1/5/2022 | 8807300000 | AIR INTAKE (USED) ASSEMBLY. IS AN AERODYNAMICLY STREAMLINED STRUCTURE IN THE FORM OF ALUMINUM ALLOY, TITANIUM AND EPOXY-BASED COMPOSITE AND GLASS FIBER HOUSING AND IS LOCATED IN THE FRONT OF THE AIRCRAFT (NON-MILITARY) | 270 | 108087.7 | United States of America | SHELTON | AK NORDSTAR JSC |
1/28/2022 | 8807100000 | PROPELLERS AND ROTORS: MCCAULEY C TYPE PROPELLERS C 2A34C204C, S/N 770271. USED. INTENDED FOR INSTALLATION ON CIVIL AIRCRAFT MODEL CESNA 182F. BASIC MATERIALS OF THE BUSHING AND BLADES - ALUMINUM ALLOYS. DIAMETER 1.95 M; NUMBER OF LOP | 57.6 | 19565.6 | United States of America | ATTING | SP PROPELLER SERVICE LLC |
1/31/2022 | 8807300000 | WINDSHIELD ASSEMBLY B/N 5-89354-3149, WITH ALUMINUM ALLOY FRAME (FRAMED WINDOW), MULTILAYER, SAFE, FOR INSTALLATION IN THE COCKPIT. FOR MAINTENANCE OF CIVIL PASSENGER AIRCRAFT BOEING737-400/500 | 21.89 | 13067.9 | United States of America | TEMPE | PJSC AIRLINE UTair |
1/24/2022 | 8807200000 | PARTS OF THE CHASSIS-SUPPORT IN THE NOSE STRUT OF THE AIRCRAFT CHASSIS, OF A COMPLEX CYLINDRICAL FORM WITH A BURT, HAS EXTERNAL THREAD AND HOLES, MATERIAL - ALUMINUM ALLOY FOR TECHNICAL PURPOSES OF CIVIL AIRCRAFT DHC-8-300, P/N 892 | 0.5 | 3189.2 | Unknown | CALGARI CANADA | AURORA AIRLINE JSC |
1/14/2022 | 8807300000 | QUICK-RELEASE PANEL (HATCH) FOR ACCESS TO HINGE ASSEMBLY OF AIRCRAFT TURBOJET ENGINE HOOD HINGE. MADE FROM ALUMINUM ALLOY (DURALUMINUM) BY THE COMBINED METHOD, HAS HOLES FOR MOUNTING. INSTALLED ON THE TOP | 3 | 30197.6 | United States of America | SIDAR RAPIDS | AVIATION COMPANY AVIASTAR TU LLC |