What was found
PIT - DURING RON CHECK, FOUND 6 INCH CRACK AT PRESSURE SIDEWALL WEB, NOSE WHEEL WELL AT BS 259.5, WL 175.6. INSTALLED SHEETMETAL DOUBLERS AND FILLERS PER TYPICAL REPAIR 53-10-12 REV A AND EA 52440. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING RON CHECK, FOUND 6 INCH CRACK AT PRESSURE SIDEWALL WEB, NOSE WHEEL WELL AT BS 259.5, WL 175.6. INSTALLED SHEETMETAL DOUBLERS AND FILLERS PER TYPICAL REPAIR 53-10-12 REV A AND EA 52440. (M)