As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PERFORMED MAJOR REPAIR BY INCORPORATING SB 670BA-53-062, FUSELAGE CTR FUSELAGE FS 855.40 TO FS 855.4. INSPECTION & MODIFICATION OF THE FASTENER HOLES IN THE FWD, MID & AFT WING SPAR FRAMES & THE ATTACHMENT ANGLE. DURING INSPECTION FOUND 9 EACH ELONGATED HOLES AT FS 797.0 RT SIDE.