What was found
INTERNAL FUSELAGE AT STA 1154 X-72 FWD PRESSURE BULKHEAD PANEL REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE AT STA 1154 X-72 FWD PRESSURE BULKHEAD PANEL REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.