As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER PART OF FRAME 38 BETWEEN STR 21L AND 21R IS CORRODED. (RESOLVED ON W/O: 36809 TASKCARD: N/R-00305 ) CORROSION REMOVED ON LOWER PART OF FRAME 38 STR 21L-21R IAW SRM 51-21-42. REPAIRED FRAME 38 PER TC EO 72-53-0233. MATERIAL THICKNESS 0.063, MATERIAL REMOVED 0.035 OUT OF LIMITS AS PER SRM 53-61-00 FIG 301 ASA RII C/W. (SUPPLEMENTAL-SDR CLOSED 10/3/06)