What was found
(LOG 0455202) CRACK (0.250 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 827 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 0455202) CRACK (0.250 IN LENGTH) ON RH FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827. BTW S-8R & S-9R. RH FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.