What was found
DURING AIRCRAFT CHECK REDUNDANT HOLE WAS FOUND COMMON TO PRESSURE DECK WEB STA 224-246. NLG W/W CEILING, DIAMETER OF THE REDUNDANT HOLE IS GREATER THAN 0.25", WHICH EXCEEDS MAXIMUM ALLOWABLE DAMAGE PER SRM 53-10-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING AIRCRAFT CHECK REDUNDANT HOLE WAS FOUND COMMON TO PRESSURE DECK WEB STA 224-246. NLG W/W CEILING, DIAMETER OF THE REDUNDANT HOLE IS GREATER THAN 0.25", WHICH EXCEEDS MAXIMUM ALLOWABLE DAMAGE PER SRM 53-10-14.