What was found
DURING C CHECK, MAINT FOUND A CRACK AT DOUBLER ANGLE FWD SIDE OF REAR BULKHEAD, BELOW LONGERON 1. STOP DRILLED TO QUARTER INCH. REPAIRED WITH 2 EA 0.025 THICK DOUBLERS PER SRM 53-01 PAGE 10. REINSTALLED ANGLE. ---CLOSED---
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK, MAINT FOUND A CRACK AT DOUBLER ANGLE FWD SIDE OF REAR BULKHEAD, BELOW LONGERON 1. STOP DRILLED TO QUARTER INCH. REPAIRED WITH 2 EA 0.025 THICK DOUBLERS PER SRM 53-01 PAGE 10. REINSTALLED ANGLE. ---CLOSED---