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 | SOLID-ROLL RINGS FROM TITANIUM ALLOY TA6V PRODUCT CODES 2KR-2446T - 1 PC, MADE FROM 8-11-12052 STEEL MPA-1130 STRENGTH. RING FORGINGS ARE PARTS OF THE LEAP-1A/-1C AIRCRAFT ENGINE FOR THE AIRBUS A320 NEO / COMAC C919 AIRCRAFT, | XXXXXXXXXX | 1 | N/A | 1249.32 | Belgium | FRANKFURTMAIN |
1/26/2024 | 8411910008 | SOLID-ROLL RINGS FROM TITANIUM ALLOY TA6V ACCORDING TO DMD 0776. PRODUCT CODE 2KP-2063T - 35 PCS, MADE FROM STEEL METALS 8-04-11250 8-12-12140 8-27-13321 TENSILE STRENGTH NOT MORE THAN 980 MPa. RINGS ARE A PART OF THE LEAP-1B ENGINE FOR THE BOEING AIRCRAF | XXXXXXXXXX | 1 | N/A | 60255.18 | Belgium | 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 |
1/24/2024 | 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 |
1/23/2024 | 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 |
1/17/2024 | 8411910008 | SOLID-ROLL RINGS FROM TITANIUM ALLOY TA6V ACCORDING TO DMD 0776. PRODUCT CODE 2KP-2065T- 20 PCS, MADE FROM STEEL 8-16-06331, STRENGTH ULTIMATE NOT MORE THAN 980 MPa. RINGS ARE A PART OF THE LEAP-1B ENGINE FOR THE BOEING 737 MAX AIRCRAFT, | XXXXXXXXXX | 1 | N/A | 35313.88 | Belgium | BEIJING |