1/4/2022 | 7616999008 | SUPPORT BEAM BETWEEN THE FRAMES OF THE POWER STRUCTURE OF THE LOWER CENTRAL PART OF THE FUSELAGE OF THE EMBRAER 170 CIVIL AVIATION ACFT: | 7.11 | 7137.63 | Brazil | WARSAW AIRPORT | PJSC AIRLINE SIBERIA |
1/2/2022 | 7616999008 | BRACKET ASSEMBLY FOR FASTENING OF THE MANIFOLD OF THE FRONT CHASSIS TURN CONTROL SYSTEM, ON THE CEILING PANEL OF THE CHASSIS COMPARTMENT OF THE EMBRAER 170 CIVIL AVIATION PASSENGER ACFT. | 0.09 | 149.31 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/2/2022 | 7616999008 | FRONT ENTRANCE DOOR ARM BRACKET EMBRAER170/175 CIV. AVIATION: | 0.01 | 361.96 | Brazil | MITRI MORI | PJSC AIRLINE SIBERIA |
1/3/2022 | 7616999008 | LOCK-LATCH PLATE OF THE HYDRAULIC SYSTEM HATCH ON THE FAIRING OF THE FUSELAGE CENTER SECTION EMBRAER170/175 CIV. AVIATION: | 0.01 | 943.36 | Brazil | SINGAPORE AIRPORT | S 7 ENGINEERING LLC |
1/26/2022 | 7616999008 | REINFORCING FLOOR PANELS IN THE CABIN OF E170 CIVIL AVIATION PASSENGER ACFT. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVE, DOES NOT CONTAIN PRECIOUS METALS). PROVIDES ADDITIONAL LOAD ON THE FLOOR PANELS: | 1.34 | 911.75 | Brazil | WERTINGEN | PJSC AIRLINE SIBERIA |
1/30/2022 | 7616999008 | FASTENING ELEMENT IN THE FORM OF A BRACKET, PORTHOLE FASTENING IN THE PASSENGER COMPARTMENT OF AIR CONDITIONS EMBRAER 170/175 OF CIVIL AVIATION: | 0.24 | 3646.9 | Brazil | SINGAPORE AIRPORT | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | VENTILATION GRILLE ASSEMBLY OF THE WALL PANEL OF THE KITCHEN UNIT ON AIR CONDITIONS EMBRAER170/175 CIVIL AVIATION. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% IMPURITY). | 0.07 | 616 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/29/2022 | 7616999008 | GUIDE PROFILE OF THE FUSELAGE STRENGTH PACKAGE ShP.19 VS, MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING, FOR MAINTENANCE OF EMBRAER 170 CIVIL AVIATION AIRCRAFT. | 0.07 | 305.93 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |
1/29/2022 | 7616999008 | GUIDE PROFILE OF THE FUSELAGE STRENGTH PACKAGE ShP.19 VS, MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING, FOR MAINTENANCE OF EMBRAER 170 CIVIL AVIATION AIRCRAFT. | 0.06 | 291.09 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |
1/29/2022 | 7616999008 | GUIDE PROFILE OF THE FUSELAGE STRENGTH SET ShP.20 VS, MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING, FOR MAINTENANCE OF EMBRAER 170 CIVIL AVIATION AIRCRAFT. | 0.05 | 220.22 | Brazil | MITRY MORY | S 7 ENGINEERING LLC |