What was found
(LOG 0415526) CRACK (0.480IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B BTW S-8L & S-9L. FUSELAGE FRAME STA 727B 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 0415526) CRACK (0.480IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 727B BTW S-8L & S-9L. FUSELAGE FRAME STA 727B BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.