What was found
(LOG 0589533) CRACK WAS FOUND OF 0.21IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 827 BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 0589533) CRACK WAS FOUND OF 0.21IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 827. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 827 BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.