What was found
DURING OP 15 MAINT CHECK, THE FUSELAGE TO WING TIE ANGLE WAS CRACKED AT STA 605, BETWEEN LONGERON 22L AND 23L. REPLACED WING TO FUSELAGE TIE ANGLE PER DOUGLAS DRAWING 5910068.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 15 MAINT CHECK, THE FUSELAGE TO WING TIE ANGLE WAS CRACKED AT STA 605, BETWEEN LONGERON 22L AND 23L. REPLACED WING TO FUSELAGE TIE ANGLE PER DOUGLAS DRAWING 5910068.