What was found
DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK, 41 INCHES FWD OF OUTFLOW VALVE AT RIGHT AFT FUSELAGE. REPAIRED PER SWA RA 1-A53-1285.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED TERMINAL CHECK, FOUND A 3 INCH CRACK, 41 INCHES FWD OF OUTFLOW VALVE AT RIGHT AFT FUSELAGE. REPAIRED PER SWA RA 1-A53-1285.