What was found
CLT - FOUND STIFFENER AND CHANNEL CRACKED .5 INCHES, NR 2 ENGINE AFT STRUT STRUCTURE. FABRICATED AND INSTALLED NEW CHANNEL REMOVED AND REPLACED STIFFENER IAW SRM 51-10-01 AND DRAWING 313H1355. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - FOUND STIFFENER AND CHANNEL CRACKED .5 INCHES, NR 2 ENGINE AFT STRUT STRUCTURE. FABRICATED AND INSTALLED NEW CHANNEL REMOVED AND REPLACED STIFFENER IAW SRM 51-10-01 AND DRAWING 313H1355. (M)