摘要 |
A method for reworking an aircraft wing, attached to an aircraft fuselage, to reduce a propensity for advanced dynamic changes is described. The reworking method includes verifying components of the aircraft wing are in a condition acceptable for reworking, removing at least one existing fastener from the wing, reworking the at least one fastener hole using a coldworking process, and installing an oversized fastener into the at least one reworked fastener hole. |
申请人 |
THE BOEING COMPANY;LIU, KO-WEI;GUZMAN, HUGO;RAMLAOUI, HASAN, I. |
发明人 |
LIU, KO-WEI;GUZMAN, HUGO;RAMLAOUI, HASAN, I. |