What was found
DURING CHECK-C MAINT, FOUND AFT FUSELAGE STA 1121 WITH 2 INCH CRACK IN CANTED BULKHEAD WEB BELOW LOUVERS ON LT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2 PAGE 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, FOUND AFT FUSELAGE STA 1121 WITH 2 INCH CRACK IN CANTED BULKHEAD WEB BELOW LOUVERS ON LT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2 PAGE 9.