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 | MOUNTING PLATE (FITTING) OF COMPLEX SHAPES, RIGIDITY ELEMENT OF ACFT FUSELAGE FRAME STRENGTH A321. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. | 0.27 | 1167.07 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | MOUNTING PLATE (FITTING) OF COMPLEX SHAPES, RIGIDITY ELEMENT OF ACFT FUSELAGE FRAME STRENGTH A321. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. | 0.05 | 236.95 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | MOUNTING PLATE (FITTING) OF COMPLEX SHAPES, RIGIDITY ELEMENT OF FRAME STRENGTH SET 30 ?? A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. | 0.06 | 250.16 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | FASTENING PLATE (FITTING) OF COMPLEX SHAPES, RIGIDITY ELEMENT OF STRENGTH SET OF FRAME 29 ?? A321, MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING | 0.06 | 246.36 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | FASTENING PLATE (FITTING) OF COMPLEX SHAPES, RIGIDITY ELEMENT OF POWER SET OF FRAME 28 ?? A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. | 0.07 | 312.65 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | MOUNTING PLATE (FITTING) OF A COMPLEX SHAPED, RIGIDITY ELEMENT OF THE STRENGTH SET OF THE A320 BC FRAME. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. | 0.16 | 593.85 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | MOUNTING PLATE (FITTING) OF A COMPLEX SHAPED, RIGIDITY ELEMENT OF THE STRENGTH SET OF THE A320 BC FRAME. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. FOR | 0.14 | 711.61 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | FASTENING PLATE (FITTING) OF COMPLEX SHAPES, RIGIDITY ELEMENT OF POWER SET OF FRAME 28 ?? A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES, DOES NOT CONTAIN PRECIOUS METALS). MANUFACTURING METHOD - STAMPING, MILLING, PAINTING. | 0.09 | 324.26 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/18/2022 | 7616999008 | POWER PAD FOR THE FRONT SEAT OF THE CREW COMMANDER OF THE SERIES: TAAI2- PASSENGER AIR GA ?319/320. MATERIAL: ALUMINUM (AL-90%, REMAINING ALLOYS) COMBINED TREATMENT, PAINTING. | 0.22 | 444.68 | France | FRANKFRUIT IN MAIN | S 7 ENGINEERING LLC |