What was found
PIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK LEFT FORWARD EMERGENCY EXIT DOOR (OVER WING EXIT). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK LEFT FORWARD EMERGENCY EXIT DOOR (OVER WING EXIT). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03 FIG 1. (M)