What was found
PIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFED .014 INCH DEEP 5 INCHES BY 1 INCH STATION 813 AT LONGERON 26R UNDER FILLET PANEL. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 37. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFED .014 INCH DEEP 5 INCHES BY 1 INCH STATION 813 AT LONGERON 26R UNDER FILLET PANEL. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 37. (M)