What was found
INSPECTION FOUND A 1.5 CRACK IN AFT PRESSURE BULKHEAD ATTACH T-ANGLE AT STA 996, LONGERON 15L. THE T-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 37A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 CRACK IN AFT PRESSURE BULKHEAD ATTACH T-ANGLE AT STA 996, LONGERON 15L. THE T-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 37A.