What was found
UPPER FUSELAGE EXTERIOR FRAME 88 BETWEEN STR B10 AND 11 LT SKIN WITH SCRATCH. DAMAGE HAS BEEN REPORTED UNDER NON ROUTINE ITEM A1E143, 2-221. REPAIR OF DAMAGE HAS BEEN ACCOMPLISHED UNDER ETD2016-190-048783, INSTRUCTION AND APPROVED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE EXTERIOR FRAME 88 BETWEEN STR B10 AND 11 LT SKIN WITH SCRATCH. DAMAGE HAS BEEN REPORTED UNDER NON ROUTINE ITEM A1E143, 2-221. REPAIR OF DAMAGE HAS BEEN ACCOMPLISHED UNDER ETD2016-190-048783, INSTRUCTION AND APPROVED.