What was found
(LOG 0455961) CRACK (0.250 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 867 BTW S-8L & S-9L. FUSELAGE FRAME STA 867 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 0455961) CRACK (0.250 IN LENGTH) ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA. 867 BTW S-8L & S-9L. FUSELAGE FRAME STA 867 BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.