What was found
DURING (H) CHECK FOUND CHAFED AREA ON AFT FUSELAGE FRAME AT FR86. REPAIRED IAW SRM 51-42-11, 51-44-11, 51-75-12.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING (H) CHECK FOUND CHAFED AREA ON AFT FUSELAGE FRAME AT FR86. REPAIRED IAW SRM 51-42-11, 51-44-11, 51-75-12.