What was found
PIT - DURING Q4 CHECK, FOUND 2.50 INCH CRACK IN SUPPORT ANGLE AT LT LAV SIDE WALL/AFT ENTRY FLOOR LEVEL AT STA 1008. INSTALLED DOUBLER PER SRM 53-05, FIG 30. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q4 CHECK, FOUND 2.50 INCH CRACK IN SUPPORT ANGLE AT LT LAV SIDE WALL/AFT ENTRY FLOOR LEVEL AT STA 1008. INSTALLED DOUBLER PER SRM 53-05, FIG 30. (X)