What was found
(LOG 0416116) CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8R & S-9R. FUSELAGE FRAME STA 500C 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 0416116) CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8R & S-9R. FUSELAGE FRAME STA 500C BTW S-8R & S-9R WAS REPAIRED UNDER AMDS 2526-01236-02B.