1/17/2022 | 7616999008 | AIRCRAFT FUSELAGE PANEL MADE FROM ALUMINUM ALLOY BY THE COMBINED METHOD. INSTALLED ON BOMBARDIER CL-600-2B19 (CANADAIR REGIONAL JET) PASSENGER ACFT. IS NOT A MILITARY/DUAL-PURPOSE PRODUCT. P/N 601R31527- | 1 | 117.16 | Canada | MOSCOW RUSSIA | FASTAIR INTERNATIONAL LLC |
1/27/2022 | 7616999008 | FITTING, CONNECTING ELEMENT OF FRAME AND STRINGER LOCATED AT AN ANGLE TO EACH OTHER. REPRESENTS A CORNER PROFILE WITH HOLES FOR FASTENING. USED FOR FASTENING THE STRINGER TO THE FRAME IN THE STRUCTURE OF THE FUSELAGE OF A PASSENGER GA A319/ | 0.04 | 295.1 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/19/2022 | 7616999008 | OTHER PRODUCTS FROM ALUMINUM. IS A PLATE OF ALUMINUM WITH MOUNTING HOLES. PART OF THE D64-0053-PRE-T-SETR5 COMPOSITE FUSELAGE PRE-ASSEMBLY KIT. SUPPLIED AS | 0.03 | 33.99 | Austria | WIENER NEUSTADT | AURAL CIVIL AVIATION PLANT |
1/22/2022 | 7616999008 | PARTITION B/N S53671217378 (ALTERN. B/N S5367121737802), IN DURALUMINUM (ALLOY OF ALUMINUM AL (BASE) WITH COPPER CU (1.2-2%), MAGNESIUM MG (2.1-2.9%) AND ZINC ZN (5.1-6.1%), COMBINED TREATMENT, PAINTED, FOR ACFT FUSELAGE STRUCTURAL REPAIR, FOR R | 1.51 | 2961.07 | Italy | MIAMI | PJSC AIRLINE UTair |
1/17/2022 | 7616999008 | AIRCRAFT FUSELAGE PANEL MADE FROM ALUMINUM ALLOY BY THE COMBINED METHOD. INSTALLED ON BOMBARDIER CL-600-2B19 (CANADAIR REGIONAL JET) PASSENGER ACFT. IS NOT A MILITARY/DUAL-PURPOSE PRODUCT. P/N 601R31527- | 1 | 182.59 | Canada | MOSCOW RUSSIA | FASTAIR INTERNATIONAL LLC |
1/27/2022 | 7616999008 | FUSELAGE FRAME BRACKET, COMPLEX SHAPED, MADE FROM ALUMINUM ALLOY. IS A PART OF THE STRUCTURAL PACKAGE OF THE FUSELAGE OF THE PASSENGER AIRCRAFT ?318/319/320/321 | 0.04 | 269.1 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/2/2022 | 7616999008 | LOCK-LATCH PLATE OF THE HYDRAULIC SYSTEM HATCH ON THE FAIRING OF THE CENTRAL SECTION OF THE FUSELAGE OF THE AC CA EMBRAER170/175. MATERIAL - ALUMINUM (AL>97%), MILLING, PAINTING. | 0 | 53.5 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/26/2022 | 7616999008 | FRAME STRIP FOR THE STRUCTURE OF THE FUSELAGE OF A320NEO PASSENGER ACFT OF CIVIL AVIATION: | 0.07 | 748.13 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/26/2022 | 7616999008 | LONGITUDINAL BEAM OF THE FUSELAGE POWER STRUCTURE IN THE AREA OF 12-16 FRAMES OF PASSENGER ACFT A319/320/321 CIVIL AVIATION: | 0.53 | 1071.95 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/26/2022 | 7616999008 | BUSHING WITHOUT A THREAD, FASTENING THE FUSELAGE PANELS OF A321 CIVIL AVIATION PASSENGER ACFT: | 0.06 | 107.07 | France | DUBAI | S 7 ENGINEERING LLC |