What was found
DURING INSPECTION, STRINGER 21 WAS FOUND TO BE CHAFED BETWEEN FRAME 20 & 21. THE STRINGER WAS REPAIRED IAW ETD 2014-145-025850-A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, STRINGER 21 WAS FOUND TO BE CHAFED BETWEEN FRAME 20 & 21. THE STRINGER WAS REPAIRED IAW ETD 2014-145-025850-A.