What was found
(LOG 2286166) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(LOG 2286166) DURING INSPECTION FOUND CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 (INBD & OUTBD FASTENER HOLES OF SUPPORT BRACKET. CRACKS ON RH FUSELAGE FRAME STA 500C BTW S-8 AND S-9 WAS REPAIRED PER AMDS 2526-01236-02B.