As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 GAP STRIP ON LT ENGINE PYLON CRACKED. BLENDED DAMAGE ON NR 2 GAP STRIP. PERFORMED HFEC AFTER BLEND OUT, NO CRACKS NOTED. AREA OF DAMAGE IS 12" BY .062" WITH TOTAL AREA OF EXPOSURE OF .744 SQ INS. IAW WITH ALLOWABLE DAMAGES 1 TABLE B FIG 103 PG 114 GAP COVER STRIP NR 2. REPLACED HEAT SHIELDS IAW CMM 54-52-17.