As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1088, S-5L~S-6L. CORROSION REMOVED LEVEL 1 AT 1088, S-5L~S-6L FROM PN 65-46882-1 ORIGINAL THICKNESS 0.064" REMOVED 0.002" AND REMAINING THICKNESS IS 0.062 AND IS WITHIN LIMITS PER SRM 53-00-01 ALLOWABLE DAMAGE 1 R134, AREA CLEAN AND PROTECTIVE I.A.W. B737-300 SRM 51-20-01 P3-7 51-10-02 P12-15 REV 134. PME: 006646 DUE DATE: 07.28.2025