What was found
FOUND DURING C-2 LETTER CHECK, NR 1 ENG PYLON UPPER SKIN TO FUSELAGE SKIN ATTACH ANGLE WAS FOUND CRACKED .5 INCHES. INSTALLED REPAIR PER SRM 54-04A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND DURING C-2 LETTER CHECK, NR 1 ENG PYLON UPPER SKIN TO FUSELAGE SKIN ATTACH ANGLE WAS FOUND CRACKED .5 INCHES. INSTALLED REPAIR PER SRM 54-04A.