What was found
AFT FUSELAGE INTERNAL BULKHEAD T-CHORD CRACKED AT BS 1809.5, LBL 27. MAJOR REPAIR ACCOMPLISHED: FABRICATED A -1 AND -2 ANGLE WITH FILLER AND REPAIRED HORIZONTAL INNER CHORD PER SRM 53-80-08, REPAIR 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE INTERNAL BULKHEAD T-CHORD CRACKED AT BS 1809.5, LBL 27. MAJOR REPAIR ACCOMPLISHED: FABRICATED A -1 AND -2 ANGLE WITH FILLER AND REPAIRED HORIZONTAL INNER CHORD PER SRM 53-80-08, REPAIR 10.