What was found
PIT - DURING Q-6 CHECK INSPECTION, FOUND CRACK 1.25 INCHES LEFT UPPER FORWARD CORNER OF MAIN ENTRANCE DOOR FUSELAGE SKIN (X-RAY INSPECTION). CUT OUT DAMAGED AREA AND INSTALLED FILLER EXTERNAL DOUBLERS PER SRM 53-05 FIG 26. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-6 CHECK INSPECTION, FOUND CRACK 1.25 INCHES LEFT UPPER FORWARD CORNER OF MAIN ENTRANCE DOOR FUSELAGE SKIN (X-RAY INSPECTION). CUT OUT DAMAGED AREA AND INSTALLED FILLER EXTERNAL DOUBLERS PER SRM 53-05 FIG 26. (W)