What was found
(LOG 0590237) CRACK WAS FOUND OF 0.28IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 400. 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 0590237) CRACK WAS FOUND OF 0.28IN OF LENGTH ON LH FUSELAGE FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. FRAME AT INBOARD FASTENER HOLE ON STA 400. BTW S-8L & S-9L. WAS REPAIRED PER AMDS 2526-01236-02A.