What was found
(LOG 0415367) CRACK (0.120 IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8L & S-9L. FUSELAGE FRAME STA 500A BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0415367) CRACK (0.120 IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500A BTW S-8L & S-9L. FUSELAGE FRAME STA 500A BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.