What was found
(LOG 0553620) CRACK OF 1)L=0.625 IN LENGTH WAS FOUND ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8R & S-9R. FUSELAGE FRAME STA 500A BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0553620) CRACK OF 1)L=0.625 IN LENGTH WAS FOUND ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8R & S-9R. FUSELAGE FRAME STA 500A BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.