What was found
INSPECTION TYPE:C1 FUSELAGE FRAME AT FS 55 AT LONGERON 24L IS CRACKED AT THE ATTACH ROD. 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 AT LONGERON 24L IS CRACKED AT THE ATTACH ROD. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.