What was found
CRACK FOUND ON THE ON THE FRAME ANGLE BS 1022 BETWEEN LONGERONS 13R TO 14R. THE CRACK IS 0.250" LONG. REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON THE ON THE FRAME ANGLE BS 1022 BETWEEN LONGERONS 13R TO 14R. THE CRACK IS 0.250" LONG. REPAIRED IAW SRM 53-00-06-2R-2, FIG 201.