What was found
UPPER FUSELAGE AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L, AT AFT FASTENER ROWS ATTACHMENT TO THE Y CHORD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L, AT AFT FASTENER ROWS ATTACHMENT TO THE Y CHORD.