As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMBER 1 PYLON LOWER SPAR HAD CHAFE MARK FROM CONTACT WITH THE CNA. BLENDED & WITHIN LIMITS IAW SRM 54-51-12 FIG 103. MAX MATERIAL LOSS IS 0.017, EXTENDED CHAFE PLATE INST IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES INSPECTION IAW SRI54-51-12-2-001-00 PARA 3 A TBL 202. FIRST INSP 49000FC OR 61200FH FROM REPAIR EMBODIMENT, WITH SUBSEQUENT INSP EVERY 21000H OR 16800C.