What was found
(LOG 0455208) CRACK (0.125 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 867 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 0455208) CRACK (0.125 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 867. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 867 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.