What was found
INSPECTION FOUND THE NR 2 ENGINE RT O/B PYLON SKIN CRACKED AT FORWARD UPPER CORNER AND AFT LOWER CORNER AT ACCESS PANEL NR 5824. THE CRACKS WERE .5 AND 2 INCH LONG. REPAIRED IAW ECRA 5430-01204.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THE NR 2 ENGINE RT O/B PYLON SKIN CRACKED AT FORWARD UPPER CORNER AND AFT LOWER CORNER AT ACCESS PANEL NR 5824. THE CRACKS WERE .5 AND 2 INCH LONG. REPAIRED IAW ECRA 5430-01204.