As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REF AMES NON ROUTINE 168798-0100-0205.GENERATING ITEM:63-5300-1- 2516.(B767-53-3-7121) CORROSION ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN, AT STA.1083, BETWEEN STR.39L AND STR.39R.#91038 REMOVED CORROSION ON THE INTERIOR SURFACE OF THE FUSELAGE SKIN A T STA1083 BETWEEN STR39L AND 39B PER B767 SRM 53-60-01 ALLOWABL E DAMAGE 1, FOUND DAMAGE TO BE BEYOND LIMITS. AMES DOCUMENT 4760 9REA11