What was found
DURING INSPECTION FOUND WEAR IN COMPOSITE MATERIAL OF ACCESS PANEL 193D. ACCESS PANEL WAS REPAIRED PER SRM 51-70-05-2R-6 PAR 4 STEP E F AND G AND SRM 51-70-05-2R-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION FOUND WEAR IN COMPOSITE MATERIAL OF ACCESS PANEL 193D. ACCESS PANEL WAS REPAIRED PER SRM 51-70-05-2R-6 PAR 4 STEP E F AND G AND SRM 51-70-05-2R-0.