What was found
CRACKED MAIN FRAME ANGLE BS 1022 BETWEEN LONGERONS 16 AND 17L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06R, 51-41-05, AND DWG 9912243, REV JS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED MAIN FRAME ANGLE BS 1022 BETWEEN LONGERONS 16 AND 17L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-00-06R, 51-41-05, AND DWG 9912243, REV JS.