What was found
FUSELAGE SKIN CRACKED AT THE FOLLOWING LOCATIONS, STA 908 STR 10R AND STA 1016 STR 10L AND STR 14R. REPAIRED PER DALFORT AEROSPACE, LP XEA X2-53-205 REV 1 DATED 2-25-98 AND BOEING SRM 53-30-3 FIGURE 42. FAA FORM 8110-3 DATED 2-25-98.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT THE FOLLOWING LOCATIONS, STA 908 STR 10R AND STA 1016 STR 10L AND STR 14R. REPAIRED PER DALFORT AEROSPACE, LP XEA X2-53-205 REV 1 DATED 2-25-98 AND BOEING SRM 53-30-3 FIGURE 42. FAA FORM 8110-3 DATED 2-25-98.