What was found
DURING D-CHECK, FOUND TOP SKIN IS CRACKED AT ONE FASTENER HOLE AT FS 385 STRINGER 4R. CUT OUT DAMAGE AREA PER SRM 53-30-3 FIG 4 AND INSTALLED DOUBLER 9 INCHES BY 8 INCHES 2024-T3 .050 PER SRM 53-30-3 FIG 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FOUND TOP SKIN IS CRACKED AT ONE FASTENER HOLE AT FS 385 STRINGER 4R. CUT OUT DAMAGE AREA PER SRM 53-30-3 FIG 4 AND INSTALLED DOUBLER 9 INCHES BY 8 INCHES 2024-T3 .050 PER SRM 53-30-3 FIG 4.