What was found
PIT - DURING RON, FUOND 1.5 INCH CRACK ON SKIN AND DOUBLER AT FORWARD PASS ENTRANCE DOOR JAMB UPPER FORWARD CORNER. INSTALLED DOUBLERS PER SRM 53-05 FIG 26. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING RON, FUOND 1.5 INCH CRACK ON SKIN AND DOUBLER AT FORWARD PASS ENTRANCE DOOR JAMB UPPER FORWARD CORNER. INSTALLED DOUBLERS PER SRM 53-05 FIG 26. (M)