What was found
INSPECTION FOUND T-ANGLE ON REAR PRESSURE BULKHEAD CORRODED AT ATTACHMENT POINTS TO FORE AND AFT BEAMS AT STA Y = 2007, X = 24L, 58L, 24R, AND 58R. THE T-ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-40-00, FIGURE 16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND T-ANGLE ON REAR PRESSURE BULKHEAD CORRODED AT ATTACHMENT POINTS TO FORE AND AFT BEAMS AT STA Y = 2007, X = 24L, 58L, 24R, AND 58R. THE T-ANGLE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-40-00, FIGURE 16.