What was found
DURING A SHOP INSPECTION, THE UPPER FRAME ANGLE WAS FOUND TO BE CRACKED. A REPAIR WAS INSTALLED PER THE S.R.M. 54-10-3. FOR NR 2 ENGINE LEFT FORWARD COWL PANEL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SHOP INSPECTION, THE UPPER FRAME ANGLE WAS FOUND TO BE CRACKED. A REPAIR WAS INSTALLED PER THE S.R.M. 54-10-3. FOR NR 2 ENGINE LEFT FORWARD COWL PANEL.