What was found
DURING SERVICE CHECK, FOUND CRACK ON THE FUSELAGE SKIN BS 2638 WL 310, BETWEEN STRINGERS 4 - 10R. REPAIRED IAW SRM 53-80-03 SEC. 48 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SERVICE CHECK, FOUND CRACK ON THE FUSELAGE SKIN BS 2638 WL 310, BETWEEN STRINGERS 4 - 10R. REPAIRED IAW SRM 53-80-03 SEC. 48 FIG 1.