What was found
PIT - C-5 - PAN HAD LONG CRACK, 0.250 INCH, DOOR PAN AT CENTER AFT STOP. INSTALLED DOUBLER PER DC-9 SRM 52-15, FIG 51. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - C-5 - PAN HAD LONG CRACK, 0.250 INCH, DOOR PAN AT CENTER AFT STOP. INSTALLED DOUBLER PER DC-9 SRM 52-15, FIG 51. (X)