What was found
FUSELAGE STA 680 LBL 5 TO LBL 22 JUST BELOW THE CENTER WING LOWER FORWARD SPAR, THE PRESSURE BULKHEAD IS CRACKED IN TWO PLACES. REMOVED CRACKED SECTION OF DOME, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 53-25, FIGURE 13.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STA 680 LBL 5 TO LBL 22 JUST BELOW THE CENTER WING LOWER FORWARD SPAR, THE PRESSURE BULKHEAD IS CRACKED IN TWO PLACES. REMOVED CRACKED SECTION OF DOME, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 53-25, FIGURE 13.