What was found
FUSELAGE FRAME AT FS 310.00 IS CORRODED, BETWEEN STRINGERS 26R & 27. REMOVED DAMAGED AREA OF FRAME & FABRICATED REPAIR PARTS & INSTALLED NEW FRAME, PN SH670-31354-3, IAW REO 67-53-21-982 DATED 21 AUG 2013. NDT PERFORMED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT FS 310.00 IS CORRODED, BETWEEN STRINGERS 26R & 27. REMOVED DAMAGED AREA OF FRAME & FABRICATED REPAIR PARTS & INSTALLED NEW FRAME, PN SH670-31354-3, IAW REO 67-53-21-982 DATED 21 AUG 2013. NDT PERFORMED.