1/13/2022 | 8411810008 | AIR POWER UNIT IS A SINGLE-SHAFT GAS TURBINE ENGINE WITH A CONSTANT SPEED OF SHAFT ROTATION, INSTALLED IN THE TAIL OF THE FUSELAGE - IN A NON-HERMETIC COMPARTMENT OF THE APU, THE ELECTRIC POWER SUPPLIED IS NOT MORE THAN 40 KW | 109 | 204756.5 | Germany | FRANKFURT AIRPORT IN MAIN | PJSC CORPORATION IRKUT |
1/27/2022 | 8411123009 | AIRCRAFT BYPASS TURBOJET ENGINE (USED), HAS 117 KN (26,300 LBF) THRUST. CONSISTS OF FAN, LP COMPRESSOR, HIGH PRESSURE COMPRESSOR, COMBUSTION CHAMBER, HIGH PRESSURE TURBINE, LOW PRESSURE TURBINE AND | 2455 | 6536431.9 | Mongolia | ULAN BATOR R MONGOLIA | AIRLINE ROYAL FLIGHT JSC |
1/20/2022 | 8411123009 | AIRCRAFT BYPASS TURBOJET ENGINE (USED), HAS 117 KN (26,300 LBF) THRUST. CONSISTS OF FAN, LP COMPRESSOR, HIGH PRESSURE COMPRESSOR, COMBUSTION CHAMBER, HIGH PRESSURE TURBINE, LOW PRESSURE TURBINE AND | 2455 | 6442652.2 | Mongolia | ULAN BATOR R MONGOLIA | AIRLINE ROYAL FLIGHT JSC |
1/17/2022 | 8411910008 | COMPLEX FORGINGS FROM TITANIUM ALLOY TI-6AL-4V. PRODUCT CODE 4Sh-1236/4W-1236 - 10 PCS, STRENGTH MPA-980. STAMPINGS ARE A PART OF THE A320NEO AIRCRAFT ENGINE NADDLE, CIVIL PURPOSE. | 64 | 4030.3 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/26/2022 | 8411910008 | STAMPINGS FROM TITANIUM ALLOY TI-6AL-4V, MANUFACTURED ACCORDING TO SPECIFICATION RMS 191, REF 4?-1236/4W-1236 - 39 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. PURPOSE - THEY ARE PARTS OF THE CIVIL AIRCRAFT ENGINE GUNDOLE | 245.2 | 15708.2 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/11/2022 | 8411910008 | COMPLEX FORGINGS FROM TITANIUM ALLOY TI-6AL-4V. PRODUCT CODE 4Sh-1236/4W-1236 - 80 PCS, STRENGTH MPA-980. STAMPINGS ARE A PART OF THE A320NEO AIRCRAFT ENGINE NADDLE, CIVIL PURPOSE. | 510.8 | 32215.3 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/25/2022 | 8411910008 | FORGINGS FROM TITANIUM ALLOY TI-6AL-4V, MANUFACTURED ACCORDING TO SPECIFICATION RMS 191, CODE 4?-1236/4W-1236 - 52 PCS. STRENGTH STRENGTH MPA - NOT LESS THAN 930. COMPLEX SHAPE OF CROSS-SECTION. PURPOSE - THEY ARE PARTS OF THE CIVIL AIRCRAFT ENGINE GUNDOLE | 327 | 20942.8 | United States of America | ONTARIO USA | OJSC CORPORATION VSMPO AVISMA |
1/26/2022 | 8411910008 | ACOUSTIC HONEYCOMB PANEL MADE OF COMPOSITE MATERIAL, DESIGNED FOR REDUCING THE NOISE OF ENGINE AIR CFM56, TO BE INSTALLED ON AN AIR ENGINE, P/N 362-050-110-0, 1 PC. FOR AC MOTIR A319/320/321.,Used | 2.2 | 1035.8 | Czechia | PRAGUE | AIRLINE URAL AIRLINES JSC |
1/26/2022 | 8411910008 | ROLLING RINGS OF COMPLEX SHAPE FROM TA6V TITANIUM ALLOY. CODES 2KRO-2328T - 16 PCS, STRENGTH MPA-1130. RING FORGINGS ARE A PART OF THE LEAP 1B AIRCRAFT ENGINE FOR BOEING CIVIL AIRCRAFT. | 3151 | 133580.8 | France | FRANKFURT MAIN GERMANY | OJSC CORPORATION VSMPO AVISMA |
1/20/2022 | 8411910008 | ROLLING RINGS OF COMPLEX SHAPE FROM TA6V TITANIUM ALLOY. CODES 2KRO-2327T - 5 PCS, STRENGTH MPA-1130. RING FORGINGS ARE A PART OF THE LEAP 1?/? AIRCRAFT ENGINE FOR AIRBUS, COMAC CIVIL AIRCRAFT. | 1020 | 43179 | France | FRANKFURT MAIN GERMANY | OJSC CORPORATION VSMPO AVISMA |