1/4/2022 | 7608208907 | PIPES NOT WELDED, FROM ALUMINUM ALLOYS, FOR REPAIR AND MAINTENANCE OF CARS. NOT SUITABLE FOR INDUSTRIAL ASSEMBLY.: | 1.1 | 19.31 | Brazil | CHEKHOV MO | VOLKSWAGEN GROUP RUS LLC |
1/27/2022 | 7604299000 | GUIDING PROFILE OF THE FUSELAGE STRENGTH PACKAGE ??.76 ?? EMBRAER170. MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING. | 0.03 | 213.37 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/29/2022 | 7616999008 | GUIDE PROFILE OF THE FUSELAGE STRENGTH PACKAGE ShP.19 VS, MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING, FOR MAINTENANCE OF EMBRAER 170 CIVIL AVIATION AIRCRAFT. | 0.07 | 305.93 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |
1/29/2022 | 7616999008 | GUIDE PROFILE OF THE FUSELAGE STRENGTH PACKAGE ShP.19 VS, MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING, FOR MAINTENANCE OF EMBRAER 170 CIVIL AVIATION AIRCRAFT. | 0.06 | 291.09 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |
1/29/2022 | 7616999008 | GUIDE PROFILE OF THE FUSELAGE STRENGTH SET ShP.20 VS, MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING, FOR MAINTENANCE OF EMBRAER 170 CIVIL AVIATION AIRCRAFT. | 0.05 | 220.22 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |