公开(公告)号：US20230166870A1

公开(公告)日：2023-06-01

申请号：US17993165

申请日：2022-11-23

Applicant: Airbus Operations SAS

Inventor： Bruno CHAUVEAU ,  Olivier COLLIN ,  Olivier CHAUVET

IPC: B64F5/40 ,  B64C1/12 ,  B29C73/10 ,  B29C73/26

CPC classification number: B64F5/40 ,  B64C1/12 ,  B29C73/10 ,  B29C73/26 ,  B29C2073/264

Abstract: A method for repairing a damaged aircraft fuselage outer skin part, the damaged skin part comprising a static pressure port around which is arranged a stopper fastened to a structure of the fuselage at which a pipe of the static pressure port opens, the method including removing the stopper from the static port, fitting a patch including an opening for housing the stopper, and re-fitting the stopper on an adjustable-thickness spacer. A repair assembly configured to apply the repair method is also provided. Advantageously, it is thus possible to recreate an aerodynamic profile in accordance with the requirements for taking static pressure of the aircraft, with a reduced down-time of the aircraft.