What was found
DURING SCHEDULED 1/2 C CHECK, FOUND FUSELAGE SKIN CRACKED AT LEFT SIDE, 2ND PASSENGER WINDOW FROM FRONT AT TOP FWD CORNER RIVET HEAD. REPAIRED PER SWA RA 1-253-1372 AND BOEING STRUCTURAL REPAIR MANUAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/2 C CHECK, FOUND FUSELAGE SKIN CRACKED AT LEFT SIDE, 2ND PASSENGER WINDOW FROM FRONT AT TOP FWD CORNER RIVET HEAD. REPAIRED PER SWA RA 1-253-1372 AND BOEING STRUCTURAL REPAIR MANUAL.