What was found
CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8L & S-9L. FUSELAGE FRAME STA 500C BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK (0.400IN LENGTH) ON FUSELAGE FRAME AT INBOARD FASTENER HOLE STA 500C BTW S-8L & S-9L. FUSELAGE FRAME STA 500C BTW S-8L & S-9L WAS REPAIRED UNDER AMDS 2526-01236-02A.