What was found
INSPECTION FOUND SKIN WEB OIL CANNED AT AFT PRESSURE BULKHEAD FORWARD SIDE RT LOWER SECTION BETWEEN S23R AND Z-CHANNEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-80-08, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND SKIN WEB OIL CANNED AT AFT PRESSURE BULKHEAD FORWARD SIDE RT LOWER SECTION BETWEEN S23R AND Z-CHANNEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-80-08, FIGURE 201.