As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN BUCKLED, RT SIDE AFT OF PIT DOOR BETWEEN FR 59-61 STR 35-39. WHEN RIVETS REMOVED FROM CLIPS, FOUND GAP BETWEEN SKIN AND CLIPS EXCEEDING .031". MAJOR REPAIR ACCOMPLISHED: REPLACED 4 CLIPS AND INSTALLED DOUBLER REPAIR AT FRAME 59 AND STRINGER 35R.