What was found
NUMEROUS FASTENER HOLES CRACKED IN FUSELAGE SKIN, STA 1016, STR 4L. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-212 REV 1, DATED 3-20-98, AND SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 3-20-98.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NUMEROUS FASTENER HOLES CRACKED IN FUSELAGE SKIN, STA 1016, STR 4L. REPAIRED PER DALFORT AEROSPACE, L.P. XEA X2-53-212 REV 1, DATED 3-20-98, AND SRM 53-30-3, FIG 42. REF: FAA FORM 8110-3 DATED 3-20-98.