What was found
EIGHT EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN AT STA 1006, STR 14L. REPAIRED PER DALFORD AEROSPACE, L.P. XEA X2-53-214, REV 1 DATED 7-29-98 AND 737 SRM 53-30-3 FIGURE 42.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EIGHT EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN AT STA 1006, STR 14L. REPAIRED PER DALFORD AEROSPACE, L.P. XEA X2-53-214, REV 1 DATED 7-29-98 AND 737 SRM 53-30-3 FIGURE 42.