What was found
RIGHT WING AFT SPAR AREA UPPER WING FIXED PANEL SUPPORT ANGLE JUST INBD AND COMMON TO THE DEFLECTION CONTROL RIB CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A6200, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING AFT SPAR AREA UPPER WING FIXED PANEL SUPPORT ANGLE JUST INBD AND COMMON TO THE DEFLECTION CONTROL RIB CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A6200, REV A.