1/26/2024 | 8411910008 | SOLID-ROLLED TITANIUM ALLOY RINGS TA6V OF COMPLEX CROSS-SECTION SHAPE. MELT 8-27-13309,8-36-11965,8-16-06331. STRENGTH ULTRA-STRENGTH MPA-NOT LESS THAN 930. RINGS ARE AN ELEMENT OF THE LEAP-1B ENGINE FOR BOEING 737MAX CIVIL AIRCRAFT | XXXXXXXXXX | 1 | N/A | 61799.28 | Belgium | BEIJING |
1/26/2024 | 8411910008 | STAMPED FORGINGS FROM TITANIUM ALLOY TA6V-PQ, MADE ACCORDING TO SPECIFICATION DMD 0777-24. HEAT 8-34-10861, 8-27-13431. TENSILE STRENGTH MPa - NOT LESS THAN 930. COMPLEX CROSS-SECTION SHAPE. ARE A PART OF THE CFM56-7 CIVIL ENGINE. | XXXXXXXXXX | 1 | N/A | 27745.76 | France | FRANKFURTMAIN |
1/26/2024 | 8411910008 | SOLID ROLLED RINGS/COILS WITH SEMI-FINISH MACHINED FROM TITANIUM ALLOY TA6V-PQ, MANUFACTURED ACCORDING TO SPECIFICATION DMD 0777-24; HEAT 8-27-13310, 8-27-13309, 8-46-12752, 8-35-10874; TENSILE STRENGTH MPa - NOT LESS THAN 930; COMPLEX SHAPE OF CROSS | XXXXXXXXXX | 1 | N/A | 110103.69 | Belgium | FRANKFURTMAIN |
1/26/2024 | 8411910008 | ROLLING RINGS MECHANICALLY PROCESSED FROM TITANIUM ALLOY TI-6AL-4V, MADE ACCORDING TO SPECIFICATION MSRR 8652. HEAT 8-04-11426. STRENGTH ULTRA-STRENGTH MPa - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. ARE A PART OF THE TRENT 7000, T1000-TEN GR ENG | XXXXXXXXXX | 1 | N/A | 54341.46 | United Kingdom | BEIJING |
1/24/2024 | 8411910008 | TITANIUM SOLID-ROLL RING/COIL WITH PRE-MECHANICAL TREATMENT FROM TITANIUM ALLOY TA6V-PQ OF COMPLEX SHAPE OF CROSS-SECTION PRODUCT CODE 2KRO-2377T-2 PCS. MELT 8-27-13307. STRENGTH ULTRA MPA-1130, COILS ARE AN ELEMENT OF CIVIL | XXXXXXXXXX | 1 | N/A | 16108.82 | Belgium | FRANKFURTMAIN |
1/24/2024 | 8411910008 | COILS WITH PRE-MECHANICAL TREATMENT FROM TITANIUM ALLOY TA6V-PQ OF COMPLEX SHAPE OF CROSS-SECTION PRODUCT CODE 2KRO-2244T-7 PCS. MELT 8-46-12752,8-34-10731 STRENGTH ULTRA MPA-NO MORE THAN 1200, COILS ARE AN ELEMENT OF THE LEAP 1A/-1C ENGINE | XXXXXXXXXX | 1 | N/A | 59286.6 | Belgium | FRANKFURTMAIN |
1/23/2024 | 8411910008 | SOLID-ROLL TITANIUM TA6V ALLOY RINGS MADE TO SPECIFICATION OOMTF145338. HEAT 8-11-12052, 8-35-10931. TENSILE STRENGTH MPa - NOT LESS THAN 930. COMPLEX CROSS-SECTION SHAPE. ARE A PART OF THE LEAP - 1A/-1C ENGINE OF AIRBUS AIRCRAFT | XXXXXXXXXX | 1 | N/A | 24986.42 | Belgium | FRANKFURTMAIN |
1/23/2024 | 8411910008 | SOLID-ROLL TITANIUM ALLOY RINGS TA6V OF COMPLEX CROSS-SECTION SHAPE PRODUCT CODE 2KR-2065T-8 PCS. HEAT 8-36-119652. STRENGTH ULTRA-STRENGTH MPA-NO MORE THAN 1200, RINGS ARE AN ELEMENT OF THE LEAP-1B ENGINE FOR BOEING 737MAX CIVIL AIRCRAFT | XXXXXXXXXX | 1 | N/A | 14125.55 | Belgium | BEIJING |
1/22/2024 | 8411910008 | SOLID-ROLL TITANIUM TA6V ALLOY RINGS, MADE TO SPECIFICATION OOMTF145338. HEAT 8-11-12052. TENSILE STRENGTH MPa - NOT LESS THAN 930. COMPLEX CROSS-SECTION SHAPE. ARE A PART OF THE LEAP - 1A/-1C ENGINE OF THE AIRBUS A320 NEO AIRCRAFT, | XXXXXXXXXX | 1 | N/A | 3747.96 | Belgium | FRANKFURTMAIN |
1/22/2024 | 8411910008 | SOLID-ROLL TITANIUM TA6V ALLOY RINGS MADE TO DMD 0776 SPECIFICATION. HEAT 8-12-12140. TENSILE STRENGTH MPa - NOT LESS THAN 930. COMPLEX CROSS-SECTION SHAPE. ARE A PART OF THE LEAP 1B ENGINE OF THE BOEING 737 MAX AIRCRAFT | XXXXXXXXXX | 1 | N/A | 25823.65 | Belgium | FRANKFURTMAIN |