As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PIT BODY FRAME WEB IS CRACKED AT TOOLING HOLE BS 970, STR 26L - 27L REMOVED ASSOCIATED PARTS TO FRAME 970 SECTION, REMOVED DAMAGE SECTION OF FRAME FROM STR 27R TO STR 24L AND 25L. FABRICATED NEW FRAME SECTION, HEAT TREATED, ALODINED AND PRIMED, PAINTED AND INSTALLED. INSTALLED REMOVED ASSOCIATED PARTS TO FRAME REF BOEING DOCUMENT NUMBER 65-16339 AND SRM 51-30-02. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.