What was found
INSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.