What was found
INSPECTION FOUND FORWARD FACE OF LAV BULKHEAD FRAME TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1309. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 29.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FORWARD FACE OF LAV BULKHEAD FRAME TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1309. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 29.