What was found
(LOG 0455181) CRACK (0.500 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500D. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 500D BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0455181) CRACK (0.500 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500D. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 500D BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.