NICKEL; 32% COPPER; 2% IRON; | 0.06 | 110.21 | United States of America | MIAMI | S 7 ENGINEERING LLC |
| 1/18/2022 | 8308200000 | EXHAUST RIVET, TUBULAR, CONSISTING OF A SLEEVE AND A ROD INSERTED INTO IT, FOR FASTENING THE FUSELAGE PANELS OF THE AIR A320. MATERIAL - MONEL (NICKEL - 64%, COPPER - 36%) | 0.04 | 403.51 | United States of America | FRANKFRUIT IN MAIN | S 7 ENGINEERING LLC |