What was found
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND TWO 3 INCH CRACKS IN THE FORWARD HORIZONTAL PRESSURE PANEL AT FS 105 UNDER COCKPIT FLOOR NOSE WHEEL WELL. REMOVED CRACKED SECTION AND INSTALLED REPAIR DOUBLER PER USAIR EA 32641. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING A Q-1/C-1 CHECK INSPECTION, FOUND TWO 3 INCH CRACKS IN THE FORWARD HORIZONTAL PRESSURE PANEL AT FS 105 UNDER COCKPIT FLOOR NOSE WHEEL WELL. REMOVED CRACKED SECTION AND INSTALLED REPAIR DOUBLER PER USAIR EA 32641. (M)