What was found
WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE AFT SKIN BUCKLED AND CORRODED BEYOND LIMITS AT FS 1690 TO FS 1720, LONG 33L TO LONG 33R. CUT OUT DAMAGED AREA AND SPLICED IN NEW SKIN PANEL PER SRM 53-2-1, FIG 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE AFT SKIN BUCKLED AND CORRODED BEYOND LIMITS AT FS 1690 TO FS 1720, LONG 33L TO LONG 33R. CUT OUT DAMAGED AREA AND SPLICED IN NEW SKIN PANEL PER SRM 53-2-1, FIG 8.