As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HEAVY CHAFE MARK FROM WING-TO-BODY FAIRING ON RT SIDE OF FUSELAGE AT BS 950D 10 TO 950D 13 WL 197 BLENDED DAMAGE REF SRM 53-30-1. ORIGINAL THICKNESS .140 REMOVED .038 AT DEEPEST BLEND OUT REMAINING MATERIAL .102 MATERIAL LOSS OUT OF LIMITS REF SRM 51-30-1. THIS IS CLASSIFIED AS A MAJOR REPAIR. AREA TO BE REPAIRED ON N/R N00256.