What was found
DURING A INSPECTION OF AREA 'A' ON THE RIGHT ENGINE TRUSS A .5 INCH CRACK. REPAIRED BY WELDING CRACK. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A INSPECTION OF AREA 'A' ON THE RIGHT ENGINE TRUSS A .5 INCH CRACK. REPAIRED BY WELDING CRACK. (M)