1/25/2022 | 7616999008 | BUSHING FROM DURALUMINIUM IN THE FORM OF A CYLINDER WITH A THROUGH AXIAL HOLE, STAMPED; APPLIED FOR FENDING THE AIR CONDITIONING SYSTEM PIPELINE IN THE CREW CABIN OF BELL 505 CIVIL HELICOPTER, INSTALLED IN THE LOWER PART OF THE FUSELAGE: | 0.01 | 4.23 | Unknown | BADHOEVEDORP | AOKAZAN AIRLINE |
1/25/2022 | 7616999008 | CLAMP IN THE FORM OF A STAMPED DURALUMINUM TAPE BENT IN THE FORM OF A RING; USED FOR FASTENING THE FUEL LINE TO THE POWERFUL FUSELAGE FRAME ON BELL 505 CIVIL HELICOPTER, OKPD2 CODE: 25.99.29 | 0.09 | 33.44 | Unknown | BADHOEVEDORP | AOKAZAN AIRLINE |
1/25/2022 | 7508900009 | SOLID RIVET IS USED FOR FASTENING FUSELAGE COVERING PANELS DURING REPAIR OF A319/A320/A321 aircraft. MADE FROM ALLOY (NI-67%, CU-30% RESIDUAL IMPURITIES). | 8 | 841.1 | Unknown | MIAMI | S 7 ENGINEERING LLC |
1/10/2022 | 8108909008 | SCREEN HEAD BOLT, FUSELAGE PANEL FIXINGS EMBRAER 170 CIT. AVIATION: | 0.1 | 720.4 | Unknown | FORT LAUDERDALE FLORIDA | S 7 ENGINEERING LLC |
1/30/2022 | 8108909008 | SCREW HEAD BOLT FOR FASTENING OF STRUCTURAL ELEMENTS OF PASSENGER GA BOEING 737 FUSELAGE: P/N BACB30NT3K10-100PCS | 0.26 | 101.2 | Unknown | MOSCOW RUSSIA | AZUR AIR LLC |
1/10/2022 | 7606129309 | SHEET (ROLL) FLAT FROM ALUMINUM ALLOY (90% - ALUMINUM, 10% - ADDITIVES. DOES NOT CONTAIN PRECIOUS METALS). INTENDED FOR REPAIR OF FUSELAGE PANELS OF B737 PASSENGER AIRCRAFT. THICKNESS - 4.06 MM. SHEETS SIZE - 366X122 CM. FOR REPAIR AND TECHNICAL | 100 | 4211.34 | Unknown | MOSCOW RUSSIA | AZUR AIR LLC |
1/27/2022 | 7606129208 | FLAT SHEET (ROLL) FROM ALUMINUM ALLOY FOR REPAIR OF FUSELAGE PANELS OF BOEING 737 CIVIL AVIATION: | 26 | 1899.12 | Unknown | BIGGLESWADE ENGLAND | S 7 ENGINEERING LLC |
1/7/2022 | 7604299000 | PROFILE (LONGITUDINAL ELEMENT) OF COMPLEX SHAPE, COMPLEX SECTION, STRUCTURAL SET OF THE FUSELAGE STRUCTURE OF A313/A320 CIVIL AVIATION PASSENGER ACFT: | 0.29 | 1319.38 | Unknown | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/6/2022 | 7318190008 | ADAPTER, INSTALLED BETWEEN THE FUSELAGE AND THE JACK IN THE TAIL PART OF THE BOEING737 ACFT. P/N ?07004-1 - 1pc | 2 | 161.85 | Unknown | MOSCOW RUSSIA | AZUR AIR LLC |
1/5/2022 | 8301409000 | MECHANICAL LOCK ASSEMBLY OF TECHNOLOGICAL HATCH OF THE FUSELAGE CENTER-SECTION FAIRING OF PASSENGER PASSENGER ACFT EMBRAER 170/175 CIVIL AVIATION: | 0.06 | 452.67 | Unknown | MUSKEGON | S 7 ENGINEERING LLC |