As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(LOG 0575883) CRACK WAS FOUND OF 0.28 IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8R & S-9R. RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500A. BTW S-8R & S-9R WAS REPAIRED UNDER CARD 2526-01236-02B.