What was found
INSPECTION FOUND THREE .125 INCH CRACKS IN SECTION 41R, RT 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 THREE .125 INCH CRACKS IN SECTION 41R, RT 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.