What was found
FOUND CRACK IN THE RT WING REAR SPAR FIXED T/E DEFLECTION CONTROL RIB, FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB SUPPORT OTBD END RIVET TAIL. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK IN THE RT WING REAR SPAR FIXED T/E DEFLECTION CONTROL RIB, FIXED PANEL LOWER HORIZONTAL BULB SEAL RETAINER WEB SUPPORT OTBD END RIVET TAIL. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.