What was found
(LOG 0631688) CRACK OF 0.562 IN LENGTH ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L. FRAME STA 380 BTW S-8L & S-9L (REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526-01236-02A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0631688) CRACK OF 0.562 IN LENGTH ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 380 BTW S-8L & S-9L. FRAME STA 380 BTW S-8L & S-9L (REF. CARD 2526-01236-01A, STEP 5) WAS REPAIRED PER ADMS 2526-01236-02A.