1/22/2022 | 7604299000 | PROFILE, OF COMPLEX FORM, IS AN ELEMENT OF LONGITUDINAL FUSELAGE STRENGTH IN THE REGION OF SHP. 34-35 BC A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). FOR MAINTENANCE OF AIRCRAFT AIRBUS A321 CIVIL AVIATION. | 1 | 1591.52 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/21/2022 | 7604299000 | COMPLEX SHAPE PROFILE IS AN ELEMENT OF THE LONGITUDINAL FUSELAGE STRENGTH IN THE AREA OF THE FIRST CARGO COMPARTMENT OF A319/A320/A321 CIVIL AVIATION PASSENGER ACFT: | 0.97 | 956.2 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7604299000 | GUIDING PROFILE OF THE FUSELAGE STRENGTH PACKAGE ??.76 ?? EMBRAER170. MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING. | 0.03 | 213.37 | Brazil | MITRI MORI | S 7 ENGINEERING LLC |
1/24/2022 | 7604299000 | COMPLEX SHAPE PROFILE IS AN ELEMENT OF THE LONGITUDINAL STRENGTH SET OF THE FUSELAGE OF A320 GA PASSENGER AC. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). | 0.54 | 2156.11 | France | DUBAI | S 7 ENGINEERING LLC |
1/13/2022 | 7604299000 | THE PROFILE, REPAIR SIZE, IS A DOCKING ELEMENT OF THE FRAME AND THE VERTICAL PARTITION SEPARATING THE NICHE OF THE MAIN STOCK OF THE CHASSIS WITH THE HERMETIC PART OF THE FUSELAGE OF THE BOEING737 AC AC. MATERIAL - ALUMINUM ALLOY (90% - ALUMINUM, 10% - ALLOYING | 0.15 | 965.35 | United States of America | SEATLE | S 7 ENGINEERING LLC |
1/22/2022 | 7604299000 | PROFILE, OF COMPLEX FORM, IS AN ELEMENT OF LONGITUDINAL FUSELAGE STRENGTH IN THE REGION OF SHP. 24-27 BC A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). FOR MAINTENANCE OF AIRCRAFT AIRBUS A321 CIVIL AVIATION. | 1 | 1333.52 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/27/2022 | 7604299000 | GUIDING PROFILE OF THE POWER SET OF THE TAIL FUSELAGE OF AC HA EMBRAER170/175. MATERIAL: ALUMINUM ALLOY (AL>90%, REMAINING ALLOYS), PRESSING, MILLING | 0.04 | 285.64 | France | MITRI MORI | S 7 ENGINEERING LLC |
1/14/2022 | 7604299000 | PROFILE OF COMPLEX SHAPE, COMPLEX SECTION, MADE OF ALUMINUM ALLOY, USED IN REPAIR OF ACFT FUSELAGE STRENGTH PACKAGE A319/A320/A321 CIVIL. AVIATION: | 0.31 | 1908.17 | Germany | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/29/2022 | 7604299000 | PROFILE OF THE POWER SIDE PANEL OF THE FUSELAGE OF THE CARGO COMPARTMENT FOR A319/A320/A321 CIVIL AVIATION ACFT: | 0.15 | 169.93 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |
1/22/2022 | 7604299000 | PROFILE, OF COMPLEX FORM, IS AN ELEMENT OF LONGITUDINAL FUSELAGE STRENGTH IN THE REGION OF SHP. 24-27 BC A320. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% ADDITIVES). FOR MAINTENANCE OF AIRCRAFT AIRBUS A321 CIVIL AVIATION. | 1 | 1075.52 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |