What was found
(LOG 0589206) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 500C BTW S-8R & S-9R. WAS REPAIRED PER AMDS 2526-01236-02B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0589206) CRACK WAS FOUND OF 0.13IN OF LENGTH ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 500C. BTW S-8R & S-9R. FRAME AT INBOARD FASTENER HOLE ON STA 500C BTW S-8R & S-9R. WAS REPAIRED PER AMDS 2526-01236-02B.