As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FUSELAGE SKIN (LENGTH 0.187") ON STA Y=1418 BTW LONG 2L AND 3L AND CRACK ON FUSELAGE SKIN (LENGTH 0.187") ON STA Y=1418 BTW LONG 2R AND 3R. CRACKS OF .187" ON SKIN WERE REPAIRED PER ETI 88-16-364 REV 6 AND ER/A 550324-14AD REV ORIGINAL.