What was found
THE FUSELAGE SKIN WAS GOUGED FORWARD OF THE C2 DOOR OPENING AT STA 1269, S31R. GOUGE AFTER BLENDING WAS 1 BY 0.8 IN. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN WAS GOUGED FORWARD OF THE C2 DOOR OPENING AT STA 1269, S31R. GOUGE AFTER BLENDING WAS 1 BY 0.8 IN. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.