What was found
DURING INSPECTION, THE RT UPPER FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 NEAR STRINGER 2R. THE SKIN WAS REPAIRED IAW ETD 2015-145-022339 REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE RT UPPER FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 NEAR STRINGER 2R. THE SKIN WAS REPAIRED IAW ETD 2015-145-022339 REV B.