What was found
INSPECTION TYPE:C1, FUSELAGE FRAME AT FS 55 WAS CRACKED AT THE ATTACH ROD AT LONG 24R. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C1, FUSELAGE FRAME AT FS 55 WAS CRACKED AT THE ATTACH ROD AT LONG 24R. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.