What was found
A 2 INCH CRACK IN NR 5 SLAT L/E RIB LWR AFT CORNER I/B OF ACT ROD END. REPAIRED PER 727 M/M 57-54-0 PG 805.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 2 INCH CRACK IN NR 5 SLAT L/E RIB LWR AFT CORNER I/B OF ACT ROD END. REPAIRED PER 727 M/M 57-54-0 PG 805.