What was found
FUSELAGE FRAME STA 1418 FROM LONGERON 5L TO 5R FAILSAFE CHORD IS CRACKED. REMOVED CRACKED CHORD RECEIVED DRILLED AND INSTALLED NEW CHORD IAW MD80 SRM 51-10-4, 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME STA 1418 FROM LONGERON 5L TO 5R FAILSAFE CHORD IS CRACKED. REMOVED CRACKED CHORD RECEIVED DRILLED AND INSTALLED NEW CHORD IAW MD80 SRM 51-10-4, 51-30-5.