3/29/2024 | 8108905008 | MECHANICALLY PROCESSED TI-6AL-4V TITANIUM ALLOY PLATES FROM MELTS 8-11-12135-2 8-23-08351 8-31-08794 8-46-12928 ARE PRODUCED BY FORGING AND ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. PURPOSE - CIVIL AIRCRAFT ENGINEERING. | XXXXXXXXXX | 1 | N/A | 238696.53 | France | OBERTSHAUSEN |
3/29/2024 | 8108905008 | MACHINED PLATES AND SHEETS ACCORDING TO AMS 4911 SPECIFICATIONS FROM TITANIUM ALLOYS TI6AL4V. FROM HEATS 8-09-11364 8-09-11373 8-17-10576 8-18-09867 8-21-08676 8-21-08688 WITH ULTRA-STRENGTH GREATER THAN 930 MPa. MADE BY ROLLING BLANKS, | XXXXXXXXXX | 1 | N/A | 385481.73 | Spain | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS AND PLATES ACCORDING TO SPECIFICATIONS WL 3.7164.1 DIN 65039 LN 9297 MADE OF TITANIUM ALLOY 3.7164.1 FROM MELT 8-22-07981 8-46-12875 TENSILE STRENGTH MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM | XXXXXXXXXX | 1 | N/A | 52153.64 | Turkey | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES, MADE TO SPECIFICATION ABS 5125, AIMS 03-18-006, IPS 03-18-006-05 FROM TITANIUM ALLOY TI6AL-4V. MELT 8-21-08702. TENSILE STRENGTH NOT LESS THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED | XXXXXXXXXX | 1 | N/A | 60161.93 | France | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES, MADE TO SPECIFICATION ABS 5125, FROM TITANIUM ALLOY TI6AL4V. MELT 8-36-12062. STRENGTH ULTRA-STRENGTH MPa - NOT LESS THAN 930, MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. PURPOSE - | XXXXXXXXXX | 1 | N/A | 16269.25 | United Kingdom | REDDITCH |
3/28/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES ACCORDING TO SPECIFICATION ABS 5125 FROM TITANIUM ALLOY TI6AL4V(GR5), MELT 8-22-07981,8-04-11488. STRENGTH ULTRA-STRENGTH MPA - MORE THAN 930. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. | XXXXXXXXXX | 1 | N/A | 16590.1 | France | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MECHANICALLY PROCESSED TI6AL4V TITANIUM ALLOY PLATES FROM 8-02-06494 MELTS, STRENGTH MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRO-VACUUM REMELT. PURPOSE - CIVIL AIRCRAFT ENGINEERING. | XXXXXXXXXX | 1 | N/A | 69766.46 | Germany | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MECHANICALLY MACHINED PLATES, MADE TO SPECIFICATION AMS 4911, FROM TITANIUM ALLOY TI6AL4V. HEAT 8-22-07953-1, 8-02-06456, 8-04-11449. TENSILE STRENGTH NOT LESS THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM | XXXXXXXXXX | 1 | N/A | 184335.02 | Brazil | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES ACCORDING TO SPECIFICATIONS ABS 5125 AIMS 03-18-001 MADE OF TITANIUM ALLOYS TI6AL-4V FROM MELTS 8-23-08350 8-47-02592 WITH A STRENGTH OF MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. | XXXXXXXXXX | 1 | N/A | 40723.26 | United Arab Emirates | OBERTSHAUSEN |
3/28/2024 | 8108905008 | MEX. PROCESSED PLATES FROM TITANIUM ALLOYS TI6AL4V. MELTING 0-15-02330. TENSILE STRENGTH NOT LESS THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. PURPOSE AND APPLICATION: WILL BE | XXXXXXXXXX | 1 | N/A | 56641.57 | Spain | OBERTSHAUSEN |