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 |
1/27/2022 | 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 |
1/1/2022 | 7616100000 | FULL BODY RIVET WITH FLAT SUCKER HEAD FOR FASTENING OF FUSELAGE PANELS OF A320 PASSENGER AIRCRAFT. MATERIAL - ALUMINUM ALLOY (90% ALUMINUM, 10% IMPURITY, DOES NOT CONTAIN PRECIOUS METALS). DIAMETER - 5 MM. | 0.07 | 147.12 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING 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 |
1/26/2022 | 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 |
1/21/2022 | 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 |
1/26/2022 | 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 |
1/21/2022 | 7616999008 | PAD ASSEMBLY OF THE POWER SET OF THE HERMETIC FRAME OF THE FORWARD FUSELAGE, FOR THE MAINTENANCE OF THE EMBRAER170 CIVIL AVIATION AIRCRAFT. | 0.34 | 1311.59 | France | MITRY MORY | S 7 ENGINEERING LLC |
1/27/2022 | 7616999008 | FITTING, RIGIDITY ELEMENT AND REINFORCEMENT OF STRUCTURAL PARTS LOCATED AT AN ANGLE TO EACH OTHER. REPRESENTS A CORNER PROFILE WITH HOLES FOR FASTENING. USED FOR FASTENING A STRINGER IN THE FUSELAGE STRUCTURE OF A PASSENGER AIRCRAFT A319/A320/ | 0.06 | 252.16 | France | HAMBURG AIRPORT GERMANY | S 7 ENGINEERING LLC |