What was found
(LOG 2287988) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9 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 2287988) DURING INSPECTION FOUND CRACK ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9. CRACKS ON LH FUSELAGE FRAME STA 380 BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02A.