What was found
INITIAL, CRACK ON FUSELAGE SKIN ON STA Y=1380 BETWEEN LONGERONS 13R-14R. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04, FIG 18.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INITIAL, CRACK ON FUSELAGE SKIN ON STA Y=1380 BETWEEN LONGERONS 13R-14R. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04, FIG 18.