What was found
FUSELAGE TENSION TIE FAIL SAFE CHORD HAS 1 EACH FASTENER HOLE CRACKED AT BS 1140 RT. REMOVED DAMAGE, MANUFACTURED & INSTALLED REPAIR ANGLES IAW AMM53-10-99 & SRM 53-40-07 REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE TENSION TIE FAIL SAFE CHORD HAS 1 EACH FASTENER HOLE CRACKED AT BS 1140 RT. REMOVED DAMAGE, MANUFACTURED & INSTALLED REPAIR ANGLES IAW AMM53-10-99 & SRM 53-40-07 REPAIR 2.