| 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 |
| 3/11/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO AMS 4911 SPECIFICATIONS FROM TITANIUM ALLOYS TI6AL4V - 10 PCS. DIMENSIONS 2.54/914.4/2438.4 MM. MADE FROM 8-1-12783 HEATS. STRENGTH MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED | XXXXXXXXXX | 1 | N/A | 9195.44 | USA | ONTARIO |
| 3/11/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO SPECIFICATIONS AMS 4911 AMS-T-9046 SQR-001 SABRE FB-120 MADE OF TITANIUM ALLOYS TI6AL4V FROM MELT 8-17-10482-1 8-12-12273 UTMOST STRENGTH MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM | XXXXXXXXXX | 1 | N/A | 30820.93 | USA | ONTARIO |
| 3/4/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO SPECIFICATIONS AMS 4901 SQR-001 SABRE FB120 MADE OF TITANIUM ALLOYS SR-70 (GRADE 4) FROM MELT 8-12-12086, STRENGTH ULTIMATE NOT MORE THAN 750 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELTING. PUR | XXXXXXXXXX | 1 | N/A | 30540.19 | USA | ONTARIO |
| 2/29/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO SPECIFICATIONS MSRR8632 ISSUE 11(TCA), AMS 4919, FROM TITANIUM ALLOYS TI6AL4V, TI6AL2SN4ZR2MO - 47 PCS. DIMENSIONS 1.27-1.6/914.4/2438.4 MM. MADE FROM HEATS 8-41-12752, 8-10-12357, 8-33-12458, 8-36-12023, 8-42-10694, 8- | XXXXXXXXXX | 0 | N/A | 49514.63 | USA | ONTARIO |
| 2/20/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO SPECIFICATIONS AMS 4911 AMS-T-9046 SQR-001 SABRE FB-120 MADE OF TITANIUM ALLOYS TI6AL4V FROM MELT 8-35-10808-1 WITH ULTRA-STRENGTH OF MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. | XXXXXXXXXX | 0 | N/A | 47998.6 | USA | ONTARIO |
| 2/12/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO AMS 4919 SPECIFICATION FROM TITANIUM ALLOYS TI6AL-2SN-4ZR-2MO/TI6AL4V. STRENGTH MORE THAN 930 . TI6AL4V - NOT LESS THAN 900 MPa. FROM HEATS: 8-36-12023, 8-23-08278, 8-23-08058, 8-45-12813. MADE BY ROLLING METHOD | XXXXXXXXXX | 0 | N/A | 152334.95 | USA | ONTARIO |
| 1/17/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO AMS 4919 SPECIFICATIONS FROM TITANIUM ALLOYS 6AL-2SN-4ZR-2MO FROM MELT 8-04-11273, STRENGTH MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. PURPOSE - CIVIL | XXXXXXXXXX | 1 | N/A | 1271.38 | USA | ONTARIO |
| 1/9/2024 | 8108905008 | MECHANICALLY PROCESSED SHEETS ACCORDING TO AMS 4911 SPECIFICATIONS FROM TITANIUM ALLOYS TI-6AL-4V FROM MELT 8-03-09541 WITH ULTRA-STRENGTH OF MORE THAN 930 MPa. MADE BY ROLLING BLANKS OBTAINED BY ELECTRIC VACUUM REMELT. PURPOSE - CIVIL AIRCRAFT CONSTRUCTI | XXXXXXXXXX | 1 | N/A | 21469.07 | USA | ONTARIO |
| 12/19/2023 | 8108905008 | MACHINED SHEETS TO AMS 4919 TI6A TITANIUM ALLOYS | XXXXXXXXXX | 0 | 0 | 7138.58 | USA | ONTARIO |