| 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 |
| 3/28/2024 | 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 | MACHINED SHEETS ACCORDING TO AMS 4911 SPECIFICATION FROM TITANIUM ALLOYS TI6AL4V WITH ULTRA-STRENGTH GREATER THAN 930 MPa FROM HEATS 8-23-08302 8-27-13426 8-18-09840 8-27-13357 8-18-09840 8-35-09384 8-35-09384 ARE MADE BY ROLLING BLANKS OBTAINED | XXXXXXXXXX | 1 | N/A | 295970.78 | USA | ONTARIO |
| 3/19/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES, MADE TO SPECIFICATION AIMS 03-18-007, ABS 5125C FROM TITANIUM ALLOY TI6AL4V. MELT 8-23-08325. TENSILE STRENGTH MPa - NOT LESS THAN 930. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. | XXXXXXXXXX | 1 | N/A | 55600.8 | France | OBERTSHAUSEN |
| 3/15/2024 | 8108905008 | MECHANICALLY MACHINED PLATES MANUFACTURED TO SPECIFICATION AMS 4911, AMS 2242, ITEM 6.4.1 FROM TITANIUM ALLOY 6AL-4V. HEAT 8-11-11846, 8-11-11648, 8-23-08276, 8-23-08280, 8-21-08636, 8-23-08275, 8-21-08635, 8-23-08281, 8-21-8634, 8-17-10572, 8-18-098 | XXXXXXXXXX | 2 | N/A | 687946.78 | France | OBERTSHAUSEN |
| 3/14/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES, MADE ACCORDING TO SPECIFICATION ABS 5125C, AIMS 03-18-007, IPS 03-18-007-02 FROM TITANIUM ALLOY TI6AL4V. HEAT 8-23-08332. TENSILE STRENGTH NOT LESS THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED | XXXXXXXXXX | 1 | N/A | 73558.54 | France | OBERTSHAUSEN |
| 3/14/2024 | 8108905008 | FUR: MACHINED PLATES TO AMS 4911, AMS 2242 TITANIUM ALLOY 6AL-4V, DIMENSIONS 10/1000/2200 MM - 184 PCS: HEAT: 8-21-08583, 8-12-12274, 8-11-12184, 8-11-12173, 8-11-12181, 8-11-12176, 8-12-12274, 8-23-08281, 8-12-12238: STRENGTH LIMIT | XXXXXXXXXX | 1 | N/A | 809751.57 | France | OBERTSHAUSEN |
| 3/11/2024 | 8108905008 | MECHANICALLY PROCESSED TI6AL4V /TI-6AL-4V TITANIUM ALLOY PLATES AND SHEETS FROM HEATS 8-02-06434 8-02-06443 8-04-11403 8-04-11468 8-17-10498 8-23-08245 8-33-12614-1 8-36-12134 8-45-12854 8-46-12875 8-47-02554 TENSILE STRENGTH MORE THAN 930 MPa, MADE | XXXXXXXXXX | 1 | N/A | 714405.11 | France | OBERTSHAUSEN |
| 3/5/2024 | 8108905008 | MECHANICALLY PROCESSED PLATES ACCORDING TO SPECIFICATIONS ABS 5125 AIMS 03-18-001 FROM TITANIUM ALLOYS TI6AL-4V - 6 PCS, DIMENSIONS 38/1070/2370 MM, FROM HEATS 8-23-08350, TENSILE STRENGTH MORE THAN 930 MPa, MADE BY ROLLING BLANKS OBTAINED | XXXXXXXXXX | 1 | N/A | 84482.58 | United Arab Emirates | OBERTSHAUSEN |
| 3/1/2024 | 8108905008 | TITANIUM PLATES FOR SIDE PANELS MADE OF TI6AL-4V ALLOY ACCORDING TO AIMS03-18-006, IPS 03-18-006-05, DRAWING D545 20906 200, DIMENSIONS 12 X 733 X 2516MM-8PCS, HEAT 8-23-08262. STRENGTH MAXIMUM MPA - MORE THAN 930. MADE BY ZAG ROLLING METHOD | XXXXXXXXXX | 1 | N/A | 42452.85 | France | OBERTSHAUSEN |