What was found
INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STA 1418, LONGERON 2L IN TAIL COMPARTMENT CEILING. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STA 1418, LONGERON 2L IN TAIL COMPARTMENT CEILING. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.