As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(LOG 0455149) CRACK (0.625 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R AND CRACK (0.125IN LENGTH) ON FUSELAGE FRAME AT OUTBOARD FASTENER HOLE STA 380 BTW S-8R & S-9R. RH FUSELAGE FRAME STA 380 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B. )