What was found
DURING MAINTENANCE CHECK, NOTED CORROSION ON THE AFT SIDE OF THE BS 1016 PRESSURE WEB AT THE FRAME ATTACHMENT BETWEEN STR 26LT AND 27LT. CUT ACCESS HOLE IN FUSELAGE SKIN AND REPAIRED PRESSURE WEB AND SKIN PER BOEING SB 737-53A1075.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING MAINTENANCE CHECK, NOTED CORROSION ON THE AFT SIDE OF THE BS 1016 PRESSURE WEB AT THE FRAME ATTACHMENT BETWEEN STR 26LT AND 27LT. CUT ACCESS HOLE IN FUSELAGE SKIN AND REPAIRED PRESSURE WEB AND SKIN PER BOEING SB 737-53A1075.