| 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 | 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-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 |
| 1/26/2024 | 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 |
| 1/25/2024 | 8411910008 | PARTS OF THE D-30KU-154 TURBOJET ENGINE OF THE TU-154M CIVIL AIRCRAFT, INTENDED FOR COMMERCIAL TRANSPORTATION OF PASSENGERS: BLADE SA 1 ST. 59-04-4867-133 PCS., SPLIT RING SA 2 ST. 40-04-4169-1 PC., | XXXXXXXXXX | 2 | N/A | 640243.56 | China | BEIJING |
| 1/24/2024 | 8411910008 | (18.2) COVERING DISC II 078.41.0504 2 PCS (P.9), COVERING DISC III 078.41.0505 2 PCS (P.10). IS A ROUND PART WITH AN AXIAL THROUGH HOLE OF 190.5 MM, WITH PROTRUSIONS, BEVELINGS AND GROOVE. USED ON THE ROTOR OF A COMPRESSOR TURBINE IN AN ENGINE | XXXXXXXXXX | 5 | N/A | 0 | India | CHANDIGARH AIRPORT |
| 1/24/2024 | 8411910008 | PARTS OF THE D-30KU-154 TURBOJET ENGINE OF THE TU-154M CIVIL AIRCRAFT, INTENDED FOR COMMERCIAL TRANSPORTATION OF PASSENGERS: RING 40-04-789-3 PCS., SPLIT RING SA 4 ST; 51-04-4099-1 PC., | XXXXXXXXXX | 1 | N/A | 574217.8 | China | BEIJING |
| 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 |