What was found
LT UNDER WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STR 43. ACCOMPLISHED REPAIR ON LT FUSELAGE WING BARREL CANTED PANEL CAP AT STA 1236 STR 43 PER EA 011-5310-52-A7214 I/R REF NRC A040820.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT UNDER WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STR 43. ACCOMPLISHED REPAIR ON LT FUSELAGE WING BARREL CANTED PANEL CAP AT STA 1236 STR 43 PER EA 011-5310-52-A7214 I/R REF NRC A040820.