1/30/2022 | 7604109000 | GUIDING RAIL, REPRESENTING A shaped SEMI-CLOSED PROFILE FROM UNALLOYED ALUMINUM, IS A PART OF THE SUSPENDED RAIL SYSTEM OF THE ZRA1 , ZRA2 SERIES. DESIGNED FOR MOVING SUSPENDED EQUIPMENT TO ACCELERATE TECHNOLOGY | 1023 | 14149.5 | France | TYCHY | INDUSTRIAL TECHNOLOGIES LLC |
1/23/2022 | 7604109000 | NON-ALLOYED ALUMINUM PROFILES: | 4.2 | 114.21 | France | MOSCOW RUSSIA | SCHHEIDER ELECTRIC JSC |
1/27/2022 | 7604299000 | GUIDING PROFILE OF THE POWER SET OF THE TAIL FUSELAGE OF AC HA EMBRAER170/175. MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING | 0.04 | 285.64 | France | MITRI MORI | S 7 ENGINEERING LLC |
1/29/2022 | 7604299000 | ALUMINUM ALLOY PROFILES: | 90 | 1762.11 | France | BORISOVSKY | GERFLOR JSC |
1/2/2022 | 7604299000 | PROFILE OF COMPLEX SHAPE, STAMPED FROM SHEET ALUMINUM, USED WHEN REPAIRING THE STRENGTH SET OF THE OPENING IN THE AREA OF THE THRESHOLD, THE FRONT DOOR OF A320 NEO ACFT | 0.9 | 2147.41 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/24/2022 | 7604299000 | ALUMINUM ALLOY PROFILES: | 0.1 | 534.52 | France | HAMBURG AIRPORT GERMANY | PJSC AEROFLOT RUSSIAN AIRLINES |
1/25/2022 | 7604299000 | POWER PROFILE FROM ALUMINUM ALLOY FOR PASSENGER ACFT ?319/?320/?321 CIVIL AVIATION: | 0.13 | 2095.9 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/22/2022 | 7604299000 | PROFILE, OF COMPLEX FORM, IS AN ELEMENT OF LONGITUDINAL FUSELAGE STRENGTH IN THE REGION OF SHP. 24-27 BC A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). FOR MAINTENANCE OF AIRCRAFT AIRBUS A321 CIVIL AVIATION. | 1 | 1201.52 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/22/2022 | 7604299000 | PROFILE, OF COMPLEX FORM, IS AN ELEMENT OF LONGITUDINAL FUSELAGE STRENGTH IN THE REGION OF SHP. 24-27 BC A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). FOR MAINTENANCE OF AIRCRAFT AIRBUS A321 CIVIL AVIATION. | 1 | 1075.52 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/22/2022 | 7604299000 | PROFILE, OF COMPLEX FORM, IS AN ELEMENT OF LONGITUDINAL FUSELAGE STRENGTH IN THE REGION OF SHP. 24-27 BC A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). FOR MAINTENANCE OF AIRCRAFT AIRBUS A321 CIVIL AVIATION. | 1 | 1333.52 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |