What was found
FUSELAGE FRAME 47 SPLICE FITTING FOUND CRACKED DURING NDT INSPECTION. COMPLIED WITH EA 6-5310-T0326855 P1. HOLE CRACKS ON FRAME 47 AND SPLICE FITTING LT, RT. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.
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. HOLE CRACKS ON FRAME 47 AND SPLICE FITTING LT, RT. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.