As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION LOCATED ON FUSELAGE SKIN UNDER SCUFF PLATE AREA AT THE L2 DOOR, STR 23L, Y1340 AND FR 65+5 INCHES TO FR 65+5.5 INCHES. NO ALLOWABLE LIMITS IN THE SRM. MAINTENANCE REWORKED AREA ON FUSELAGE SKIN UNDER THE SCUFF PLATE AT THE L2 DOOR FROM FR 65+5 INCHES TO FR 65+5.5 INCHES AT STR 23L AND Y1340 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5341-06151-SS1.