What was found
SECONDARY NRC FROM NRC 00115: AFTER STIFFENETR REMOVAL, CRACK WAS FOUND ON SKIN OF ACCESS PANEL 171CL. SKIN OF ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430 REV:--
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SECONDARY NRC FROM NRC 00115: AFTER STIFFENETR REMOVAL, CRACK WAS FOUND ON SKIN OF ACCESS PANEL 171CL. SKIN OF ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430 REV:--