What was found
#1 ENGINE PYLON INNER SKIN HAS EXFOLITATION CORROSION FWD OF THE VENT PANEL OPENING. DOT 8-001. AUDIT COMPLETE.ALL WORK ACCOMPLISHED PER EO-87960-REQ1 AND VT-MAE EA 757-5450-27-A3329
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
#1 ENGINE PYLON INNER SKIN HAS EXFOLITATION CORROSION FWD OF THE VENT PANEL OPENING. DOT 8-001. AUDIT COMPLETE.ALL WORK ACCOMPLISHED PER EO-87960-REQ1 AND VT-MAE EA 757-5450-27-A3329