1/18/2022 | 8807300000 | STAMPINGS FROM TITANIUM ALLOY TI-10V-2FE-3AL, MANUFACTURED ACCORDING TO SPECIFICATION BMS 7-260 COMPLEX SHAPE OF CROSS-SECTION, CODE 3?-614/3W-614 (161W4202-1) - 11 PCS. STRENGTH IS NOT LESS THAN 1100 MPA. ARE ELEMENTS OF THE B777 AIRPLANE WING | 2331.2 | 157053.3 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/31/2022 | 8807200000 | STAMPINGS FROM TITANIUM ALLOY TI-10V-2FE-3AL ACCORDING TO BMS 7-260 SPECIFICATION: CODE 162W2004-3 (3Sh-1035)-7PCS. THOSE. ALLOWANCES (PART OF STAMPS) CODE 3Sh-1035-6ShT (WEIGHT 13.2KG). COMPLEX FORM OF CROSS-SECTION. USED FOR THE MANUFACTURE OF CHASSIS PARTS | 550.2 | 45024.1 | United States of America | LEETSDALE | OJSC CORPORATION VSMPO AVISMA |
1/31/2022 | 8807200000 | STAMPINGS MACHINED FROM TITANIUM ALLOY TI-6AL-4V, ACCORDING TO SPECIFICATION BMS 7-247, CODE 3SHO-1185/3WO-1185 - 1 PC. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. ARE A PART OF THE AIRCRAFT CHASSIS B737MAX CIVIL | 162 | 20429.9 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/26/2022 | 8807300000 | STAMPINGS FROM TI-6AL-4V TITANIUM ALLOY, MANUFACTURED ACCORDING TO SPECIFICATION AMS 4928, CODE 2TG-130/2TG-130 (251W1211-3) - 23 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. ARE ELEMENTS OF THE WING OF THE B777 CIVIL AIRCRAFT | 188.6 | 10338.9 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/24/2022 | 8807300000 | STAMPINGS FROM TITANIUM ALLOY TI-10V-2FE-3AL, MANUFACTURED ACCORDING TO SPECIFICATION BMS 7-260, CODE 2TNO-54/2TNO-54 (734-17397) - 8 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 1100. COMPLEX SHAPE OF CROSS-SECTION. ARE ELEMENTS OF THE B777 AIRPLANE WING | 80 | 15489.8 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/20/2022 | 8807200000 | STAMPINGS FROM TITANIUM ALLOY TI-10V-2FE-3AL, ACCORDING TO SPECIFICATION BMS 7-260, REF 3?-1388/36W-1388 - 10 PCS. TEMPLATES (PARTS OF STAMPINGS) - 8PCS / 8.0KG. STRENGTH STRENGTH MPA - NOT LESS THAN 1100. COMPLEX SHAPE OF CROSS-SECTION. ARE A PART OF THE CHASSIS | 382.6 | 26584.5 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/17/2022 | 8807300000 | STAMPINGS FROM TITANIUM ALLOY TI-6AL-4V, ACCORDING TO SPECIFICATION AIMS 03-20-002, CODE 4SHO-1058/4WO-1058 (D545 20933 200) - 17 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. ARE A PART OF THE A320NEO WING PYLON | 118.08 | 12018.2 | France | FRANKFURT MAIN GERMANY | OJSC CORPORATION VSMPO AVISMA |
1/17/2022 | 8807300000 | STAMPINGS FROM TITANIUM ALLOY TI-6AL-4V, ACCORDING TO SPECIFICATION AIMS 03-20-002, CODE 4SHO-987/4WO-987 (D545 15917 200) - 18 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. ARE A PART OF THE A320NEO WING PYLON | 259.68 | 22235.8 | France | FRANKFURT MAIN GERMANY | OJSC CORPORATION VSMPO AVISMA |
1/17/2022 | 8807300000 | STAMPINGS FROM TITANIUM ALLOY TI-6AL-4V, ACCORDING TO SPECIFICATION AIMS 03-20-001, CODE 4Sh-840A / 4W-840A (V572 50800 201) - 5 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. PART OF THE WING PYLON OF A350 CIVIL AIRCRAFT | 290 | 11317.1 | France | FRANKFURT MAIN GERMANY | OJSC CORPORATION VSMPO AVISMA |
1/17/2022 | 8807300000 | STAMPINGS FROM TITANIUM ALLOY TI-6AL-4V, ACCORDING TO SPECIFICATION AIMS 03-20-001, REF 3?-1221.030/3W-1221.030 - 1 pc. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. THEY ARE PARTS OF THE WING OF A350-900 CIVIL AIRCRAFT. | 327.6 | 23670.4 | France | FRANKFURT MAIN GERMANY | OJSC CORPORATION VSMPO AVISMA |