What was found
INSPECTION FOUND FOUR .125 INCH CRACKS IN SECTION 41, LT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FOUR .125 INCH CRACKS IN SECTION 41, LT FORWARD FUSELAGE EXTERNAL SKIN PANEL. THE CRACKED AREA WAS CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND EA 5310-01188.