What was found
PIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK IN ANGLE AT STA 1338 TOP CENTER OF AFT PRESSURE BULKHEAD FWD SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 PG 9. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK IN ANGLE AT STA 1338 TOP CENTER OF AFT PRESSURE BULKHEAD FWD SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 PG 9. (W)