What was found
LEFT SIDE FORWARD FUSELAGE INTERIOR STRUCTURE: FRAME 5 IS CRACKED FOR SEVERAL INCHES ALONG ITS ATTACHMENT AREA TO NODE-6 INNER STRAP. FRAME 5 REPAIRED WITH A SPLICE INSTALLED IN REFERENCE TO ATR72 SRM 53-11-40-300-802-A01-001-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT SIDE FORWARD FUSELAGE INTERIOR STRUCTURE: FRAME 5 IS CRACKED FOR SEVERAL INCHES ALONG ITS ATTACHMENT AREA TO NODE-6 INNER STRAP. FRAME 5 REPAIRED WITH A SPLICE INSTALLED IN REFERENCE TO ATR72 SRM 53-11-40-300-802-A01-001-01.