As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C1 HFEC & VISUAL INSPECTION DETECTED A CRACK ON THE C-4 (D-PIT) UPPER FWD DOOR JAMB CORNER. CRACK RUNS FROM FASTENER HOLE TO EDGE OF CUTOUT. REMOVED EXISTING DOUBLER. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER. REAMED DISCREPANT FASTENER HOLES IAW SRM 53 53-02-0 FIG 21 AND SAA EA 008-5330-01-A0827.