What was found
PIT - DURING C-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN MAIN ENTRANCE DOOR TOP AFT DOOR STOP SKIN BOTH LAYERS. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 26A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING C-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN MAIN ENTRANCE DOOR TOP AFT DOOR STOP SKIN BOTH LAYERS. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 26A. (M)