What was found
(LOG 0455948) CRACK (0.500 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 400 BTW S-8L & S-9L. FUSELAGE FRAME STA 400 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 0455948) CRACK (0.500 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 400 BTW S-8L & S-9L. FUSELAGE FRAME STA 400 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.