As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H AFT DRAG ANGLE IS CRACKED ON FWD END AT APPROXIMATELY 67.5% REAR SPAR DATUM, WL 102.5. (FILED CLOSED)COMPLIED WITH REPAIRS TO LH AFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT DRAG ANGLE PER SRM TASK 55-31-00-201-001-A01, AND REO 670-55-31-165 REV --, DATED 08-10-2023. COMPLETED STRUCTURAL MAJOR REPAIR RII FORM 51-900-1002-SKY. MAJOR REPAIR FORM M-337 ALSO COMPLETED.