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 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 |
3/27/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO SPECIFICATIONS MSRR 8632 RRES 9000 SABRE (AEROSPACE) MADE OF TITANIUM ALLOYS TI6AL4V WITH ULTRA-STRENGTH MORE THAN 930 MPa FROM HEATS 8-35-11024 ARE MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. | XXXXXXXXXX | 1 | N/A | 134493.53 | United Kingdom | REDDITCH |
3/26/2024 | 8108905008 | MECHANICALLY PROCESSED TITANIUM ALLOY SHEETS TI6AL4V - 20 PCS. DIMENSIONS 1.4/1000/2000MM, MELT 8-03-09554. STRENGTH ULTRA MPA - MORE THAN 930. MANUFACTURED BY ROLLING A BLANK OBTAINED BY ELECTRIC VACUUM REMELTING ACCORDING TO SPECIFICATIONS ACCORDING TO | XXXXXXXXXX | 1 | N/A | 15837.1 | Turkey | OBERTSHAUSEN |
3/25/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS, MANUFACTURED ACCORDING TO SPECIFICATIONS AMS 4911, AMS 4901, AMS 4919. FROM TITANIUM ALLOY TI6AL4V, CP-70 (GRADE 4), TI6AL-2SN-4ZR-2MO. HEAT 8-45-12813, 0-24-18266, 8-34-10882, 8-18-09840. TENSILE STRENGTH MPa - 930, 900, 75 | XXXXXXXXXX | 1 | N/A | 45586.18 | USA | ONTARIO |
3/25/2024 | 8108905008 | TI6AL4V ALLOY PLATES ACCORDING TO THE LATEST REVISIONS OF ASTM B 265, ISO 5832-3 SPECIFICATIONS IN EFFECT AT VSMPO, STRENGTH MAXIMUM MPa - NOT MORE THAN 900. MELTING 36-12038-2. MANUFACTURED BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. | XXXXXXXXXX | 1 | N/A | 3112.27 | India | OBERTSHAUSEN |
3/22/2024 | 8108905008 | MECHANICALLY MACHINED PLATES ACCORDING TO ABS 5125 SPECIFICATIONS AIMS 03-18-001 2TA 56 MADE OF TITANIUM ALLOY TI6AL4V FROM HEATS 8-04-11482 8-17-10529 8-17-10603 8-22-07999 8-27-13461 8-27-13476 8-31-08798 8-41-12810 TENSILE STRENGTH MORE THAN 930 MPa. M | XXXXXXXXXX | 1 | N/A | 605932.76 | United Kingdom | REDDITCH |
3/20/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO AMS 4911 SPECIFICATIONS FROM TITANIUM ALLOYS TI6AL4V. FROM HEATS 8-34-10882, THE ULTIMATE STRENGTH IS MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELTING. PURPOSE - MANUFACTURING | XXXXXXXXXX | 1 | N/A | 669.78 | France | OBERTSHAUSEN |
3/20/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS, MADE TO SPECIFICATIONS AMS 4919, AMS-T-9046, SABRE (AEROSPACE), SQR-001, ASQR-01, FB120, AMS 2809 FROM TITANIUM ALLOY TI6AL-2SN-4ZR-2MO. HEAT 8-11-12068, 8-33-12562. STRENGTH MAXIMUM MPa - NOT LESS THAN 900. MADE | XXXXXXXXXX | 1 | N/A | 134175.68 | USA | ONTARIO |