What was found
INSPECTION FOUND A 1.5 INCH CRACK IN LONGERON END FITTING AT STA 1156, LONGERON 40R. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-33-01, 51-35-01, AND 51-21-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN LONGERON END FITTING AT STA 1156, LONGERON 40R. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-33-01, 51-35-01, AND 51-21-01.