What was found
RT ENGINE TAIL PIPE EXHAUST FAIRING, STIFFENER GOUGED ADJACENT TO ACCESS PANEL AT 6 O`CLOCK POSITION ACCESS PANEL STIFFENER IAW CMM 78-11-00-300-818-A01, REPAIR SRS 084. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT ENGINE TAIL PIPE EXHAUST FAIRING, STIFFENER GOUGED ADJACENT TO ACCESS PANEL AT 6 O`CLOCK POSITION ACCESS PANEL STIFFENER IAW CMM 78-11-00-300-818-A01, REPAIR SRS 084. (K)