1/6/2022 | 7606111000 | STRIPS (RECTANGULAR TAPE) FROM UNALLOYED ALUMINUM 1100, COATED, 0.25MM THICKNESS. USED IN THE PRODUCTION OF ALUMINUM-COMPOSITE PANELS AS A FRONT AND BACK SIDE. | 4771 | 20551.5 | China | NINGBO CHINA | ALPHA ALUMINUM LLC |
1/3/2022 | 7606111000 | STRIPS (RECTANGULAR TAPE) FROM UNALLOYED ALUMINUM 1100, COATED, THICKNESS 0.25 - 0.5 MM. USED IN THE PRODUCTION OF ALUMINUM-COMPOSITE PANELS AS A FRONT AND BACK SIDE. | 28081 | 104508.5 | China | NINGBO CHINA | ALPHA ALUMINUM LLC |
1/3/2022 | 7606111000 | STRIPS (RECTANGULAR TAPE) FROM UNALLOYED ALUMINUM 1100, COATED, 0.25 MM THICKNESS. USED IN THE PRODUCTION OF ALUMINUM-COMPOSITE PANELS AS A FRONT AND BACK SIDE. | 16517 | 57860.9 | China | NINGBO CHINA | ALPHA ALUMINUM LLC |
1/27/2022 | 7606119900 | ALUMINUM HONEYCOMB PANEL, FOR INTERNAL AND EXTERNAL WALL CLADDING, GENERAL APPLICATIONS: | 7386.3 | 83664.9 | Spain | MIRANDOLA ITALY | BAUTREYD LLC |
1/24/2022 | 7606111000 | 1-ALUMINUM PAINTED RECTANGULAR COMPOSITE PANELS. THEY ARE A MULTILAYER MATERIAL CONSISTING OF TWO OUTER ALUMINUM SHEETS (ALUMINUM~99.2%) AND A MINERAL-FILLED INTERNAL LAYER. USED FOR FURTHER PRODUCTION | 39891 | 88837.5 | China | SHANGHA CHINA | BILDEX LLC |
1/21/2022 | 7606111000 | ALUMINUM PAINTED RECTANGULAR COMPOSITE PANELS. THEY ARE A MULTILAYER MATERIAL CONSISTING OF TWO OUTER ALUMINUM SHEETS (ALUMINUM~99.2%) AND A MINERAL-FILLED INTERNAL LAYER. USED FOR FURTHER PRODUCTION | 136074 | 304014.3 | China | SHANGHA CHINA | BILDEX LLC |
1/3/2022 | 7606129208 | FLAT SHEET (ROLL) FROM ALUMINUM ALLOY FOR REPAIR OF CENTRAL CONTROL PANELS IN THE CREW CABIN OF EMBRAER 170 CIVIL AVIATION ACFT: | 493 | 7696.38 | Unknown | BIGGLESWADE ENGLAND | S 7 ENGINEERING LLC |
1/10/2022 | 7606129309 | SHEET (ROLL) FLAT FROM ALUMINUM ALLOY (90% - ALUMINUM, 10% - ADDITIVES. DOES NOT CONTAIN PRECIOUS METALS). INTENDED FOR REPAIR OF FUSELAGE PANELS OF B737 PASSENGER AIRCRAFT. THICKNESS - 4.06 MM. SHEETS SIZE - 366X122 CM. FOR REPAIR AND TECHNICAL | 100 | 4211.34 | Unknown | MOSCOW RUSSIA | AZUR AIR LLC |
1/25/2022 | 7606129208 | ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS) FOR STRUCTURAL REPAIR OF PANELS OF A PASSENGER AIR CONDITIONER PANELS OF BOEING CIVIL AVIATION: | 20.45 | 1484.6 | Unknown | BIELANA WROCLAWSKI | S 7 ENGINEERING LLC |
1/27/2022 | 7606129208 | FLAT SHEET (ROLL) FROM ALUMINUM ALLOY FOR REPAIR OF FUSELAGE PANELS OF BOEING 737 CIVIL AVIATION: | 26 | 1899.12 | Unknown | BIGGLESWADE ENGLAND | S 7 ENGINEERING LLC |