What was found
FUSELAGE FRAME 47 SPLICE FITTING FOUND CRACKED DURING NDT INSPECTION. COMPLIED WITH EA 6-5310-T0326855 P1. FUSELAGE, MAINFRAME, AD 2006 - 01-10-SB A300-53-6123, HOLE CRACKS ON FRAME 47 & SPLICE FITTING LT & RT. THIS IS A MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME 47 SPLICE FITTING FOUND CRACKED DURING NDT INSPECTION. COMPLIED WITH EA 6-5310-T0326855 P1. FUSELAGE, MAINFRAME, AD 2006 - 01-10-SB A300-53-6123, HOLE CRACKS ON FRAME 47 & SPLICE FITTING LT & RT. THIS IS A MAJOR REPAIR.