What was found
DURING INSPECT, FUSE SKIN EXT FWD UP PANEL FS 256 TO 275 LONG 17R AND 18R PREV REPAIR IMPROPER. MAINT REPAIRED IAW SRM 53-04 FIG 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECT, FUSE SKIN EXT FWD UP PANEL FS 256 TO 275 LONG 17R AND 18R PREV REPAIR IMPROPER. MAINT REPAIRED IAW SRM 53-04 FIG 38.