What was found
PIT - DURING C-2 CHECK, FOUND .20 INCH CRACK AT RADIUS OF INNER PAN LOWER AFT CORNER BELOW BAYONET. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-05 FIG 26A. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING C-2 CHECK, FOUND .20 INCH CRACK AT RADIUS OF INNER PAN LOWER AFT CORNER BELOW BAYONET. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-05 FIG 26A. (X)