1/1/2022 | 7616999008 | SEALING FOR THE OPENING SECTION OF THE FRONT LEFT DOOR OF THE PASSENGER COMPARTMENT HA EMBRAER 170. MATERIAL - ALUMINUM. | 1 | 866.6 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/6/2022 | 7616999008 | GASKET, INSTALLATION OF THE LOCK FASTENING OF THE PYLON ACCESS HATCH OF THE ENGINE OF THE PASSENGER ACTION GA EMBRAER170. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). MANUFACTURING METHOD - STAMPING. | 0.02 | 166.22 | Brazil | WEST SUSSEX UK | 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 |
1/2/2022 | 7616999008 | BRACKET FOR FASTENING AN ACCESS HATCH TO THE ELECTRICAL EQUIPMENT COMPARTMENT OF PASSENGER ACFT EMBRAER 170/175. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). P/N: | 0.04 | 170.23 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/6/2022 | 7616999008 | GASKET OF THE HINGE OF THE PYLON ACCESS HATCH OF THE ENGINE OF PASSENGER AC HA EMBRAER 170. MATERIAL - ALUMINUM ALLOY (90% - ALUMINUM, 10% - ADDITIVES). MANUFACTURING METHOD - STAMPING. | 0.01 | 138.72 | Brazil | WEST SUSSEX UK | S 7 ENGINEERING LLC |
1/26/2022 | 7616999008 | SLOT-HINGE ASSEMBLY OF FLAP DRIVE MECHANISM FOR EMBRAER 170 AIR. MATERIAL - ALUMINUM ALLOY (AL>90%) | 0.39 | 1751.5 | Brazil | CRAWLEY UNITED KINGDOM | 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 |
1/27/2022 | 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 |