What was found
INSPECTION FOUND A 1.5 INCH CRACK ON SUPPORT ANGLE UNDER BODY FILLET JUST ABOVE WING AT FS 1341R. THE CRACKED AREA WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 53-53-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK ON SUPPORT ANGLE UNDER BODY FILLET JUST ABOVE WING AT FS 1341R. THE CRACKED AREA WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01 AND 53-53-01.