What was found
FUSELAGE SKIN CHAFED BY A FLEX DUCT AT FRAME 30(F/S 10172) AND STRINGER L18. REPAIRED IAW SRM 53-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CHAFED BY A FLEX DUCT AT FRAME 30(F/S 10172) AND STRINGER L18. REPAIRED IAW SRM 53-00-01.