What was found
RH FUSELAGE WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STGR 43. REPAIRED IAW EA 011-5310-52-A7215, I/R3
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RH FUSELAGE WING BARREL CANTED PANEL DRAG ANGLE IS CRACKED AT STA 1236 STGR 43. REPAIRED IAW EA 011-5310-52-A7215, I/R3