What was found
TUL - TOP FLANGE OF CABIN FLOOR BEAM CRACKED AT HOLE, STA 1110 LBL 7 INCHES. CORROSION THE CAUSE OF CRACK. REPAIRED FLOOR BEAM PER SRM 53-10-8 FIG 8 PG 47. TST: 76,923 HOURS. CYCLES: 52,656. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - TOP FLANGE OF CABIN FLOOR BEAM CRACKED AT HOLE, STA 1110 LBL 7 INCHES. CORROSION THE CAUSE OF CRACK. REPAIRED FLOOR BEAM PER SRM 53-10-8 FIG 8 PG 47. TST: 76,923 HOURS. CYCLES: 52,656. (X)