What was found
(LOG 0416127) CRACK (0.200IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827 BTW S-8R & S-9R. 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 0416127) CRACK (0.200IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 827 BTW S-8R & S-9R. FUSELAGE FRAME STA 827 BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.