What was found
CRACK ON INTERNAL SKIN OF ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00726-WIP1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INTERNAL SKIN OF ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00726-WIP1.