What was found
RT WING OTBD MID FLAP, T/E COVE PANEL CTR BY SUPPORT LINKS 2 EA CRACKS, (1) CRACK ABOUT 13" LONG AND SECOND CRACK ABOUT 6" LONG. (REPAIRED IAW SRM 57-53-01, FIG 201, REPAIR 3.)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING OTBD MID FLAP, T/E COVE PANEL CTR BY SUPPORT LINKS 2 EA CRACKS, (1) CRACK ABOUT 13" LONG AND SECOND CRACK ABOUT 6" LONG. (REPAIRED IAW SRM 57-53-01, FIG 201, REPAIR 3.)